- Y Diweddaraf sydd Ar Gael (Diwygiedig)
- Pwynt Penodol mewn Amser (31/12/2020)
- Gwreiddiol (Fel y’i mabwysiadwyd gan yr UE)
Commission Regulation (EU) 2017/2400 of 12 December 2017 implementing Regulation (EC) No 595/2009 of the European Parliament and of the Council as regards the determination of the CO2 emissions and fuel consumption of heavy-duty vehicles and amending Directive 2007/46/EC of the European Parliament and of the Council and Commission Regulation (EU) No 582/2011 (Text with EEA relevance)
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Vehicle groups for vehicles of category N
a In these vehicle classes tractors are treated as rigid lorries but with specific curb weight of tractor. | ||||||||||
b Sub-group ‘ v ’ of vehicle groups 4, 5, 9 and 10: these mission profiles are exclusively applicable to vocational vehicles. | ||||||||||
(*) EMS — European Modular System | ||||||||||
T = Tractor R = Rigid lorry & standard body T1, T2 = Standard trailers ST = Standard semitrailer D = Standard dolly] | ||||||||||
Description of elements relevant to the classification in vehicle groups | Vehicle group | Allocation of mission profile and vehicle configuration | ||||||||
---|---|---|---|---|---|---|---|---|---|---|
Axle configuration | Chassis configuration | Technically permissible maximum laden mass (tons) | Long haul | Long haul (EMS) | Regional delivery | Regional delivery (EMS) | Urban delivery | Municipal utility | Construction | |
4 × 2 | Rigid lorry | > 3,5 –7,5 | (0) | |||||||
Rigid lorry (or tractor) a | > 7,5 – 10 | 1 | R | R | ||||||
Rigid lorry (or tractor) a | > 10 – 12 | 2 | R+T1 | R | R | |||||
Rigid lorry (or tractor) a | > 12 – 16 | 3 | R | R | ||||||
Rigid lorry | > 16 | 4 | R+T2 | R | R | R | ||||
Tractor | > 16 | 5 | T+ST | T+ST+T2 | T+ST | T+ST+T2 | T+ST | |||
Rigid lorry | > 16 | 4v b | R | R | ||||||
Tractor | > 16 | 5v b | T+ST | |||||||
4 × 4 | Rigid lorry | > 7,5 – 16 | (6) | |||||||
Rigid lorry | > 16 | (7) | ||||||||
Tractor | > 16 | (8) | ||||||||
6 × 2 | Rigid lorry | all weights | 9 | R+T2 | R+D+ST | R | R+D+ST | R | ||
Tractor | all weights | 10 | T+ST | T+ST+T2 | T+ST | T+ST+T2 | ||||
Rigid lorry | all weights | 9v b | R | R | ||||||
Tractor | all weights | 10v b | T+ST | |||||||
6 × 4 | Rigid lorry | all weights | 11 | R+T2 | R+D+ST | R | R+D+ST | R | R | |
Tractor | all weights | 12 | T+ST | T+ST+T2 | T+ST | T+ST+T2 | T+ST | |||
6 × 6 | Rigid lorry | all weights | (13) | |||||||
Tractor | all weights | (14) | ||||||||
8 × 2 | Rigid lorry | all weights | (15) | |||||||
8 × 4 | Rigid lorry | all weights | 16 | R | ||||||
8 × 6 8 × 8 | Rigid lorry | all weights | (17) |
Textual Amendments
F1 Substituted by Commission Regulation (EU) 2019/318 of 19 February 2019 amending Regulation (EU) 2017/2400 and Directive 2007/46/EC of the European Parliament and of the Council as regards the determination of the CO2 emissions and fuel consumption of heavy-duty vehicles (Text with EEA relevance).
A data management system covering sourcing, storing, handling and retrieving of the input information and input data for the simulation tool as well as handling certificates on the CO2 emissions and fuel consumption related properties of a component families, separate technical unit families and system families. The data management system shall at least:
ensure application of correct input information and input data to specific vehicle configurations
ensure correct calculation and application of standard values;
verify by means of comparing cryptographic hashes that the input files of component families, separate technical unit families and system families which are used for the simulation corresponds to the input data of the component families, separate technical unit families and system families for which the certification has been granted;
include a protected database for storing the input data relating to the component families, separate technical unit families or system families and the corresponding certificates of the CO2 emissions and fuel consumption related properties;
ensure correct management of the changes of specification and updates of components, separate technical units and systems;
enable tracing of the components, separate technical units and systems after the vehicle is produced.
A data management system covering retrieving of the input information and input data and calculations by means of the simulation tool and storing of the output data. The data management system shall at least:
ensure a correct application of cryptographic hashes;
include a protected database for storing the output data;
Process for consulting the dedicated electronic distribution platform referred to in Article 5(2) and Article 10(1) and (2), as well as downloading and installing the latest versions of the simulation tool.
Appropriate training of staff working with the simulation tool.
The approval authority shall also verify the following:
the functioning of the processes set out in points 1.1.1, 1.1.2 and 1.1.3 and the application of the requirement set out in point 1.1.4;
that the processes used during the demonstration are applied in the same manner in all the production facilities manufacturing the vehicle group concerned;
the completeness of the description of the data and process flows of operations related to the determination of the CO2 emissions and fuel consumption of the vehicles.
For the purpose of point (a) of the second paragraph, The verification shall include determination of the CO2 emissions and fuel consumption of at leaste one vehicle from each of the vehicle groups for which the licence has been applied for.
of the licence to operate simulation tool with regard to Regulation (EC) No 595/2009 as implemented by Regulation (EU) 2017/2400.
Licence number:
Reason for extension: …
This Annex describes the list of parameters to be provided by the vehicle manufacturer as input to the simulation tool. The applicable XML schema as well as example data are available at the dedicated electronic distribution platform.
[F1‘ Parameter ID ’ : Unique identifier as used in the simulation tool for a specific input parameter or set of input data]
‘Type’: Data type of the parameter
sequence of characters in ISO8859-1 encoding
sequence of characters in ISO8859-1 encoding, no leading/trailing whitespace
date and time in UTC time in the format: YYYY-MM-DDTHH:MM:SSZ with italic letters denoting fixed characters e.g. ‘2002-05-30T09:30:10Z’
value with an integral data type, no leading zeros, e.g. ‘1800’
fractional number with exactly X digits after the decimal sign (‘.’) and no leading zeros e.g. for ‘double, 2’: ‘2345.67’; for ‘double, 4’: ‘45.6780’
‘Unit’ … physical unit of the parameter
‘corrected actual mass of the vehicle’ shall mean the mass as specified under the ‘actual mass of the vehicle’ in accordance with Commission Regulation (EC) No 1230/2012(1) with an exception for the tank(s) which shall be filled to at least 50 % of its or their capacity/ies, without superstructure and corrected by the additional weight of the non-installed standard equipment as specified in point 4.3 and the mass of a standard body, standard semi-trailer or standard trailer to simulate the complete vehicle or complete vehicle-(semi-)trailer combination.
All parts that are mounted on and above the main frame are regarded as superstructure parts if they are only installed for facilitating a superstructure, independent of the necessary parts for in running order conditions.
Input parameters ‘ Vehicle/General ’
a In case of multiple PTOs mounted to the transmission, only the component with the highest losses according to point 3.6 of Annex IX, for its combination of criteria ‘ PTOShaftsGearWheels ’ and ‘ PTOShaftsOtherElements ’ , shall be declared.] | ||||
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
Manufacturer | P235 | token | [-] | |
ManufacturerAddress | P252 | token | [-] | |
Model | P236 | token | [-] | |
VIN | P238 | token | [-] | |
Date | P239 | dateTime | [-] | Date and time when the component-hash is created |
LegislativeClass | P251 | string | [-] | Allowed values: ‘ N2 ’ , ‘ N3 ’ |
VehicleCategory | P036 | string | [-] | Allowed values: ‘ Rigid Lorry ’ , ‘ Tractor ’ |
AxleConfiguration | P037 | string | [-] | Allowed values: ‘ 4×2 ’ , ‘ 6×2 ’ , ‘ 6×4 ’ , ‘ 8×4 ’ |
CurbMassChassis | P038 | int | [kg] | |
GrossVehicleMass | P041 | int | [kg] | |
IdlingSpeed | P198 | int | [1/min] | |
RetarderType | P052 | string | [-] | Allowed values: ‘ None ’ , ‘ Losses included in Gearbox ’ , ‘ Engine Retarder ’ , ‘ Transmission Input Retarder ’ , ‘ Transmission Output Retarder ’ |
RetarderRatio | P053 | double, 3 | [-] | |
AngledriveType | P180 | string | [-] | Allowed values: ‘ None ’ , ‘ Losses included in Gearbox ’ , ‘ Separate Angledrive ’ |
PTOShaftsGearWheels a | P247 | string | [-] | Allowed values: ‘ none ’ , ‘ only the drive shaft of the PTO ’ , ‘ drive shaft and/or up to 2 gear wheels ’ , ‘ drive shaft and/or more than 2 gear wheels ’ , ‘ only one engaged gearwheel above oil level ’ |
PTOOtherElements a | P248 | string | [-] | Allowed values: ‘ none ’ , ‘ shift claw, synchronizer, sliding gearwheel ’ , ‘ multi-disc clutch ’ , ‘ multi-disc clutch, oil pump ’ |
CertificationNumberEngine | P261 | token | [-] | |
CertificationNumberGearbox | P262 | token | [-] | |
CertificationNumberTorqueconverter | P263 | token | [-] | |
CertificationNumberAxlegear | P264 | token | [-] | |
CertificationNumberAngledrive | P265 | token | [-] | |
CertificationNumberRetarder | P266 | token | [-] | |
CertificationNumberTyre | P267 | token | [-] | |
CertificationNumberAirdrag | P268 | token | [-] | |
ZeroEmissionVehicle | P269 | boolean | [-] | |
VocationalVehicle | P270 | boolean | [-] | |
NgTankSystem | P275 | string | [-] | Allowed values: ‘ Compressed ’ , ‘ Liquefied ’ Only relevant for vehicles with engines of fuel type ‘ NG PI ’ (P193) |
Sleeper cab | P276 | boolean | [-] |
Input parameters ‘Vehicle/AxleConfiguration’ per wheel axle
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
TwinTyres | P045 | boolean | [-] | |
AxleType | P154 | string | [-] | Allowed values: ‘VehicleNonDriven’, ‘VehicleDriven’ |
Steered | P195 | boolean |
Input parameters ‘Vehicle/Auxiliaries’
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
Fan/Technology | P181 | string | [-] | Allowed values: ‘Crankshaft mounted - Electronically controlled visco clutch’, ‘Crankshaft mounted - Bimetallic controlled visco clutch’, ‘Crankshaft mounted - Discrete step clutch’, ‘Crankshaft mounted - On/off clutch’, ‘Belt driven or driven via transm. - Electronically controlled visco clutch’, ‘Belt driven or driven via transm. - Bimetallic controlled visco clutch’, ‘Belt driven or driven via transm. - Discrete step clutch’, ‘Belt driven or driven via transm. - On/off clutch’, ‘Hydraulic driven - Variable displacement pump’, ‘Hydraulic driven - Constant displacement pump’, ‘Electrically driven - Electronically controlled’ |
SteeringPump/Technology | P182 | string | [-] | Allowed values: ‘Fixed displacement’, ‘Fixed displacement with elec. control’, ‘Dual displacement’, ‘Variable displacement mech. controlled’, ‘Variable displacement elec. controlled’, ‘Electric’ Separate entry for each steered wheel axle required |
ElectricSystem/Technology | P183 | string | [-] | Allowed values: ‘Standard technology’, ‘Standard technology - LED headlights, all’ |
PneumaticSystem/Technology | P184 | string | [-] | Allowed values: ‘Small’, ‘Small + ESS’, ‘Small + visco clutch’ , ‘Small + mech. clutch’, ‘Small + ESS + AMS’, ‘Small + visco clutch + AMS’, ‘Small + mech. clutch + AMS’, ‘Medium Supply 1-stage’, ‘Medium Supply 1-stage + ESS’, ‘Medium Supply 1-stage + visco clutch’ , ‘Medium Supply 1-stage + mech. clutch’, ‘Medium Supply 1-stage + ESS + AMS’, ‘Medium Supply 1-stage + visco clutch + AMS’, ‘Medium Supply 1-stage + mech. clutch + AMS’, ‘Medium Supply 2-stage’, ‘Medium Supply 2-stage + ESS’, ‘Medium Supply 2-stage + visco clutch’ , ‘Medium Supply 2-stage + mech. clutch’, ‘Medium Supply 2-stage + ESS + AMS’, ‘Medium Supply 2-stage + visco clutch + AMS’, ‘Medium Supply 2-stage + mech. clutch + AMS’, ‘Large Supply’, ‘Large Supply + ESS’, ‘Large Supply + visco clutch’ , ‘Large Supply + mech. clutch’, ‘Large Supply + ESS + AMS’, ‘Large Supply + visco clutch + AMS’, ‘Large Supply + mech. clutch + AMS’; ‘Vacuum pump’ |
[F1HVAC/Technology | P185 | string | [-] | Allowed values: ‘ None ’ , ‘ Default ’] |
Input parameters ‘Vehicle/EngineTorqueLimits’ per gear (optional)
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
Gear | P196 | integer | [-] | only gear numbers need to be specified where vehicle related engine torque limits according to point 6 are applicable |
MaxTorque | P197 | integer | [Nm] |
Input parameters for ZE-HDVs, He-HDVs and dual-fuel vehicles
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
Manufacturer | P235 | token | [-] | |
ManufacturerAddress | P252 | token | [-] | |
Model | P236 | token | [-] | |
VIN | P238 | token | [-] | |
Date | P239 | dateTime | [-] | Date and time when the component-hash is created |
LegislativeClass | P251 | string | [-] | Allowed values: ‘ N2 ’ , ‘ N3 ’ |
VehicleCategory | P036 | string | [-] | Allowed values: ‘ Rigid Lorry ’ , ‘ Tractor ’ |
CurbMassChassis | P038 | int | [kg] | |
GrossVehicleMass | P041 | int | [kg] | |
MaxNetPower1 | P277 | int | [W] | If He-HDV = Y: highest maximum net power of all energy converters, which are linked to the vehicle driveline or the wheels |
MaxNetPower2 | P278 | int | [W] | If He-HDV = Y: second highest maximum net power of all energy converters, which are linked to the vehicle driveline or the wheels |
ZE-HDV | P269 | boolean | [-] | |
He-HDV | P279 | boolean | [-] | |
DualFuelVehicle | P280 | boolean | [-] | ] |
Textual Amendments
Input parameters ‘ Advanced driver assistance systems ’
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
EngineStopStart | P271 | boolean | [-] | In accordance with point 8.1.1 |
EcoRollWithoutEngineStop | P272 | boolean | [-] | In accordance with point 8.1.2 |
EcoRollWithEngineStop | P273 | boolean | [-] | In accordance with point 8.1.3 |
PredictiveCruiseControl | P274 | string | [-] | In accordance with point 8.1.4, allowed values: ‘ 1,2 ’ , ‘ 1,2,3 ’] |
This corrected actual mass shall be based on vehicles equipped in such a way that they are compliant to all regulatory acts of Annex IV and Annex XI to Directive 2007/46/EC applicable to the particular vehicle class.
Front under-run protection in accordance with Regulation (EC) No 661/2009 of the European Parliament and of the Council(2)
Rear under-run protection in accordance with Regulation (EC) No 661/2009 of the European Parliament and of the Council
Lateral protection in accordance with Regulation (EC) No 661/2009 of the European Parliament and of the Council
Fifth wheel in accordance with Regulation (EC) No 661/2009 of the European Parliament and of the Council
For vehicles of groups 1, 2 and 3
45 kg
40 kg
8,5 kg/m × wheel base [m] – 2,5 kg
[ F3 ]
For vehicles of groups 4, 5, 9 to 12 and 16
50 kg
45 kg
14 kg/m × wheel base [m] – 17 kg
210 kg
Textual Amendments
In case of vehicles equipped with:
a hydraulically driven axles, the axle shall be treated as a non-drivable one and the manufacturer shall not take it into consideration for establishing an axle configuration of a vehicle;
a mechanically driven axles, the axle shall be treated as a drivable one and the manufacturer shall take it into consideration for establishing an axle configuration of a vehicle;
For the highest 50 % of the gears (e.g. for gears 7 to 12 of a 12 gear transmission) the vehicle manufacturer may declare a gear dependent maximum engine torque limit which is not higher than 95 % of the maximum engine torque.
Engine stop-start during vehicle stops: system which automatically shuts down and restarts the internal combustion engine during vehicle stops to reduce engine idling time. For automatic engine shut down the maximum time delay after the vehicle stop shall be not longer than 3 seconds.
Eco-roll without engine stop-start: system which automatically decouples the internal combustion engine from the drivetrain during specific downhill driving conditions with low negative gradients. During these phases the internal combustion engine is operated in engine idling. The system shall be active at least at all cruise control set speeds above 60 km/h.
Eco-roll with engine stop-start: system which automatically decouples the internal combustion engine from the drivetrain during specific downhill driving conditions with low negative slopes. During these phases the internal combustion engine is shut down after a short time delay and keeps shut down during the main share of the eco-roll phase. The system shall be active at least at all cruise control set speeds of above 60 km/h.
Predictive cruise control (PCC): systems which optimise the usage of potential energy during a driving cycle based on an available preview of road gradient data and the use of a GPS system. A PCC system declared in the input to the simulation tool shall have a gradient preview distance longer than 1 000 metres and cover all following functionalities:
Crest coasting
Approaching a crest the vehicle velocity is reduced before the point where the vehicle starts accelerating by gravity alone compared to the set speed of the cruise control so that the braking during the following downhill phase can be reduced.
Acceleration without engine power
During downhill driving with a low vehicle velocity and a high negative slope the vehicle acceleration is performed without any engine power usage so that the downhill braking can be reduced.
Dip coasting
During downhill driving when the vehicle is braking at the overspeed velocity, PCC increases the overspeed for a short period of time to end the downhill event with a higher vehicle velocity. Overspeed is a higher vehicle speed than the set speed of the cruise control system.
A PCC system can be declared as input to the simulation tool if either the functionalities set out in points (1) and (2) or points (1), (2) and (3) are covered.
Table 7 | ||||
Combinations of advanced driver assistance systems as input parameters into the simulation tool | ||||
Combination No | Engine stop-start during vehicle stops | Eco-roll without engine stop-start | Eco-roll with engine stop-start | Predictive cruise control |
---|---|---|---|---|
1 | yes | no | no | no |
2 | no | yes | no | no |
3 | no | no | yes | no |
4 | no | no | no | yes |
5 | yes | yes | no | no |
6 | yes | no | yes | no |
7 | yes | no | no | yes |
8 | no | yes | no | yes |
9 | no | no | yes | yes |
10 | yes | yes | no | yes |
11 | yes | no | yes | yes |
The manufacturer's records file will be produced by the simulation tool and shall at least contain the following information:
Engine stop-start during vehicle stops (yes/no) …
Eco-roll without engine stop-start (yes/no) …
Eco-roll with engine stop-start (yes/no) …
Predictive cruise control (yes/no) …]
Average vehicle speed | CO 2 emissions | Fuel consumption | |||||
---|---|---|---|---|---|---|---|
Long haul | … km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Long haul (EMS) | … km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Regional delivery | … km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Regional delivery (EMS) | … km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Urban delivery | … km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Municipal utility | … km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Construction | … km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Average vehicle speed | CO 2 emissions | Fuel consumption | |||||
---|---|---|---|---|---|---|---|
Long haul | … km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Long haul (EMS) | … km/h | … g/km | … g/t-km | …g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Regional delivery | …km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Regional delivery (EMS) | … km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Urban delivery | … km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Municipal utility | … km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Construction | … km/h | … g/km | … g/t-km | … g/m 3 -km | … l/100km | … l/t-km | … l/m 3 -km |
Simulation tool version | [X.X.X] |
Date and time of the simulation | [-] |
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
The engine test procedure described in this Annex shall produce input data relating to engines for the simulation tool.
For the purposes of this Annex the definitions according to UN/ECE Regulation 49 Rev.06 and, in addition to these, the following definitions shall apply:
‘engine CO2-family’ means a manufacturer's grouping of engines, as defined in paragraph 1 of Appendix 3;
‘CO2-parent engine’ means an engine selected from an engine CO2-family as specified in Appendix 3;
‘NCV’ means net calorific value of a fuel as specified in paragraph 3.2;
‘specific mass emissions’ means the total mass emissions divided by the total engine work over a defined period expressed in g/kWh;
‘specific fuel consumption’ means the total fuel consumption divided by the total engine work over a defined period expressed in g/kWh;
‘FCMC’ means fuel consumption mapping cycle;
‘Full load’ means the delivered engine torque/power at a certain engine speed when the engine is operated at maximum operator demand.
The definitions in paragraphs 3.1.5 and 3.1.6. of Annex 4 to UN/ECE Regulation 49 Rev.06 shall not apply.
The calibration laboratory facilities shall comply with the requirements of either ISO/TS 16949, ISO 9000 series or ISO/IEC 17025. All laboratory reference measurement equipment, used for calibration and/or verification, shall be traceable to national or international standards.
Engines shall be grouped into engine CO2-families defined in accordance with Appendix 3. Paragraph 4.1 explains which testruns shall be performed for the purpose of certification of one specific engine CO2-family.
All testruns performed for the purpose of certification of one specific engine CO2-family defined in accordance with Appendix 3 to this Annex shall be conducted on the same physical engine and without any changes to the setup of the engine dynamometer and the engine system, apart from the exceptions defined in paragraph 4.2 and Appendix 3.
The tests shall be conducted under ambient conditions meeting the following conditions over the whole testrun:
The parameter fa describing the laboratory test conditions, determined in accordance with paragraph 6.1 of Annex 4 to UN/ECE Regulation 49 Rev.06, shall be within the following limits: 0,96 ≤ fa ≤ 1,04.
The absolute temperature (Ta) of the engine intake air expressed in Kelvin, determined in accordance with paragraph 6.1 of Annex 4 to UN/ECE Regulation 49 Rev.06 shall be within the following limits: 283 K ≤ Ta ≤ 303 K.
The atmospheric pressure expressed in kPa, determined in accordance with paragraph 6.1 of Annex 4 to UN/ECE Regulation 49 Rev.06 shall be within the following limits: 90 kPa ≤ ps ≤ 102 kPa.
If tests are performed in test cells that are able to simulate barometric conditions other than those existing in the atmosphere at the specific test site, the applicable fa value shall be determined with the simulated values of atmospheric pressure by the conditioning system. The same reference value for the simulated atmospheric pressure shall be used for the intake air and exhaust path and all other relevant engine systems. The actual value of the simulated atmospheric pressure for the intake air and exhaust path and all other relevant engine systems shall be within the limits specified in subpoint (3).
In cases where the ambient pressure in the atmosphere at the specific test site exceeds the upper limit of 102 kPa, tests in accordance with this Annex may still be performed. In this case tests shall be performed with the specific ambient air pressure in the atmosphere.
In cases where the test cell has the ability to control temperature, pressure and/or humidity of engine intake air independent of the atmospheric conditions the same settings for those parameters shall be used for all testruns performed for the purpose of certification of one specific engine CO2-family defined in accordance with Appendix 3 to this Annex.
The test engine shall be installed in accordance with paragraphs 6.3 to 6.6 of Annex 4 to UN/ECE Regulation 49 Rev.06.
If auxiliaries/equipment necessary for operating the engine system are not installed as required in accordance with paragraph 6.3 of Annex 4 to UN/ECE Regulation 49 Rev.06, all measured engine torque values shall be corrected for the power required for driving these components for the purpose of this Annex in accordance with paragraph 6.3 of Annex 4 to UN/ECE Regulation 49 Rev.06.
The power consumption of the following engine components resulting in the engine torque required for driving these engine components shall be determined in accordance with Appendix 5 to this Annex:
fan
electrically powered auxiliaries/equipment necessary for operating the engine system
In the case of a closed crankcase, the manufacturer shall ensure that the engine's ventilation system does not permit the emission of any crankcase gases into the atmosphere. If the crankcase is of an open type, the emissions shall be measured and added to the tailpipe emissions, following the provisions set out in paragraph 6.10. of Annex 4 to UN/ECE Regulation 49 Rev.06.
During all testruns the charge air cooling system used on the test bed shall be operated under conditions which are representative for in-vehicle application at reference ambient conditions. The reference ambient conditions are defined as 293 K for air temperature and 101,3 kPa for pressure.
The laboratory charge air cooling for tests according to this regulation should comply with the provisions specified in paragraph 6.2 of Annex 4 to UN/ECE Regulation 49 Rev.06.
During all testruns the engine cooling system used on the test bed shall be operated under conditions which are representative for in-vehicle application at reference ambient conditions. The reference ambient conditions are defined as 293 K for air temperature and 101,3 kPa for pressure.
The engine cooling system should be equipped with thermostats according to the manufacturer specification for vehicle installation. If either a non-operational thermostat is installed or no thermostat is used, subpoint (3) shall apply. The setting of the cooling system shall be performed in accordance with subpoint (4).
If no thermostat is used or a non-operational thermostat is installed, the test bed system shall reflect the behavior of the thermostat under all test conditions. The setting of the cooling system shall be performed in accordance with subpoint (4).
[F1The engine coolant flow rate (or alternatively the pressure difference across the engine side of the heat exchanger) and the engine coolant temperature shall be set to a value representative for in-vehicle application at reference ambient conditions when the engine is operated at rated speed and full load with the engine thermostat in fully open position. This setting defines the coolant reference temperature. For all testruns performed for the purpose of certification of one specific engine within one engine CO 2 -family, the cooling system setting shall not be changed, neither on the engine side nor on the test bed side of the cooling system. The temperature of the test bed side cooling medium shall be kept reasonably constant by good engineering judgement. The cooling medium on the test bed side of the heat exchanger shall not exceed the nominal thermostat opening temperatur downstream of the heat exchanger.]
For all testruns performed for the purpose of certification of one specific engine within one engine CO2-family the engine coolant temperature shall be maintained between the nominal value of the thermostat opening temperature declared by the manufacturer and the coolant reference temperature in accordance with subpoint (4) as soon as the engine coolant has reached the declared thermostat opening temperature after engine cold start.
For the WHTC coldstart test performed in accordance with paragraph 4.3.3, the specific initial conditions are specified in paragraphs 7.6.1. and 7.6.2 of Annex 4 to UN/ECE Regulation 49 Rev.06. If simulation of the thermostat behaviour in accordance with subpoint (3) is applied, there shall be no coolant flow across the heat exchanger as long as the engine coolant has not reached the declared nominal thermostat opening temperature after cold start.
The respective reference fuel for the engine systems under test shall be selected from the fuel types listed in Table 1. The fuel properties of the reference fuels listed in Table 1 shall be those specified in Annex IX to Commission Regulation (EU) No 582/2011.
To ensure that the same fuel is used for all testruns performed for the purpose of certification of one specific engine CO2-family no refill of the tank or switch to another tank supplying the engine system shall occur. Exceptionally a refill or switch may be allowed if it can be ensured that the replacement fuel has exactly the same properties as the fuel used before (same production batch).
The NCV for the fuel used shall be determined by two separate measurements in accordance with the respective standards for each fuel type defined in Table 1. The two separate measurements shall be performed by two different labs independent from the manufacturer applying for certification. The lab performing the measurements shall comply with the requirements of ISO/IEC 17025. The approval authority shall ensure that the fuel sample used for determination of the NCV is taken from the batch of fuel used for all testruns.
If the two separate values for the NCV are deviating by more than 440 Joule per gram fuel, the values determined shall be void and the measurement campaign shall be repeated.
[F1The mean value of the two separate NCV that are not deviating by more than 440 Joule per gram fuel shall be documented in MJ/kg rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06.]
For gas fuels the standards for determining the NCV according to Table 1 contain the calculation of the calorific value based on the fuel composition. The gas fuel composition for determining the NCV shall be taken from the analysis of the reference gas fuel batch used for the certification tests. For the determination of the gas fuel composition used for determining the NCV only one single analysis by a lab independent from the manufacturer applying for certification shall be performed. For gas fuels the NCV shall be determined based on this single analysis instead of a mean value of two separate measurements.
[F2For gas fuels, switches between fuel tanks of different production batches are allowed exceptionally; in that case, the NCV of each used fuel batch should be calculated and the highest value should be documented.]
Reference fuels for testing
Fuel type / engine type | Reference fuel type | Standard used for determination of NCV |
---|---|---|
Diesel / CI | B7 | at least ASTM D240 or DIN 59100-1 (ASTM D4809 is recommended) |
Ethanol / CI | ED95 | at least ASTM D240 or DIN 59100-1 (ASTM D4809 is recommended) |
Petrol / PI | E10 | at least ASTM D240 or DIN 59100-1 (ASTM D4809 is recommended) |
Ethanol / PI | E85 | at least ASTM D240 or DIN 59100-1 (ASTM D4809 is recommended) |
LPG / PI | LPG Fuel B | ASTM 3588 or DIN 51612 |
[F1Natural gas / PI | G 25 or G R | ISO 6976 or ASTM 3588] |
The lubricating oil for all testruns performed in accordance with this Annex shall be a commercially available oil with unrestricted manufacturer approval under normal in-service conditions as defined in paragraph 4.2 of Annex 8 to UN/ECE Regulation 49 Rev.06. Lubricants for which the usage is restricted to certain special operation conditions of the engine system or having an unusually short oil change interval shall not be used for the purpose of testruns in accordance with this Annex. The commercially available oil shall not be modified by any means and no additives shall be added.
All testruns performed for the purpose of certification of the CO2 emissions and fuel consumption related properties of one specific engine CO2-family shall be performed with the same type of lubricating oil.
All fuel flows consumed by the whole engine system shall be captured by the fuel flow measurement system. Additional fuel flows not directly supplied to the combustion process in the engine cylinders shall be included in the fuel flow signal for all testruns performed. Additional fuel injectors (e.g. cold start devices) not necessary for the operation of the engine system shall be disconnected from the fuel supply line during all testruns performed.
The measurement equipment shall meet the requirements of paragraph 9 of Annex 4 to UN/ECE Regulation 49 Rev.06.
Notwithstanding the requirements defined in paragraph 9 of Annex 4 to UN/ECE Regulation 49 Rev.06, the measurement systems listed in Table 2 shall meet the limits defined in Table 2.
Requirements of measurement systems
a ‘Accuracy’ means the deviation of the analyzer reading from a reference value which is traceable to a national or international standard. | ||||||
b ‘Rise time’ means the difference in time between the 10 percent and 90 percent response of the final analyzer reading (t90 – t10). | ||||||
c The ‘max calibration’ values shall be 1,1 times the maximum predicted value expected during all testruns for the respective measurement system. | ||||||
Linearity | ||||||
---|---|---|---|---|---|---|
Measurement system | Intercept| xmin × (a1 – 1) + a0 | | Slopea1 | Standard error of estimate SEE | Coefficient of determinationr2 | Accuracya | Rise timeb |
Engine speed | ≤ 0,2 % max calibrationc | 0,999 - 1,001 | ≤ 0,1 % max calibrationc | ≥ 0,9985 | 0,2 % of reading or 0,1 % of max. calibrationc of speed whichever is larger | ≤ 1 s |
Engine torque | ≤ 0,5 % max calibrationc | 0,995 - 1,005 | ≤ 0,5 % max calibrationc | ≥ 0,995 | 0,6 % of reading or 0,3 % of max. calibrationc of torque whichever is larger | ≤ 1 s |
Fuel mass flow for liquid fuels | ≤ 0,5 % max calibrationc | 0,995 - 1,005 | ≤ 0,5 % max calibrationc | ≥ 0,995 | 0,6 % of reading or 0,3 % of max. calibrationc of flow whichever is larger | ≤ 2 s |
Fuel mass flow for gaseous fuels | ≤ 1 % max calibrationc | 0,99 - 1,01 | ≤ 1 % max calibrationc | ≥ 0,995 | 1 % of reading or 0,5 % of max. calibrationc of flow whichever is larger | ≤ 2 s |
Electrical Power | ≤ 1 % max calibrationc | 0,98 - 1,02 | ≤ 2 % max calibrationc | ≥ 0,990 | n.a. | ≤ 1 s |
Current | ≤ 1 % max calibrationc | 0,98 - 1,02 | ≤ 2 % max calibrationc | ≥ 0,990 | n.a. | ≤ 1 s |
Voltage | ≤ 1 % max calibrationc | 0,98 - 1,02 | ≤ 2 % max calibrationc | ≥ 0,990 | n.a. | ≤ 1 s |
‘xmin’, used for calculation of the intercept value in Table 2, shall be 0,9 times the minimum predicted value expected during all testruns for the respective measurement system.
The signal delivery rate of the measurement systems listed in Table 2, except for the fuel mass flow measurement system, shall be at least 5 Hz (≥ 10 Hz recommended). The signal delivery rate of the fuel mass flow measurement system shall be at least 2 Hz.
All measurement data shall be recorded with a sample rate of at least 5 Hz (≥ 10 Hz recommended).
A verification of the demanded requirements defined in Table 2 shall be performed for each measurement system. At least 10 reference values between xmin and the ‘max calibration’ value defined in accordance with paragraph 3.5 shall be introduced to the measurement system and the response of the measurement system shall be recorded as measured value.
For the linearity verification the measured values shall be compared to the reference values by using a least squares linear regression in accordance with paragraph A.3.2 of Appendix 3 to Annex 4 to UN/ECE Regulation 49 Rev.06.
All measurement data shall be determined in accordance with Annex 4 to UN/ECE Regulation 49 Rev.06, unless stated otherwise in this Annex.
Table 3 gives an overview of all testruns to be performed for the purpose of certification of one specific engine CO2-family defined in accordance with Appendix 3.
The fuel consumption mapping cycle in accordance with paragraph 4.3.5 and the recording of the engine motoring curve in accordance with paragraph 4.3.2 shall be omitted for all other engines except the CO2-parent engine of the engine CO2-family.
In the case that upon request of the manufacturer the provisions defined in Article 15(5) of this Regulation are applied, the fuel consumption mapping cycle in accordance with paragraph 4.3.5 and the recording of the engine motoring curve in accordance with paragraph 4.3.2 shall be performed additionally for that specific engine.
Overview of testruns to be performed
Testrun | Reference to paragraph | Required to be run for CO2-parent engine | Required to be run for other engines within CO2-family |
---|---|---|---|
Engine full load curve | 4.3.1 | yes | yes |
Engine motoring curve | 4.3.2 | yes | no |
WHTC test | 4.3.3 | yes | yes |
WHSC test | 4.3.4 | yes | yes |
Fuel consumption mapping cycle | 4.3.5 | yes | no |
Changing of the target value for the engine idle speed controller to a lower value in the electronic control unit of the engine shall be allowed for all testruns in which idle operation occurs, in order to prevent interference between the engine idle speed controller and the test bed speed controller.
The engine full load curve shall be recorded in accordance with paragraphs 7.4.1. to 7.4.5. of Annex 4 to UN/ECE Regulation 49 Rev.06.
The recording of the engine motoring curve in accordance with this paragraph shall be omitted for all other engines except the CO2-parent engine of the engine CO2-family defined in accordance with Appendix 3. In accordance with paragraph 6.1.3 the engine motoring curve recorded for the CO2-parent engine of the engine CO2-family shall also be applicable to all engines within the same engine CO2-family.
In the case that upon request of the manufacturer the provisions defined in Article 15(5) of this Regulation are applied, the recording of the engine motoring curve shall be performed additionally for that specific engine.
The engine motoring curve shall be recorded in accordance with option (b) in paragraph 7.4.7. of Annex 4 to UN/ECE Regulation 49 Rev.06. This test shall determine the negative torque required to motor the engine between maximum and minimum mapping speed with minimum operator demand.
The test shall be continued directly after the full load curve mapping according to paragraph 4.3.1. At the request of the manufacturer, the motoring curve may be recorded separately. In this case the engine oil temperature at the end of the full load curve testrun performed in accordance with paragraph 4.3.1 shall be recorded and the manufacturer shall prove to the satisfaction of the an approval authority, that the engine oil temperature at the starting point of the motoring curve meets the aforementioned temperature within ± 2 K.
At the start of the testrun for the engine motoring curve the engine shall be operated with minimum operator demand at maximum mapping speed defined in paragraph 7.4.3. of Annex 4 to UN/ECE Regulation 49 Rev.06. As soon as the motoring torque value has stabilized within ± 5 % of its mean value for at least 10 seconds, the data recording shall start and the engine speed shall be decreased at an average rate of 8 ± 1 min– 1/s from maximum to minimum mapping speed, which are defined in paragraph 7.4.3. of Annex 4 to UN/ECE Regulation 49 Rev.06.
The WHTC test shall be performed in accordance with Annex 4 to UN/ECE Regulation 49 Rev.06. The weighted emission test results shall meet the applicable limits defined in Regulation (EC) No 595/2009.
The engine full load curve recorded in accordance with paragraph 4.3.1 shall be used for the denormalization of the reference cycle and all calculations of reference values performed in accordance with paragraphs 7.4.6, 7.4.7 and 7.4.8 of Annex 4 to UN/ECE Regulation 49 Rev.06.
In addition to the provisions defined in Annex 4 to UN/ECE Regulation 49 Rev.06 the actual fuel mass flow consumed by the engine in accordance with paragraph 3.4 shall be recorded.
The WHSC test shall be performed in accordance with Annex 4 to UN/ECE Regulation 49 Rev.06. The emission test results shall meet the applicable limits defined in Regulation (EC) No 595/2009.
The engine full load curve recorded in accordance with paragraph 4.3.1 shall be used for the denormalization of the reference cycle and all calculations of reference values performed in accordance with paragraphs 7.4.6, 7.4.7 and 7.4.8 of Annex 4 to UN/ECE Regulation 49 Rev.06.
In addition to the provisions defined in Annex 4 to UN/ECE Regulation 49 Rev.06 the actual fuel mass flow consumed by the engine in accordance with paragraph 3.4 shall be recorded.
The fuel consumption mapping cycle (FCMC) in accordance with this paragraph shall be omitted for all other engines except the CO2-parent engine of the engine CO2-family. The fuel map data recorded for the CO2-parent engine of the engine CO2-family shall also be applicable to all engines within the same engine CO2-family.
In the case that upon request of the manufacturer the provisions defined in Article 15(5) of this Regulation are applied, the fuel consumption mapping cycle shall be performed additionally for that specific engine.
The engine fuel map shall be measured in a series of steady state engine operation points, as defined according to paragraph 4.3.5.2. The metrics of this map are the fuel consumption in g/h depending on engine speed in min-1 and engine torque in Nm.
If an after-treatment regeneration event occurs during the FCMC for engines equipped with exhaust after-treatment systems that are regenerated on a periodic basis defined in accordance with paragraph 6.6 of Annex 4 to UN/ECE Regulation 49 Rev.06, all measurements at that engine speed mode shall be void. The regeneration event shall be completed and afterwards the procedure shall be continued as described in paragraph 4.3.5.1.1.
If an unexpected interruption, malfunction or error occurs during the FCMC, all measurements at that engine speed mode shall be void and one of the following options how to continue shall be chosen by the manufacturer:
the procedure shall be continued as described in paragraph 4.3.5.1.1
the whole FCMC shall be repeated in accordance with paragraphs 4.3.5.4 and 4.3.5.5
The engine shall be started and warmed up in accordance with paragraph 7.4.1. of Annex 4 to UN/ECE Regulation 49 Rev.06. After warm-up, the engine shall be preconditioned by operating the engine for 20 minutes at mode 9, as defined in Table 1 of paragraph 7.2.2. of Annex 4 to UN/ECE Regulation 49 Rev.06.
The engine full load curve recorded in accordance with paragraph 4.3.1 shall be used for the denormalization of the reference values of mode 9 performed in accordance with paragraphs 7.4.6, 7.4.7 and 7.4.8 of Annex 4 to UN/ECE Regulation 49 Rev.06.
Directly after completion of preconditioning, the target values for engine speed and torque shall be changed linearly within 20 to 46 seconds to the highest target torque setpoint at the next higher target engine speed setpoint than the particular target engine speed setpoint where the interruption of the FCMC occurred. If the target setpoint is reached within less than 46 seconds, the remaining time up to 46 seconds shall be used for stabilization.
For stabilization the engine operation shall continue from that point in accordance with the test sequence specified in paragraph 4.3.5.5 without recording of measurement values.
When the highest target torque setpoint at the particular target engine speed setpoint where the interruption occurred is reached, the recording of measurement values shall be continued from that point on in accordance with the test sequence specified in paragraph 4.3.5.5.
The grid of target setpoints is fixed in a normalized way and consists of 10 target engine speed setpoints and 11 target torque setpoints. Conversion of the normalized setpoint definition to the actual target values of engine speed and torque setpoints for the individual engine under test shall be based on the engine full load curve of the CO2-parent engine of the engine CO2-family defined in accordance with Appendix 3 to this Annex and recorded in accordance with paragraph 4.3.1.
The 10 target engine speed setpoints are defined by 4 base target engine speed setpoints and 6 additional target engine speed setpoints.
The engine speeds nidle, nlo, npref, n95h and nhi shall be determined from the engine full load curve of the CO2-parent engine of the engine CO2-family defined in accordance with Appendix 3 to this Annex and recorded in accordance with paragraph 4.3.1 by applying the definitions of characteristic engine speeds in accordance with paragraph 7.4.6. of Annex 4 to UN/ECE Regulation 49 Rev.06.
The engine speed n57 shall be determined by the following equation:
n57 = 0,565 × (0,45 × nlo + 0,45 × npref + 0,1 × nhi – nidle) × 2,0327 + nidle
The 4 base target engine speed setpoints are defined as follows:
Base engine speed 1: nidle
Base engine speed 2: nA = n57 – 0,05 × (n95h – nidle)
Base engine speed 3: nB = n57 + 0,08 × (n95h – nidle)
Base engine speed 4: n95h
The potential distances between the speed setpoints shall be determined by the following equations:
dnidleA_44 = (nA – nidle) / 4
dnB95h_44 = (n95h – nB) / 4
dnidleA_35 = (nA – nidle) / 3
dnB95h_35 = (n95h – nB) / 5
dnidleA_53 = (nA – nidle) / 5
dnB95h_53 = (n95h – nB) / 3
The absolute values of potential deviations between the two sections shall be determined by the following equations:
dn44 = ABS(dnidleA_44 – dnB95h_44)
dn35 = ABS(dnidleA_35 – dnB95h_35)
dn53 = ABS(dnidleA_53 – dnB95h_53)
[F1The 6 additional target engine speed setpoints shall be determined in accordance with the following provisions:
If dn 44 is smaller than or equal to (dn 35 + 5) and also smaller than or equal to (dn 53 + 5), the 6 additional target engine speeds shall be determined by dividing each of the two ranges, one from n idle to n A and the other from n B to n 95h , into 4 equidistant sections.
If (dn 35 + 5) is smaller than dn 44 and also dn 35 is smaller than dn 53 , the 6 additional target engine speeds shall be determined by dividing the range from n idle to n A into 3 equidistant sections and the range from n B to n 95h , into 5 equidistant sections.
If (dn 53 + 5) is smaller than dn 44 and also dn 53 is smaller than dn 35 , the 6 additional target engine speeds shall be determined by dividing the range from n idle to n A into 5 equidistant sections and the range from n B to n 95h , into 3 equidistant sections.]
Figure 1 exemplarily illustrates the definition of the target engine speed setpoints according to subpoint (1) above.
The 11 target torque setpoints are defined by 2 base target torque setpoints and 9 additional target torque setpoints. The 2 base target torque setpoints are defined by zero engine torque and the maximum engine full load of the CO2-parent engine determined in accordance with paragraph 4.3.1. (overall maximum torque Tmax_overall). The 9 additional target torque setpoints are determined by dividing the range from zero torque to overall maximum torque, Tmax_overall, into 10 equidistant sections.
[F1All target torque setpoints at a particular target engine speed setpoint that exceed the limit value defined by the full load torque value at this particular target engine speed setpoint minus 5 percent of T max_overall , shall be replaced by one single target torque setpoint at full load torque at this particular target engine speed setpoint. Each of these replacement setpoints shall be measured only once during the FCMC test sequence defined in accordance with paragraph 4.3.5.5. Figure 2 exemplarily illustrates the definition of the target torque setpoints.]
The following measurement data shall be recorded:
engine speed
engine torque corrected in accordance with paragraph 3.1.2
fuel mass flow consumed by the whole engine system in accordance with paragraph 3.4
Gaseous pollutants according to the definitions in UN/ECE Regulation 49 Rev.06. Particulate pollutants and ammonia emissions are not required to be monitored during the FCMC testrun.
The measurement of gaseous pollutants shall be carried out in accordance with paragraphs 7.5.1, 7.5.2, 7.5.3, 7.5.5, 7.7.4, 7.8.1, 7.8.2, 7.8.4 and 7.8.5 of Annex 4 to UN/ECE Regulation 49 Rev.06.
For the purpose of paragraph 7.8.4 of Annex 4 to UN/ECE Regulation 49 Rev.06, the term ‘test cycle’ in the paragraph referred to shall be the complete sequence from preconditioning in accordance with paragraph 4.3.5.4 to ending of the test sequence in accordance with paragraph 4.3.5.5.
The dilution system, if applicable, and the engine shall be started and warmed up in accordance with paragraph 7.4.1. of Annex 4 to UN/ECE Regulation 49 Rev.06.
After warm-up is completed, the engine and sampling system shall be preconditioned by operating the engine for 20 minutes at mode 9, as defined in Table 1 of paragraph 7.2.2. of Annex 4 to UN/ECE Regulation 49 Rev.06, while simultaneously operating the dilution system.
The engine full load curve of the CO2-parent engine of the engine CO2-family and recorded in accordance with paragraph 4.3.1 shall be used for the denormalization of the reference values of mode 9 performed in accordance with paragraphs 7.4.6, 7.4.7 and 7.4.8 of Annex 4 to UN/ECE Regulation 49 Rev.06.
Directly after completion of preconditioning, the target values for engine speed and torque shall be changed linearly within 20 to 46 seconds to match the first target setpoint of the test sequence according to paragraph 4.3.5.5. If the first target setpoint is reached within less than 46 seconds, the remaining time up to 46 seconds shall be used for stabilization.
The test sequence consists of steady state target setpoints with defined engine speed and torque at each target setpoint in accordance with paragraph 4.3.5.2 and defined ramps to move from one target setpoint to the next.
The highest target torque setpoint at each target engine speed shall be operated with maximum operator demand.
The first target setpoint is defined at the highest target engine speed setpoint and highest target torque setpoint.
The following steps shall be performed to cover all target setpoints:
The engine shall be operated for 95 ± 3 seconds at each target setpoint. The first 55 ± 1 seconds at each target setpoint are considered as a stabilization period,. During the following period of 30 ± 1 seconds the engine speed mean value shall be controlled as follows:
The engine speed mean value shall be held at the target engine speed setpoint within ± 1 percent of the highest target engine speed.
Except for the points at full load, the engine torque mean value shall be held at the target torque setpoint within a tolerance of ± 20 Nm or ± 2 percent of the overall maximum torque, Tmax_overall, whichever is greater.
The recorded values in accordance with paragraph 4.3.5.3 shall be stored as averaged value over the period of 30 ± 1 seconds. The remaining period of 10 ± 1 seconds may be used for data post-processing and storage if necessary. During this period the engine target setpoint shall be kept.
After the measurement at one target setpoint is completed, the target value for engine speed shall be kept constant within ± 20 min– 1 of the target engine speed setpoint and the target value for torque shall be decreased linearly within 20±1 seconds to match the next lower target torque setpoint. Then the measurement shall be performed according to subpoint (1).
After the zero torque setpoint has been measured in subpoint (1), the target engine speed shall be decreased linearly to the next lower target engine speed setpoint while at the same time the target torque shall be increased linearly to the highest target torque setpoint at the next lower target engine speed setpoint within 20 to 46 seconds. If the next target setpoint is reached within less than 46 seconds, the remaining time up to 46 seconds shall be used for stabilization. Then the measurement shall be performed by starting the the stabilization procedure according to subpoint (1) and afterwards the target torque setpoints at constant target engine speed shall be adjusted according to subpoint (2).
Figure 3 illustrates the three different steps to be performed at each measurement setpoint for the test according to subpoint (1) above.
Figure 4 exemplarily illustrates the sequence of steady state measurement setpoints to be followed for the test.
Gaseous pollutants in accordance with paragraph 4.3.5.3 shall be monitored during the FCMC. The definitions of characteristic engine speeds in accordance with paragraph 7.4.6. of Annex 4 to UN/ECE R.49.06 shall apply.
The control area for emission monitoring during the FCMC shall be determined in accordance with paragraphs 4.3.5.6.1.1 and 4.3.5.6.1.2.
The engine speed range for the control area shall be defined based on the engine full load curve of the CO2-parent engine of the engine CO2-family defined in accordance with Appendix 3 to this Annex and recorded in accordance with paragraph 4.3.1.
The control area shall include all engine speeds greater than or equal to the 30th percentile cumulative speed distribution, determined from all engine speeds including idle speed sorted in ascending order, over the hotstart WHTC test cycle performed in accordance with paragraph 4.3.3 (n30) for the engine full load curve referred to the subpoint (1).
The control area shall include all engine speeds lower than or equal to nhi determined from the engine full load curve referred to in the subpoint (1)
The lower boundary of the engine torque range for the control area shall be defined based on the engine full load curve of the engine with the lowest rating of all engines within the engine CO2-family and recorded in accordance with paragraph 4.3.1.
The control area shall include all engine load points with a torque value greater than or equal to 30 percent of the maximum torque value determined from the engine full load curve referred to in subpoint (1).
Notwithstanding the provisions of subpoint (2), speed and torque points below 30 percent of the maximum power value, determined from the engine full load curve referred to in subpoint (1), shall be excluded from the control area.
Notwithstanding the provisions of subpoints (2) and (3), the upper boundary of the control area shall be based on the engine full load curve of the CO2-parent engine of the engine CO2-family defined in accordance with Appendix 3 to this Annex and recorded in accordance with paragraph 4.3.1. The torque value for each engine speed determined from the engine full load curve of the CO2-parent engine shall be increased by 5 percent of the overall maximum torque, Tmax_overall, defined in accordance with paragraph 4.3.5.2.2. The modified increased engine full load curve of the CO2-parent engine shall be used as upper boundary of the control area.
Figure 5 exemplarily illustrates the definition of the engine speed, torque and power range for the control area.
The control area defined in accordance with paragraph 4.3.5.6.1 shall be divided into a number of grid cells for emission monitoring during the FCMC.
The grid shall comprise of 9 cells for engines with a rated speed less than 3 000 min– 1 and 12 cells for engines with a rated speed greater than or equal to 3 000 min– 1. The grids shall be defined in accordance with the following provisions:
The outer boundaries of the grids are aligned to the control area defined according to paragraph 4.3.5.6.1.
2 vertical lines spaced at equal distance between engine speeds n30 and 1,1 times n95h for 9 cell grids, or 3 vertical lines spaced at equal distance between engine speeds n30 and 1,1 times n95h for 12 cell grids.
2 lines spaced at equal distance of engine torque (i.e. 1/3) at each vertical line of engine speed defined by subpoints (1) and (2)
All engine speed values in min-1 and all torque values in Newtonmeters defining the boundaries of the grid cells shall be rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06.
Figure 6 exemplarily illustrates the definition of the grid cells for the control area in the case of 9 cell grid.
The specific mass emissions of the gaseous pollutants shall be determined as average value for each grid cell defined in accordance with paragraph 4.3.5.6.2. The average value for each grid cell shall be determined as arithmetical mean value of the specific mass emissions over all engine speed and torque points measured during the FCMC located within the same grid cell.
The specific mass emissions of the single engine speed and torque measured during the FCMC shall be determined as averaged value over the 30 ± 1 seconds measurement period defined in accordance with subpoint (1) of paragraph 4.3.5.5.
If an engine speed and torque point is located directly on a line that separates different grid cells from each other, this engine speed and load point shall be taken into account for the average values of all adjacent grid cells.
The calculation of the total mass emissions of each gaseous pollutant for each engine speed and torque point measured during the FCMC, mFCMC,i in grams, over the 30 ± 1 seconds measurement period in accordance with subpoint (1) of paragraph 4.3.5.5 shall be carried out in accordance with paragraph 8 of Annex 4 to UN/ECE Regulation 49 Rev.06.
The actual engine work for each engine speed and torque point measured during the FCMC, WFCMC,i in kWh, over the 30 ± 1 seconds measurement period in accordance with subpoint (1) of paragraph 4.3.5.5 shall be determined from the engine speed and torque values recorded in accordance with paragraph 4.3.5.3.
The specific mass emissions of gaseous pollutants eFCMC,i in g/kWh for each engine speed and torque point measured during the FCMC shall be determined by the following equation:
eFCMC,i = mFCMC,i / WFCMC,i
A linear regression analysis of the actual values of engine speed (nact), engine torque (Mact) and engine power (Pact) on the respective reference values (nref, Mref, Pref) shall be performed for the FCMC. The actual values for nact, Mact and Pact shall be the determined from the values recorded in accordance with paragraph 4.3.5.3.
The ramps to move from one target setpoint to the next shall be excluded from this regression analysis.
To minimize the biasing effect of the time lag between the actual and reference cycle values, the entire engine speed and torque actual signal sequence may be advanced or delayed in time with respect to the reference speed and torque sequence. If the actual signals are shifted, both speed and torque shall be shifted by the same amount in the same direction.
The method of least squares shall be used for the regression analysis in accordance with paragraphs A.3.1 and A.3.2 of Appendix 3 to Annex 4 to UN/ECE Regulation 49 Rev.06, with the best-fit equation having the form as defined in paragraph 7.8.7 of Annex 4 to UN/ECE Regulation 49 Rev.06. It is recommended that this analysis be performed at 1 Hz.
For the purposes of this regression analysis only, omissions of points are permitted where noted in Table 4 (Permitted point omissions from regression analysis) of Annex 4 to UN/ECE Regulation 49 Rev.06 before doing the regression calculation. Additionally, all engine torque and power values at points with maximum operator demand shall be omitted for the purposes of this regression analysis only. However, points omitted for the purposes of regression analysis shall not be omitted for any other calculations in accordance with this Annex. Point omission may be applied to the whole or to any part of the cycle.
For the data to be considered valid, the criteria of Table 3 (Regression line tolerances for the WHSC) of Annex 4 to UN/ECE Regulation 49 Rev.06 shall be met.
The data obtained from the FCMC tests is valid if the specific mass emissions of the regulated gaseous pollutants determined for each grid cell in accordance with paragraph 4.3.5.6.3 meet the applicable limits for gaseous pollutants defined in paragraph 5.2.2 of Annex 10 to UN/ECE Regulation 49 Rev.06. In the case that the number of engine speed and torque points within the same grid cell is less than 3, this paragraph shall not apply for that specific grid cell.
All calculations defined in this paragraph shall be performed specifically for each engine within one engine CO2-family.
[F1Total engine work over a cycle or a defined period shall be determined from the recorded values of engine power determined in accordance with paragraph 3.1.2 of this Annex and paragraphs 6.3.5 and 7.4.8 of Annex 4 to UN/ECE Regulation 49 Rev.06.]
The engine work over a complete testcycle or over each WHTC-sub-cycle shall be determined by integrating of recorded values of engine power in accordance with the following formula:
where:
=
total engine work over the time period from t0 to t1
=
time at the start of the time period
=
time at the end of the time period
=
number of recorded values over the time period from t0 to t1
=
recorded engine power values over the time period from t0 to t1 in chronological order, where k runs from 0 at t0 to n at t1
Any recorded negative values for the fuel consumption shall be used directly and shall not be set equal to zero for the calculations of the integrated value.
The total fuel mass consumed by the engine over a complete testcycle or over each WHTC-sub-cycle shall be determined by integrating recorded values of fuel massflow in accordance with the following formula:
where:
=
total fuel mass consumed by the engine over the time period from t0 to t1
=
time at the start of the time period
=
time at the end of the time period
=
number of recorded values over the time period from t0 to t1
=
recorded fuel massflow values over the time period from t0 to t1 in chronological order, where k runs from 0 at t0 to n at t1
The correction and balancing factors, which have to be provided as input for the simulation tool, are calculated by the engine pre-processing tool based on the measured specific fuel consumption figures of the engine determined in accordance with paragraphs 5.3.1 and 5.3.2.
The specific fuel consumption figures needed for the WHTC correction factor shall be calculated from the actual measured values for the hotstart WHTC recorded in accordance with paragraph 4.3.3 as follows:
SFCmeas, Urban = Σ FCmeas, WHTC-Urban / Wact, WHTC-Urban
SFCmeas, Rural = Σ FCmeas, WHTC- Rural / Wact, WHTC- Rural
SFCmeas, MW = Σ FCmeas, WHTC-MW / Wact, WHTC-M)
where:
=
Specific fuel consumption over the WHTC-sub-cycle i [g/kWh]
=
Total fuel mass consumed by the engine over the WHTC-sub-cycle i [g] determined in accordance with paragraph 5.2
=
Total engine work over the WHTC sub-cycle i [kWh] determined in accordance with paragraph 5.1
The 3 different sub-cycles of the WHTC – urban, rural and motorway – shall be defined as follows:
urban: from cycle start to ≤ 900 seconds from cycle start
rural: from > 900 seconds to ≤ 1 380 seconds from cycle start
motorway (MW): from > 1 380 seconds from cycle start to cycle end
The specific fuel consumption figures needed for the cold-hot emission balancing factor shall be calculated from the actual measured values for both, the hotstart and coldstart WHTC test recorded in accordance with paragraph 4.3.3. The calculations shall be performed for both, the hotstart and coldstart WHTC separately as follows:
SFCmeas, hot = Σ FCmeas, hot / Wact, hot
SFCmeas, cold = Σ FCmeas, cold / Wact, cold
where:
=
Specific fuel consumption [g/kWh]
=
Total fuel consumption over the WHTC [g] determined in accordance with paragraph 5.2 of this Annex
=
Total engine work over the WHTC [kWh] determined in accordance with paragraph 5.1 of this Annex
The specific fuel consumption over the WHSC shall be calculated from the actual measured values for the WHSC recorded in accordance with paragraph 4.3.4 as follows:
SFCWHSC = (Σ FCWHSC) / (WWHSC)
where:
=
Specific fuel consumption over WHSC [g/kWh]
=
Total fuel consumption over the WHSC [g] determined in accordance with paragraph 5.2 of this Annex
=
Total engine work over the WHSC [kWh] determined in accordance with paragraph 5.1 of this Annex
The calculated specific fuel consumption over the WHSC, SFCWHSC, determined in accordance with paragraph 5.3.3 shall be adjusted to a corrected value, SFCWHSC,corr, in order to account for the difference between the NCV of the fuel used during testing and the standard NCV for the respective engine fuel technology in accordance with the following equation:
where:
=
Corrected specific fuel consumption over WHSC [g/kWh]
=
Specific fuel consumption over WHSC [g/kWh]
=
NCV of the fuel used during testing determined in accordance with paragraph 3.2 [MJ/kg]
=
Standard NCV in accordance with Table 4 [MJ/kg]
Standard net calorific values of fuel types
Fuel type / engine type | Reference fuel type | Standard NCV [MJ/kg] |
---|---|---|
Diesel / CI | B7 | 42,7 |
Ethanol / CI | ED95 | 25,7 |
Petrol / PI | E10 | 41,5 |
Ethanol / PI | E85 | 29,1 |
LPG / PI | LPG Fuel B | 46,0 |
[F1Natural gas / PI | G 25 or G R | 45,1] |
In the case that reference fuel of the type B7 (Diesel /CI) in accordance with paragraph 3.2 was used during testing, the standardization correction in accordance with paragraph 5.3.3.1 shall not be performed and the corrected value, SFCWHSC,corr, shall be set to the uncorrected value SFCWHSC.
For engines equipped with exhaust after-treatment systems that are regenerated on a periodic basis defined in accordance with paragraph 6.6.1 of Annex 4 to UN/ECE Regulation 49 Rev.06, fuel consumption shall be adjusted to account for regeneration events by a correction factor.
This correction factor, CFRegPer, shall be determined in accordance with paragraph 6.6.2 of Annex 4 to UN/ECE Regulation 49 Rev.06.
For engines equipped with exhaust after-treatment systems with continuous regeneration, defined in accordance with paragraph 6.6 of Annex 4 to UN/ECE Regulation 49 Rev.06, no correction factor shall be determined and the value of the factor CFRegPer shall be set to 1.
The engine full load curve recorded in accordance with paragraph 4.3.1 shall be used for the denormalization of the WHTC reference cycle and all calculations of reference values performed in accordance with paragraphs 7.4.6, 7.4.7 and 7.4.8 of Annex 4 to UN/ECE Regulation 49 Rev.06.
In addition to the provisions defined in Annex 4 to UN/ECE Regulation 49 Rev.06 the actual fuel mass flow consumed by the engine in accordance with paragraph 3.4 shall be recorded for each WHTC hot start test performed in accordance with paragraph 6.6.2 of Annex 4 to UN/ECE Regulation 49 Rev.06.
The specific fuel consumption for each WHTC hot start test performed shall be calculated by the following equation:
SFCmeas, m = (Σ FCmeas, m) / (Wact, m)
where:
=
Specific fuel consumption [g/kWh]
=
Total fuel consumption over the WHTC [g] determined in accordance with paragraph 5.2 of this Annex
=
Total engine work over the WHTC [kWh] determined in accordance with paragraph 5.1 of this Annex
=
Index defining each individual WHTC hot start test
The specific fuel consumption values for the individual WHTC tests shall be weighted by the following equation:
where:
=
the number of WHTC hot start tests without regeneration
=
the number of WHTC hot start tests with regeneration (minimum number is one test)
=
the average specific fuel consumption from all WHTC hot start tests without regeneration [g/kWh]
=
the average specific fuel consumption from all WHTC hot start tests with regeneration [g/kWh]
The correction factor, CFRegPer, shall be calculated by the following equation:
The engine pre-processing tool shall be executed for each engine within one engine CO2-family using the input defined in paragraph 6.1.
The output data of the engine pre-processing tool shall be the final result of the engine test procedure and shall be documented.
The following input data shall be generated by the test procedures specified in this Annex and shall be the input to the engine pre-processing tool.
The input data shall be the engine full load curve of the CO2-parent engine of the engine CO2-family defined in accordance with Appendix 3 to this Annex and recorded in accordance with paragraph 4.3.1.
In the case that upon request of the manufacturer the provisions defined in Article 15(5) of this Regulation are applied, the engine full load curve of that specific engine recorded in accordance with paragraph 4.3.1 shall be used as input data.
The input data shall be provided in the file format of ‘comma separated values’ with the separator character being the Unicode Character ‘COMMA’ (U+002C) (‘,’). The first line of the file shall be used as a header and not contain any recorded data. The recorded data shall start from the second line of the file.
The first column of the file shall be the engine speed in min– 1 rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06. The second column shall be the torque in Nm rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06.
The input data shall be the engine full load curve of the engine recorded in accordance with paragraph 4.3.1.
The input data shall be provided in the file format of ‘comma separated values’ with the separator character being the Unicode Character ‘COMMA’ (U+002C) (‘,’). The first line of the file shall be used as a header and not contain any recorded data. The recorded data shall start from the second line of the file.
The first column of the file shall be the engine speed in min– 1 rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06. The second column shall be the torque in Nm rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06.
The input data shall be the engine motoring curve of the CO2-parent engine of the engine CO2-family defined in accordance with Appendix 3 to this Annex and recorded in accordance with paragraph 4.3.2.
In the case that upon request of the manufacturer the provisions defined in Article 15(5) of this Regulation are applied, the engine motoring curve of that specific engine recorded in accordance with paragraph 4.3.2 shall be used as input data.
The input data shall be provided in the file format of ‘comma separated values’ with the separator character being the Unicode Character ‘COMMA’ (U+002C) (‘,’). The first line of the file shall be used as a header and not contain any recorded data. The recorded data shall start from the second line of the file.
The first column of the file shall be the engine speed in min– 1 rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06. The second column shall be the torque in Nm rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06.
The input data shall be the values of engine speed, engine torque and fuel massflow determined for the CO2-parent engine of the engine CO2-family defined in accordance with Appendix 3 to this Annex and recorded in accordance with paragraph 4.3.5.
In the case that upon request of the manufacturer the provisions defined in Article 15(5) of this Regulation are applied, the values of engine speed, engine torque and fuel massflow determined for that specific engine recorded in accordance with paragraph 4.3.5 shall be used as input data.
The input data shall only consist of the average measurement values of engine speed, engine torque and fuel massflow over the 30 ± 1 seconds measurement period determined in accordance with subpoint (1) of paragraph 4.3.5.5.
The input data shall be provided in the file format of ‘comma separated values’ with the separator character being the Unicode Character ‘COMMA’ (U+002C) (‘,’). The first line of the file shall be used as a header and not contain any recorded data. The recorded data shall start from the second line of the file.
The first column of the file shall be the engine speed in min– 1 rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06. The second column shall be the torque in Nm rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06. The third column shall be the fuel massflow in g/h rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06.
The input data shall be the three values for specific fuel consumption over the different sub-cycles of the WHTC – urban, rural and motorway – in g/kWh determined in accordance with paragraph 5.3.1.
The values shall be rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06.
The input data shall be the two values for specific fuel consumption over the hotstart and coldstart WHTC in g/kWh determined in accordance with paragraph 5.3.2.
The values shall be rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06.
The input data shall be the correction factor CFRegPer determined in accordance with paragraph 5.4.
For engines equipped with exhaust after-treatment systems with continuous regeneration, defined in accordance with paragraph 6.6.1 of Annex 4 to UN/ECERegulation 49 Rev.06, this factor shall be set to 1 in accordance with paragraph5.4.
The value shall be rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06.
The input data shall be the NCV of the test fuel in MJ/kg determined in accordance with paragraph 3.2.
[F1The value shall be rounded to 2 places to the right of the decimal point in accordance with ASTM E 29-06.]
The input data shall be the type of the test fuel selected in accordance with paragraph 3.2.
The input data shall be the engine idle speed, nidle, in min– 1 of the CO2-parent engine of the engine CO2-family defined in accordance with Appendix 3 to this Annex as declared by the manufacturer in the application for certification in the information document drawn up in accordance with the model set out in Appendix 2.
In the case that upon request of the manufacturer the provisions defined in Article 15(5) of this Regulation are applied, the engine idle speed of that specific engine shall be used as input data.
The value shall be rounded to the nearest whole number in accordance with ASTM E 29-06.
The input data shall be the engine idle speed, nidle, in min– 1 of the engine as declared by the manufacturer in the application for certification in the information document drawn up in accordance with the model set out in Appendix 2 to this Annex.
The value shall be rounded to the nearest whole number in accordance with ASTM E 29-06.
The input data shall be the displacement in ccm of the engine as declared by the manufacturer at the application for certification in the information document drawn up in accordance with the model set out in Appendix 2 to this Annex.
The value shall be rounded to the nearest whole number in accordance with ASTM E 29-06.
The input data shall be the rated speed in min– 1 of the engine as declared by the manufacturer at the application for certification in point 3.2.1.8. of the information document in accordance with Appendix 2 to this Annex.
The value shall be rounded to the nearest whole number in accordance with ASTM E 29-06.
The input data shall be the rated power in kW of the engine as declared by the manufacturer at the application for certification in point 3.2.1.8. of the information document in accordance with Appendix 2 to this Annex.
The value shall be rounded to the nearest whole number in accordance with ASTM E 29-06.
The input data shall be the name of the engine manufacturer as a sequence of characters in ISO8859-1 encoding.
The input data shall be the name of the engine model as a sequence of characters in ISO8859-1 encoding.
The input data shall be an unique identifier of the technical report compiled for the type approval of the specific engine. This identifier shall be provided as a sequence of characters in ISO8859-1 encoding.
Communication concerning:
| Administration stamp |
of a certificate on CO2 emission and fuel consumption related properties of an engine family in accordance with Commission Regulation (EU) 2017/2400.
Commission Regulation (EU) 2017/2400 as last amended by ….
Certification number:
Hash:
Reason for extension:
Attachments:
Information package. Test report.
Letters A, B, C, D, E corresponding to engine CO2-family members shall be replaced by the actual engine CO2-family members' names.
In case when for a certain engine characteristic same value/description applies for all engine CO2-family members the cells corresponding to A-E shall be merged.
In case the engine CO2-family consists of more than 5 members, new columns may be added.
The ‘Appendix to information document’ shall be copied and filled in for each engine within an CO2-family separately.
Explanatory footnotes can be found at the very end of this Appendix.
CO2-parent engine | Engine CO2-family members | ||||||
---|---|---|---|---|---|---|---|
A | B | C | D | E | |||
0. | General | ||||||
0.l. | Make (trade name of manufacturer) | ||||||
0.2. | Type | ||||||
0.2.1. | Commercial name(s) (if available) | ||||||
0.5. | Name and address of manufacturer | ||||||
0.8. | Name(s) and address (es) of assembly plant(s) | ||||||
0.9. | Name and address of the manufacturer's representative (if any) |
Parent engine or engine type | Engine CO2-family members | |||||||||
---|---|---|---|---|---|---|---|---|---|---|
A | B | C | D | E | ||||||
3.2. | Internal combustion engine | |||||||||
3.2.1. | Specific engine information | |||||||||
3.2.1.1. | Working principle: positive ignition/compression ignition (1)Cycle four stroke/two stroke/ rotary (1) | |||||||||
3.2.1.2. | Number and arrangement of cylinders | |||||||||
3.2.1.2.1. | Bore (3) mm | |||||||||
3.2.1.2.2. | Stroke (3) mm | |||||||||
3.2.1.2.3. | Firing order | |||||||||
3.2.1.3. | Engine capacity (4) cm3 | |||||||||
3.2.1.4. | Volumetric compression ratio (5) | |||||||||
3.2.1.5. | Drawings of combustion chamber, piston crown and, in the case of positive ignition engines, piston rings | |||||||||
3.2.1.6. | Normal engine idling speed (5) min– 1 | |||||||||
3.2.1.6.1. | High engine idling speed (5) min– 1 | |||||||||
3.2.1.7. | Carbon monoxide content by volume in the exhaust gas with the engine idling (5): % as stated by the manufacturer (positive ignition engines only) | |||||||||
3.2.1.8. | Maximum net power (6) … kW at … min– 1 (manufacturer's declared value) | |||||||||
3.2.1.9. | Maximum permitted engine speed as prescribed by the manufacturer (min– 1) | |||||||||
3.2.1.10. | Maximum net torque (6) (Nm) at (min– 1) (manufacturer's declared value) | |||||||||
3.2.1.11. | Manufacturer references of the documentation package required by paragraphs 3.1., 3.2. and 3.3. of UN/ECE Regulation 49 Rev. 06 enabling the Type Approval Authority to evaluate the emission control strategies and the systems on-board the engine to ensure the correct operation of NOx control measures | |||||||||
3.2.2. | Fuel | |||||||||
[F13.2.2.2. | Heavy duty vehicles Diesel/Petrol/LPG/NG/Ethanol (ED95)/Ethanol (E85) ( 1 ) | ] | ||||||||
3.2.2.2.1. | Fuels compatible with use by the engine declared by the manufacturer in accordance with paragraph 4.6.2. of UN/ECE Regulation 49 Rev. 06 (as applicable) | |||||||||
3.2.4. | Fuel feed | |||||||||
3.2.4.2. | By fuel injection (compression ignition only): Yes/No (1) | |||||||||
3.2.4.2.1. | System description | |||||||||
3.2.4.2.2. | Working principle: direct injection/pre-chamber/swirl chamber (1) | |||||||||
3.2.4.2.3. | Injection pump | |||||||||
3.2.4.2.3.1. | Make(s) | |||||||||
3.2.4.2.3.2. | Type(s) | |||||||||
3.2.4.2.3.3. | Maximum fuel delivery (1) (5) … mm3 /stroke or cycle at an engine speed of … min– 1 or, alternatively, a characteristic diagram(When boost control is supplied, state the characteristic fuel delivery and boost pressure versus engine speed) | |||||||||
3.2.4.2.3.4. | Static injection timing (5) | |||||||||
3.2.4.2.3.5. | Injection advance curve (5) | |||||||||
3.2.4.2.3.6. | Calibration procedure: test bench/engine (1) | |||||||||
3.2.4.2.4. | Governor | |||||||||
3.2.4.2.4.1. | Type | |||||||||
3.2.4.2.4.2. | Cut-off point | |||||||||
3.2.4.2.4.2.1. | Speed at which cut-off starts under load (min– 1) | |||||||||
3.2.4.2.4.2.2. | Maximum no-load speed (min– 1) | |||||||||
3.2.4.2.4.2.3. | Idling speed (min– 1) | |||||||||
3.2.4.2.5. | Injection piping | |||||||||
3.2.4.2.5.1. | Length (mm) | |||||||||
3.2.4.2.5.2. | Internal diameter (mm) | |||||||||
3.2.4.2.5.3. | Common rail, make and type | |||||||||
3.2.4.2.6. | Injector(s) | |||||||||
3.2.4.2.6.1. | Make(s) | |||||||||
3.2.4.2.6.2. | Type(s) | |||||||||
3.2.4.2.6.3. | Opening pressure (5): | kPa or characteristic diagram (5) | ||||||||
3.2.4.2.7. | Cold start system | |||||||||
3.2.4.2.7.1. | Make(s) | |||||||||
3.2.4.2.7.2. | Type(s) | |||||||||
3.2.4.2.7.3. | Description | |||||||||
3.2.4.2.8. | Auxiliary starting aid | |||||||||
3.2.4.2.8.1. | Make(s) | |||||||||
3.2.4.2.8.2. | Type(s) | |||||||||
3.2.4.2.8.3. | System description | |||||||||
3.2.4.2.9. | Electronic controlled injection: Yes/No (1) | |||||||||
3.2.4.2.9.1. | Make(s) | |||||||||
3.2.4.2.9.2. | Type(s) | |||||||||
3.2.4.2.9.3. | Description of the system (in the case of systems other than continuous injection give equivalent details) | |||||||||
3.2.4.2.9.3.1. | Make and type of the control unit (ECU) | |||||||||
3.2.4.2.9.3.2. | Make and type of the fuel regulator | |||||||||
3.2.4.2.9.3.3. | Make and type of the air-flow sensor | |||||||||
3.2.4.2.9.3.4. | Make and type of fuel distributor | |||||||||
3.2.4.2.9.3.5. | Make and type of the throttle housing | |||||||||
3.2.4.2.9.3.6. | Make and type of water temperature sensor | |||||||||
3.2.4.2.9.3.7. | Make and type of air temperature sensor | |||||||||
3.2.4.2.9.3.8. | Make and type of air pressure sensor | |||||||||
3.2.4.2.9.3.9. | Software calibration number(s) | |||||||||
3.2.4.3. | By fuel injection (positive ignition only): Yes/No (1) | |||||||||
3.2.4.3.1. | Working principle: intake manifold (single-/multi-point/direct injection (1)/other specify) | |||||||||
3.2.4.3.2. | Make(s) | |||||||||
3.2.4.3.3. | Type(s) | |||||||||
3.2.4.3.4. | System description (In the case of systems other than continuous injection give equivalent details) | |||||||||
3.2.4.3.4.1. | Make and type of the control unit (ECU) | |||||||||
3.2.4.3.4.2. | Make and type of fuel regulator | |||||||||
3.2.4.3.4.3. | Make and type of air-flow sensor | |||||||||
3.2.4.3.4.4. | Make and type of fuel distributor | |||||||||
3.2.4.3.4.5. | Make and type of pressure regulator | |||||||||
3.2.4.3.4.6. | Make and type of micro switch | |||||||||
3.2.4.3.4.7. | Make and type of idling adjustment screw | |||||||||
3.2.4.3.4.8. | Make and type of throttle housing | |||||||||
3.2.4.3.4.9. | Make and type of water temperature sensor | |||||||||
3.2.4.3.4.10. | Make and type of air temperature sensor | |||||||||
3.2.4.3.4.11. | Make and type of air pressure sensor | |||||||||
3.2.4.3.4.12. | Software calibration number(s) | |||||||||
3.2.4.3.5. | Injectors: opening pressure (5) (kPa) or characteristic diagram (5) | |||||||||
3.2.4.3.5.1. | Make | |||||||||
3.2.4.3.5.2. | Type | |||||||||
3.2.4.3.6. | Injection timing | |||||||||
3.2.4.3.7. | Cold start system | |||||||||
3.2.4.3.7.1. | Operating principle(s) | |||||||||
3.2.4.3.7.2. | Operating limits/settings (1) (5) | |||||||||
3.2.4.4. | Feed pump | |||||||||
3.2.4.4.1. | Pressure (5) (kPa) or characteristic diagram (5) | |||||||||
3.2.5. | Electrical system | |||||||||
3.2.5.1. | Rated voltage (V), positive/negative ground (1) | |||||||||
3.2.5.2. | Generator | |||||||||
3.2.5.2.1. | Type | |||||||||
3.2.5.2.2. | Nominal output (VA) | |||||||||
3.2.6. | Ignition system (spark ignition engines only) | |||||||||
3.2.6.1. | Make(s) | |||||||||
3.2.6.2. | Type(s) | |||||||||
3.2.6.3. | Working principle | |||||||||
3.2.6.4. | Ignition advance curve or map (5) | |||||||||
3.2.6.5. | Static ignition timing (5) (degrees before TDC) | |||||||||
3.2.6.6. | Spark plugs | |||||||||
3.2.6.6.1. | Make | |||||||||
3.2.6.6.2. | Type | |||||||||
3.2.6.6.3. | Gap setting (mm) | |||||||||
3.2.6.7. | Ignition coil(s) | |||||||||
3.2.6.7.1. | Make | |||||||||
3.2.6.7.2. | Type | |||||||||
3.2.7. | Cooling system: liquid/air (1) | |||||||||
3.2.7.2. | Liquid | |||||||||
3.2.7.2.1. | Nature of liquid | |||||||||
3.2.7.2.2. | Circulating pump(s): Yes/No (1) | |||||||||
3.2.7.2.3. | Characteristics | |||||||||
3.2.7.2.3.1. | Make(s) | |||||||||
3.2.7.2.3.2. | Type(s) | |||||||||
3.2.7.2.4. | Drive ratio(s) | |||||||||
3.2.7.3. | Air | |||||||||
3.2.7.3.1. | Fan: Yes/No (1) | |||||||||
3.2.7.3.2. | Characteristics | |||||||||
3.2.7.3.2.1. | Make(s) | |||||||||
3.2.7.3.2.2. | Type(s) | |||||||||
3.2.7.3.3. | Drive ratio(s) | |||||||||
3.2.8. | Intake system | |||||||||
3.2.8.1. | Pressure charger: Yes/No (1) | |||||||||
3.2.8.1.1. | Make(s) | |||||||||
3.2.8.1.2. | Type(s) | |||||||||
3.2.8.1.3. | Description of the system (e.g. maximum charge pressure … kPa, wastegate, if applicable) | |||||||||
3.2.8.2. | Intercooler: Yes/No (1) | |||||||||
3.2.8.2.1. | Type: air-air/air-water (1) | |||||||||
3.2.8.3. | Intake depression at rated engine speed and at 100 % load (compression ignition engines only) | |||||||||
3.2.8.3.1. | Minimum allowable (kPa) | |||||||||
3.2.8.3.2. | Maximum allowable (kPa) | |||||||||
3.2.8.4. | Description and drawings of inlet pipes and their accessories (plenum chamber, heating device, additional air intakes, etc.) | |||||||||
3.2.8.4.1. | Intake manifold description (include drawings and/or photos) | |||||||||
3.2.9. | Exhaust system | |||||||||
3.2.9.1. | Description and/or drawings of the exhaust manifold | |||||||||
3.2.9.2. | Description and/or drawing of the exhaust system | |||||||||
3.2.9.2.1. | Description and/or drawing of the elements of the exhaust system that are part of the engine system | |||||||||
3.2.9.3. | Maximum allowable exhaust back pressure at rated engine speed and at 100 % load (compression ignition engines only)(kPa) (7) | |||||||||
3.2.9.7. | Exhaust system volume (dm3) | |||||||||
3.2.9.7.1. | Acceptable Exhaust system volume: (dm3) | |||||||||
3.2.10. | Minimum cross-sectional areas of inlet and outlet ports and port geometry | |||||||||
3.2.11. | Valve timing or equivalent data | |||||||||
3.2.11.1. | Maximum lift of valves, angles of opening and closing, or timing details of alternative distribution systems, in relation to dead centers. For variable timing system, minimum and maximum timing | |||||||||
3.2.11.2. | Reference and/or setting range (7) | |||||||||
3.2.12. | Measures taken against air pollution | |||||||||
3.2.12.1.1. | Device for recycling crankcase gases: Yes/No (1)If yes, description and drawingsIf no, compliance with paragraph 6.10. of Annex 4 of UN/ECE Regulation 49 Rev. 06 required | |||||||||
3.2.12.2. | Additional pollution control devices (if any, and if not covered by another heading) | |||||||||
3.2.12.2.1. | Catalytic converter: Yes/No (1) | |||||||||
3.2.12.2.1.1. | Number of catalytic converters and elements (provide this information below for each separate unit) | |||||||||
3.2.12.2.1.2. | Dimensions, shape and volume of the catalytic converter(s) | |||||||||
3.2.12.2.1.3. | Type of catalytic action | |||||||||
3.2.12.2.1.4. | Total charge of precious metals | |||||||||
3.2.12.2.1.5. | Relative concentration | |||||||||
3.2.12.2.1.6. | Substrate (structure and material) | |||||||||
3.2.12.2.1.7. | Cell density | |||||||||
3.2.12.2.1.8. | Type of casing for the catalytic converter(s) | |||||||||
3.2.12.2.1.9. | Location of the catalytic converter(s) (place and reference distance in the exhaust line) | |||||||||
3.2.12.2.1.10. | Heat shield: Yes/No (1) | |||||||||
3.2.12.2.1.11. | Regeneration systems/method of exhaust after treatment systems, description | |||||||||
3.2.12.2.1.11.5. | Normal operating temperature range (K) | |||||||||
3.2.12.2.1.11.6. | Consumable reagents: Yes/No (1) | |||||||||
3.2.12.2.1.11.7. | Type and concentration of reagent needed for catalytic action | |||||||||
3.2.12.2.1.11.8. | Normal operational temperature range of reagent K | |||||||||
3.2.12.2.1.11.9. | International standard | |||||||||
3.2.12.2.1.11.10. | Frequency of reagent refill: continuous/maintenance (1) | |||||||||
3.2.12.2.1.12. | Make of catalytic converter | |||||||||
3.2.12.2.1.13. | Identifying part number | |||||||||
3.2.12.2.2. | Oxygen sensor: Yes/No (1) | |||||||||
3.2.12.2.2.1. | Make | |||||||||
3.2.12.2.2.2. | Location | |||||||||
3.2.12.2.2.3. | Control range | |||||||||
3.2.12.2.2.4. | Type | |||||||||
3.2.12.2.2.5. | Indentifying part number | |||||||||
3.2.12.2.3. | Air injection: Yes/No (1) | |||||||||
3.2.12.2.3.1. | Type (pulse air, air pump, etc.) | |||||||||
3.2.12.2.4. | Exhaust gas recirculation (EGR): Yes/No (1) | |||||||||
3.2.12.2.4.1. | Characteristics (make, type, flow, etc) | |||||||||
3.2.12.2.6. | Particulate trap (PT): Yes/No (1) | |||||||||
3.2.12.2.6.1. | Dimensions, shape and capacity of the particulate trap | |||||||||
3.2.12.2.6.2. | Design of the particulate trap | |||||||||
3.2.12.2.6.3. | Location (reference distance in the exhaust line) | |||||||||
3.2.12.2.6.4. | Method or system of regeneration, description and/or drawing | |||||||||
3.2.12.2.6.5. | Make of particulate trap | |||||||||
3.2.12.2.6.6. | Indentifying part number | |||||||||
3.2.12.2.6.7. | Normal operating temperature (K) and pressure (kPa) ranges | |||||||||
3.2.12.2.6.8. | In the case of periodic regeneration | |||||||||
3.2.12.2.6.8.1.1. | Number of WHTC test cycles without regeneration (n) | |||||||||
3.2.12.2.6.8.2.1. | Number of WHTC test cycles with regeneration (nR) | |||||||||
3.2.12.2.6.9. | Other systems: Yes/No (1) | |||||||||
3.2.12.2.6.9.1. | Description and operation | |||||||||
3.2.12.2.7. | On-board-diagnostic (OBD) system | |||||||||
3.2.12.2.7.0.1. | Number of OBD engine families within the engine family | |||||||||
3.2.12.2.7.0.2. | List of the OBD engine families (when applicable) | OBD engine family 1: … | ||||||||
OBD engine family 2: … | ||||||||||
etc … | ||||||||||
3.2.12.2.7.0.3. | Number of the OBD engine family the parent engine / the engine member belongs to | |||||||||
3.2.12.2.7.0.4. | Manufacturer references of the OBD-Documentation required by paragraph 3.1.4. (c) and paragraph 3.3.4. of UN/ECE Regulation 49 Rev. 06 and specified in Annex 9A of UN/ECE Regulation 49 Rev. 06 for the purpose of approving the OBD system | |||||||||
3.2.12.2.7.0.5. | When appropriate, manufacturer reference of the Documentation for installing in a vehicle an OBD equipped engine system | |||||||||
3.2.12.2.7.2. | List and purpose of all components monitored by the OBD system (8) | |||||||||
3.2.12.2.7.3. | Written description (general working principles) for | |||||||||
3.2.12.2.7.3.1. | Positive-ignition engines (8) | |||||||||
3.2.12.2.7.3.1.1. | Catalyst monitoring (8) | |||||||||
3.2.12.2.7.3.1.2. | Misfire detection (8) | |||||||||
3.2.12.2.7.3.1.3. | Oxygen sensor monitoring (8) | |||||||||
3.2.12.2.7.3.1.4. | Other components monitored by the OBD system | |||||||||
3.2.12.2.7.3.2. | Compression-ignition engines (8) | |||||||||
3.2.12.2.7.3.2.1. | Catalyst monitoring (8) | |||||||||
3.2.12.2.7.3.2.2. | Particulate trap monitoring (8) | |||||||||
3.2.12.2.7.3.2.3. | Electronic fuelling system monitoring (8) | |||||||||
3.2.12.2.7.3.2.4. | DeNOx system monitoring (8) | |||||||||
3.2.12.2.7.3.2.5. | Other components monitored by the OBD system (8) | |||||||||
3.2.12.2.7.4. | Criteria for MI activation (fixed number of driving cycles or statistical method) (8) | |||||||||
3.2.12.2.7.5. | List of all OBD output codes and formats used (with explanation of each) (8) | |||||||||
3.2.12.2.7.6.5. | OBD Communication protocol standard (8) | |||||||||
3.2.12.2.7.7. | Manufacturer reference of the OBD related information required by of paragraphs 3.1.4. (d) and 3.3.4. of UN/ECE Regulation 49 Rev. 06 for the purpose of complying with the provisions on access to vehicle OBD, or | |||||||||
3.2.12.2.7.7.1. | As an alternative to a manufacturer reference provided in paragraph 3.2.12.2.7.7. reference of the attachment to this annex that contains the following table, once completed according to the given example:Component - Fault code - Monitoring strategy - Fault detection criteria - MI activation criteria - Secondary parameters – Preconditioning - Demonstration testSCR Catalyst - P20EE - NOx sensor 1 and 2 signals - Difference between sensor 1 and sensor 2 signals - 2nd cycle - Engine speed, engine load, catalyst temperature, reagent activity, exhaust mass flow - One OBD test cycle (WHTC, hot part) - OBD test cycle (WHTC, hot part) | |||||||||
3.2.12.2.8. | Other system (description and operation) | |||||||||
3.2.12.2.8.1. | Systems to ensure the correct operation of NOx control measures | |||||||||
3.2.12.2.8.2. | Engine with permanent deactivation of the driver inducement, for use by the rescue services or in vehicles designed and constructed for use by the armed services, civil defence, fire services and forces responsible for maintaining public order: Yes/No (1) | |||||||||
3.2.12.2.8.3. | Number of OBD engine families within the engine family considered when ensuring the correct operation of NOx control measures | |||||||||
3.2.12.2.8.4. | List of the OBD engine families (when applicable) | OBD engine family 1: … OBD engine family 2: … etc … | ||||||||
3.2.12.2.8.5. | Number of the OBD engine family the parent engine / the engine member belongs to | |||||||||
3.2.12.2.8.6. | Lowest concentration of the active ingredient present in the reagent that does not activate the warning system (CDmin) (% vol) | |||||||||
3.2.12.2.8.7. | When appropriate, manufacturer reference of the Documentation for installing in a vehicle the systems to ensure the correct operation of NOx control measures | |||||||||
3.2.17. | Specific information related to gas fuelled engines for heavy-duty vehicles (in the case of systems laid out in a different manner, supply equivalent information) | |||||||||
3.2.17.1. | Fuel: LPG /NG-H/NG-L /NG-HL (1) | |||||||||
3.2.17.2. | Pressure regulator(s) or vaporiser/pressure regulator(s) (1) | |||||||||
3.2.17.2.1. | Make(s) | |||||||||
3.2.17.2.2. | Type(s) | |||||||||
3.2.17.2.3. | Number of pressure reduction stages | |||||||||
3.2.17.2.4. | Pressure in final stage minimum (kPa) – maximum. (kPa) | |||||||||
3.2.17.2.5. | Number of main adjustment points | |||||||||
3.2.17.2.6. | Number of idle adjustment points | |||||||||
3.2.17.2.7. | Type approval number | |||||||||
3.2.17.3. | Fuelling system: mixing unit / gas injection / liquid injection / direct injection (1) | |||||||||
3.2.17.3.1. | Mixture strength regulation | |||||||||
3.2.17.3.2. | System description and/or diagram and drawings | |||||||||
3.2.17.3.3. | Type approval number | |||||||||
3.2.17.4. | Mixing unit | |||||||||
3.2.17.4.1. | Number | |||||||||
3.2.17.4.2. | Make(s) | |||||||||
3.2.17.4.3. | Type(s) | |||||||||
3.2.17.4.4. | Location | |||||||||
3.2.17.4.5. | Adjustment possibilities | |||||||||
3.2.17.4.6. | Type approval number | |||||||||
3.2.17.5. | Inlet manifold injection | |||||||||
3.2.17.5.1. | Injection: single point/multipoint (1) | |||||||||
3.2.17.5.2. | Injection: continuous/simultaneously timed/sequentially timed (1) | |||||||||
3.2.17.5.3. | Injection equipment | |||||||||
3.2.17.5.3.1. | Make(s) | |||||||||
3.2.17.5.3.2. | Type(s) | |||||||||
3.2.17.5.3.3. | Adjustment possibilities | |||||||||
3.2.17.5.3.4. | Type approval number | |||||||||
3.2.17.5.4. | Supply pump (if applicable) | |||||||||
3.2.17.5.4.1. | Make(s) | |||||||||
3.2.17.5.4.2. | Type(s) | |||||||||
3.2.17.5.4.3. | Type approval number | |||||||||
3.2.17.5.5. | Injector(s) | |||||||||
3.2.17.5.5.1. | Make(s) | |||||||||
3.2.17.5.5.2. | Type(s) | |||||||||
3.2.17.5.5.3. | Type approval number | |||||||||
3.2.17.6. | Direct injection | |||||||||
3.2.17.6.1. | Injection pump/pressure regulator (1) | |||||||||
3.2.17.6.1.1. | Make(s) | |||||||||
3.2.17.6.1.2. | Type(s) | |||||||||
3.2.17.6.1.3. | Injection timing | |||||||||
3.2.17.6.1.4. | Type approval number | |||||||||
3.2.17.6.2. | Injector(s) | |||||||||
3.2.17.6.2.1. | Make(s) | |||||||||
3.2.17.6.2.2. | Type(s) | |||||||||
3.2.17.6.2.3. | Opening pressure or characteristic diagram (1) | |||||||||
3.2.17.6.2.4. | Type approval number | |||||||||
3.2.17.7. | Electronic control unit (ECU) | |||||||||
3.2.17.7.1. | Make(s) | |||||||||
3.2.17.7.2. | Type(s) | |||||||||
3.2.17.7.3. | Adjustment possibilities | |||||||||
3.2.17.7.4. | Software calibration number(s) | |||||||||
3.2.17.8. | NG fuel-specific equipment | |||||||||
3.2.17.8.1. | Variant 1 (only in the case of approvals of engines for several specific fuel compositions) | |||||||||
3.2.17.8.1.0.1. | Self-adaptive feature? Yes/No (1) | |||||||||
[ F3 ] | ||||||||||
3.2.17.8.1.1. | methane (CH4) … basis (%mole) ethane (C2H6) … basis (%mole) propane (C3H8) … basis (%mole) butane (C4H10) … basis (%mole) C5/C5+: … basis (%mole) oxygen (O2) … basis (%mole) inert (N2, He etc) … basis (%mole) | min (%mole) min (%mole) min (%mole) min (%mole) min (%mole) min (%mole) min (%mole) | max (%mole) max (%mole) max (%mole) max (%mole) max (%mole) max (%mole) max (%mole) | |||||||
3.5.5. | Specific fuel consumption and correction factors | |||||||||
3.5.5.1. | Specific fuel consumption over WHSC ‘SFCWHSC’ in accordance with paragraph 5.3.3 g/kWh | |||||||||
3.5.5.2. | Corrected specific fuel consumption over WHSC ‘SFCWHSC, corr’ in accordance with paragraph 5.3.3.1: … g/kWh | |||||||||
3.5.5.3. | Correction factor for WHTC urban part (from output of engine pre-processing tool) | |||||||||
3.5.5.4. | Correction factor for WHTC rural part (from output of engine pre-processing tool) | |||||||||
3.5.5.5. | Correction factor for WHTC motorway part (from output of engine pre-processing tool) | |||||||||
3.5.5.6. | Cold-hot emission balancing factor (from output of engine pre-processing tool) | |||||||||
3.5.5.7. | Correction factor for engines equipped with exhaust after-treatment systems that are regenerated on a periodic basis CFRegPer (from output of engine pre-processing tool) | |||||||||
3.5.5.8. | Correction factor to standard NCV (from output of engine pre-processing tool) | |||||||||
3.6. | Temperatures permitted by the manufacturer | |||||||||
3.6.1. | Cooling system | |||||||||
3.6.1.1. | Liquid cooling Maximum temperature at outlet (K) | |||||||||
3.6.1.2. | Air cooling | |||||||||
3.6.1.2.1. | Reference point | |||||||||
3.6.1.2.2. | Maximum temperature at reference point (K) | |||||||||
3.6.2. | Maximum outlet temperature of the inlet intercooler (K) | |||||||||
3.6.3. | Maximum exhaust temperature at the point in the exhaust pipe(s) adjacent to the outer flange(s) of the exhaust manifold(s) or turbocharger(s) (K) | |||||||||
3.6.4. | Fuel temperature Minimum (K) – maximum (K)For diesel engines at injection pump inlet, for gas fuelled engines at pressure regulator final stage | |||||||||
3.6.5. | Lubricant temperatureMinimum (K) – maximum (K) | |||||||||
3.8. | Lubrication system | |||||||||
3.8.1. | Description of the system | |||||||||
3.8.1.1. | Position of lubricant reservoir | |||||||||
3.8.1.2. | Feed system (by pump/injection into intake/mixing with fuel, etc.) (1) | |||||||||
3.8.2. | Lubricating pump | |||||||||
3.8.2.1. | Make(s) | |||||||||
3.8.2.2. | Type(s) | |||||||||
3.8.3. | Mixture with fuel | |||||||||
3.8.3.1. | Percentage | |||||||||
3.8.4. | Oil cooler: Yes/No (1) | |||||||||
3.8.4.1. | Drawing(s) | |||||||||
3.8.4.1.1. | Make(s) | |||||||||
3.8.4.1.2. | Type(s) |
If auxiliaries/equipment required are not fitted to the engine and/or
If auxiliaries/equipment not required are fitted to the engine.
Power absorbed at engine speeds specific for emissions test
Equipment | |||||
---|---|---|---|---|---|
Idle | Low speed | High speed | Preferred speed (2) | n95h | |
Pa Auxiliaries/equipment required according to Annex 4, Appendix 6 of UN/ECE Regulation 49 Rev. 06 | |||||
Pb Auxiliaries/equipment not required according to Annex 4, Appendix 6 of UN/ECE Regulation 49 Rev. 06 |
Value of fan constant Cind-fan for different engine speeds
Value | Engine speed | Engine speed | Engine speed | Engine speed | Engine speed | Engine speed | Engine speed | Engine speed | Engine speed | Engine speed |
---|---|---|---|---|---|---|---|---|---|---|
1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | 9 | 10 | |
engine speed [min– 1] | ||||||||||
fan constant Cind-fan,i |
… min– 1
… min– 1
… min– 1
… min– 1
… min– 1
… min– 1
… min– 1
… kW
… min– 1
… Nm
The engine CO2-family, as determined by the manufacturer, shall comply with the membership criteria defined in accordance with paragraph 5.2.3. of Annex 4 to UN/ECE Regulation 49 Rev.06. An engine CO2-family may consist of only one engine.
In addition to those membership criteria, the engine CO2-family, as determined by the manufacturer, shall comply with the membership criteria listed in paragraph 1.1 to 1.9 of this Appendix.
In addition to the parameters listed below, the manufacturer may introduce additional criteria allowing the definition of families of more restricted size. These parameters are not necessarily parameters that have an influence on the level of fuel consumption.
The CO2-parent engine of the engine CO2-family shall be selected in accordance with the following criteria:
From the number of engine CO2-families to be tested determined in accordance with paragraph 2 of this Appendix, the first two CO2-families shall be those with the highest production volumes.
The remaining number of engine CO2-families to be tested shall be randomly selected from all existing engine CO2-families and shall be agreed between the manufacturer and the approval authority.
[F1The minimum number of engines to be tested for each engine CO 2 -family, n COP,min , shall be determined by dividing n COP,base by n COP,fam , both values determined in accordance with point 2. The result for n COP,min shall be rounded to the nearest integer. If the resulting value for n COP,min is smaller than 4 it shall be set to 4, if it is greater than 19 it shall be set to 19.]
For each of the engine CO2-families determined in accordance with paragraph 3 of this Appendix a minimum number of nCOP,min engines within that family shall be tested in order to reach a pass decision in accordance with paragraph 9 of this Appendix.
The number of testruns to be performed within an engine CO2-family shall be randomly assigned to the different engines within that CO2-family and this assignment shall be agreed between the manufacturer and the approval authority.
Conformity of the certified CO2 emissions and fuel consumption related properties shall be verified by testing the engines in the WHSC test in accordance with paragraph 4.3.4.
All boundary conditions as specified in this Annex for the certification testing shall apply, except for the following:
The laboratory test conditions in accordance with paragraph 3.1.1 of this Annex. The conditions in accordance with paragraph 3.1.1 are recommended and shall not be mandatory. Deviations may occur under certain ambient conditions at the testing site and should be minimized by the use of good engineering judgment.
In case reference fuel of the type B7 (Diesel / CI) in accordance with paragraph 3.2 of this Annex is used, the determination of the NCV in accordance with paragraph 3.2 of this Annex shall not be required.
In case market fuel or reference fuel other than B7 (Diesel / CI) is used, the NCV of the fuel shall be determined in accordance with the applicable standards defined in Table 1 of this Annex. With exemption of gas engines the NCV measurement shall be performed by only one lab independent from the engine manufacturer instead of two as required in accordance with paragraph 3.2 of this Annex. [F1NCV for reference gas fuels (G 25 /G R , LPG fuel B) shall be calculated in accordance with the applicable standards in Table 1 of this Annex from the fuel analysis submitted by the reference gas fuel supplier.]
The lubricating oil shall be the one filled during engine production and shall not be changed for the purpose of testing conformity of CO2 emissions and fuel consumption related properties.
all the engines that are tested
newly produced engine, with the determination of an evolution coefficient as follows:
The specific fuel consumption shall be measured over the WHSC test once on the newly manufactured engine with a maximum run-in time of 15 hours in accordance with point 5.1 of this Appendix and in the second test before the maximum of 125 hours set in point 5.2 of this Appendix on the first engine tested.
The values for the specific fuel consumption of both tests shall be adjusted to a corrected value in accordance with paragraphs 7.2 and 7.3 of this Appendix for the respective fuel used during each of the two tests.
The evolution coefficient of the fuel consumption shall be calculated by dividing the corrected specific fuel consumption of the second test by the corrected specific fuel consumption of the first test. The evolution coefficient may have a value less than one.
for the engine used for determination of the evolution coefficient in accordance with point 5.3 (b) of this Appendix, the value from the second test
for the other engines, the values determined on the newly manufactured engine with a maximum run-in time of 15 hours in accordance with point 5.1 of this Appendix multiplied by the evolution coefficient determined in accordance with point 5.3 (b)(C) of this Appendix
The target value to assess the conformity of the certified CO2 emissions and fuel consumption related properties shall be the corrected specific fuel consumption over the WHSC, SFCWHSC,corr, in g/kWh determined in accordance with paragraph 5.3.3 and documented in the information document as part of the certificates set out in Appendix 2 to this Annex for the specific engine tested.
For diesel engines, the limit values for the assessment of conformity of one single engine tested shall be the target value determined in accordance with point (6) + 4 percent.
For gas engines, the limit values for the assessment of conformity of one single engine tested shall be the target value determined in accordance with point (6) + 5 percent.]
If the cumulative number of nonconforming tests at the nth test determined in accordance with point 9.3 of this Appendix is less than or equal to the pass decision number for the sample size given in Table 4 of Appendix 3 to UN/ECE Regulation 49 Rev.06, a pass decision is reached.
If the cumulative number of nonconforming tests at the nth test determined in accordance with point 9.3 of this Appendix is greater than or equal to the fail decision number for the sample size given in Table 4 of Appendix 3 to UN/ECE Regulation 49 Rev.06, a fail decision is reached.
Otherwise, an additional engine is tested in accordance with paragraph 4 of this Appendix and the calculation procedure in accordance with point 9.3 of this Appendix is applied to the sample increased by one more unit.
The engine torque shall be measured at engine motoring with and without fan engaged with the following procedure:
Install the fan according to product instruction before the test starts.
Warm up phase: The engine shall be warmed up according to the recommendation of the manufacturer and by practicing good engineering judgement (eg operating the engine for 20 minutes at mode 9, as defined in Table 1 of paragraph 7.2.2. of Annex 4 to UN/ECE Regulation 49 Rev.06).
[F1Stabilization phase: After the warm-up or optional warm-up step (v) is completed the engine shall be operated with minimum operator demand (motoring) at engine speed n pref for 130 ± 2 seconds with the fan disengaged (n fan_disengage < 0,75 * n engine * r fan ). The first 60 ± 1 seconds of this period are considered as a stabilization period, during which the actual engine speed shall be held within ± 5 min – 1 of n pref .]
Measurement phase: During the following period of 60 ± 1 seconds the actual engine speed shall be held within ± 2 min– 1 of npref and the coolant temperature within ± 5 °C while the torque for motoring the engine with the fan disengaged, the fan speed and the engine speed shall be recorded as an average value over this period of 60 ± 1 seconds. The remaining period of 10 ± 1 seconds shall be used for data post-processing and storage if necessary.
Optional warmup phase: Upon manufacturer's request and according to good engineering judgement step (ii) can be repeated (e.g. if the temperature has dropped more than 5 °C)
Stabilization phase: After the optional warm-up is completed the engine shall be operated with minimum operator demand (motoring) at engine speed npref for 130 ± 2 seconds with the fan engaged (nfan_engage > 0,9 * nengine * rfan) The first 60 ± 1 seconds of this period are considered as a stabilization period, during which the actual engine speed shall be held within ± 5 min– 1 of npref.
Measurement phase: During the following period of 60 ± 1 seconds the actual engine speed shall be held within ± 2 min– 1 of npref and the coolant temperature within ± 5 °C while the torque for motoring the engine with the fan engaged, the fan speed and the engine speed shall be recorded as an average value over this period of 60 ± 1 seconds. The remaining period of 10±1 seconds shall be used for data post-processing and storage if necessary.
Steps (iii) to (vii) shall be repeated at engine speeds n95h and nhi instead of npref, with an optional warmup step (v) before each stabilization step if needed to maintain a stable coolant temperature (± 5 °C), according to good engineering judgement.
If the standard deviation of all calculated Ci according to the equation below at the three speeds npref, n95h and nhi is equal or higher than 3 percent, the measurement shall be performed for all engine speeds defining the grid for the fuel mapping procedure (FCMC) according to paragraph 4.3.5.2.1.
The actual fan constant shall be calculated from the measurement data according to the following equation:
where:
fan constant at certain engine speed
measured engine torque at motoring with fan disengaged (Nm)
measured engine torque at motoring with fan engaged (Nm)
fan speed with fan engaged (min– 1)
fan speed with fan disengaged min– 1)
ratio of the speed of the engine-side of the fan clutch to the speed of the crankshaft]
If the standard deviation of all calculated Ci at the three speeds npref, n95h and nhi is less than 3 %, an average value Cavg-fan determined over the three speeds npref, n95h and nhi shall be used for the fan constant.
If the standard deviation of all calculated Ci at the three speeds npref, n95h and nhi is equal or higher than 3 %, individual values determined for all engine speeds according to point (ix) shall be used for the fan constant Cind-fan,i. The value of the fan constant for the actual engine speed Cfan, shall be determined by linear interpolation between the individual values Cind-fan,i of the fan constant.
The engine torque for driving the fan shall be calculated according to the following equation:
Mfan = Cfan · nfan 2 · 10– 6
where:
engine torque for driving fan (Nm)
fan constant Cavg-fan or Cind-fan,i corresponding to nengine
The mechanical power consumed by the fan shall be calculated from the engine torque for driving the fan and the actual engine speed. Mechanical power and engine torque shall be taken into account in accordance with paragraph 3.1.2.
The electric power supplied externally to electric engine components shall be measured. This measured value shall be corrected to mechanical power by dividing it by a generic efficiency value of 0,65. This mechanical power and the corresponding engine torque shall be taken into account in accordance with paragraph 3.1.2.
In the case of an engine being certified in accordance with this Annex, the engine shall bear:
1 for Germany;
2 for France;
3 for Italy;
4 for the Netherlands;
5 for Sweden;
6 for Belgium;
7 for Hungary;
8 for the Czech Republic;
9 for Spain;
11 for the United Kingdom;
12 for Austria;
13 for Luxembourg;
17 for Finland;
18 for Denmark;
19 for Romania;
20 for Poland;
21 for Portugal;
23 for Greece;
24 for Ireland;
25 for Croatia;
26 for Slovenia;
27 for Slovakia;
29 for Estonia;
32 for Latvia;
34 for Bulgaria;
36 for Lithuania;
49 for Cyprus;
50 for Malta
For this Regulation, the sequence number shall be 00.
The above certification mark affixed to an engine shows that the type concerned has been certified in Poland (e20), pursuant to this Regulation. The first two digits (00) are indicating the sequence number assigned to the latest technical amendment to this Regulation. The following letter indicates that the certificate was granted for an engine (E). The last four digits (0004) are those allocated by the approval authority to the engine as the base approval number.
The above certification mark affixed to an engine shows that the type concerned has been certified in Poland (e20), pursuant to Regulation (EU) No 582/2011. The ‘ D ’ indicates Diesel followed by a ‘ C ’ for the emission stage followed by four digits (0004) which are those allocated by the approval authority to the engine as the base approval number for Regulation (EU) No 582/2011. After the slash the first two figures are indicating the sequence number assigned to the latest technical amendment to this Regulation, followed by a letter ‘ E ’ for engine, followed by four digits allocated by the approval authority for the purpose of certification in accordance with this Regulation ( ‘ base approval number ’ to this regulation).]
eX*YYYY/YYYY*ZZZZ/ZZZZ*E*0000*00
Section 1 | Section 2 | Section 3 | Additional letter to Section 3 | Section 4 | Section 5 |
---|---|---|---|---|---|
Indication of country issuing the certification | HDV CO 2 certification Regulation (2017/2400) | Latest amending Regulation (ZZZZ/ZZZZ) | E — engine | Base certification number 0000 | Extension 00] |
This Appendix describes the list of parameters to be provided by the component manufacturer as input to the simulation tool. The applicable XML schema as well as example data are available at the dedicated electronic distribution platform.
The XML is automatically generated by the engine pre-processing tool.
Unique identifier as used in the simulation tool for a specific input parameter or set of input data]
Data type of the parameter
sequence of characters in ISO8859-1 encoding
sequence of characters in ISO8859-1 encoding, no leading/trailing whitespace
date and time in UTC time in the format: YYYY-MM-DDTHH:MM:SSZ with italic letters denoting fixed characters e.g. ‘2002-05-30T09:30:10Z’
value with an integral data type, no leading zeros, e.g. ‘1800’
fractional number with exactly X digits after the decimal sign (‘.’) and no leading zeros e.g. for ‘double, 2’: ‘2345.67’; for ‘double, 4’: ‘45.6780’
physical unit of the parameter
Input parameters ‘Engine/General’
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
Manufacturer | P200 | token | [-] | |
Model | P201 | token | [-] | |
[F1CertificationNumber | P202 | token | [-] | ] |
Date | P203 | dateTime | [-] | Date and time when the component-hash is created |
AppVersion | P204 | token | [-] | Version number of engine pre-processing tool |
Displacement | P061 | int | [cm3] | |
IdlingSpeed | P063 | int | [1/min] | |
RatedSpeed | P249 | int | [1/min] | |
RatedPower | P250 | int | [W] | |
MaxEngineTorque | P259 | int | [Nm] | |
WHTCUrban | P109 | double, 4 | [-] | |
WHTCRural | P110 | double, 4 | [-] | |
WHTCMotorway | P111 | double, 4 | [-] | |
BFColdHot | P159 | double, 4 | [-] | |
CFRegPer | P192 | double, 4 | [-] | |
CFNCV | P260 | double, 4 | [-] | |
[F1FuelType | P193 | string | [-] | Allowed values: ‘ Diesel CI ’ , ‘ Ethanol CI ’ , ‘ Petrol PI ’ , ‘ Ethanol PI ’ , ‘ LPG PI ’ , ‘ NG PI ’ , ‘ NG CI ’] |
Input parameters ‘Engine/FullloadCurve’ for each grid point in the full load curve
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
EngineSpeed | P068 | double, 2 | [1/min] | |
MaxTorque | P069 | double, 2 | [Nm] | |
DragTorque | P070 | double, 2 | [Nm] |
Input parameters ‘Engine/FuelMap’ for each grid point in the fuel map
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
EngineSpeed | P072 | double, 2 | [1/min] | |
Torque | P073 | double, 2 | [Nm] | |
FuelConsumption | P074 | double, 2 | [g/h] |
This Appendix describes the most important evaluation steps and underlying basic equations that are performed by the engine pre-processing tool. The following steps are performed during evaluation of the input data in the order listed:
This annex describes the certification provisions regarding the torque losses of transmissions, torque converter (TC), other torque transferring components (OTTC) and additional driveline components (ADC) for heavy duty vehicles. In addition it defines calculation procedures for the standard torque losses.
Torque converter (TC), other torque transferring components (OTTC) and additional driveline components (ADC) can be tested in combination with a transmission or as a separate unit. In the case that those components are tested separately the provisions of section 4, 5 and 6 apply. Torque losses resulting from the drive mechanism between the transmission and those components can be neglected.
For the purposes of this Annex the following definitions shall apply:
‘Transfer case’ means a device that splits the engine power of a vehicle and directs it to the front and rear drive axles. It is mounted behind the transmission and both front and rear drive shafts connect to it. It comprises either a gearwheel set or a chain drive system in which the power is distributed from the transmission to the axles. The transfer case will typically have the ability to shift between standard drive mode (front or rear wheel drive), high range traction mode (front and rear wheel drive), low range traction mode and neutral;
‘Gear ratio’ means the forward gear ratio of the speed of the input shaft (towards prime mover) to the speed of the output shaft (towards driven wheels) without slip (i = nin/nout );
‘Ratio coverage’ means the ratio of the largest to the smallest forward gear ratios in a transmission: φtot = imax/imin ;
‘Compound transmission’ means a transmission, with a large number of forward gears and/or large ratio coverage, composed of sub-transmissions, which are combined to use most power-transferring parts in several forward gears;
‘Main section’ means the sub-transmission that has the largest number of forward gears in a compound transmission;
‘Range section’ means a sub-transmission normally in series connection with the main section in a compound transmission. A range section usually has two shiftable forward gears. The lower forward gears of the complete transmission are embodied using the low range gear. The higher gears are embodied using the high range gear;
‘Splitter’ means a design that splits the main section gears in two (usually) variants, low- and high split gears, whose gear ratios are close compared to the ratio coverage of the transmission. A splitter can be a separate sub-transmission, an add-on device, integrated with the main section or a combination thereof;
‘Tooth clutch’ means a clutch where torque is transferred mainly by normal forces between mating teeth. A tooth clutch can either be engaged or disengaged. It is operated in load-free conditions, only (e.g., at gear shifts in a manual transmission);
‘Angle drive’ means a device that transmits rotational power between non-parallel shafts, often used with transversely oriented engine and longitudinal input to driven axle;
‘Friction clutch’ means clutch for transfer of propulsive torque, where torque is sustainably transferred by friction forces. A friction clutch can transmit torque while slipping, it can thereby (but does not have to) be operated at start-offs and at powershifts (retained power transfer during a gear shift);
‘Synchroniser’ means a type of tooth clutch where a friction device is used to equalise the speeds of the rotating parts to be engaged;
‘Gear mesh efficiency’ means the ratio of output power to input power when transmitted in a forward gear mesh with relative motion;
‘Crawler gear’ means a low forward gear (with speed reduction ratio that is larger than for the non-crawler gears) that is designed to be used infrequently, e.g., at low-speed manoeuvres or occasional up-hill start-offs;
‘Power take-off (PTO)’ means a device on a transmission or an engine to which an auxiliary driven device, e.g., a hydraulic pump, can be connected;
‘Power take-off drive mechanism’ means a device in a transmission that allows the installation of a power take-off (PTO);
‘Lock-up clutch’ means a friction clutch in a hydrodynamic torque converter; it can connect the input and output sides, thereby eliminating the slip;
‘Start-off clutch’ means a clutch that adapts speed between engine and driven wheels when the vehicle starts off. The start-off clutch is usually located between engine and transmission;
‘Synchronised Manual Transmission (SMT)’ means a manually operated transmission with two or more selectable speed ratios that are obtained using synchronisers. Ratio changing is normally achieved during a temporary disconnection of the transmission from the engine using a clutch (usually the vehicle start-off clutch);
‘Automated Manual Transmission or Automatic Mechanically-engaged Transmission (AMT)’ means an automatically shifting transmission with two or more selectable speed ratios that are obtained using tooth clutches (un-/synchronised). Ratio changing is achieved during a temporary disconnection of the transmission from the engine. The ratio shifts are performed by an electronically controlled system managing the timing of the shift, the operation of the clutch between engine and gearbox and the speed and torque of the engine. The system selects and engages the most suitable forward gear automatically, but can be overridden by the driver using a manual mode;
‘Dual Clutch Transmission (DCT)’ means an automatically shifting transmission with two friction clutches and several selectable speed ratios that are obtained by the use of tooth clutches. The ratio shifts are performed by an electronically controlled system managing the timing of the shift, the operation of the clutches and the speed and torque of the engine. The system selects the most suitable gear automatically, but can be overridden by the driver using a manual mode;
‘Retarder’ means an auxiliary braking device in a vehicle powertrain; aimed for permanent braking;
‘Case S’ means the serial arrangement of a torque converter and the connected mechanical parts of the transmission;
‘Case P’ means the parallel arrangement of a torque converter and the connected mechanical parts of the transmission (e.g. in power split installations);
‘Automatic Powershifting Transmission (APT)’ means an automatically shifting transmission with more than two friction clutches and several selectable speed ratios that are obtained mainly by the use of those friction clutches. The ratio shifts are performed by an electronically controlled system managing the timing of the shift, the operation of the clutches and the speed and torque of the engine. The system selects the most suitable gear automatically, but can be overridden by the driver using a manual mode. Shifts are normally performed without traction interruption (friction clutch to friction clutch);
‘Oil conditioning system’ means an external system that conditions the oil of a transmission at testing. The system circulates oil to and from the transmission. The oil is thereby filtered and/or temperature conditioned;
‘Smart lubrication system’ means a system that will affect the load independent losses (also called spin losses or drag losses) of the transmission depending on the input torque and/or power flow through the transmission. Examples are controlled hydraulic pressure pumps for brakes and clutches in an APT, controlled variable oil level in the transmission, controlled variable oil flow/pressure for lubrication and cooling in the transmission. Smart lubrication can also include control of the oil temperature of the transmission, but smart lubrication systems that are designed only for controlling the temperature are not considered here, since the transmission testing procedure has fixed testing temperatures;
‘Transmission electric auxiliary’ means an electric auxiliary used for the function of the transmission during running steady state operation. A typical example is an electric cooling/lubrication pump (but not electric gear shift actuators and electronic control systems including electric solenoid valves, since they are low energy consumers, especially at steady state operation);
‘Oil type viscosity grade’ means a viscosity grade as defined by SAE J306;
‘Factory fill oil’ means the oil type viscosity grade that is used for the oil fill in the factory and which is intended to stay in the transmission, torque converter, other torque transferring component or in an additional driveline component for the first service interval;
‘Gearscheme’ means the arrangement of shafts, gearwheels and clutches in a transmission;
‘Powerflow’ means the transfer path of power from input to output in a transmission via shafts, gearwheels and clutches.
For testing the losses of a transmission the torque loss map for each individual transmission type shall be measured. Transmissions may be grouped into families with similar or equal CO2-relevant data following the provisions of Appendix 6 to this Annex.
For the determination of the transmission torque losses, the applicant for a certificate shall apply one of the following methods for each single forward gear (crawler gears excluded).
Option 1: Measurement of the torque independent losses, calculation of the torque dependent losses.
Option 2: Measurement of the torque independent losses, measurement of the torque loss at maximum torque and interpolation of the torque dependent losses based on a linear model
Option 3: Measurement of the total torque loss.
The torque loss Tl ,in on the input shaft of the transmission shall be calculated by
Tl,in (nin , Tin , gear) = T l,in,min_loss + fT * Tin + floss_corr * Tin + T l,in,min_el + fel_corr * Tin
The correction factor for the torque dependent hydraulic torque losses shall be calculated by
The correction factor for the torque dependent electric torque losses shall be calculated by
The torque loss at the input shaft of the transmission caused by the power consumption of transmission electric auxiliary shall be calculated by
where:
=
Torque loss related to input shaft [Nm]
=
Torque independent loss at minimum hydraulic loss level (minimum main pressure, cooling/lubrication flows etc.), measured with free rotating output shaft from testing without load [Nm]
=
Torque independent loss at maximum hydraulic loss level (maximum main pressure, cooling/lubrication flows etc.), measured with free rotating output shaft from testing without load [Nm]
=
Loss correction for hydraulic loss level depending on input torque [-]
=
Speed at the transmission input shaft (downstream of torque converter, if applicable) [rpm]
=
Torque loss coefficient = 1 – ηT
=
Torque at the input shaft [Nm]
=
Torque dependent efficiency (to be calculated); for a direct gear fT = 0,007 (ηT = 0,993) [-]
=
Loss correction for electric power loss level depending on input torque [-]
=
Additional torque loss on input shaft by electric consumers [Nm]
=
Additional torque loss on input shaft by electric consumers corresponding to minimum electric power [Nm]
=
Additional torque loss on input shaft by electric consumers corresponding to maximum electric power [Nm]
=
Electric power consumption of electric consumers in transmission measured during transmission loss testing [W]
=
Maximum allowed input torque for any forward gear in the transmission [Nm]
In case of multiple parallel and nominally equal power flows, e.g., twin countershafts or several planet gearwheels in a planetary gear set, that can be treated as one power flow in this section.
:
ηm = 0,986
:
ηm = 0,993
:
ηm = 0,97
(Angle drive losses may alternatively be determined by separate testing as described in paragraph 6. of this Annex)
η Tg = η b * η m,1 * η m,2 * […] * η m,n
fTg = 1 – η Tg
Tl,inTg = fTg * Tin
where:
=
Torque dependent efficiency of the ring-to-planet gear mesh = 99,3 % [-]
=
Torque dependent efficiency of the planet-to-sun gear mesh = 98,6 % [-]
=
Number of teeth of the sun gearwheel of the range section [-]
=
Number of teeth of the ring gearwheel of the range section [-]
The planetary range section shall be regarded as an additional gear mesh within the countershaft main section, and its torque dependent efficiency ηlowrange shall be included in the determination of the total torque dependent efficiencies ηTg for the low-range gears in the calculation in 3.1.1.4.
In this case, for each indirect gear g, the following steps shall be performed:
Nsun–carrier = Nsun – Ncarrier
Nring–carrier = Nring – Ncarrier
where:
=
Rotational speed of sun gearwheel [rad/s]
=
Rotational speed of ring gearwheel [rad/s]
=
Rotational speed of carrier [rad/s]
For each ordinary, non-planetary gear set, the power P shall be calculated by:
P 1 = N 1 · T 1
P 2 = N 2 · T 2
where:
=
Power of gear mesh [W]
=
Rotational speed of gearwheel [rad/s]
=
Torque of gearwheel [Nm]
For each planetary gear set, the virtual power of sun Pv,sun and ring gearwheels Pv,ring shall be calculated by:
Pv,sun = Tsun · (Nsun – Ncarrier ) = Tsun · Nsun/carrier
Pv,ring = Tring · (Nring – Ncarrier ) = Tring · Nring/carrier
where:
=
Virtual power of sun gearwheel [W]
=
Virtual power of ring gearwheel [W]
=
Torque of sun gearwheel [Nm]
=
Torque of carrier [Nm]
=
Torque of ring gearwheel [Nm]
Negative virtual power results shall indicate power leaving the gear set, positive virtual power results shall indicate power going into the gear set.
The loss-adjusted powers Padj of the gear meshes shall be computed in the following way:
For each ordinary, non-planetary gear set, the negative power shall be multiplied by the appropriate torque dependent efficiency ηm :
Pi > 0 ⇒ Pi,adj = Pi
Pi < 0 ⇒ Pi,adj = Pi · η mi
where:
=
Loss-adjusted powers of the gear meshes [W]
=
Torque dependent efficiency (appropriate to gear mesh; see 3.1.1.2.) [-]
For each planetary gear set, the negative virtual power shall be multiplied by the torque-dependent efficiencies of sun-to-planet ηmsun and ring-to-planet ηmring :
Pv,i ≥ 0 ⇒ Pi,adj = Pv,i
Pv,i < 0 ⇒ Pi,adj = Pi · ηmsun · ηmring
where:
=
Torque dependent efficiency of sun-to-planet [-]
=
Torque dependent efficiency of ring-to-planet [-]
Pm,loss = ΣPi,adj
where:
=
All gearwheels with a fix rotational axis [-]
=
Torque dependent gear mesh power loss of the transmission system [W]
fT,bear = 1 – η bear = 1 – 0,995 = 0,005
and the torque dependent loss coefficient for the gear mesh
shall be added to receive the total torque dependent loss coefficient fT for the transmission system:
fT = fT,gearmesh + fT,bear
where:
=
Total torque dependent loss coefficient for the transmission system [-]
=
Torque dependent loss coefficient for the bearings [-]
=
Torque dependent loss coefficient for the gear meshes [-]
=
Fixed input power of the transmission; Pin = (1 Nm * 1 rad/s) [W]
Tl,inT = fT * Tin
where:
=
Torque dependent loss related to input shaft [Nm]
=
Torque at the input shaft [Nm]
The transmission used for the measurements shall be in accordance with the drawing specifications for series production transmissions and shall be new.
Modifications to the transmission to meet the testing requirements of this Annex, e.g. for the inclusion of measurement sensors or adaption of an external oil conditioning system are permitted.
The tolerance limits in this paragraph refer to measurement values without sensor uncertainty.
[F1Total tested time per transmission individual and gear shall not exceed 5 times the actual testing time per gear (allowing re-testing of transmission if needed due to measuring or rig error).]
The same transmission individual may be used for a maximum of 10 different tests, e.g. for tests of transmission torque losses for variants with and without retarder (with different temperature requirements) or with different oils. If the same transmission individual is used for tests of different oils, the recommended factory fill oil shall be tested first.
It is not permitted to run a certain test multiple times to choose a test series with the lowest results.
Upon request of the approval authority the applicant for a certificate shall specify and prove the conformity with the requirements defined in this Annex.
To subtract influences caused by the test rig setup (e.g. bearings, clutches) from the measured torque losses, differential measurements are permitted to determine these parasitic torques. The measurements shall be performed at the same speed steps and same test rig bearing temperature(s) ± 3 K used for the testing. The torque sensor measurement uncertainty shall be below 0,3 Nm.
On request of the applicant a run-in procedure may be applied to the transmission. The following provisions shall apply for a run-in procedure.
The ambient temperature during the test shall be in a range of 25 °C ± 10 K.
The ambient temperature shall be measured 1 m laterally from the transmission.
The ambient temperature limit shall not apply for the run-in procedure.
Except for the oil, no external heating is allowed.
During measurement (except stabilization) the following temperature limits shall apply:
For SMT/AMT/DCT transmissions, the drain plug oil temperature shall not exceed 83 °C when measuring without retarder and 87 °C with retarder mounted to the transmission. If measurements of a transmission without retarder are to be combined with separate measurements of a retarder, the lower temperature limit shall apply to compensate for the retarder drive mechanism and step-up gear and for the clutch in case of a disengageable retarder.
For torque converter planetary transmissions and for transmissions having more than two friction clutches, the drain plug oil temperature shall not exceed 93 °C without retarder and 97 °C with retarder.
To apply the above defined increased temperature limits for testing with retarder, the retarder shall be integrated in the transmission or have an integrated cooling or oil system with the transmission.
During the run-in, the same oil temperature specifications as for regular testing shall apply.
Exceptional oil temperature peaks up to 110 °C are allowed for the following conditions:
during run-in procedure up to maximum of 10 % of the applied run-in time,
during stabilization time.
The oil temperature shall be measured at the drain plug or in the oil sump.
New, recommended first fill oil for the European market shall be used in the test. The same oil fill may be used for run-in and torque measurement.
If multiple oils are recommended for first fill, they are considered to be equal if the oils have a kinematic viscosity within 10 % of each other at the same temperature (within the specified tolerance band for KV100). Any oil with lower viscosity than the oil used in the test shall be considered to result in lower losses for the tests performed within this option. Any additional first fill oil must fall either in the 10 % tolerance band or have lower viscosity than the oil in the test to be covered by the same certificate.
The oil level shall meet the nominal specifications for the transmission.
If an external oil conditioning system is used, the oil inside the transmission shall be kept to the specified volume that corresponds to the specified oil level.
To guarantee that the external oil conditioning system is not influencing the test, one test point shall be measured with the conditioning system both on and off. The deviation between the two measurements of the torque loss (= input torque) shall be less than 5 %. The test point is specified as follows:
gear = highest indirect gear,
input speed = 1 600 rpm,
temperatures as specified under 3.1.2.5.
For transmissions with hydraulic pressure control or a smart lubrication system, the measurement of torque independent losses shall be performed with two different settings: first with the transmission system pressure set to at least the minimum value for conditions with engaged gear and a second time with the maximum possible hydraulic pressure (see 3.1.6.3.1).
The calibration laboratory facilities shall comply with the requirements of either ISO/TS 16949, ISO 9000 series or ISO/IEC 17025. All laboratory reference measurement equipment, used for calibration and/or verification, shall be traceable to national (international) standards.
The torque sensor measurement uncertainty shall be below 0,3 Nm.
The use of torque sensors with higher measurement uncertainties is allowed if the part of the uncertainty exceeding 0,3 Nm can be calculated and is added to the measured torque loss as described in 3.1.8. Measurement uncertainty.
The uncertainty of the speed sensors shall not exceed ± 1 rpm.
The uncertainty of the temperature sensors for the measurement of the ambient temperature shall not exceed ± 1,5 K.
The uncertainty of the temperature sensors for the measurement of the oil temperature shall not exceed ± 1,5 K.
The uncertainty of the pressure sensors shall not exceed 1 % of the maximum measured pressure.
The uncertainty of the voltmeter shall not exceed 1 % of the maximum measured voltage.
The uncertainty of the amperemeter shall not exceed 1 % of the maximum measured current.
At least the following signals shall be recorded during the measurement:
Input torques [Nm]
Input rotational speeds [rpm]
Ambient temperature [°C]
Oil temperature [°C]
If the transmission is equipped with a shift and/or clutch system that is controlled by hydraulic pressure or with a mechanically driven smart lubrication system, additionally to be recorded:
Oil pressure [kPa]
If the transmission is equipped with transmission electric auxiliary, additionally to be recorded:
Voltage of transmission electric auxiliary [V]
Current of transmission electric auxiliary [A]
For differential measurements for the compensation of influences caused by the test rig setup, additionally shall be recorded:
Test rig bearing temperature [°C]
The sampling and recording rate shall be 100 Hz or higher.
A low pass filter shall be applied to reduce measurement errors.
The zero-signal of the torque sensor(s) shall be measured. For the measurement the sensor(s) shall be installed in the test rig. The drivetrain of the test rig (input & output) shall be free of load. The measured signal deviation from zero shall be compensated.
The torque loss shall be measured for the following speed steps (speed of the input shaft): 600, 900, 1 200, 1 600, 2 000, 2 500, 3 000, […] rpm up to the maximum speed per gear according to the specifications of the transmission or the last speed step before the defined maximum speed.
The speed ramp (time for the change between two speed steps) shall not extend 20 seconds.
If the transmission is equipped with smart lubrication systems and/or transmission electric auxiliaries, the measurement shall be conducted with two measurement settings of of these systems:
A first measurement sequence (3.1.6.3.2. to 3.1.6.3.4.) shall be performed with the lowest power consumption by hydraulical and electrical systems when operated in the vehicle (low loss level).
The second measurement sequence shall be performed with the systems set to work with the highest possible power consumption when operated in the vehicle (high loss level).
The measurements shall be performed beginning with the lowest up to the highest speed.
For each speed step a minimum of 5 seconds stabilization time within the temperature limits defined in 3.1.2.5 is required. If needed, the stabilization time may be extended by the manufacturer to maximum 60 seconds. Oil and ambient temperatures shall be recorded during the stabilization.
After the stabilization time, the measurement signals listed in 3.1.5. shall be recorded for the test point for 05-15 seconds.
Each measurement shall be performed two times per measurement setting.
Tloss = Tin
Pel = I * U
It is allowed to subtract influences caused by the test rig setup from the torque losses (3.1.2.2.).
The part of the calculated total uncertainty UT,loss exceeding 0,3 Nm shall be added to Tloss for the reported torque loss Tloss,rep . If UT,loss is smaller than 0,3 Nm, then Tloss,rep = Tloss .
Tloss,rep = Tloss + MAX (0, (UT,loss – 0,3 Nm))
The total uncertainty UT,loss of the torque loss shall be calculated based on the following parameters:
Temperature effect
Parasitic loads
Calibration error (incl. sensitivity tolerance, linearity, hysteresis and repeatability)
The total uncertainty of the torque loss (UT,loss ) is based on the uncertainties of the sensors at 95 % confidence level. The calculation shall be done as the square root of the sum of squares (‘Gaussian law of error propagation’).
wpara = senspara * ipara
where:
=
Measured torque loss (uncorrected) [Nm]
=
Reported torque loss (after uncertainty correction) [Nm]
=
Total expanded uncertainty of torque loss measurement at 95 % confidence level [Nm]
=
Uncertainty of input torque loss measurement [Nm]
=
Uncertainty by temperature influence on current torque signal [Nm]
=
Temperature influence on current torque signal per Kref, declared by sensor manufacturer [%]
=
Uncertainty by temperature influence on zero torque signal (related to nominal torque) [Nm]
=
Temperature influence on zero torque signal per Kref (related to nominal torque), declared by sensor manufacturer [%]
=
Reference temperature span for uTKC and uTK0, wtk0 and wtkc, declared by sensor manufacturer [K]
=
Difference in sensor temperature between calibration and measurement [K]. If the sensor temperature cannot be measured, a default value of ΔK = 15 K shall be used.
=
Current/measured torque value at torque sensor [Nm]
=
Nominal torque value of torque sensor [Nm]
=
Uncertainty by torque sensor calibration [Nm]
=
Relative calibration uncertainty (related to nominal torque) [%]
=
Calibration advancement factor (if declared by sensor manufacturer, otherwise = 1)
=
Uncertainty by parasitic loads [Nm]
=
senspara * ipara
Relative influence of forces and bending torques caused by misalignment
=
Maximum influence of parasitic loads for specific torque sensor declared by sensor manufacturer [%]; if no specific value for parasitic loads is declared by the sensor manufacturer, the value shall be set to 1,0 %
=
Maximum influence of parasitic loads for specific torque sensor depending on test setup (A/B/C, as defined below).
=
A) 10 % in case of bearings isolating the parasitic forces in front of and behind the sensor and a flexible coupling (or cardan shaft) installed functionally next to the sensor (downstream or upstream); furthermore, these bearings can be integrated in a driving/braking machine (e.g. electric machine) and/or in the transmission as long as the forces in the machine and/or transmission are isolated from the sensor. See figure 1.
=
B) 50 % in case of bearings isolating the parasitic forces in front of and behind the sensor and no flexible coupling installed functionally next to the sensor; furthermore, these bearings can be integrated in a driving/braking machine (e.g. electric machine) and/or in the transmission as long as the forces in the machine and/or transmission are isolated from the sensor. See figure 2.
=
C) 100 % for other setups
Option 2 describes the determination of the torque loss by a combination of measurements and linear interpolation. Measurements shall be performed for the torque independent losses of the transmission and for one load point of the torque dependent losses (maximum input torque). Based on the torque losses at no load and at maximum input torque, the torque losses for the input torques in between shall be calculated with the torque loss coefficient fTlimo .
The torque loss Tl,in on the input shaft of the transmission shall be calculated by
Tl,in (nin , Tin , gear) = Tl,in,min_loss + fTlimo * Tin + T l,in,min_el + fel_corr * Tin
The torque loss coefficient based on the linear model fTlimo shall be calculated by
where:
=
Torque loss related to input shaft [Nm]
=
Drag torque loss at transmission input, measured with free rotating output shaft from testing without load [Nm]
=
Speed at the input shaft [rpm]
=
Torque loss coefficient based on linear model [-]
=
Torque at the input shaft [Nm]
=
Maximum tested torque at the input shaft (normally 100 % input torque, refer to 3.2.5.2. and 3.4.4.) [Nm]
=
Torque loss related to input shaft with Tin = Tin,maxT
=
Loss correction for electric power loss level depending on input torque [-]
=
Additional torque loss on input shaft by electric consumers [Nm]
=
Additional torque loss on input shaft by electric consumers corresponding to minimum electric power [Nm]
The correction factor for the torque dependent electric torque losses fel_corr and the torque loss at the input shaft of the transmission caused by the power consumption of transmission electric auxiliary Tl,in,el shall be calculated as described in paragraph 3.1.
As specified for Option 1 in 3.1.2.1.
As specified for Option 1 in 3.1.2.2.
As specified for Option 1 in 3.1.2.3.
As specified for Option 3 in 3.3.2.1.
As specified for Option 1 in 3.1.2.5.1.
As specified for Option 1 in 3.1.2.5.2.
As specified for Option 1 in 3.1.2.5.3 and 3.1.2.5.4.
As specified for Option 3 in 3.3.3.4.
As specified for Option 1 in 3.1.3. for the measurement of the torque independent losses.
As specified for Option 3 in 3.3.4. for the measurement of the torque dependent losses.
As specified for Option 1 in 3.1.4. for the measurement of the torque independent losses.
As specified for Option 3 in 3.3.5. for the measurement of the torque dependent losses.
As specified for Option 1 in 3.1.5 for the measurement of the torque independent losses.
As specified for Option 3 in 3.3.7 for the measurement of the torque dependent losses.
The torque loss map to be applied to the simulation tool contains the torque loss values of a transmission depending on rotational input speed and input torque.
To determine the torque loss map for a transmission, the basic torque loss map data shall be measured and calculated as specified in this paragraph. The torque loss results shall be complemented in accordance with 3.4 and formatted in accordance with Appendix 12 for the further processing by the simulation tool.
Torque range:
The torque losses for each gear shall be measured at 100 % of the maximum transmission input torque per gear.
In the case the output torque exceeds 10 kNm (for a theoretical loss free transmission) or the input power exceeds the specified maximum input power, point 3.4.4. shall apply.
As specified for Option 3 in 3.3.8.
As specified for Option 1 in 3.1.8. for the measurement of the torque independent losses.
As specified for Option 3 in 3.3.9. for the measurement of the torque dependent loss.
Option 3 describes the determination of the torque loss by full measurement of the torque dependent losses including the torque independent losses of the transmission.
As specified for Option 1 in 3.1.2.1.
As specified for Option 1 in 3.1.2.2.
As specified for Option 1 in 3.1.2.3.
As specified for Option 1 in 3.1.2.4. with an exception for the following:
The pre-conditioning shall be performed on the direct drive gear without applied torque to the output shaft or target torque on the output shaft set to zero. If the transmission is not equipped with a direct drive gear, the gear with the ratio closest to 1:1 shall be used.
or
The requirements as specified in 3.1.2.4. shall apply, with an exception for the following:
The pre-conditioning shall be performed on the direct drive gear without applied torque to the output shaft or the torque on the output shaft being within +/- 50 Nm. If the transmission is not equipped with a direct drive gear, the gear with the ratio closest to 1:1 shall be used.
or, if the test rig includes a (master friction) clutch at the input shaft:
The requirements as specified in 3.1.2.4. shall apply, with an exception for the following:
The pre-conditioning shall be performed on the direct drive gear without applied torque to the output shaft or without applied torque to the input shaft. If the transmission is not equipped with a direct drive gear, the gear with the ratio closest to 1:1 shall be used.
The transmission would then be driven from the output side. Those proposals could also be combined.
As specified for Option 1 in 3.1.2.5.1.
As specified for Option 1 in 3.1.2.5.2.
As specified for Option 1 in 3.1.2.5.3 and 3.1.2.5.4.
The requirements as specified in 3.1.2.5.5. shall apply, diverging in the following:
The test point for the external oil conditioning system is specified as follows:
highest indirect gear,
input speed = 1 600 rpm,
input torque = maximum input torque for the highest indirect gear
The test rig shall be driven by electric machines (input and output).
Torque sensors shall be installed at the input and output side of the transmission.
Other requirements as specified in 3.1.3. shall apply.
For the measurement of the torque independent losses, the measurement equipment requirements as specified for Option 1 in 3.1.4. shall apply.
For the measurement of the torque dependent losses, the following requirements shall apply:
The torque sensor measurement uncertainty shall be below 5 % of the measured torque loss or 1 Nm (whichever value is larger).
The use of torque sensors with higher measurement uncertainties is allowed if the parts of the uncertainty exceeding 5 % or 1 Nm can be calculated and the smaller of those parts is added to the measured torque loss.
The torque measurement uncertainty shall be calculated and included as described under 3.3.9.
Other measurement equipment requirements as specified for Option 1 in 3.1.4. shall apply.
As specified in 3.1.6.1.
The torque loss shall be measured for the following speed steps (speed of the input shaft): 600, 900, 1 200, 1 600, 2 000, 2 500, 3 000, […] rpm up to the maximum speed per gear according to the specifications of the transmission or the last speed step before the defined maximum speed.
The speed ramp (time for the change between two speed steps) shall not exceed 20 seconds.
For each speed step the torque loss shall be measured for the following input torques: 0 (free rotating output shaft), 200, 400, 600, 900, 1 200, 1 600, 2 000, 2 500, 3 000, 3 500, 4 000, […] Nm up to the maximum input torque per gear according to the specifications of the transmission or the last torque step before the defined maximum torque and/or the last torque step before the output torque of 10 kNm.
In the case the output torque exceeds 10 kNm (for a theoretical loss free transmission) or the input power exceeds the specified maximum input power, point 3.4.4. shall apply.
The torque ramp (time for the change between two torque steps) shall not exceed 15 seconds (180 seconds for option 2).
To cover the complete torque range of a transmission in the above defined map, different torque sensors with limited measurement ranges may be used on the input/output side. Therefore the measurement may be divided into sections using the same set of torque sensors. The overall torque loss map shall be composed of these measurement sections.
At least the following signals shall be recorded during the measurement:
Input and output torques [Nm]
Input and output rotational speeds [rpm]
Ambient temperature [°C]
Oil temperature [°C]
If the transmission is equipped with a shift and/or clutch system that is controlled by hydraulic pressure or with a mechanically driven smart lubrication system, additionally to be recorded:
Oil pressure [kPa]
If the transmission is equipped with transmission electric auxiliary, additionally to be recorded:
Voltage of transmission electric auxiliary [V]
Current of transmission electric auxiliary [A]
For differential measurements for compensation of influences by test rig setup, additionally to be recorded:
Test rig bearing temperature [°C]
The sampling and recording rate shall be 100 Hz or higher.
A low pass filter shall be applied to avoid measurement errors.
Pel = I * U
It is allowed to subtract influences caused by the test rig setup from the torque losses (3.3.2.2.).
The part of the calculated total uncertainty UT,loss exceeding 5 % of Tloss or 1 Nm (ΔUT,loss ), whichever value of ΔUT,loss is smaller, shall be added to Tloss for the reported torque loss Tloss,rep . If UT,loss is smaller than 5 % of Tloss or 1 Nm, then Tloss,rep = Tloss .
Tloss,rep = Tloss + MAX (0, ΔUT,loss )
ΔUT,loss = MIN ((UT,loss – 5 % * Tloss ), (UT,loss – 1 Nm))
For each measurement set, the total uncertainty UT,loss of the torque loss shall be calculated based on the following parameters:
Temperature effect
Parasitic loads
Calibration error (incl. sensitivity tolerance, linearity, hysteresis and repeatability)
The total uncertainty of the torque loss (UT,loss ) is based on the uncertainties of the sensors at 95 % confidence level. The calculation shall be done as the square root of the sum of squares (‘Gaussian law of error propagation’).
wpara = senspara * ipara
where:
=
Measured torque loss (uncorrected) [Nm]
=
Reported torque loss (after uncertainty correction) [Nm]
=
Total expanded uncertainty of torque loss measurement at 95 % confidence level [Nm]
=
Uncertainty of input/output torque loss measurement separately for input and output torque sensor[Nm]
=
Gear ratio [-]
=
Uncertainty by temperature influence on current torque signal [Nm]
=
Temperature influence on current torque signal per Kref, declared by sensor manufacturer [%]
=
Uncertainty by temperature influence on zero torque signal (related to nominal torque) [Nm]
=
Temperature influence on zero torque signal per Kref (related to nominal torque), declared by sensor manufacturer [%]
=
Reference temperature span for uTKC and uTK0, wtk0 and wtkc, declared by sensor manufacturer [K]
=
Difference in sensor temperature between calibration and measurement [K]. If the sensor temperature cannot be measured, a default value of ΔK = 15 K shall be used.
=
Current/measured torque value at torque sensor [Nm]
=
Nominal torque value of torque sensor [Nm]
=
Uncertainty by torque sensor calibration [Nm]
=
Relative calibration uncertainty (related to nominal torque) [%]
=
calibration advancement factor (if declared by sensor manufacturer, otherwise = 1)
=
Uncertainty by parasitic loads [Nm]
=
senspara * ipara
Relative influence of forces and bending torques caused by misalignment [%]
=
Maximum influence of parasitic loads for specific torque sensor declared by sensor manufacturer [%]; if no specific value for parasitic loads is declared by the sensor manufacturer, the value shall be set to 1,0 %
=
Maximum influence of parasitic loads for specific torque sensor depending on test setup (A/B/C, as defined below).
=
A) 10 % in case of bearings isolating the parasitic forces in front of and behind the sensor and a flexible coupling (or cardan shaft) installed functionally next to the sensor (downstream or upstream); furthermore, these bearings can be integrated in a driving/braking machine (e.g. electric machine) and/or in the transmission as long as the forces in the machine and/or transmission are isolated from the sensor. See figure 3.
=
B) 50 % in case of bearings isolating the parasitic forces in front of and behind the sensor and no flexible coupling installed functionally next to the sensor; furthermore, these bearings can be integrated in a driving/braking machine (e.g. electric machine) and/or in the transmission as long as the forces in the machine and/or transmission are isolated from the sensor. See figure 4.
=
C) 100 % for other setups
For each gear a torque loss map covering the defined input speed and input torque steps shall be determined with one of the specified testing options or standard torque loss values. For the input file for the simulation tool, this basic torque loss map shall be complemented as described in the following:
Calculated fallback values (Appendix 8)
Option 1
Option 2 or 3 in combination with a torque sensor for higher output torques (if required)
For cases (i) and (ii) in Option 2, the torque losses at load shall be measured at the input torque that corresponds to output torque 10 kNm and/or the specified maximum input power.
The torque converter characteristics to be determined for the simulation tool input consist of Tpum 1000 (the reference torque at 1 000 rpm input speed) and μ (the torque ratio of the torque converter). Both are depending on the speed ratio v (= output (turbine) speed / input (pump) speed for the torque converter) of the torque converter.
For determination of the characteristics of the TC, the applicant for a certificate shall apply the following method, irrespective of the chosen option for the assessment of the transmission torque losses.
To take the two possible arrangements of the TC and the mechanical transmission parts into account, the following differentiation between case S and P shall apply:
:
TC and mechanical transmission parts in serial arrangement
:
TC and mechanical transmission parts in parallel arrangement (power split installation)
For case S arrangements the TC characteristics may be evaluated either separate from the mechanical transmission or in combination with the mechanical transmission. For case P arrangements the evaluation of TC characteristic is only possible in combination with the mechanical transmission. However, in this case and for the hydromechanical gears subject to measurement the whole arrangement, torque converter and mechanical transmission, is considered as a TC with similar characteristic curves as a sole torque converter.
For the determination of the torque converter characteristics two measurement options may be applied:
Option A: measurement at constant input speed
Option B: measurement at constant input torque according to SAE J643
The manufacturer may choose option A or B for case S and case P arrangements.
For the input to the simulation tool, the torque ratio μ and reference torque Tpum of the torque converter shall be measured for a range of v ≤ 0,95 (= vehicle propulsion mode). The range of v ≥ 1,00 (= vehicle coasting mode) may either be measured or covered by using the standard values of Table 1.
In case of measurements together with a mechanical transmission the overrun point may be different from v = 1,00 and therefor the range of measured speed ratios shall be adjusted accordingly.
In case of use of standard values the data on torque converter characteristics provided to the simulation tool shall only cover the range of v ≤ 0,95 (or the adjusted speed ratio). The simulation tool automatically adds the standard values for overrun conditions.
Default values for v ≥ 1,00
v | μ | Tpum 1000 |
---|---|---|
1,000 | 1,0000 | 0,00 |
1,100 | 0,9999 | – 40,34 |
1,222 | 0,9998 | – 80,34 |
1,375 | 0,9997 | – 136,11 |
1,571 | 0,9996 | – 216,52 |
1,833 | 0,9995 | – 335,19 |
2,200 | 0,9994 | – 528,77 |
2,500 | 0,9993 | – 721,00 |
3,000 | 0,9992 | – 1 122,0 |
3,500 | 0,9991 | – 1 648,0 |
4,000 | 0,9990 | – 2 326,0 |
4,500 | 0,9989 | – 3 182,0 |
5,000 | 0,9988 | – 4 242,0 |
The torque converter used for the measurements shall be in accordance with the drawing specifications for series production torque converters.
Modifications to the TC to meet the testing requirements of this Annex, e.g. for the inclusion of measurement sensors are permitted.
Upon request of the approval authority the applicant for a certificate shall specify and prove the conformity with the requirements defined in this Annex.
The input oil temperature to the TC shall meet the following requirements:
The oil temperature for measurements of the TC separate from the transmission shall be 90 °C + 7/– 3 K.
The oil temperature for measurements of the TC together with the transmission (case S and case P) shall be 90 °C + 20/– 3 K.
The oil temperature shall be measured at the drain plug or in the oil sump.
In case the TC characteristics are measured separately form the transmission, the oil temperature shall be measured prior to entering the converter test drum/bench.
The input TC oil flow rate and output oil pressure of the TC shall be kept within the specified operational limits for the torque converter, depending on the related transmission type and the tested maximum input speed.
As specified for transmission testing in 3.1.2.5.3 and 3.1.2.5.4.
The torque converter shall be installed on a testbed with a torque sensor, speed sensor and an electric machine installed at the input and output shaft of the TC.
The calibration laboratory facilities shall comply with the requirements of either ISO/TS 16949, ISO 9000 series or ISO/IEC 17025. All laboratory reference measurement equipment, used for calibration and/or verification, shall be traceable to national (international) standards.
The torque sensor measurement uncertainty shall be below 1 % of the measured torque value.
The use of torque sensors with higher measurement uncertainties is allowed if the part of the uncertainty exceeding 1 % of the measured torque can be calculated and is added to the measured torque loss as described in 4.1.7.
The uncertainty of the speed sensors shall not exceed ± 1 rpm.
The uncertainty of the temperature sensors for the measurement of the ambient temperature shall not exceed ± 1,5 K.
The uncertainty of the temperature sensors for the measurement of the oil temperature shall not exceed ± 1,5 K.
As specified in 3.1.6.1.
1 000 rpm ≤ npum ≤ 2 000 rpm
At least the following signals shall be recorded during the measurement:
Input (pump) torque Tc,pum [Nm]
Output (turbine) torque Tc,tur [Nm]
Input rotational (pump) speed npum [rpm]
Output rotational (turbine) speed ntur [rpm]
TC input oil temperature KTCin [°C]
The sampling and recording rate shall be 100 Hz or higher.
A low pass filter shall be applied to avoid measurement errors.
for the calculation of ΔUT,pum/tur: smallest averaged torque value for Tc,pum/tur
for the calculation of torque ratio μ: largest averaged torque value for Tc,pum
for the calculation of torque ratio μ: smallest averaged torque value for Tc,tur
for the calculation of reference torque Tpum1000: smallest averaged torque value for Tc,pum
The part of the calculated measurement uncertainty UT,pum/tur exceeding 1 % of the measured torque Tc,pum/tur shall be used to correct the characteristic value of the TC as defined below.
ΔUT,pum/tur = MAX (0, (UT,pum/tur – 0,01 * Tc,pum/tur))
The uncertainty UT,pum/tur of the torque measurement shall be calculated based on the following parameter:
Calibration error (incl. sensitivity tolerance, linearity, hysteresis and repeatability)
The uncertainty UT,pum/tur of the torque measurement is based on the uncertainties of the sensors at 95 % confidence level.
UT,pum/tur = 2 * ucal
where:
=
Current / measured torque value at input/output torque sensor (uncorrected) [Nm]
=
Input (pump) torque (after uncertainty correction) [Nm]
=
Uncertainty of input / output torque measurement at 95 % confidence level separately for input and output torque sensor[Nm]
=
Nominal torque value of torque sensor [Nm]
=
Uncertainty by torque sensor calibration [Nm]
=
Relative calibration uncertainty (related to nominal torque) [%]
=
Calibration advancement factor (if declared by sensor manufacturer, otherwise = 1)
For each measurement point, the following calculations shall be applied to the measurement data:
The torque ratio of the TC shall be calculated by
The speed ratio of the TC shall be calculated by
The reference torque at 1 000 rpm shall be calculated by
where:
=
Torque ratio of the TC [-]
=
Speed ratio of the TC [-]
=
Input (pump) torque (corrected) [Nm]
=
Input rotational (pump) speed [rpm]
=
Output rotational (turbine) speed [rpm]
=
Reference torque at 1 000 rpm [Nm]
As specified in 4.1.1.
As specified in 4.1.2.
As specified in 4.1.3.
As specified in 4.1.4.
As specified in 4.1.5.
As specified in 4.1.6.
As specified in 3.1.6.1.
As specified in 4.1.8.
As specified in 4.1.9.
As specified in 4.1.9.
As specified in 4.1.11.
The scope of this section includes engine retarders, transmission retarders, driveline retarders, and components that are treated in the simulation tool as a retarder. These components include vehicle starting devices like a single wet transmission input clutch or hydro-dynamic clutch.
The retarder drag torque loss is a function of the retarder rotor speed. Since the retarder can be integrated in different parts of the vehicle driveline, the retarder rotor speed depends on the drive part (= speed reference) and step-up ratio between drive part and retarder rotor as shown in Table 2.
Retarder rotor speeds
where:
=
step-up ratio = retarder rotor speed/drive part speed
=
transmission ratio = transmission input speed/transmission output speed
Retarder configurations that are integrated in the engine and cannot be separated from the engine shall be tested in combination with the engine. This section does not cover these non-separable engine integrated retarders.
Retarders that can be disconnected from the driveline or the engine by any kind of clutch are considered to have zero rotor speed in disconnected condition and therefore have no power losses.
The retarder drag losses shall be measured with one of the following two methods:
Measurement on the retarder as a stand-alone unit
Measurement in combination with the transmission
In case the losses are measured on the retarder as stand-alone unit, the results are affected by the torque losses in the bearings of the test setup. It is permitted to measure these bearing losses and subtract them from the retarder drag loss measurements.
The manufacturer shall guarantee that the retarder used for the measurements is in accordance with the drawing specifications for series production retarders.
Modifications to the retarder to meet the testing requirements of this Annex, e.g. for the inclusion of measurement sensors or the adaption of an external oil conditioning systems are permitted.
Based on the family described in Appendix 6 to this Annex, measured drag losses for transmissions with retarder can be used for the same (equivalent) transmission without retarder.
The use of the same transmission unit for measuring the torque losses of variants with and without retarder is permitted.
Upon request of the approval authority the applicant for a certificate shall specify and prove the conformity with the requirements defined in this Annex.
On request of the applicant a run-in procedure may be applied to the retarder. The following provisions shall apply for a run-in procedure.
The ambient temperature during the test shall be in a range of 25 °C ± 10 K.
The ambient temperature shall be measured 1 m laterally from the retarder.
For magnetic retarders the minimum ambient pressure shall be 899 hPa according to International Standard Atmosphere (ISA) ISO 2533.
For hydrodynamic retarders:
Except for the fluid, no external heating is allowed.
In case of testing as stand-alone unit, the retarder fluid temperature (oil or water) shall not exceed 87 °C.
In case of testing in combination with transmission, the oil temperature limits for transmission testing shall apply.
New, recommended first fill oil for the European market shall be used in the test.
For water retarders the water quality shall meet the specifications set out by the manufacturer for the retarder. The water pressure shall be set to a fixed value close to vehicle condition (1 ± 0,2 bar relative pressure at retarder input hose).
If several oils are recommended for first fill, they are considered to be equal if the oils have a kinematic viscosity within 50 % of each other at the same temperature (within the specified tolerance band for KV100).
The oil/water level shall meet the nominal specifications for the retarder.
The electric machine, the torque sensor, and speed sensor shall be mounted at the input side of the retarder or transmission.
The installation of the retarder (and transmission) shall be done with an inclination angle as for installation in the vehicle according to the homologation drawing ± 1° or at 0° ± 1°.
As specified for transmission testing in 3.1.4.
As specified for transmission testing in 3.1.6.1.
The torque loss measurement sequence for the retarder testing shall follow the provisions for the transmission testing defined in 3.1.6.3.2. to 3.1.6.3.5.
When the retarder is tested as stand-alone unit, torque loss measurements shall be conducted using the following speed points:
200, 400, 600, 900, 1 200, 1 600, 2 000, 2 500, 3 000, 3 500, 4 000, 4 500, 5 000, continued up to the maximum retarder rotor speed.
[F1The load-independent torque loss for the complete transmission including retarder shall be measured as defined in point 3.1. for transmission testing in one of the higher transmission gears:
= T l,in,withret]
The retarder and related parts shall be replaced with parts required for the equivalent transmission variant without retarder. The measurement of point (1) shall be repeated.
= Tl,in,withoutret
The load-independent torque loss for the retarder system shall be determined by calculating the differences between the two test data sets
= Tl,in,retsys = Tl,in,withret – Tl,in,withoutret
As specified for transmission testing in 3.1.5.
All recorded data shall be checked and processed as defined for transmission testing in 3.1.7.
The angle drive losses shall be determined using one of the following cases:
For the torque loss measurement of a separate angle drive, the three options as defined for the determination of the transmission losses shall apply:
:
Measured torque independent losses and calculated torque dependent losses (Transmission test option 1)
:
Measured torque independent losses and measured torque dependent losses at full load (Transmission test option 2)
:
Measurement under full load points (Transmission test option 3)
The measurement of the angle drive losses shall follow the procedure described for the related transmission test option in paragraph 3 diverging in the following requirements:
From 200 rpm (at the shaft to which the angle drive is connected) up to the maximum speed according to specifications of the angle drive or the last speed step before the defined maximum speed.
In case the angle drive is tested in combination with a transmission, the testing shall follow one of the defined options for transmission testing:
:
Measured torque independent losses and calculated torque dependent losses (Transmission test option 1)
:
Measured torque independent losses and measured torque dependent losses at full load (Transmission test option 2)
:
Measurement under full load points (Transmission test option 3)
The torque loss for the complete transmission including angle drive shall be measured as defined for the applicable transmission testing option
= Tl,in,withad
The angle drive and related parts shall be replaced with parts required for the equivalent transmission variant without angle drive. The measurement of point (1) shall be repeated.
= Tl,in,withoutad
The torque loss for the angle drive system shall be determined by calculating the differences between the two test data sets
= Tl,in,adsys = Tl,in,withad – Tl,in,withoutad
Sample size conformity testing
Total annual production of transmissions | Number of tests |
---|---|
0 – 1 000 | 0 |
> 1 000-10 000 | 1 |
> 10 000-30 000 | 2 |
> 30 000 | 3 |
> 100 000 | 4 |
For conformity of the certified CO2 emissions and fuel consumption related properties testing the following method shall apply upon prior agreement between an approval authority and the applicant for a certificate:
If other boundary conditions for oil type, oil temperature and inclination angle are used, the manufacturer shall clearly show the influence of these conditions and those used for certification regarding efficiency.
In the case Option 2 was used for certification testing, the torque independent losses for the two speeds defined in point 3 of 8.1.2.2.2. shall be measured. The torque dependent losses at maximum torque shall be measured at the same two speeds. The torque losses at the three highest torque steps shall be interpolated as described by the certification procedure.
In the case Option 3 was used for certification testing, the torque losses for the 18 operating points defined in 8.1.2.2.2. shall be measured.
Gears to use:
The 3 highest gears of the transmission shall be used for testing.
Torque range:
The 3 highest torque steps as reported for certification shall be tested.
Speed range:
The two transmission input speeds of 1 200 rpm and 1 600 rpm shall be tested.
where:
=
Efficiency of each operation point 1 to 18
=
Output torque [Nm]
=
Input torque [Nm]
=
Input speed [rpm]
=
Output speed [rpm]
The efficiency of the tested transmission during conformity of the certified CO2 emissions and fuel consumption related properties test ηA,CoP shall not be lower than X % of the type approved transmission efficiency ηA,TA .
ηA,TA – ηA,CoP ≤ X
[F1X shall be replaced by 1,5 % for SMT/AMT/DCT transmissions and 3 % for APT transmissions or transmission with more than 2 friction shift clutches.]
Communication concerning:
| Administration stamp |
of a certificate with regard to Regulation (EC) No 595/2009 as implemented by Regulation (EU) 2017/2400.
Regulation (EC) No XXXXX and Regulation (EU) 2017/2400 as last amended by ….
certification number:
Hash:
Reason for extension:
Attachments:
Information document
Test report
Information document no.: | Issue: Date of issue: Date of Amendment: |
pursuant to …
[F1Transmission type/family (if applicable):]
…
Parent transmission | Family members | ||||
or transmission type | |||||
#1 | #2 | #3 | |||
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1 gear
2 gear
3 gear
4 gear
5 gear
6 gear
7 gear
8 gear
9 gear
10 gear
11 gear
12 gear
n gear
No.: | Description: | Date of issue: |
---|---|---|
1 | Information on Transmission test conditions | … |
2 | … |
Information document no.: | Issue: Date of issue: Date of Amendment: |
pursuant to …
[F1TC type/family (if applicable):]
…
Parent TC or | Family members | ||||
TC type | #1 | #2 | #3 | ||
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
No.: | Description: | Date of issue: |
---|---|---|
1 | Information on Torque Converter test conditions | … |
2 | … |
yes/no
yes/no
Information document no.: | Issue: Date of issue: Date of Amendment: |
pursuant to …
[F1OTTC type/family (if applicable):]
…
Parent OTTC | Family member | ||||
#1 | #2 | #3 | |||
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
No.: | Description: | Date of issue: |
---|---|---|
1 | Information on OTTC test conditions | … |
2 | … |
with transmission
yes/no
with engine
yes/no
drive mechanism
yes/no
direct
yes/no
Information document no.: | Issue: Date of issue: Date of Amendment: |
pursuant to …
[F1ADC type/family (if applicable):]
…
Parent-ADC | Family member | ||||
#1 | #2 | #3 | |||
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
No.: | Description: | Date of issue: |
---|---|---|
1 | Information on ADC test conditions | … |
2 | … |
with transmission | yes/no |
drive mechanism | yes/no |
direct | yes/no |
A transmission, torque converter, other torque transferring components or additional driveline components family is characterized by design and performance parameters. These shall be common to all members within the family. The manufacturer may decide which transmission, torque converter, other torque transferring components or additional driveline components belong to a family, as long as the membership criteria listed in this Appendix are respected. The related family shall be approved by the Approval Authority. The manufacturer shall provide to the Approval Authority the appropriate information relating to the members of the family.
In some cases there may be interaction between parameters. This shall be taken into consideration to ensure that only transmissions, torque converter, other torque transferring components or additional driveline components with similar characteristics are included within the same family. These cases shall be identified by the manufacturer and notified to the Approval Authority. It shall then be taken into account as a criterion for creating a new transmission, torque converter, other torque transferring components or additional driveline components family.
In case of devices or features, which are not listed in paragraph 9. and which have a strong influence on the level of performance, this equipment shall be identified by the manufacturer on the basis of good engineering practice, and shall be notified to the Approval Authority. It shall then be taken into account as a criterion for creating a new transmission, torque converter, other torque transferring components or additional driveline components family.
If members within a family incorporate other features which may be considered to affect the torque losses, these features shall also be identified and taken into account in the selection of the parent.
Gear ratio, gearscheme and powerflow (for forward gears only, crawler gears excluded);
Center distance for countershaft transmissions;
Type of bearings at corresponding positions (if fitted);
Type of shift elements (tooth clutches, including synchronisers or friction clutches) at corresponding positions (where fitted).
Single gear width ± 1 mm;
Total number of forward gears;
Number of tooth shift clutches;
Number of synchronizers;
Number of friction clutch plates (except for single dry clutch with 1 or 2 plates);
Outer diameter of friction clutch plates (except for single dry clutch with 1 or 2 plates);
Surface roughness of the teeth;
Number of dynamic shaft seals;
Oil flow for lubrication and cooling per input shaft revolution;
Oil viscosity (± 10 %);
System pressure for hydraulically controlled gearboxes;
Specified oil level in reference to central axis and in accordance with the drawing specification (based on average value between lower and upper tolerance) in static or running condition. The oil level is considered as equal if all rotating transmission parts (except for the oil pump and the drive thereof) are located above the specified oil level;
Specified oil level (± 1mm).
The parent transmission shall be selected using the following criteria listed below.
Highest single gear width for Option 1 or highest Single gear width ± 1 mm for Option 2 or Option 3;
Highest total number of gears;
Highest number of tooth shift clutches;
Highest number of synchronizers;
Highest number of friction clutch plates (except for single dry clutch with 1 or 2 plates);
Highest value of the outer diameter of friction clutch plates (except for single dry clutch with 1 or 2 plates);
Highest value for the surface roughness of the teeth;
Highest number of dynamic shaft seals;
Highest oil flow for lubrication and cooling per input shaft revolution;
Highest oil viscosity;
Highest system pressure for hydraulically controlled gearboxes;
Highest specified oil level in reference to central axis and in accordance with the drawing specification (based on average value between lower and upper tolerance) in static or running condition. The oil level is considered as equal if all rotating transmission parts (except for the oil pump and the drive thereof) are located above the specified oil level;
Highest specified oil level (± 1 mm).
Outer torus diameter;
Inner torus diameter;
Arrangement of pump (P), turbine (T) and stator (S) in flow direction;
Torus width;
Oil type according to test specification;
Blade design;
Outer torus diameter;
Inner torus diameter;
Arrangement of pump (P), turbine (T) and stator (S) in flow direction;
Torus width;
Oil type according to test specification;
Blade design
Gear scheme and power flow in torque converter mode
Type of bearings at corresponding positions (if fitted)
Type of cooling/lubrication pump (referring to parts list)
Type of shift elements (tooth clutches (including synchronisers) or friction clutches) at corresponding positions where fitted
Oil level according to drawing in reference to central axis.
As long as all criteria listed in 5.1.1 are identical every member of the torque converter without mechanical transmission family can be selected as parent.
The parent hydrodynamic torque converter with mechanical transmission (parallel arrangement) shall be selected using the following criteria listed below.
Highest oil level according to drawing in reference to central axis.
Outer torus diameter;
Torus width;
Blade design;
Operating fluid.
Drum design (electro magnetic retarder or permanent magnetic retarder);
Outer rotor diameter;
Cooling blade design;
Blade design.
Outer torus diameter;
Torus width;
Blade design.
Outer torus diameter - inner torus diameter (OD-ID);
Number of blades;
Operating fluid viscosity (± 50 %).
Outer rotor diameter - inner rotor diameter (OD-ID);
Number of rotors;
Number of cooling blades / blades;
Number of arms.
Operating fluid viscosity (± 10 %);
Outer torus diameter - inner torus diameter (OD-ID);
Number of blades.
Highest value: outer torus diameter – inner torus diameter (OD-ID);
Highest number of blades;
Highest operating fluid viscosity.
Highest outer rotor diameter – highest inner rotor diameter (OD-ID);
Highest number of rotors;
Highest number of cooling blades/blades;
Highest number of arms.
Highest operating fluid viscosity (± 10 %);
Highest outer torus diameter – highest inner torus diameter (OD-ID);
Highest number of blades.
Gear ratio and gearscheme;
Angle between input/output shaft;
Type of bearings at corresponding positions
Single gear width;
Number of dynamic shaft seals;
Oil viscosity (± 10 %);
Surface roughness of the teeth;
Specified oil level in reference to central axis and in accordance with the drawing specification (based on average value between lower and upper tolerance) in static or running condition. The oil level is considered as equal if all rotating transmission parts (except for the oil pump and the drive thereof) are located above the specified oil level.
Highest single gear width;
Highest number of dynamic shaft seals;
Highest oil viscosity (± 10 %);
Highest surface roughness of the teeth;
Highest specified oil level in reference to central axis and in accordance with the drawing specification (based on average value between lower and upper tolerance) in static or running condition. The oil level is considered as equal if all rotating transmission parts (except for the oil pump and the drive thereof) are located above the specified oil level.
In the case of a component being certified in accordance with this Annex, the component shall bear:
1 for Germany;
2 for France;
3 for Italy;
4 for the Netherlands;
5 for Sweden;
6 for Belgium;
7 for Hungary;
8 for the Czech Republic;
9 for Spain;
11 for the United Kingdom;
12 for Austria;
13 for Luxembourg;
17 for Finland;
18 for Denmark;
19 for Romania;
20 for Poland;
21 for Portugal;
23 for Greece;
24 for Ireland;
25 for Croatia;
26 for Slovenia;
27 for Slovakia;
29 for Estonia;
32 for Latvia;
34 for Bulgaria;
36 for Lithuania;
49 for Cyprus;
50 for Malta
For this Regulation, the sequence number shall be 00.
For this Regulation, the alphabetical character shall be the one laid down in Table 1.
[F1G | Transmission] |
C | Torque Converter (TC) |
O | Other torque transferring component (OTTC) |
D | Additional driveline component (ADC) |
The above certification mark affixed to a transmission, torque converter (TC), other torque transferring component (OTTC) or additional driveline component (ADC) shows that the type concerned has been certified in Poland (e20), pursuant to this Regulation. The first two digits (00) are indicating the sequence number assigned to the latest technical amendment to this Regulation. The following digit indicates that the certification was granted for a transmission (G). The last four digits (0004) are those allocated by the approval authority to the transmission, as the base approval number.]
In the case described in first paragraph, if a torque converter or other torque transferring component have not been certified, ‘–’ instead of the certification number shall be indicated on the transmission next to the alphabetical character specified in point 1.4.
eX*YYYY/YYYY*ZZZZ/ZZZZ*X*0000*00
Section 1 | Section 2 | Section 3 | Additional letter to Section 3 | Section 4 | Section 5 |
---|---|---|---|---|---|
Indication of country issuing the certificate | HDV CO 2 certification Regulation (2017/2400) | Latest amending Regulation (ZZZZ/ZZZZ) | See Table 1 of this appendix | Base certification number 0000 | Extension 00] |
Calculated fallback values based on the maximum rated torque of the transmission:
The torque loss Tl,in related to the input shaft of the transmission shall be calculated by
where:
=
Torque loss related to the input shaft [Nm]
=
Drag torque at x rpm [Nm]
=
Additional angle drive gear drag torque at x rpm [Nm]
(if applicable)
=
Speed at the input shaft [rpm]
=
1-η
=
efficiency
=
0,01 for direct gear, 0,04 for indirect gears
=
0,04 for angle drive gear (if applicable)
=
Torque at the input shaft [Nm]
For transmissions with tooth shift clutches (Synchronised Manual Transmissions (SMT), Automated Manual Transmissions or Automatic Mechanically engaged Transmissions (AMT) and Dual Clutch Transmissions (DCT)) the drag torque Tdx is calculated by
where:
=
Maximum allowed input torque in any forward gear of transmission [Nm]
=
max(Tmax,in,gear)
=
Maximum allowed input torque in gear, where gear = 1, 2, 3,… top gear). For transmissions with hydrodynamic torque converter this input torque shall be the torque at transmission input before torque converter.
For transmissions with friction shift clutches (> 2 friction clutches) the drag torque Tdx is calculated by
Here, ‘friction clutch’ is used in the context of a clutch or brake that operates with friction, and is required for sustained torque transfer in at least one gear.
For transmissions including an angle drive (e.g. bevel gear), the additional angle drive drag torque Taddx shall be included in the calculation of Tdx :
(only if applicable)
Generic torque converter model based on standard technology:
For the determination of the torque converter characteristics a generic torque converter model depending on specific engine characteristics may be applied.
The generic TC model is based on the following characteristic engine data:
=
Maximum engine speed at maximum power (determined from the engine full-load curve as calculated by the engine pre-processing tool) [rpm]
=
Maximum engine torque (determined from the engine full-load curve as calculated by the engine pre-processing tool) [Nm]
Thereby the generic TC characteristics are valid only for a combination of the TC with an engine sharing the same specific characteristic engine data.
Description of the four-point model for the torque capacity of the TC:
Generic torque capacity and generic torque ratio:
where:
=
Speed ratio at overrun point; [-]
For TC with rotating housing (Trilock-Type) vs typically is 1. For other TC concepts, especially power split concepts, vs may have values different from 1.
=
Stall point; v 0 = 0 [rpm]
The model requires the following definitions for the calculation of the generic torque capacity:
Stall point:
Stall point at 70 % nominal engine speed.
Engine torque in stall point at 80 % maximum engine torque.
Engine/Pump reference torque in stall point:
Intermediate point:
Intermediate speed ratio vm = 0,6 * vs
Engine/pump reference torque in intermediate point at 80 % of reference torque in stall point:
Coupling point:
Coupling point at 90 % overrun conditions: vc = 0,90 * vs
Engine/pump reference torque in clutch point at 50 % of reference torque in stall point:
Overrun point:
Reference torque at overrun conditions = vs :
The model requires the following definitions for the calculation of the generic torque ratio:
Stall point:
Torque ratio at stall point v0 = vs = 0:
Intermediate point:
Linear interpolation between stall point and coupling point
Coupling point:
Torque ratio at coupling point vc = 0,9 * vs :
Overrun point:
Torque ratio at overrun conditions = vs :
Efficiency:
n = μ * v
Linear interpolation between the calculated specific points shall be used.
Calculated standard torque loss values for other torque transferring components:
For hydrodynamic retarders (oil or water), the retarder drag torque shall be calculated by
For magnetic retarders (permanent or electro-magnetic), the retarder drag torque shall be calculated by:
where:
=
Retarder drag loss [Nm]
=
Retarder rotor speed [rpm] (see paragraph 5.1 of this Annex)
=
Step-up ratio = retarder rotor speed/drive component speed (see paragraph 5.1 of this Annex)
Consistent with the standard torque loss values for the combination of a transmission with a geared angle drive in Appendix 8, the standard torque losses of a geared angle drive without transmission shall be calculated from:
where:
=
Torque loss related to the input shaft of transmission [Nm]
=
Additional angle drive gear drag torque at x rpm [Nm]
(if applicable)
=
Speed at the input shaft of transmission [rpm]
=
1-η;
=
efficiency
=
0,04 for angle drive gear
=
Torque at the input shaft of transmission [Nm]
=
Maximum allowed input torque in any forward gear of transmission [Nm]
=
max(Tmax,in,gear)
=
Maximum allowed input torque in gear, where gear = 1, 2, 3,… top gear)
The standard torque losses obtained by the calculations above may be added to the torque losses of a transmission obtained by Options 1-3 in order to obtain the torque losses for the combination of the specific transmission with an angle drive.
This Appendix describes the list of parameters to be provided by the transmission, torque converter (TC), other torque transferring components (OTTC) and additional driveline components (ADC) manufacturer as input to the simulation tool. The applicable XML schema as well as example data are available at the dedicated electronic distribution platform.
Unique identifier as used in ‘Simulation tool’ for a specific input parameter or set of input data
Data type of the parameter
sequence of characters in ISO8859-1 encoding
sequence of characters in ISO8859-1 encoding, no leading/trailing whitespace
date and time in UTC time in the format: YYYY-MM-DDTHH:MM:SSZ with italic letters denoting fixed characters e.g. ‘2002-05-30T09:30:10Z’
value with an integral data type, no leading zeros, e.g. ‘1800’
fractional number with exactly X digits after the decimal sign (‘.’) and no leading zeros e.g. for ‘double, 2’: ‘2345.67’; for ‘double, 4’: ‘45.6780’
physical unit of the parameter
Input parameters ‘ Transmission/General ’
a DCT shall be declared as transmission type AMT.] | ||||
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
Manufacturer | P205 | token | [-] | |
Model | P206 | token | [-] | |
CertificationNumber | P207 | token | [-] | |
Date | P208 | dateTime | [-] | Date and time when the component-hash is created |
AppVersion | P209 | token | [-] | |
TransmissionType | P076 | string | [-] | Allowed values a : ‘SMT’, ‘AMT’, ‘APT-S’, ‘APT-P’ |
MainCertificationMethod | P254 | string | [-] | Allowed values: ‘ Option 1 ’ , ‘ Option 2 ’ , ‘ Option 3 ’ , ‘ Standard values ’ |
Input parameters ‘Transmission/Gears’ per gear
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
GearNumber | P199 | integer | [-] | |
Ratio | P078 | double, 3 | [-] | |
MaxTorque | P157 | integer | [Nm] | optional |
MaxSpeed | P194 | integer | [1/min] | optional |
Input parameters ‘Transmission/LossMap’ per gear and for each grid point in the loss map
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
InputSpeed | P096 | double, 2 | [1/min] | |
InputTorque | P097 | double, 2 | [Nm] | |
TorqueLoss | P098 | double, 2 | [Nm] |
Input parameters ‘TorqueConverter/General’
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
Manufacturer | P210 | token | [-] | |
Model | P211 | token | [-] | |
[F1CertificationNumber | P212 | token | [-] | ] |
Date | P213 | dateTime | [-] | Date and time when the component-hash is created |
AppVersion | P214 | string | [-] | |
CertificationMethod | P257 | string | [-] | Allowed values: ‘Measured’, ‘Standard values’ |
Input parameters ‘TorqueConverter/Characteristics’ for each grid point in the characteristic curve
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
SpeedRatio | P099 | double, 4 | [-] | |
TorqueRatio | P100 | double, 4 | [-] | |
InputTorqueRef | P101 | double, 2 | [Nm] |
Input parameters ‘Angledrive/General’ (only required if component applicable)
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
Manufacturer | P220 | token | [-] | |
Model | P221 | token | [-] | |
[F1CertificationNumber | P222 | token | [-] | ] |
Date | P223 | dateTime | [-] | Date and time when the component-hash is created |
AppVersion | P224 | string | [-] | |
Ratio | P176 | double, 3 | [-] | |
CertificationMethod | P258 | string | [-] | Allowed values: ‘Option 1’, ‘Option 2’, ‘Option 3’, ‘Standard values’ |
Input parameters ‘Angledrive/LossMap’ for each grid point in the loss map (only required if component applicable)
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
InputSpeed | P173 | double, 2 | [1/min] | |
InputTorque | P174 | double, 2 | [Nm] | |
TorqueLoss | P175 | double, 2 | [Nm] |
Input parameters ‘Retarder/General’ (only required if component applicable)
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
Manufacturer | P225 | token | [-] | |
Model | P226 | token | [-] | |
[F1CertificationNumber | P227 | token | [-] | ] |
Date | P228 | dateTime | [-] | Date and time when the component-hash is created |
AppVersion | P229 | string | [-] | |
CertificationMethod | P255 | string | [-] | Allowed values: ‘Measured’, ‘Standard values’ |
Input parameters ‘Retarder/LossMap’ for each grid point in the characteristic curve (only required if component applicable)
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
RetarderSpeed | P057 | double, 2 | [1/min] | |
TorqueLoss | P058 | double, 2 | [Nm] |
This Annex describes the certification provisions regarding the torque losses of propulsion axles for heavy duty vehicles. Alternatively to the certification of axles the calculation procedure for the standard torque loss as defined in Appendix 3 to this Annex can be applied for the purpose of the determination of vehicle specific CO2 emissions.
For the purposes of this Annex the following definitions shall apply:
‘Single reduction axle (SR)’ means a driven axle with only one gear reduction, typically a bevel gear set with or without hypoid offset.
‘Single portal axle (SP)’ means an axle, that has typically a vertical offset between the rotating axis of the crown gear and the rotating axis of the wheel due to the demand of a higher ground clearance or a lowered floor to allow a low floor concept for inner city buses. Typically, the first reduction is a bevel gear set, the second one a spur gear set with vertical offset close to the wheels.
‘Hub reduction axle (HR)’ means a driven axle with two gear reductions. The first is typically a bevel gear set with or without hypoid offset. The other is a planetary gear set, what is typically placed in the area of the wheel hubs.
‘Single reduction tandem axle (SRT)’ means a driven axle that is basically similar to a single driven axle, but has also the purpose to transfer torque from the input flange over an output flange to a further axle. The torque can be transferred with a spur gear set close at the input flange to generate a vertical offset for the output flange. Another possibility is to use a second pinion at the bevel gear set, what takes off torque at the crown wheel.
‘Hub reduction tandem axle (HRT)’ means a hub reduction axle, what has the possibility to transfer torque to the rear as described under single reduction tandem axle (SRT).
‘Axle housing’ means the housing parts that are needed for structural capability as well as for carrying the driveline parts, bearings and sealings of the axle.
‘Pinion’ means a part of a bevel gear set which usually consists of two gears. The pinion is the driving gear which is connected with the input flange. In case of a SRT / HRT, a second pinion can be installed to take off torque from the crown wheel.
‘Crown wheel’ means a part of a bevel gear set which usually consists of two gears. The crown wheel is the driven gear and is connected with the differential cage.
‘Hub reduction’ means the planetary gear set that is installed commonly outside the planetary bearing at hub reduction axles. The gear set consists of three different gears. The sun, the planetary gears and the ring gear. The sun is in the centre, the planetary gears are rotating around the sun and are mounted to the planetary carrier that is fixed to the hub. Typically, the number of planetary gears is between three and five. The ring gear is not rotating and fixed to the axle beam.
‘Planetary gear wheels’ means the gears that rotate around the sun within the ring gear of a planetary gear set. They are assembled with bearings on a planetary carrier, what is joined to a hub.
‘Oil type viscosity grade’ means a viscosity grade as defined by SAE J306.
‘Factory fill oil’ means the oil type viscosity grade that is used for the oil fill in the factory and which is intended to stay in the axle for the first service interval.
‘Axle line’ means a group of axles that share the same basic axle-function as defined in the family concept.
‘Axle family’ means a manufacturer's grouping of axles which through their design, as defined in Appendix 4 of this Annex, have similar design characteristics and CO2 and fuel consumption properties.
‘Drag torque’ means the required torque to overcome the inner friction of an axle when the wheel ends are rotating freely with 0 Nm output torque.
‘Mirror inverted axle casing’ means the axle casing is mirrored regarding to the vertical plane.
‘Axle input’ means the side of the axle on which the torque is delivered to the axle.
‘Axle output’ means the side(s) of the axle where the torque is delivered to the wheels.
The axle gears and all bearings, except wheel end bearings used for the measurements, shall not be used.
On request of the applicant different gear ratios can be tested in one axle housing using the same wheel ends.
Different axle ratios of hub reduction axles and single portal axles (HR, HRT, SP) may be measured by exchanging the hub reduction only. The provisions as specified in Appendix 4 to this Annex shall apply.
The total run-time for the optional run-in and the measurement of an individual axle (except for the axle housing and wheel-ends) shall not exceed 120 hours.
For testing the losses of an axle the torque loss map for each ratio of an individual axle shall be measured, however axles can be grouped in axle families following the provisions of Appendix 4 to this Annex.
On request of the applicant a run-in procedure may be applied to the axle. The following provisions shall apply for a run-in procedure.
The temperature in the test cell shall be maintained to 25 °C ± 10 °C. The ambient temperature shall be measured within a distance of 1 m to the axle housing. Forced heating of the axle may only be applied by an external oil conditioning system as described in 4.1.5.
The oil temperature shall be measured at the centre of the oil sump or at any other suitable point in accordance with good engineering practice. In case of external oil conditioning, alternatively the oil temperature can be measured in the outlet line from the axle housing to the conditioning system within 5 cm downstream the outlet. In both cases the oil temperature shall not exceed 70 °C.
Only recommended factory fill oils as specified by the axle manufacturer shall be used for the measurement. In the case of testing different gear ratio variants with one axle housing, new oil shall be filled in for each single measurement.
If different oils with multiple viscosity grades are specified for the factory fill, the manufacturer shall choose the oil with the highest viscosity grade for performing the measurements on the parent axle.
If more than one oil within the same viscosity grade is specified within one axle family as factory fill oil, the applicant may choose one oil of these for the measurement related to certification.
The oil level or filling volume shall be set to the maximum level as defined in the manufacturer's maintenance specifications.
An external oil conditioning and filtering system is permitted. The axle housing may be modified for the inclusion of the oil conditioning system.
The oil conditioning system shall not be installed in a way which would enable changing oil levels of the axle in order to raise efficiency or to generate propulsion torques in accordance with good engineering practice.
For the purpose of the torque loss measurement different test set-ups are permitted as described in paragraph 4.2.3 and 4.2.4.
In case of a tandem axle, each axle shall be measured separately. The first axle with longitudinal differential shall be locked. The output shaft of drive-through axles shall be installed freely rotatable.
A test set-up considered ‘Type A’ consists of a dynamometer on the axle input side and at least one dynamometer on the axle output side(s). Torque measuring devices shall be installed on the axle input- and output- side(s). For type A set-ups with only one dynamometer on the output side, the free rotating end of the axle shall be locked.
To avoid parasitic losses, the torque measuring devices shall be positioned as close as possible to the axle input- and output- side(s) being supported by appropriate bearings.
Additionally mechanical isolation of the torque sensors from parasitic loads of the shafts, for example by installation of additional bearings and a flexible coupling or lightweight cardan shaft between the sensors and one of these bearings can be applied. Figure 1 shows an example for a test test-up of Type A in a two dynamometer lay-out.
For Type A test set-up configurations the manufacturer shall provide an analysis of the parasitic loads. Based on this analysis the approval authority shall decide about the maximum influence of parasitic loads. However the value ipara cannot be lower than 10 %.
Any other test set-up configuration is called test set-up Type B. The maximum influence of parasitic loads ipara for those configurations shall be set to 100 %.
Lower values for ipara may be used in agreement with the approval authority.
To determine the torque loss map for an axle, the basic torque loss map data shall be measured and calculated as specified in paragraph 4.4. [F1The torque loss results shall be complemented in accordance with 4.4.8 and formatted in accordance with Appendix 6 for the further processing by the simulation tool.]
The calibration laboratory facilities shall comply with the requirements of either ISO/TS 16949, ISO 9000 series or ISO/IEC 17025. All laboratory reference measurement equipment, used for calibration and/or verification, shall be traceable to national (international) standards.
The torque measurement uncertainty shall be calculated and included as described in paragraph 4.4.7.
The sample rate of the torque sensors shall be in accordance with 4.3.2.1.
The uncertainty of the rotational speed sensors for the measurement of input and output speed shall not exceed ± 2 rpm.
The uncertainty of the temperature sensors for the measurement of the ambient temperature shall not exceed ± 1 °C.
The uncertainty of the temperature sensors for the measurement of the oil temperature shall not exceed ± 0,5 °C.
The following signals shall be recorded for the purpose of the calculation of the torque losses:
Input and output torques [Nm]
Input and/or output rotational speeds [rpm]
Ambient temperature [°C]
Oil temperature [°C]
Temperature at the torque sensor
Torque: 1 kHz
Rotational speed: 200 Hz
Temperatures: 10 Hz
Signal filtering may be applied in agreement with the approval authority. Any aliasing effect shall be avoided.
The extent of the torque loss map to be measured is limited to:
either an output torque of 10 kNm
or an input torque of 5 kNm
or the maximum engine power tolerated by the manufacturer for a specific axle or in case of multiple driven axles according to the nominal power distribution.
If the radius of the smallest tire is reduced (e.g. product development) after completing the measurement of an axle or when the physic boundaries of the test stand are reached (e.g. by product development changes), the missing points may be extrapolated by the manufacturer out of the existing map. The extrapolated points shall not exceed more than 10 % of all points in the map and the penalty for these points is 5 % torque loss to be added on the extrapolated points.
:
250 Nm steps
:
500 Nm steps
:
1 000 Nm steps
:
2 000 Nm steps
If the maximum input torque is limited by the manufacturer, the last torque step to be measured is the one below this maximum without consideration of any losses. In that case an extrapolation of the torque loss shall be applied up to the torque corresponding to the manufacturer's limitation with the linear regression based on the torque steps of the corresponding speed step.
The range of test speeds shall comprise from 50 rpm wheel speed to the maximum speed. The maximum test speed to be measured is defined by either the maximum axle input speed or the maximum wheel speed, whichever of the following conditions is reached first:
The maximum applicable axle input speed may be limited to design specification of the axle.
The maximum wheel speed is measured under consideration of the smallest applicable tire diameter at a vehicle speed of 90 km/h for trucks and 110 km/h for coaches. If the smallest applicable tire diameter is not defined, paragraph 4.3.4.1 shall apply.
The wheel speed step width for testing shall be 50 rpm.
For each speed step the torque loss shall be measured for each output torque step starting from 250 Nm upward to the maximum and downward to the minimum. The speed steps can be run in any order. [F2The torque measurement sequence shall be performed and recorded twice.]
Interruptions of the sequence for cooling or heating purposes are permitted.
[F1The measurement duration for each single grid point shall be 5-20 seconds.]
[F1The recorded values for each grid point within the 5-20 seconds interval in accordance with point 4.4.2 shall be averaged to an arithmetic mean.]
All four averaged intervals of corresponding speed and torque grid points from both sequences measured each upward and downward shall be averaged to an arithmetic mean and result into one torque loss value.
where:
=
Torque loss of the axle at the input side [Nm]
=
Input torque [Nm]
=
Axle gear ratio [-]
=
Output torque [Nm]
The total uncertainty UT,loss of the torque loss shall be calculated based on the following parameters:
Temperature effect
Parasitic loads
Uncertainty (incl. sensitivity tolerance, linearity, hysteresis and repeatability)
The total uncertainty of the torque loss (UT,loss) is based on the uncertainties of the sensors at 95 % confidence level. The calculation shall be done for each applied sensor (e.g. three machine lay out: UT,in, UT,out,1, UTout,2) as the square root of the sum of squares (‘Gaussian law of error propagation’).
wpara = senspara * ipara
where:
=
Uncertainty of input/output torque loss measurement separately for input and output torque; [Nm]
=
Axle gear ratio [-]
=
Uncertainty by temperature influence on current torque signal; [Nm]
=
Temperature influence on current torque signal per Kref, declared by sensor manufacturer; [%]
=
Uncertainty by temperature influence on zero torque signal (related to nominal torque) [Nm]
=
Temperature influence on zero torque signal per Kref (related to nominal torque), declared by sensor manufacturer; [%]
=
Reference temperature span for tkc and tk0, declared by sensor manufacturer; [°C]
=
Absolute difference in sensor temperature measured at torque sensor between calibration and measurement; If the sensor temperature cannot be measured, a default value of ΔK = 15 K shall be used [°C]
=
Current/measured torque value at torque sensor; [Nm]
=
Nominal torque value of torque sensor; [Nm]
=
Uncertainty by torque sensor calibration; [Nm]
=
Relative calibration uncertainty (related to nominal torque); [%]
=
calibration advancement factor (if declared by sensor manufacturer, otherwise = 1)
=
Uncertainty by parasitic loads; [Nm]
=
senspara * ipara
Relative influence of forces and bending torques caused by misalignment
=
Maximum influence of parasitic loads for specific torque sensor declared by sensor manufacturer [%]; if no specific value for parasitic loads is declared by the sensor manufacturer, the value shall be set to 1,0 %
=
Maximum influence of parasitic loads for specific torque sensor depending on test set-up as indicated in section 4.2.3 and 4.2.4 of this annex.
In the case the calculated uncertainties UT,in/out are below the following limits, the reported torque loss Tloss,rep shall be regarded as equal to the measured torque loss Tloss .
UT,in : 7,5 Nm or 0,25 % of the measured torque, whichever allowed uncertainty value is higher
UT,out : 15 Nm or 0,25 % of the measured torque, whichever allowed uncertainty value is higher
In the case of higher calculated uncertainties, the part of the calculated uncertainty exceeding the above specified limits shall be added to Tloss for the reported torque loss Tloss,rep as follows:
If the limits of UT,in are exceeded:
Tloss,rep = Tloss + ΔUTin
ΔUT,in = MIN((UT,in – 0,25 % * Tc) or (UT,in – 7,5 Nm))
If limits of UT,out out are exceeded:
Tloss,rep = Tloss + ΔUT,out/igear
ΔUT,out = MIN((UT,out – 0,25 % * Tc) or (UT,out – 15Nm))
where:
=
Uncertainty of input/output torque loss measurement separately for input and output torque; [Nm]
=
Axle gear ratio [-]
=
The part of the calculated uncertainty exceeding the specified limits
T loss,rep,tdm = T loss,rep, 1 + T loss,rep, 2
T in,tdm = T in, 1 + T in, 2]
Sample size for conformity testing
Production number | Number of test for SR axles | Number of tests for other axles than SR axles |
---|---|---|
0 – 40 000 | 2 | 1 |
40 001 – 50 000 | 2 | 2 |
50 001 – 60 000 | 3 | 2 |
60 001 – 70 000 | 4 | 2 |
70 001 – 80 000 | 5 | 2 |
80 001 and more | 5 | 3 |
Torque loss measurement according to this Annex by following the full procedure limited to the grid points described in 6.2.
Torque loss measurement according to this Annex by following the full procedure limited to the grid points described in 6.2, with exception of the run-in procedure. In order to consider the run-in characteristic of an axle, a corrective factor may be applied. This factor shall be determined according to good engineering judgement and with agreement of the approval authority.
Measurement of drag torque according to paragraph 6.3. The manufacturer may choose a run-in procedure according to good engineering judgement up to 100 h.
The control areas shall be selected depending on the axle line:
SR axles including tandem combinations: Control areas 5, 6, 8 and 9
HR axles including tandem combinations: Control areas 2, 3, 4 and 5
The selected point shall be located in the centre of the area referring to the speed range and the applicable torque range for the according speed.
In order to have a corresponding point for comparison with the loss map measured for certification, the selected point shall be moved to the closest measured point from the approved map.
where:
=
Efficiency of the grid point from each single control area 1 to 9
=
Output torque [Nm]
=
Input torque [Nm]
=
axle ratio [-]
For SR axles:
For HR axles:
where:
=
average efficiency for low speed
=
average efficiency for mid speed
=
average efficiency for high speed
=
simplified averaged efficiency for axle
[F1If a torque loss measurement in accordance with points 6.1(a) or (b) is conducted, the average efficiency of the tested axle during conformity of the certified CO 2 emissions and fuel consumption related properties procedure shall not be lower than 1,5 % for SR axles and 2,0 % for all other axles lines below the corresponding average efficiency of the type approved axle.
If a measurement of drag torque in accordance with point 6.1(c) is conducted, the drag torque of the tested axle during conformity of the certified CO 2 emissions and fuel consumption related properties procedure shall be lower than the corresponding drag torque of the type approved axle or within the tolerance indicated in Table 2.]
Axleline | Tolerances for axles measured in CoP after run-inComparison to Td0 | Tolerances for axles measured in CoP without run inComparison to Td0 | ||||||
---|---|---|---|---|---|---|---|---|
for i | tolerance Td0_input [Nm] | for i | tolerance Td0_input [Nm] | for i | tolerance Td0_input Nm] | for i | tolerance Td0_input [Nm] | |
SR | ≤ 3 | 15 | > 3 | 12 | ≤ 3 | 25 | > 3 | 20 |
SRT | ≤ 3 | 16 | > 3 | 13 | ≤ 3 | 27 | > 3 | 21 |
SP | ≤ 6 | 11 | > 6 | 10 | ≤ 6 | 18 | > 6 | 16 |
HR | ≤ 7 | 10 | > 7 | 9 | ≤ 7 | 16 | > 7 | 15 |
HRT | ≤ 7 | 11 | > 7 | 10 | ≤ 7 | 18 | > 7 | 16 |
=
gear ratio.
of a certificate on CO2 emission and fuel consumption related properties of an axle family in accordance with Commission Regulation (EU) 2017/2400.
Commission Regulation (EU) 2017/2400 as last amended by …
Certification number:
Hash:
Reason for extension:
Attachments:
Information document
Test report
Information document no.: | Issue: Date of issue: Date of Amendment: |
pursuant to …
[F1Axle type/family (if applicable):]
…
Parent axle | Family member | ||||
or axle type | #1 | #2 | #3 | ||
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
1.1 | Axle line (SR, HR, SP, SRT, HRT) | … | … | … | … | ||
1.2 | Axle gear ratio | … | … | … | … | ||
1.3 | Axle housing (number/ID/drawing) | … | … | … | … | ||
1.4 | Gear specifications | … | … | … | |||
1.4.1 | Crown wheel diameter; [mm] | … | … | ||||
1.4.2 | Vertical offset pinion/crown wheel; [mm] | … |
Angle between pinion axle and crown wheel axle; [°]
No.: | Description: | Date of issue: |
---|---|---|
1 | … | … |
2 | … |
The standard torque losses for axles are shown in Table 1. The standard table values consist of the sum of a generic constant efficiency value covering the load dependent losses and a generic basic drag torque loss to cover the drag losses at low loads.
Tandem axles shall be calculated using a combined efficiency for an axle including drive-thru (SRT, HRT) plus the matching single axle (SR, HR).
Generic efficiency and drag loss
Basic function | Generic efficiencyη | Drag torque(wheel side)Td0 = T0 + T1 * igear |
---|---|---|
Single reduction axle (SR) | 0,98 | T0 = 70 Nm T1 = 20 Nm |
Single reduction tandem axle (SRT) / single portal axle (SP) | 0,96 | T0 = 80 Nm T1 = 20 Nm |
Hub reduction axle (HR) | 0,97 | T0 = 70 Nm T1 = 20 Nm |
Hub reduction tandem axle (HRT) | 0,95 | T0 = 90 Nm T1 = 20 Nm |
The basic drag torque (wheel side) Td0 is calculated by
Td0 = T0 + T1 * igear
using the values from Table 1.
The standard torque loss Tloss,std on the wheel side of the axle is calculated by
where:
=
Standard torque loss at the wheel side [Nm]
=
Basis drag torque over the complete speed range [Nm]
=
Axle gear ratio [-]
=
Generic efficiency for load dependent losses [-]
=
Output torque [Nm]
An axle family is characterized by design and performance parameters. These shall be common to all axles within the family. The axle manufacturer may decide which axle belongs to an axle family, as long as the family criteria of paragraph 4 are respected. In addition to the parameters listed in paragraph 4, the axle manufacturer may introduce additional criteria allowing the definition of families of more restricted size. These parameters are not necessarily parameters that have an influence on the level of performance. The axle family shall be approved by the approval authority. The manufacturer shall provide to the approval authority the appropriate information relating to the performance of the members of the axle family.
In some cases there may be interaction between parameters. This shall be taken into consideration to ensure that only axles with similar characteristics are included within the same axle family. These cases shall be identified by the manufacturer and notified to the approval authority. It shall then be taken into account as a criterion for creating a new axle family.
In case of parameters, which are not listed in paragraph 3 and which have a strong influence on the level of performance, this parameters shall be identified by the manufacturer on the basis of good engineering practice, and shall be notified to the approval authority.
Single reduction axle (SR)
Hub reduction axle (HR)
Single portal axle (SP)
Single reduction tandem axle (SRT)
Hub reduction tandem axle (HRT)
Same inner axle housing geometry between differential bearings and horizontal plane of centre of pinion shaft according to drawing specification (Exception for single portal axles (SP)). Geometry changes due to an optional integration of a differential lock are permitted within the same axle family. In case of mirror inverted axle casings of axles, the mirror inverted axles can be combined in the same axle family as the origin axles, under the premise, that the bevel gear sets are adapted to the other running direction (change of spiral direction).
[F1Crown wheel diameter (+ 1,5 %/– 8 % ref. to the largest drawing diameter)]
Vertical hypoid offset pinion/crown wheel within ± 2 mm
In case of single portal axles (SP): Pinion angle with respect to horizontal plane within ± 5°
In case of single portal axles (SP): Angle between pinion axle and crown wheel axle within ± 3,5°
In case of hub reduction and single portal axles (HR, HRT, FHR, SP): Same number of planetary gear and spur wheels
[F1Gear ratio of every gear step within an axle in a range of 2, as long as only one gear set is changed]
Oil level within ± 10 mm or oil volume ± 0,5 litre referring to drawing specification and the installation position in the vehicle
Same oil type viscosity grade (recommended factory fill)
For all bearings: same bearing rolling/sliding circle diameter (inner/outer) and width within ± 2 mm ref. to drawing
[F3. . . . .]
In the case of an axle being type approved accordant to this Annex, the axle shall bear:
[F1The manufacturer's name or trade mark]
The make and identifying type indication as recorded in the information referred to in paragraph 0.2 and 0.3 of Appendix 2 to this Annex
The certification mark as a rectangle surrounding the lower-case letter ‘e’ followed by the distinguishing number of the Member State which has granted the certificate:
1 for Germany;
2 for France;
3 for Italy;
4 for the Netherlands;
5 for Sweden;
6 for Belgium;
7 for Hungary;
8 for the Czech Republic;
9 for Spain;
11 for the United Kingdom;
12 for Austria;
13 for Luxembourg;
17 for Finland;
18 for Denmark;
19 for Romania;
20 for Poland;
21 for Portugal;
23 for Greece;
24 for Ireland;
25 for Croatia;
26 for Slovenia;
27 for Slovakia;
29 for Estonia;
32 for Latvia;
34 for Bulgaria;
36 for Lithuania;
49 for Cyprus;
50 for Malta
For this Regulation, the sequence number shall be 00.
The above certification mark affixed to an axle shows that the type concerned has been approved in Poland (e20), pursuant to this Regulation. The first two digits (00) are indicating the sequence number assigned to the latest technical amendment to this Regulation. The following letter indicates that the certificate was granted for an axle (L). The last four digits (0004) are those allocated by the type-approval authority to the axle as the base certification number.
eX*YYYY/YYYY*ZZZZ/ZZZZ*L*0000*00
Section 1 | Section 2 | Section 3 | Additional letter to Section 3 | Section 4 | Section 5 |
---|---|---|---|---|---|
Indication of country issuing the certificate | HDV CO 2 certification Regulation (2017/2400) | Latest amending Regulation (ZZZZ/ZZZZ) | L = Axle | Base certification number 0000 | Extension 00] |
This Appendix describes the list of parameters to be provided by the component manufacturer as input to the simulation tool. The applicable XML schema as well as example data are available at the dedicated electronic distribution platform.
Unique identifier as used in the simulation tool for a specific input parameter or set of input data]
Data type of the parameter
sequence of characters in ISO8859-1 encoding
sequence of characters in ISO8859-1 encoding, no leading/trailing whitespace
date and time in UTC time in the format: YYYY-MM-DD T HH:MM:SS Z with italic letters denoting fixed characters e.g. ‘2002-05-30T09:30:10Z’
value with an integral data type, no leading zeros, e.g. ‘1800’
fractional number with exactly X digits after the decimal sign (‘.’) and no leading zeros e.g. for ‘double, 2’: ‘2345.67’; for ‘double, 4’: ‘45.6780’
physical unit of the parameter
Input parameters ‘Axlegear/General’
Parameter name | Param ID | Type | Unit | Description/Reference |
---|---|---|---|---|
Manufacturer | P215 | token | [-] | |
Model | P216 | token | [-] | |
[F1CertificationNumber | P217 | token | [-] | ] |
Date | P218 | dateTime | [-] | Date and time when the component-hash is created |
AppVersion | P219 | token | [-] | |
LineType | P253 | string | [-] | Allowed values: ‘Single reduction axle’, ‘Single portal axle’, ‘Hub reduction axle’, ‘Single reduction tandem axle’, ‘Hub reduction tandem axle’ |
Ratio | P150 | double, 3 | [-] | |
CertificationMethod | P256 | string | [-] | Allowed values: ‘Measured’, ‘Standard values’ |
Input parameters ‘Axlegear/LossMap’ for each grid point in the loss map
Parameter name | Param ID | Type | Unit | Description/Reference |
---|---|---|---|---|
InputSpeed | P151 | double, 2 | [1/min] | |
InputTorque | P152 | double, 2 | [Nm] | |
TorqueLoss | P153 | double, 2 | [Nm] |
This Annex sets out the test procedure for verifying air drag data.
For the purposes of this Annex the following definitions shall apply:
‘Active aero device’ means measures which are activated by a control unit to reduce the air drag of the total vehicle.
‘Aero accessories’ mean optional devices which have the purpose to influence the air flow around the total vehicle.
‘A-pillar’ means the connection by a supporting structure between the cabin roof and the front bulkhead.
‘Body in white geometry’ means the supporting structure incl. the windshield of the cabin.
‘B-pillar’ means the connection by a supporting structure between the cabin floor and the cabin roof in the middle of the cabin.
‘Cab bottom’ means the supporting structure of the cabin floor.
‘Cabin over frame’ means distance from frame to cabin reference point in vertical Z. Distance is measured from top of horizontal frame to cabin reference point in vertical Z.
‘Cabin reference point’ means the reference point (X/Y/Z = 0/0/0) from the CAD coordinate system of the cabin or a clearly defined point of the cabin package e.g. heel point.
‘Cabin width’ means the horizontal distance of the left and right B-pillar of the cabin.
‘Constant speed test’ means measurement procedure to be carried out on a test track in order to determine the air drag.
‘Dataset’ means the data recorded during a single passing of a measurement section.
‘EMS’ means the European Modular System (EMS) in accordance with Council Directive 96/53/EC.
‘Frame height’ means distance of wheel center to top of horizontal frame in Z.
‘Heel point’ means the point which is representing the heel of shoe location on the depressed floor covering, when the bottom of shoe is in contact with the undepressed accelerator pedal and the ankle angle is at 87°. (ISO 20176:2011)
‘Measurement area(s)’ means designated part(s) of the test track consisting of at least one measurement section and a preceded stabilisation section.
‘Measurement section’ means a designated part of the test track which is relevant for data recording and data evaluation.
‘Roof height’ means distance in vertical Z from cabin reference point to highest point of roof w/o sunroof
The constant speed test procedure shall be applied to determine the air drag characteristics. During the constant speed test the main measurement signals driving torque, vehicle speed, air flow velocity and yaw angle shall be measured at two different constant vehicle speeds (low and high speed) under defined conditions on a test track. The measurement data recorded during the constant speed test shall be entered into the air drag pre-processing tool which determines product of drag coefficient by cross sectional area for zero crosswind conditions Cd · Acr (0) as input for the simulation tool. The applicant for a certificate shall declare a value Cd · Adeclared in a range from equal up to a maximum of + 0,2 m2 higher than Cd · Acr (0). The value Cd · Adeclared shall be the input for the simulation tool CO2 simulation tool and the reference value for conformity of the certified CO2 emissions and fuel consumption related properties testing.
[F1Vehicles which are not member of a family shall use the standard values for C d ·A declared as described in Appendix 7 to this Annex. In this case no input data on air drag shall be provided. The allocation of standard values is done automatically by the simulation tool.]
Circuit track (drivable in one direction (*)):
with two measurement areas, one on each straight part, with maximum deviation of less than 20 degrees);
or
Circuit or straight line track (drivable in both directions):
with one measurement area (or two with the above named maximum deviation); two options: alternating driving direction after each test section; or after a selectable set of test sections e.g. ten times driving direction 1 followed by ten times driving direction 2.
On the test track measurement section(s) of a length of 250 m with a tolerance of ± 3 m shall be defined.
A measurement area shall consist of at least one measurement section and a stabilisation section. The first measurement section of a measurement area shall be preceded by a stabilisation section to stabilise the speed and torque. The stabilisation section shall have a length of minimum 25 m. The test track layout shall enable that the vehicle enters the stabilisation section already with the intended maximum vehicle speed during the test.
Latitude and longitude of start and end point of each measurement section shall be determined with an accuracy of better or equal 0,15 m 95 % Circular Error Probable (DGPS accuracy).
The measurement section and the stabilization section have to be a straight line.
The average longitudinal slope of each measurement and the stabilisation section shall not exceed ± 1 per cent. Slope variations on the measurement section shall not lead to velocity and torque variations above the thresholds specified in 3.10.1.1 items vii. and viii. of this Annex.
The test track shall consist of asphalt or concrete. The measurement sections shall have one surface. Different measurement sections are allowed to have different surfaces.
There shall be a standstill area on the test track where the vehicle can be stopped to perform the zeroing and the drift check of the torque measurement system.
There shall be no obstacles within 5 m distance to both sides of the vehicle. Safety barriers up to a height of 1 m with more than 2,5 m distance to the vehicle are permitted. Any bridges or similar constructions over the measurement sections are not allowed. The test track shall have enough vertical clearance to allow the anemometer installation on the vehicle as specified in 3.4.7 of this Annex.
The manufacturer shall define whether the altitude correction shall be applied in the test evaluation. In case an altitude correction is applied, for each measurement section the altitude profile shall be made available. The data shall meet the following requirements:
The altitude profile shall be measured at a grid distance of lower or equal than 50 m in driving direction.
For each grid point the longitude, the latitude and the altitude shall be measured at least at one point (‘altitude measurement point’) on each side of the centre line of the lane and then be processed to an average value for the grid point.
The grid points as provided to the air drag pre-processing tool shall have a distance to the centre line of the measurement section of less than 1 m.
The positioning of the altitude measurement points to the centre line of the lane (perpendicular distance, number of points) shall be chosen in a way that the resulting altitude profile is representative for the gradient driven by the test vehicle.
The altitude profile shall have an accuracy of ± 1cm or better.
The measurement data shall not be older than 10 years. A renewal of the surface in the measurement area requires a new altitude profile measurement.
Average wind speed: ≤ 5 m/s
Gust wind speed (1s central moving average): ≤ 8 m/s
Items i. and ii. are applicable for the datasets recorded in the high speed test and the misalignment calibration test but not for the low speed tests.
Average yaw angle (β):
≤ 3 degrees for datasets recorded in the high speed test
≤ 5 degrees for datasets recorded during misalignment calibration test
The validity of wind conditions is checked by the air drag pre-processing based on the signals recorded at the vehicle after application of the boundary layer correction. Measurement data collected under conditions exceeding the above named limits are automatically excluded from the calculation.
Best or second best label for rolling resistance which is available at the moment the test is performed
Maximum tread depth of 10 mm on the complete vehicle including trailer
[F1Tyres inflated to the highest allowable pressure of the tyre manufacturer within a tolerance of ± 0,2 bar]
The device is always activated and effective to reduce the air drag at vehicle speed over 60 km/h
The device is installed and effective in a similar manner on all vehicles of the family.
If i. and ii. are not applicable the active aero device has to be fully deactivated during the constant speed test.
The calibration laboratory shall comply with the requirements of either ISO/TS 16949, ISO 9000 series or ISO/IEC 17025. All laboratory reference measurement equipment, used for calibration and/or verification, shall be traceable to national (international) standards.
Hub torque meter
Rim torque meter
Half shaft torque meter
Non linearity: < ± 6 Nm
Repeatability: < ± 6 Nm
Crosstalk: < ± 1 % FSO (only applicable for rim torque meters)
Measurement rate: ≥ 20 Hz
where:
‘Non linearity’ means the maximum deviation between ideal and actual output signal characteristics in relation to the measurand in a specific measuring range.
‘Repeatability’ means closeness of the agreement between the results of successive measurements of the same measurand carried out under the same conditions of measurement.
‘Crosstalk’ means signal at the main output of a sensor (My), produced by a measurand (Fz) acting on the sensor, which is different from the measurand assigned to this output. Coordinate system assignment is defined according to ISO 4130.
‘FSO’ means full scale output of calibrated range.
The recorded torque data shall be corrected for the instrument error determined by the supplier.
The vehicle speed is determined by the air drag pre-processing tool based on the CAN-bus front axle signal which is calibrated based on either:
:
a reference speed calculated by a delta-time from two fixed opto-electronic barriers (see 3.4.4 of this Annex) and the known length(s) of the measurement section(s) or
:
a delta-time determined speed signal from the position signal of a DGPS and the known length(s) of the measurement section(s), derived by the DGPS coordinates
For the vehicle speed calibration the data recorded during the high speed test are used.
For the calculation of rotational speed of the wheels at the driven axle the CAN engine speed signal together with the transmission ratios (gears for low speed test and high speed test, axle ratio) shall be made available. For the CAN engine speed signal it shall be demonstrated that the signal provided to the air drag pre-processing tool is identical to the signal to be used for in-service testing as set out in Annex I of Regulation (EU) No 582/2011.
For vehicles with torque converter which are not able to drive the low speed test with closed lockup clutch additionally the cardan shaft speed signal and the axle ratio or the average wheel speed signal for the driven axle shall be provided to the air drag pre-processing tool. It shall be demonstrated that the engine speed calculated from this additional signal is within 1 % range compared to the CAN engine speed. This shall be demonstrated for the average value over a measurement section driven at the lowest possible vehicle speed in the torque converter locked mode and at the applicable vehicle speed for the high speed test.
The signal of the barriers shall be made available to the air drag pre-processing tool for triggering begin and end of the measurement section and the calibration of the vehicle speed signal. The measurement rate of the trigger signal shall be greater or equal to 100 Hz. Alternatively a DGPS system can be used.
Required accuracy:
:
< 3 m 95 % Circular Error Probable
:
≥ 4 Hz
Required accuracy:
:
0,15 m 95 % Circular Error Probable
:
≥ 100 Hz
Ambient pressure and humidity of the ambient air are determined from a stationary weather station. This meteorological instrumentation shall be positioned in a distance less than 2 000 m to one of the measurement areas, and shall be positioned at an altitude exceeding or equal that of the measurement areas.
Required accuracy:
:
± 1 °C
:
± 5 % RH
:
± 1 mbar
:
≤ 6 minutes
A mobile anemometer shall be used to measure air flow conditions, i.e. air flow velocity and yaw angle (β) between total air flow and vehicle longitudinal axis.
The anemometer shall be calibrated in facility according to ISO 16622. The accuracy requirements according to Table 1 have to be fulfilled:
Anemometer accuracy requirements
Air speed range[m/s] | Accuracy air speed[m/s] | Accuracy yaw angle in yaw angle range of 180 ± 7 degrees[degrees] |
---|---|---|
20 ± 1 | ± 0,7 | ± 1,0 |
27 ± 1 | ± 0,9 | ± 1,0 |
35 ± 1 | ± 1,2 | ± 1,0 |
The mobile anemometer shall be installed on the vehicle in the prescribed position:
X position:
truck: front face ± 0,3 m of the semi-trailer or box-body
Y position: plane of symmetry within a tolerance ± 0,1 m
Z position:
The installation height above the vehicle shall be one third of total vehicle height with in a tolerance of 0,0 m to + 0,2 m.
The instrumentation shall be done as exact as possible using geometrical/optical aids. Any remaining misalignment is subject to the misalignment calibration to be performed in accordance with 3.6 of this Annex.
The ambient air temperature shall be measured on the pole of the mobile anemometer. The installation height shall be maximum 600 mm below the mobile anemometer. The sensor shall be shielded to the sun.
Required accuracy: ± 1 °C
Update rate: ≥ 1 Hz
The temperature of the proving ground shall be recorded on vehicle by means of a contactless IR sensor by wideband (8 to 14 μm). For tarmac and concrete an emissivity factor of 0,90 shall be used. The IR sensor shall be calibrated according to ASTM E2847.
Required accuracy at calibration: Temperature: ± 2,5 °C
Update rate: ≥ 1 Hz
On each applicable combination of measurement section and driving direction the constant speed test procedure consisting of the low speed, high speed and low speed test sequence as specified below shall be performed in the same direction.
maximum speed: 95 km/h;
minimum speed: 85 km/h or 3 km/h less than the maximum vehicle speed the vehicle can be operated at the test track, whichever value is lower.
Installation of torque meters on the driven axles of the test vehicle and check of installation and signal data according to the manufacturer specification.
Documentation of relevant general vehicle data for the official testing template in accordance with 3.7 of this Annex.
For the calculation of the acceleration correction by the air drag pre-processing tool the actual vehicle weight shall be determined before the test within a range of ± 500 kg.
Check of tyres for the maximum allowable inflation pressure and documentation of tyre pressure values.
Preparation of opto-electronic barriers at the measurement section(s) or check of proper function of the DGPS system.
Installation of mobile anemometer on the vehicle and/or control of the installation, position and orientation. A misalignment calibration test has to be performed every time the anemometer has been mounted newly on the vehicle.
[F1Check of vehicle setup regarding the height and geometry, with running engine. The maximum height of the vehicle shall be determined by measuring at the four corners of the box/semi-trailer.]
Adjustment the height of the semi-trailer to the target value and redo determination of maximum vehicle height if necessary.
Mirrors or optical systems, roof fairing or other aerodynamic devices shall be in their regular driving condition.
Drive the vehicle minimum 90 minutes at the target speed of the high speed test to warm-up the system. A repeated warm up (e.g. after a configuration change, an invalid test etc.) shall be at least as long as the standstill time. The warm-up phase can be used to perform the misalignment calibration test as specified in 3.6 of this Annex.
[F2In case it is not possible to maintain high speed for a complete round, e.g. due to curves being too narrow, it is allowed to deviate from target speed requirement during the curves, including the nearby straight portions that are needed for slowing down and accelerating the vehicle.
Deviations shall be minimized as far as possible.
Alternatively, the warm-up phase may be performed on a nearby road, if the target speed is maintained within ± 10 km/h for 90 % of the warm-up time. The part of the warm-up phase used for driving from the road to the standstill area of the test track for zeroing of the torque meters shall be included in the other warm-up phase set out in point 3.5.3.4. The time for this part shall not exceed 20 minutes. The speed and time during the warm-up phase shall be recorded by the measurement equipment.]
The zeroing of the torque meters shall be performed as follows:
Bring the vehicle to a standstill
Lift the instrumented wheels off the ground
Perform the zeroing of the amplifier reading of the torque meters
The standstill phase shall not exceed 10 minutes.
Perform the first measurement at low speed. It shall be ensured that:
the vehicle is driven through the measurement section along a straight line as straight as possible
the average driving speed is in accordance with 3.5.1 of this Annex for the measurement section and the preceding stabilisation section
the stability of the driving speed inside the measurement sections and the stabilisation sections is in accordance with 3.10.1.1 item vii. of this Annex
the stability of the measured torque inside the measurement sections and the stabilisation sections is in accordance with 3.10.1.1 item viii. of this Annex
the beginning and the end of the measurement sections are clearly recognizable in the measurement data via a recorded trigger signal (opto-electronic barriers plus recorded GPS data) or via use of a DGPS system
driving at the parts of the test track outside the measurement sections and the preceding stabilisation sections shall be performed without any delay. Any unnecessary manoeuvres shall be avoided during these phases (e.g. driving in sinuous lines)
the maximum time for the low speed test shall not exceed 20 minutes in order to prevent cool down of the tires.
Perform the measurement at the high speed. It shall be ensured that:
the vehicle is driven through the measurement section along a straight line as straight as possible
the average driving speed is in accordance with 3.5.2 of this Annex for the measurement section and the preceding stabilisation section
the stability of the driving speed inside the measurement sections and the stabilisation sections is in accordance with 3.10.1.1 item vii. of this Annex
the stability of the measured torque inside the measurement sections and the stabilisation sections is in accordance with 3.10.1.1 item viii. of this Annex
the beginning and the end of the measurement sections are clearly recognizable in the measurement data via a recorded trigger signal (opto-electronic barriers plus recorded GPS data) or via use of a DGPS system
in the driving phases outside the measurement sections and the preceding stabilization sections any unnecessary manoeuvres shall be avoided (e.g. driving in sinuous lines, unnecessary accelerations or decelerations)
the distance between the measured vehicle to another driven vehicle on the test track shall be at least 500 m.
at least 10 valid passings per heading are recorded
The high speed test can be used to determine the misalignment of the anemometer if the provisions stated in 3.6 are fulfilled.
Perform the second measurement at the low speed directly after the high speed test. Similar provisions as for the first low speed test shall be fulfilled.
Directly after the finalisation of the second low speed test the drift check of the torque meters shall be performed in accordance to the following procedure:
Bring the vehicle to standstill
Lift the instrumented wheels off the ground
The drift of each torque meter calculated from the average of the minimum sequence of 10 seconds shall be less than 25 Nm.
Exceeding this limit leads to an invalid test.
The misalignment of the anemometer shall be determined by a misalignment calibration test on the test track.
Prepare the opto-electronic barriers at the 250 m ± 3 m section, or check the proper function of the DGPS System.
Check the vehicle setup regarding the height and geometry in accordance with 3.5.3.1 of this Annex. Adjust the height of the semi-trailer to the requirements as specified in appendix 4 to this Annex if necessary
No prescriptions for warm-up are applicable
Perform the misalignment calibration test by at least 5 valid passings as described above.
the anemometer has been dismounted from the vehicle
the anemometer has been moved
a different tractor or truck is used
[F1the air drag family has been changed]
In addition to the recording of the modal measurement data, the testing shall be documented in a template which contains at least the following data:
General vehicle description (specifications see Appendix 2 - Information Document)
Actual maximum vehicle height as determined according to 3.5.3.1 item vii.
Start time and date of the test
Vehicle mass within a range of ± 500 kg
Tyre pressures
Filenames of measurement data
Documentation of extraordinary events (with time and number of measurement sections), e.g.
close passing of another vehicle
manoeuvres to avoid accidents, driving errors
technical errors
measurement errors
Datasets became invalid due to events during the measurement (see 3.7 item vii)
Instrument saturation during the measurement sections (e.g. high wind gusts which might have led to anemometer signal saturation)
Measurements in which the permitted limits for the torque meter drift were exceeded
The following tables show the requirements for the measurement data recording and the preparatory data processing for the input into the air drag pre-processing tool:
Table 2 for the vehicle data file
Table 3 for the ambient conditions file
Table 4 for the measurement section configuration file
Table 5 for the measurement data file
Table 6 for the altitude profile files (optional input data)
[F1A detailed description of the requested data formats, the input files and the evaluation principles can be found in the technical documentation of the air drag pre-processing tool.] The data processing shall be applied as specified in section 3.8 of this Annex.
Input data for the air drag pre-processing tool – vehicle data file
a Specification of transmission ratios with at least 3 digits after decimal separator | ||
b If the wheel speed signal is provided to the air drag pre-processing tool (option for vehicles with torque converters, see section 3.4.3 the axle ratio shall be set to ‘1.000’. | ||
c Input only required if value is lower than 88 km/h. | ||
Input data | Unit | Remarks |
---|---|---|
Vehicle group code | [-] | 1 - 17 for trucks |
Vehicle configuration with trailer | [-] | if the vehicle was measured without trailer (input ‘No’) or with trailer i.e. as a truck/trailer or tractor semitrailer combination (input ‘Yes’) |
Vehicle test mass | [kg] | actual mass during measurements |
[F1Gross vehicle mass | [kg] | gross vehicle mass of the rigid lorry or tractor (w/o trailer or semitrailer)] |
Axle ratio | [-] | axle transmission ratioa b |
Gear ratio high speed | [-] | transmission ratio of gear engaged during high speed testa |
Gear ratio low speed | [-] | transmission ratio of gear engaged during low speed testa |
Anemometer height | [m] | height above ground of the measurement point of installed anemometer |
Vehicle height | [m] | maximum vehicle height according to 3.5.3.1 item vii. |
[F1Gear box type | [-] | manual or automated transmission: ‘ SMT ’ , ‘ AMT ’ , ‘ DCT ’ , automatic transmission with torque converter: ‘ APT ’] |
Vehicle maximum speed | [km/h] | maximum speed the vehicle can be practically operated at the test trackc |
Input data for the air drag pre-processing tool – ambient conditions file
Signal | Column identifier in input file | Unit | Measurement rate | Remarks |
---|---|---|---|---|
Time | <t> | [s] since day start (first day) | — | — |
Ambient temperature | <t_amb_stat> | [°C] | At least 1 averaged value per 6 minutes | Stationary weather station |
Ambient pressure | <p_amb_stat> | [mbar] | Stationary weather station | |
Relative air humidity | <rh_stat> | [%] | Stationary weather station |
Input data for air drag pre-processing tool – measurement section configuration file]
Input data | Unit | Remarks |
---|---|---|
Trigger signal used | [-] | 1 = trigger signal used; 0 = no trigger signal used |
Measurement section ID | [-] | user defined ID number |
Driving direction ID | [-] | user defined ID number |
Heading | [°] | heading of the measurement section |
Length of the measurement section | [m] | — |
Latitude start point of section | decimal degrees or decimal minutes | standard GPS, unit decimal degrees: minimum 5 digits after decimal separator |
Longitude start point of section | standard GPS, unit decimal minutes: minimum 3 digits after decimal separator | |
Latitude end point of section | DGPS, unit decimal degrees: minimum 7 digits after decimal separator | |
Longitude end point of section | DGPS, unit decimal minutes: minimum 5 digits after decimal separator | |
Path and/or filename of altitude file | [-] | only required for the constant speed tests (not the misalignment test) and if the altitude correction is enabled. |
Input data for the air drag pre-processing tool – measurement data file
Signal | Column identifier in input file | Unit | Measurement rate | Remarks |
---|---|---|---|---|
Time | <t> | [s] since day start (of first day) | 100 Hz | rate fixed to 100 Hz; time signal used for correlation with weather data and for check of frequency |
(D)GPS latitude | <lat> | decimal degrees or decimal minutes | GPS: ≥ 4 Hz DGPS: ≥ 100 Hz | standard GPS, unit decimal degrees: minimum 5 digits after decimal separator |
(D)GPS longitude | <long> | standard GPS, unit decimal minutes: minimum 3 digits after decimal separator DGPS, unit decimal degrees: minimum 7 digits after decimal separator DGPS, unit decimal minutes: minimum 5 digits after decimal separator | ||
(D)GPS heading | <hdg> | [°] | ≥ 4Hz | |
DGPS velocity | <v_veh_GPS> | [km/h] | ≥ 20 Hz | |
Vehicle velocity | <v_veh_CAN> | [km/h] | ≥ 20 Hz | raw CAN bus front axle signal |
Air speed | <v_air> | [m/s] | ≥ 4 Hz | raw data (instrument reading) |
Inflow angle (beta) | <beta> | [°] | ≥ 4 Hz | raw data (instrument reading); ‘180°’ refers to air flow from front |
Engine speed or cardan speed | <n_eng> or <n_card> | [rpm] | ≥ 20 Hz | cardan speed for vehicles with torque converter not locked during low speed test |
Torque meter (left wheel) | <tq_l> | [Nm] | ≥ 20 Hz | — |
Torque meter (right wheel) | <tq_r> | [Nm] | ≥ 20 Hz | |
Ambient temperature on vehicle | <t_amb_veh> | [°C] | ≥ 1 Hz | |
Trigger signal | <trigger> | [-] | 100 Hz | optional signal; required if measurement sections are identified by opto electronic barriers (option ‘trigger_used=1’) |
Proving ground temperature | <t_ground> | [°C] | ≥ 1 Hz | |
Validity | <valid> | [-] | — | optional signal (1=valid; 0=invalid); |
Input data for the air drag pre-processing tool – altitude profile file
Input data | Unit | Remarks |
---|---|---|
Latitude | decimal degrees or decimal minutes | unit decimal degrees: minimum 7 digits after decimal separator |
Longitude | unit decimal minutes: minimum 5 digits after decimal separator | |
Altitude | [m] | minimum 2 digits after decimal separator |
This sections sets out the criteria to obtain valid results in the air drag pre-processing tool.
the average vehicle speed is inside the criteria as defined in 3.5.2
the ambient temperature is inside the range as described in 3.2.2. This criterion is checked by the air drag pre-processing tool based on the ambient temperature measured on the vehicle.
the proving ground temperature is in the range as described in 3.2.3
valid average wind speed conditions according to point 3.2.5 item i
valid gust wind speed conditions according to point 3.2.5 item ii
valid average yaw angle conditions according to point 3.2.5 item iii
stability criteria for vehicle speed met:
Low speed test:
where:
=
average of vehicle speed per measurement section [km/h]
=
central moving average of vehicle speed with Xms seconds time base [km/h]
=
time needed to drive 25 m distance at actual vehicle speed [s]
High speed test:
where:
=
average of vehicle speed per measurement section [km/h]
=
1 s central moving average of vehicle speed [km/h]
stability criteria for vehicle torque met:
Low speed test:
where:
=
average of Tsum per measurement section
=
average torque from gradient force
=
average gradient force over measurement section
=
average effective rolling radius over measurement section (formula see item ix.) [m]
=
TL+TR ; sum of corrected torque values left and right wheel [Nm]
=
central moving average of Tsum with Xms seconds time base
=
time needed to drive 25 m distance at actual vehicle speed [s]
High speed test
where:
=
average of Tsum per measurement section [Nm]
=
average torque from gradient force (see Low speed test) [Nm]
=
TL+TR ; sum of corrected torque values left and right wheel [Nm]
=
1 s central moving average of Tsum [Nm]
valid heading of the vehicle passing a measurement section (< 10° deviation from target heading applicable for low speed test, high speed test and misalignment test)
driven distance inside measurement section calculated from the calibrated vehicle speed does not differ from target distance by more than 3 meters (applicable for low speed test and high speed test)
[F1plausibility check for engine speed or cardan speed whichever is applicable passed:
Engine speed check for high speed test:
where:
=
transmission ratio of the gear selected in high speed test [-]
=
axle transmission ratio [-]
=
average vehicle speed (high speed measurement section) [km/h]
=
1 s central moving average of engine speed (high speed measurement section) [rpm]
=
average engine speed (high speed measurement section) [rpm]
=
average effective rolling radius for a single high speed measurement section [m]
=
reference effective rolling radius calculated from all valid high speed measurement sections (number = n) [m]
Engine speed check for low speed test:
where:
=
transmission ratio of the gear selected in low speed test [-]
=
axle transmission ratio [-]
=
average vehicle speed (low speed measurement section) [km/h]
=
central moving average of engine speed with X ms seconds time base (low speed measurement section) [rpm]
=
average engine speed (low speed measurement section) [rpm]
=
time needed to drive 25 metre distance at low speed [s]
=
average effective rolling radius for a single low speed measurement section [m]
=
reference effective rolling radius calculated from all valid measurement sections for low speed test 1 or low speed test 2 (number = n) [m]
The plausibility check for cardan speed is performed in an analogue way with n eng,1s replaced by n card,1s (1 s central moving average of cardan speed in the high speed measurement section) and n eng,float replaced by n card,float (moving average of cardan speed with X ms seconds time base in the low speed measurement section) and i gear set to a value of 1.]
the particular part of the measurement data was not marked as ‘invalid’ in the air drag pre-processing tool input file.
no valid dataset is available from low speed test 1 or/and low speed test 2
less than two valid datasets from the high speed test are available
test track requirements as described in 3.1.1 not met
less than 10 datasets per heading available (high speed test)
less than 5 valid datasets per heading available (misalignment calibration test)
the rolling resistance coefficients (RRC) for the first and the second low speed test differ more than 0,40 kg/t. This criterion is checked for each combination of measurement section and driving direction separately.
the average vehicle speed is inside the criteria as defined in 3.5.2 for the high speed test
valid average wind speed conditions according to point 3.2.5 item i
valid gust wind speed conditions according to point 3.2.5 item ii
valid average yaw angle conditions according to point 3.2.5 item iii
the average vehicle speeds from all valid datasets from each driving directions differ by more than 2 km/h.
less than 5 datasets per heading available
Base value for the declaration of the air drag value is the final result for Cd · Acr (0) as calculated by the air drag pre-processing tool. The applicant for a certificate shall declare a value Cd · Adeclared in a range from equal up to a maximum of + 0,2 m2 higher than Cd · Acr (0). This tolerance shall take into account uncertainties in the selection of the parent vehicles as the worst case for all testable members of the family. The value Cd · Adeclared shall be the input for the simulation tool and the reference value for conformity of the certified CO2 emissions and fuel consumption related properties testing.
[F1Several declared values C d ·A declared can be created based on a single measured C d ·A cr (0) as long as the family provisions in accordance with point 4 of Appendix 5 are fulfilled.]
Communication concerning:
| Administration stamp |
of a certificate on CO2 emission and fuel consumption related properties of an air drag family in accordance with Commission Regulation (EU) 2017/2400.
Commission Regulation (EU) 2017/2400 as last amended by …
Certification number:
Hash:
Reason for extension:
Attachments:
Information package. Test report.
Description sheet No: | Issue: from: Amendment: |
pursuant to …
Air Drag type or family (if applicable):
General remark: For simulation tool input data an electronic file format needs to be defined which can be used for data import to the simulation tool. The simulation tool input data may differ from the data requested in the information document and vice versa (to be defined). A data file is especially necessary wherever large data such as efficiency maps need to be handled (no manual transfer/input necessary). U.K.
…
Parent air drag | Family members | ||||
or air drag type | #1 | #2 | #3 | ||
No: | Description: | Date of issue: |
---|---|---|
1. | Information on test conditions | … |
2. | … |
Vehicle Height Requirements
Vehicle group | Minimum vehicle height [m] | Maximum vehicle height [m] |
---|---|---|
1 | 3,40 | 3,60 |
2 | 3,50 | 3,75 |
3 | 3,70 | 3,90 |
4 | 3,85 | 4,00 |
5 | 3,90 | 4,00 |
[F19 | similar values as for rigid lorry with same maximum gross vehicle weight (group 1, 2, 3 or 4)] | |
10 | 3,90 | 4,00 |
Table 8 | |
Allocation of standard bodies and semitrailer for constant speed testing | |
Vehicle group | Standard body or trailer |
---|---|
1 | B1 |
2 | B2 |
3 | B3 |
4 | B4 |
5 | ST1 |
9 | depending on maximum gross vehicle weight:
|
10 | ST1 |
Table 9 for standard body ‘B1’
Table 10 for standard body ‘B2’
Table 11 for standard body ‘B3’
Table 12 for standard body ‘B4’
Table 13 for standard body ‘B5’
Mass indications as given in Table 9 to Table 13 are not subject to inspection for air drag testing.
Specifications of standard body ‘B1’
Specification | Unit | External dimension(tolerance) | Remarks |
---|---|---|---|
Length | [mm] | 6 200 | |
Width | [mm] | 2 550 (– 10) | |
Height | [mm] | 2 680 (± 10) | box: external height: 2 560 longitudinal beam: 120 |
Corner radius side & roof with front panel | [mm] | 50 - 80 | |
Corner radius side with roof panel | [mm] | 50 - 80 | |
Remaining corners | [mm] | broken with radius ≤ 10 | |
Mass | [kg] | 1 600 | has not be verified during air drag testing |
Specifications of standard body ‘B2’
Specification | Unit | External dimension(tolerance) | Remarks |
---|---|---|---|
Length | [mm] | 7 400 | |
Width | [mm] | 2 550 (– 10) | |
Height | [mm] | 2 760 (± 10) | box: external height: 2 640 longitudinal beam: 120 |
Corner radius side & roof with front panel | [mm] | 50 - 80 | |
Corner radius side with roof panel | [mm] | 50 - 80 | |
Remaining corners | [mm] | broken with radius ≤ 10 | |
Mass | [kg] | 1 900 | has not be verified during air drag testing |
Specifications of standard body ‘B3’
Specification | Unit | External dimension(tolerance) | Remarks |
---|---|---|---|
Length | [mm] | 7 450 | |
Width | [mm] | 2 550 (– 10) | legal limit (96/53/EC), internal ≥ 2 480 |
Height | [mm] | 2 880 (± 10) | box: external height: 2 760 longitudinal beam: 120 |
Corner radius side & roof with front panel | [mm] | 50 - 80 | |
Corner radius side with roof panel | [mm] | 50 - 80 | |
Remaining corners | [mm] | broken with radius ≤ 10 | |
Mass | [kg] | 2 000 | has not be verified during air drag testing |
Specifications of standard body ‘B4’
Specification | Unit | External dimension(tolerance) | Remarks |
---|---|---|---|
Length | [mm] | 7 450 | |
Width | [mm] | 2 550 (– 10) | |
Height | [mm] | 2 980 (± 10) | box: external height: 2 860 longitudinal beam: 120 |
Corner radius side & roof with front panel | [mm] | 50 - 80 | |
Corner radius side with roof panel | [mm] | 50 - 80 | |
Remaining corners | [mm] | broken with radius ≤ 10 | |
Mass | [kg] | 2 100 | has not be verified during air drag testing |
Specifications of standard body ‘B5’
Specification | Unit | External dimension(tolerance) | Remarks |
---|---|---|---|
Length | [mm] | 7 820 | internal ≥ 7 650 |
Width | [mm] | 2 550 (– 10) | legal limit (96/53/EC), internal ≥ 2 460 |
Height | [mm] | 2 980 (± 10) | box: external height: 2 860 longitudinal beam: 120 |
Corner radius side & roof with front panel | [mm] | 50 - 80 | |
Corner radius side with roof panel | [mm] | 50 - 80 | |
Remaining corners | [mm] | broken with radius ≤ 10 | |
Mass | [kg] | 2 200 | has not be verified during air drag testing |
Type and chassis configuration of standard semitrailer ‘ST1’
Type of trailer | 3-axle semi-trailer w/o steering axle(s) |
---|---|
Chassis configuration |
|
[F1Specifications standard semitrailer ‘ ST1 ’]
Specification | Unit | External dimension(tolerance) | Remarks |
---|---|---|---|
Total length | [mm] | 13 685 | |
Total width (Body width) | [mm] | 2 550 (– 10) | |
Body height | [mm] | 2 850 (± 10) | max. full height: 4 000 (96/53/EC) |
Full height, unloaded | [mm] | 4 000 (– 10) | height over the complete length specification for semi-trailer, not relevant for checking of vehicle height during constant speed test |
Trailer coupling height, unloaded | [mm] | 1 150 | specification for semitrailer, not subject to inspection during constant speed test |
Wheelbase | [mm] | 7 700 | |
Axle distance | [mm] | 1 310 | 3-axle assembly, 24t (96/53/EC) |
Front overhang | [mm] | 1 685 | radius: 2 040 (legal limit, 96/53/EC) |
Front wall | flat wall with attachments for compressed air and electricity | ||
Corner front/side panel | [mm] | broken with a strip and edge radii ≤ 5 | secant of a circle with the kingpin as centre and a radius of 2 040 (legal limit, 96/53/EC) |
Remaining corners | [mm] | broken with radius ≤ 10 | |
Toolbox dimension vehicle x-axis | [mm] | 655 | Tolerance: ± 10 % of target value |
Toolbox dimension vehicle y-axis | [mm] | 445 | Tolerance: ± 5 % of target value |
Toolbox dimension vehicle z-axis | [mm] | 495 | Tolerance: ± 5 % of target value |
Side underride protection length | [mm] | 3 045 | 2 stripes at each side, acc. ECE- R 73, Amendment 01 (2010), +/– 100 depending on wheelbase |
Stripe profile | [mm2] | 100 × 30 | ECE- R 73, Amendment 01 (2010) |
Technical gross vehicle weight | [kg] | 39 000 | legal GVWR: 24 000 (96/53/EC) |
Vehicle curb weight | [kg] | 7 500 | has not be verified during air drag testing |
Allowable axle load | [kg] | 24 000 | legal limit (96/53/EC) |
Technical axle load | [kg] | 27 000 | 3 × 9 000 |
An air drag family is characterized by design and performance parameters. These shall be common to all vehicles within the family. The manufacturer may decide which vehicles belong to an air drag family as long as the membership criteria listed in paragraph 4 are respected. The air drag family shall be approved by the approval authority. The manufacturer shall provide to the approval authority the appropriate information relating to the air drag of the members of the air drag family.
In some cases there may be interaction between parameters. This shall be taken into consideration to ensure that only vehicles with similar characteristics are included within the same air drag family. These cases shall be identified by the manufacturer and notified to the approval authority. It shall then be taken into account as a criterion for creating a new air drag family.
In addition to the parameters listed in paragraph 4, the manufacturer may introduce additional criteria allowing the definition of families of more restricted size.
Same cabin width and body in white geometry up to B-pillar and above the heel point excluding the cab bottom (e.g. engine tunnel). All members of the family stay within a range of ± 10 mm to the parent vehicle.
Same roof height in vertical Z. All members of the family stay within a range of ± 10 mm to the parent vehicle.
Same height of cabin over frame. This criterion is fulfilled if the height difference of the cabins over frame stays within Z < 175mm.
The fulfillment of the family concept requirements shall be demonstrated by CAD (computer-aided design) data.
Provisions for transfer of air drag values to other vehicle classes
Vehicle group | Transfer formula | Remarks |
---|---|---|
1 | Vehicle group 2 – 0,2 m2 | Only allowed if value for related family in group 2 was measured |
2 | Vehicle group 3 – 0,2 m2 | Only allowed if value for related family in group 3 was measured |
3 | Vehicle group 4 – 0,2 m2 | |
4 | No transfer allowed | |
5 | No transfer allowed | |
9 | Vehicle group 1,2,3,4 + 0,1 m2 | Applicable group for transfer has to match with gross vehicle weight. Transfer of already transferred values allowed. |
10 | Vehicle group 1,2,3,5 + 0,1 m2 | |
11 | Vehicle group 9 | Transfer of already transferred values allowed |
12 | Vehicle group 10 | Transfer of already transferred values allowed |
[F116 | Vehicle group 9 + 0,3 m 2 | Applicable vehicle group for transfer has to match with gross vehicle weight. Transfer to already transferred values allowed.] |
The ambient temperature of the constant speed test shall be within a range of ± 5 °C to the value from the certification measurement. This criterion is verified based on the average temperature from the first low speed tests as calculated by the air drag pre-processing tool.
The high speed test shall be performed in a vehicle speed range within ± 2 km/h to the value from the certification measurement.
All conformity of the certified CO2 emissions and fuel consumption related properties tests shall be supervised by the approval authority.
[F2For calculation of C d A cr (0) value the air drag pre-processing tool version of the parent air drag in accordance with Attachment 1 of Appendix 2 to this Annex shall be used.]
Table 17 | |
Number of vehicles to be tested for conformity with the certified CO2 emissions and fuel consumption related properties per year of production | |
Number of CoP tested vehicles | Number of CoP relevant vehicles produced the year before |
---|---|
2 | ≤ 25 000 |
3 | ≤ 50 000 |
4 | ≤ 75 000 |
5 | ≤ 100 000 |
6 | 100 001 and more |
For the purpose of establishing the production numbers, only air drag data which fall under the requirements of this Regulation and which did not get standard air drag values according to Appendix 8 of this Annex shall be considered.
Only vehicles from the production line shall be tested.
Only vehicles which fulfil the provisions for constant speed testing as laid down in section 3.3 of the main part of this Annex shall be selected.
Tires are considered part of the measurement equipment and can be selected by the manufacturer.
Vehicles in families where the air drag value has been determined via transfer from other vehicles according to Appendix 5 point 5 are not subject to conformity of the certified CO2 emissions and fuel consumption related properties testing.
Vehicles which use standard values for air drag according to Appendix 8 are not subject to conformity of the certified CO2 emissions and fuel consumption related properties testing.
The first two vehicles per manufacturer to be tested for conformity with the certified CO2 emissions and fuel consumption related properties tested shall be selected from the two biggest families in terms of vehicle production. Additional vehicles shall be selected by the approval authority.
Table 18 | |
Standard values for Cd · Adeclared | |
Vehicle group | Standard valueCd · Adeclared [m2] |
---|---|
1 | 7,1 |
2 | 7,2 |
3 | 7,4 |
4 | 8,4 |
5 | 8,7 |
9 | 8,5 |
10 | 8,8 |
11 | 8,5 |
12 | 8,8 |
16 | 9,0 |
Table 19 | |
Standard delta air drag values for trailer influence | |
Trailer | Standard delta air drag values for trailer influence [m2] |
---|---|
T1 | 1,3 |
T2 | 1,5 |
Table 20 | |
Standard delta Cd Acr (0) values for EMS influence | |
EMS configuration | Standard delta air drag values for EMS influence [m2] |
---|---|
(Class 5 tractor + ST1) + T2 | 1,5 |
(Class 9/11 truck) + dolly + ST 1 | 2,1 |
(Class 10/12 tractor + ST1) + T2 | 1,5 |
In the case of a vehicle being type approved accordant to this Annex, the cabin shall bear:
[F1The manufacturer's name or trade mark]
The make and identifying type indication as recorded in the information referred to in paragraph 0.2 and 0.3 of Appendix 2 to this Annex
The certification mark as a rectangle surrounding the lower-case letter ‘e’ followed by the distinguishing number of the Member State which has granted the certificate:
1 for Germany;
2 for France;
3 for Italy;
4 for the Netherlands;
5 for Sweden;
6 for Belgium;
7 for Hungary;
8 for the Czech Republic;
9 for Spain;
11 for the United Kingdom;
12 for Austria;
13 for Luxembourg;
17 for Finland;
18 for Denmark;
19 for Romania;
20 for Poland;
21 for Portugal;
23 for Greece;
24 for Ireland;
25 for Croatia;
26 for Slovenia;
27 for Slovakia;
29 for Estonia;
32 for Latvia;
34 for Bulgaria;
36 for Lithuania;
49 for Cyprus;
50 for Malta
The certification mark shall also include in the vicinity of the rectangle the ‘base certification number’ as specified for Section 4 of the type-approval number set out in Annex VII to Directive 2007/46/EC, preceded by the two figures indicating the sequence number assigned to the latest technical amendment to this Regulation and by a character ‘P’ indicating that the approval has been granted for an air drag.
For this Regulation, the sequence number shall be 00.
The above certification mark affixed to a cabin shows that the type concerned has been approved in Poland (e20), pursuant to this Regulation. The first two digits (00) are indicating the sequence number assigned to the latest technical amendment to this Regulation. The following letter indicates that the certificate was granted for an air drag (P). The last four digits (0004) are those allocated by the type-approval authority to the engine as the base certification number.
The certification mark shall be affixed to the cabin in such a way as to be indelible and clearly legible. It shall be visible when the cabin is installed on the vehicle and shall be affixed to a part necessary for normal cabin operation and not normally requiring replacement during cabin life. [F1The markings, labels, plates or stickers must be durable for the useful life of the cabin and must be clearly legible and indelible.] The manufacturer shall ensure that the markings, labels, plates or sticker cannot be removed without destroying or defacing them.
eX*YYYY/YYYY*ZZZZ/ZZZZ*P*0000*00
Section 1 | Section 2 | Section 3 | Additional letter to section 3 | Section 4 | Section 5 |
---|---|---|---|---|---|
Indication of country issuing the certificate | HDV CO 2 certification Regulation (2017/2400) | Latest amending Regulation (ZZZZ/ZZZZ) | P = Air drag | Base certification number 0000 | Extension 00] |
This Appendix describes the list of parameters to be provided by the vehicle manufacturer as input to the simulation tool. The applicable XML schema as well as example data are available at the dedicated electronic distribution platform.
The XML is automatically generated by the air drag pre-processing tool.
Unique identifier as used in the simulation tool for a specific input parameter or set of input data
Data type of the parameter
sequence of characters in ISO8859-1 encoding
sequence of characters in ISO8859-1 encoding, no leading/trailing whitespace
date and time in UTC time in the format: YYYY-MM-DD T HH:MM:SS Z with italic letters denoting fixed characters e.g. ‘2002-05-30T09:30:10Z’
value with an integral data type, no leading zeros, e.g. ‘ 1800 ’
fractional number with exactly X digits after the decimal sign ( ‘ . ’ ) and no leading zeros e.g. for ‘ double, 2 ’ : ‘ 2345.67 ’ ; for ‘ double, 4 ’ : ‘ 45.6780 ’
physical unit of the parameter
Input parameters ‘ AirDrag ’
Parameter name | Parameter ID | Type | Unit | Description/Reference |
---|---|---|---|---|
Manufacturer | P240 | token | ||
Model | P241 | token | ||
CertificationNumber | P242 | token | Identifier of the component as used in the certification process | |
Date | P243 | date | Date and time when the component hash is created | |
AppVersion | P244 | token | Number identifying the version of the air drag pre-processing tool | |
CdxA_0 | P245 | double, 2 | [m 2 ] | Final result of the air drag pre-processing tool. |
TransferredCdxA | P246 | double, 2 | [m 2 ] | CdxA_0 transferred to related families in other vehicle groups in accordance with Table 16 of Appendix 5. In case no transfer rule was applied CdxA_0 shall be provided. |
DeclaredCdxA | P146 | double, 2 | [m 2 ] | Declared value for air drag family |
In case standard values in accordance with Appendix 7 shall be used in the simulation tool, no input data for air drag component shall be provided. The standard values are allocated automatically in accordance with the vehicle group scheme.]
This Annex describes the provisions regarding the power consumption of auxiliaries for heavy duty vehicles for the purpose of the determination of vehicle specific CO2 emissions.
[F1The power consumption of the following auxiliaries shall be considered within the simulation tool by using technology specific average standard power values:]
Fan
Steering system
Electric system
Pneumatic system
Air Conditioning (AC) system
Transmission Power Take Off (PTO)
[F1The standard values are integrated in the simulation tool and automatically used by choosing the corresponding technology.]
For the purposes of this Annex the following definitions shall apply:
‘Crankshaft mounted fan’ means a fan installation where the fan is driven in the prolongation of the crankshaft, often by a flange;
‘Belt or transmission driven fan’ means a fan that is installed in a position where additional belt, tension system or transmission is needed;
‘Hydraulic driven fan’ means a fan propelled by hydraulic oil, often installed away from the engine. A hydraulic system with oil system, pump and valves are influencing losses and efficiencies in the system;
‘Electrically driven fan’ means a fan propelled by an electric motor. The efficiency for complete energy conversion, included in/out from battery, is considered;
‘Electronically controlled visco clutch’ means a clutch in which a number of sensor inputs together with SW logic are used to electronically actuate the fluid flow in the visco clutch;
‘Bimetallic controlled visco clutch’ means a clutch in which a bimetallic connection is used to convert a temperature change into mechanical displacement. The mechanical displacement is then working as an actuator for the visco clutch;
‘Discrete step clutch’ means a mechanical device where the grade of actuation can be made in distinct steps only (not continuous variable).
‘On/off clutch’ means a mechanical clutch which is either fully engaged or fully disengaged;
‘Variable displacement pump’ means a device that converts mechanical energy to hydraulic fluid energy. The amount of fluid pumped per revolution of the pump can be varied while the pump is running;
‘Constant displacement pump’ means a device that converts mechanical energy to hydraulic fluid energy. The amount of fluid pumped per revolution of the pump cannot be varied while the pump is running;
‘Electric motor control’ means the use of an electric motor to propel the fan. The electrical machine converts electrical energy into mechanical energy. Power and speed are controlled by conventional technology for electric motors;
‘Fixed displacement pump (default technology)’ means a pump having an internal limitation of the flow rate;
‘Fixed displacement pump with electronic control’ means a pump using an electronic control of the flow rate;
‘Dual displacement pump’ means a pump with two chambers (with the same or different displacement) which can be combined or only one of these is used. It is characterised by an internal limitation of flow rate;
‘Variable displacement pump mech. controlled’ means a pump where the displacement is mechanically controlled internally (internal pressure scales);
‘Variable displacement pump elec. controlled’ means a pump where the displacement is mechanically controlled internally (internal pressure scales). Additionally, the flow rate is elec. controlled by a valve;
[F1‘ Electric steering pump ’ means a hydraulic pump driven by an electric motor;]
‘Baseline air compressor’ means a conventional air compressor without any fuel saving technology;
‘Air compressor with Energy Saving System (ESS)’ means a compressor reducing the power consumption during blow off, e.g. by closing intake side, ESS is controlled by system air pressure;
‘Compressor clutch (visco)’ means a disengageable compressor where the clutch is controlled by the system air pressure (no smart strategy), minor losses during disengaged state caused by visco clutch;
‘Compressor clutch (mechanically)’ means a disengageable compressor where the clutch is controlled by the system air pressure (no smart strategy);
‘Air Management System with optimal regeneration (AMS)’ means an electronic air processing unit that combines an electronically controlled air dryer for optimized air regeneration and an air delivery preferred during overrun conditions (requires a clutch or ESS).
‘Light Emitting Diodes (LED)’ mean semiconductor devices that emit visible light when an electrical current passes through them.
‘Air conditioning system’ means a system consisting of a refrigerant circuit with compressor and heat exchangers to cool down the interior of a truck cab or bus body.
‘Power take-off (PTO)’ means a device on a transmission or an engine to which an auxiliary driven device, e.g., a hydraulic pump, can be connected; a power take-off is usually optional;
‘Power take-off drive mechanism’ means a device in a transmission that allows the installation of a power take-off (PTO);
‘Tooth clutch’ means a (manoeuvrable) clutch where torque is transferred mainly by normal forces between mating teeth. A tooth clutch can either be engaged or disengaged. It is operated in load-free conditions only (e.g. at gear shifts in a manual transmission);
‘Synchroniser’ means a type of tooth clutch where a friction device is used to equalise the speeds of the rotating parts to be engaged;
‘Multi-disc clutch’ means a clutch where several friction linings are arranged in parallel whereby all friction pairs get the same pressing force. Multi-disc clutches are compact and can be engaged and disengaged under load. They may be designed as dry or wet clutches;
‘Sliding wheel’ means a gearwheel used as shift element where the shifting is realized by moving the gearwheel on its shaft into or out of the gear mesh of the mating gear.
For the fan power the standard values shown in Table 1 shall be used depending on mission profile and technology:
Mechanical power demand of the fan
Fan drive cluster | Fan control | Fan power consumption [W] | ||||
---|---|---|---|---|---|---|
Long haul | Regional delivery | Urban delivery | Municipal utility | Construction | ||
Crankshaft mounted | Electronically controlled visco clutch | 618 | 671 | 516 | 566 | 1 037 |
Bimetallic controlled visco clutch | 818 | 871 | 676 | 766 | 1 277 | |
Discrete step clutch | 668 | 721 | 616 | 616 | 1 157 | |
On/off cluch | 718 | 771 | 666 | 666 | 1 237 | |
Belt driven or driven via transmission | Electronic controlled visco clutch | 989 | 1 044 | 833 | 933 | 1 478 |
Bimetallic controlled visco clutch | 1 189 | 1 244 | 993 | 1 133 | 1 718 | |
Discrete step clutch | 1 039 | 1 094 | 983 | 983 | 1 598 | |
On/off cluch | 1 089 | 1 144 | 1 033 | 1 033 | 1 678 | |
Hydraulically driven | Variable displacement pump | 938 | 1 155 | 832 | 917 | 1 872 |
Constant displacement pump | 1 200 | 1 400 | 1 000 | 1 100 | 2 300 | |
Electrically driven | Electronically | 700 | 800 | 600 | 600 | 1 400 |
If a new technology within a fan drive cluster (e.g. crankshaft mounted) cannot be found in the list the highest power values within that cluster shall be taken. If a new technology cannot be found in any cluster the values of the worst technology at all shall be taken (hydraulic driven constant displacement pump)
For the steering pump power the standard values [W] shown in Table 2 shall be used depending on the application in combination with correction factors:
Mechanical power demand of steering pump
Identification of vehicle configuration | Steering power consumption P [W] | ||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Number of axles | Axle configuration | Chassis configuration | Technically permissible maximum laden mass (tons) | Vehicle group | Long haul | Regional delivery | Urban delivery | Municipal utility | Construction | ||||||||||
U+F | B | S | U + F | B | S | U + F | B | S | U + F | B | S | U + F | B | S | |||||
2 | 4 × 2 | Rigid lorry + (Tractor) | > 7,5 - 10 | 1 | 240 | 20 | 20 | 220 | 20 | 30 | |||||||||
Rigid lorry + (Tractor) | > 10 - 12 | 2 | 340 | 30 | 0 | 290 | 30 | 20 | 260 | 20 | 30 | ||||||||
Rigid lorry + (Tractor) | > 12 - 16 | 3 | 310 | 30 | 30 | 280 | 30 | 40 | |||||||||||
Rigid lorry | > 16 | 4 | 510 | 100 | 0 | 490 | 40 | 40 | 430 | 40 | 50 | 430 | 30 | 50 | 580 | 30 | 70 | ||
Tractor | > 16 | 5 | 600 | 120 | 0 | 540 | 90 | 40 | 640 | 50 | 80 | ||||||||
4 × 4 | Rigid lorry | > 7,5 - 16 | 6 | — | |||||||||||||||
Rigid lorry | > 16 | 7 | — | ||||||||||||||||
Tractor | > 16 | 8 | — | ||||||||||||||||
3 | 6 × 2/2 – 4 | Rigid lorry | all | 9 | 600 | 120 | 0 | 490 | 60 | 40 | 440 | 50 | 50 | 430 | 30 | 50 | 640 | 50 | 80 |
Tractor | all | 10 | 450 | 120 | 0 | 440 | 90 | 40 | 640 | 50 | 80 | ||||||||
6 × 4 | Rigid lorry | all | 11 | 600 | 120 | 0 | 490 | 60 | 40 | 430 | 30 | 50 | 640 | 50 | 80 | ||||
Tractor | all | 12 | 450 | 120 | 0 | 440 | 90 | 40 | 640 | 50 | 80 | ||||||||
6 × 6 | Rigid lorry | all | 13 | — | |||||||||||||||
Tractor | all | 14 | |||||||||||||||||
4 | 8 × 2 | Rigid lorry | all | 15 | — | ||||||||||||||
8 × 4 | Rigid lorry | all | 16 | 640 | 50 | 80 | |||||||||||||
8 × 6/8 × 8 | Rigid lorry | all | 17 | — |
where:
=
Unloaded – pumping oil without steering pressure demand
=
Friction – friction in the pump
=
Banking – steer correction due to banking of the road or side wind
=
Steering – steer pump power demand due to cornering and manoeuvring.]
To consider the effect of different technologies, technology depending scaling factors as shown in Table 3 and Table 4 shall be applied.
Scaling factors depending on technology
Factor c1 depending on technology | |||
---|---|---|---|
Technology | c1,U + F | c1,B | c1,S |
Fixed displacement | 1 | 1 | 1 |
Fixed displacement with electronical control | 0,95 | 1 | 1 |
Dual displacement | 0,85 | 0,85 | 0,85 |
Variable displacement, mech. controlled | 0,75 | 0,75 | 0,75 |
Variable displacement, elec. controlled | 0,6 | 0,6 | 0,6 |
Electric | 0 | 1,5/ηalt | 1/ηalt |
with ηalt = alternator efficiency = const. = 0,7
[F1If a new technology is not listed, the technology ‘ fixed displacement ’ shall be considered in the simulation tool.]
Scaling factor depending on number of steered axles
Factor c2 depending on number of steered axles | |||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Number of steered axles | Long haul | Regional delivery | Urban delivery | Municipal utility | Construction | ||||||||||
c2,U+F | c2,B | c2,S | c2,U+F | c2,B | c2,S | c2,U+F | c2,B | c2,S | c2,U+F | c2,B | c2,S | c2,U+F | c2,B | c2,S | |
1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 | 1 |
2 | 1 | 0,7 | 0,7 | 1,0 | 0,7 | 0,7 | 1,0 | 0,7 | 0,7 | 1,0 | 0,7 | 0,7 | 1,0 | 0,7 | 0,7 |
3 | 1 | 0,5 | 0,5 | 1,0 | 0,5 | 0,5 | 1,0 | 0,5 | 0,5 | 1,0 | 0,5 | 0,5 | 1,0 | 0,5 | 0,5 |
4 | 1,0 | 0,5 | 0,5 | 1,0 | 0,5 | 0,5 | 1,0 | 0,5 | 0,5 | 1,0 | 0,5 | 0,5 | 1,0 | 0,5 | 0,5 |
The final power demand is calculated by:
If different technologies are used for multi-steered axles, the mean values of the corresponding factors c1 shall be used.
The final power demand is calculated by:
Ptot = Σi(PU + F * mean(c1,U +F ) * (c2i,U + F)) + Σi(PB * mean(c1,B) * (c2i,B)) + Σi(PS * mean(c1,S) * (c2i,S))
where:
=
Total power demand [W]
=
Power demand [W]
=
Correction factor depending on technology
=
Correction factor depending on number of steered axles
=
Unloaded + friction [-]
=
Banking [-]
=
Steering [-]
=
Number of steered axles [-]
For the electric system power the standard values [W] as shown in Table 5 shall be used depending on the application and technology in combination with the alternator efficiencies:
Electrical power demand of electric system
Technologies influencing electric power consumption | Electric power consumption [W] | ||||
---|---|---|---|---|---|
Long haul | Regional delivery | Urban delivery | Municipal utility | Construction | |
Standard technology electric power [W] | 1 200 | 1 000 | 1 000 | 1 000 | 1 000 |
LED main front headlights | – 50 | – 50 | – 50 | – 50 | – 50 |
To derive the mechanical power, an alternator technology dependent efficiency factor as shown in Table 6 shall be applied.
Alternator efficiency factor
Alternator (power conversion) technologiesGeneric efficiency values for specific technologies | Efficiency ηalt | ||||
---|---|---|---|---|---|
Long haul | Regional delivery | Urban delivery | Municipal utility | Construction | |
Standard alternator | 0,7 | 0,7 | 0,7 | 0,7 | 0,7 |
[F1If the technology used in the vehicle is not listed, the technology ‘ standard alternator ’ shall be considered in the simulation tool.]
The final power demand is calculated by:
where:
=
Total power demand [W]
=
Electrical power demand [W]
=
Alternator efficiency [-]
For pneumatic systems working with over pressure the standard power values [W] as shown in Table 7 shall be used depending on application and technology.
Mechanical power demand of pneumatic systems (over pressure)
Size of air supply | Technology | Long Haul | Regional Delivery | Urban Delivery | Municipal Utility | Construction |
---|---|---|---|---|---|---|
Pmean | Pmean | Pmean | Pmean | Pmean | ||
[W] | [W] | [W] | [W] | [W] | ||
small displ. ≤ 250 cm3 1 cyl./2 cyl. | Baseline | 1 400 | 1 300 | 1 200 | 1 200 | 1 300 |
+ ESS | – 500 | – 500 | – 400 | – 400 | – 500 | |
+ visco clutch | – 600 | – 600 | – 500 | – 500 | – 600 | |
+ mech. clutch | – 800 | – 700 | – 550 | – 550 | – 700 | |
+ AMS | – 400 | – 400 | – 300 | – 300 | – 400 | |
medium 250 cm3 < displ. ≤ 500 cm3 1 cyl./2 cyl. 1-stage | Baseline | 1 600 | 1 400 | 1 350 | 1 350 | 1 500 |
+ ESS | – 600 | – 500 | – 450 | – 450 | – 600 | |
+ visco clutch | – 750 | – 600 | – 550 | – 550 | – 750 | |
+ mech. clutch | – 1 000 | – 850 | – 800 | – 800 | – 900 | |
+ AMS | – 400 | – 200 | – 200 | – 200 | – 400 | |
medium 250 cm3 < displ. ≤ 500 cm3 1 cyl./2 cyl. 2-stage | Baseline | 2 100 | 1 750 | 1 700 | 1 700 | 2 100 |
+ ESS | – 1 000 | – 700 | – 700 | – 700 | – 1 100 | |
+ visco clutch | – 1 100 | – 900 | – 900 | – 900 | – 1 200 | |
+ mech. clutch | – 1 400 | – 1 100 | – 1 100 | – 1 100 | – 1 300 | |
+ AMS | – 400 | – 200 | – 200 | – 200 | – 500 | |
large displ. > 500 cm3 1 cyl./2 cyl. 1-stage/2-stage | Baseline | 4 300 | 3 600 | 3 500 | 3 500 | 4 100 |
+ ESS | – 2 700 | – 2 300 | – 2 300 | – 2 300 | – 2 600 | |
+ visco clutch | – 3 000 | – 2 500 | – 2 500 | – 2 500 | – 2 900 | |
+ mech. clutch | – 3 500 | – 2 800 | – 2 800 | – 2 800 | – 3 200 | |
+ AMS | – 500 | – 300 | – 200 | – 200 | – 500 |
For pneumatic systems working with vacuum (negative pressure) the standard power values [W] as shown in Table 8 shall be used.
Mechanical power demand of pneumatic systems (vacuum pressure)
Long Haul | Regional Delivery | Urban Delivery | Municipal Utility | Construction | |
---|---|---|---|---|---|
Pmean | Pmean | Pmean | Pmean | Pmean | |
[W] | [W] | [W] | [W] | [W] | |
Vacuum pump | 190 | 160 | 130 | 130 | 130 |
Fuel saving technologies can be considered by subtracting the corresponding power demand from the power demand of the baseline compressor.
The following combinations of technologies are not considered:
ESS and clutches
Visco clutch and mechanical clutch
In case of a two-stage compressor, the displacement of the first stage shall be used to describe the size of the air compressor system
For vehicles having an air conditioning system, the standard values [W] as shown in Table 9 shall be used depending on the application.
Mechanical power demand of AC system
Identification of vehicle configuration | AC power consumption [W] | ||||||||
---|---|---|---|---|---|---|---|---|---|
Number of axles | Axle configuration | Chassis configuration | Technically permissible maximum laden mass (tons) | Vehicle group | Long haul | Regional delivery | Urban delivery | Municipal utility | Construction |
2 | 4 × 2 | Rigid lorry + (Tractor) | > 7,5 - 10 | 1 | 150 | 150 | |||
Rigid lorry + (Tractor) | > 10 - 12 | 2 | 200 | 200 | 150 | ||||
Rigid lorry + (Tractor) | > 12 - 16 | 3 | 200 | 150 | |||||
Rigid lorry | > 16 | 4 | 350 | 200 | 150 | 300 | 200 | ||
Tractor | > 16 | 5 | 350 | 200 | 200 | ||||
4 × 4 | Rigid lorry | > 7,5 - 16 | 6 | — | |||||
Rigid lorry | > 16 | 7 | — | ||||||
Tractor | > 16 | 8 | — | ||||||
3 | 6 × 2/2 – 4 | Rigid lorry | all | 9 | 350 | 200 | 150 | 300 | 200 |
Tractor | all | 10 | 350 | 200 | 200 | ||||
6 × 4 | Rigid lorry | all | 11 | 350 | 200 | 300 | 200 | ||
Tractor | all | 12 | 350 | 200 | 200 | ||||
6 × 6 | Rigid lorry | all | 13 | — | |||||
Tractor | all | 14 | |||||||
4 | 8 × 2 | Rigid lorry | all | 15 | — | ||||
8 × 4 | Rigid lorry | all | 16 | 200 | |||||
8 × 6/8 × 8 | Rigid lorry | all | 17 | —] |
For vehicles with PTO and/or PTO drive mechanism installed on the transmission, the power consumption shall be considered by determined standard values. The corresponding standard values represent these power losses in usual drive mode when the PTO is switched off/disengaged. [F1Application related power consumptions at engaged PTO are added by the simulation tool and are not described in the following.]
Mechanical power demand of switched off/disengaged power take-off
Design variants regarding power losses (in comparison to a transmission without PTO and / or PTO drive mechanism) | |||
---|---|---|---|
Additional drag loss relevant parts | PTO incl. drive mechanism | only PTO drive mechanism | |
Shafts / gear wheels | Other elements | Power loss [W] | Power loss [W] |
only one engaged gearwheel positioned above the specified oil level (no additional gearmesh) | — | — | 0 |
only the drive shaft of the PTO | tooth clutch (incl. synchroniser) or sliding gearwheel | 50 | 50 |
only the drive shaft of the PTO | multi-disc clutch | 1 000 | 1 000 |
only the drive shaft of the PTO | multi-disc clutch and oil pump | 2 000 | 2 000 |
drive shaft and/or up to 2 engaged gearwheels | tooth clutch (incl. synchroniser) or sliding gearwheel | 300 | 300 |
drive shaft and/or up to 2 engaged gearwheels | multi-disc clutch | 1 500 | 1 500 |
drive shaft and/or up to 2 engaged gearwheels | multi-disc clutch and oil pump | 3 000 | 3 000 |
drive shaft and/or more than 2 engaged gearwheels | tooth clutch (incl. synchroniser) or sliding gearwheel | 600 | 600 |
drive shaft and/or more than 2 engaged gearwheels | multi-disc clutch | 2 000 | 2 000 |
drive shaft and/or more than 2 engaged gearwheels | multi-disc clutch and oil pump | 4 000 | 4 000 |
This Annex describes the certification provisions for tyre with regard to its rolling resistance coefficient. For the calculation of the vehicle rolling resistance to be used as the simulation tool input, the applicable tyre rolling resistance coefficient Cr for each tyre supplied to the original equipment manufacturers and the related tyre test load FZTYRE shall be declared by the applicant for pneumatic tyre approval.
For the purposes of this Annex, in addition to the definitions contained in UN/ECE Regulation No. 54 and in UN/ECE Regulation No.117, the following definitions shall apply:
‘Rolling resistance coefficient Cr’ means a ratio of the rolling resistance to the load on the tyre
‘The load on the tyre FZTYRE’ means a load applied to the tyre during the rolling resistance test.
‘Type of tyre’ means a range of tyres which do not differ in such characteristics as:
Manufacturer's name;
Brand name or trade mark
Tyre class (in accordance with Regulation (EC) No 661/2009)
Tyre-size designation;
Tyre structure (diagonal (bias-ply), radial);
Category of use (normal tyre, snow tyre, special use tyre) as defined in UN/ECE Regulation No.117;
Speed category (categories);
Load-capacity index (indices);
Trade description/commercial name;
Declared tyre rolling resistance coefficient
The tyre rolling resistance coefficient shall be the value measured and aligned in accordance with Regulation (EC) No 1222/2009, Annex I part A, expressed in N/kN and rounded to the first decimal place, according to ISO 80000-1 Appendix B, section B.3, rule B (example 1).
The tyre manufacturer shall test either in a laboratory of Technical Services as defined in Article 41 of Directive 2007/46/EC which carry out in its own facility the test referred to in paragraph 3.2, or in its own facilities in the case:
of the presence and responsibility of a representative of a Technical Service designated by an approval authority, or
the tyre manufacturer is designated as a technical service of Category A in accordance with Directive 2007/46/EC Art.41.
quick response (QR) code,
barcode,
radio-frequency identification (RFID),
an additional marking, or
other tool fulfilling the requirements of 3.4.1.
CERTIFICATE ON CO 2 EMISSIONS AND FUEL CONSUMPTION RELATED PROPERTIES OF A TYRE FAMILY
of a certificate on CO 2 emission and fuel consumption related properties of a tyre family in accordance with Commission Regulation (EU) 2017/2400, as amended by Commission Regulation (EU) 2019/318
Certification number: …
Hash: …
Reason for extension: …
Manufacturer's name …
Brand name or trade mark
Tyre class (in accordance with Regulation (EC) No 661/2009) …
Tyre-size designation …
Tyre structure (diagonal (bias-ply); radial) …
Category of use (normal tyre, snow tyre, special use tyre) …
Speed category (categories) …
Load-capacity index (indices) …
Trade description/commercial name …
Declared tyre rolling resistance coefficient …
Technology: | Code: |
… | … |
declared rolling resistance level of the tyre (in N/kN rounded to the first decimal place, in accordance with ISO 80000-1 Appendix B, section B.3, rule B ( example 1 ))
Cr , … [N/kN]
tyre test load in accordance with Regulation (EC) No 1222/2009 Annex I part A (85 % of single load, or 85 % of maximum load capacity for single application specified in applicable tyre standards manuals if not marked on tyre.)
F ZTYRE … [N]
Alignment equation: …
Tyre size designation and service description:
Tyre brand/ trade description:
Reference inflation pressure: kPa
Measurement method:
Test speed: km/h
Load FZTYRE : N
Test inflation pressure, initial: kPa
Distance from the tyre axis to the drum outer surface under steady state conditions, rL: m
Test rim width and material:
Ambient temperature: °C
Skim test load (except deceleration method): N
Initial value (or average in the case of more than 1): N/kN
Temperature corrected: … N/kN
Temperature and drum diameter corrected: N/kN
[F1Alignment equation:]
[F2Rolling resistance level of the tyre (in N/kN rounded to the first decimal place, in accordance with ISO80000-1 Appendix B, section B.3, rule B (example 1)) C r,aligned : … [N/kN]]
This Appendix describes the list of parameters to be provided by the component manufacturer as input to the simulation tool. The applicable XML schema as well as example data are available at the dedicated electronic distribution platform.
Unique identifier as used in the simulation tool for a specific input parameter or set of input data]
Data type of the parameter
sequence of characters in ISO8859-1 encoding
sequence of characters in ISO8859-1 encoding, no leading/trailing whitespace
date and time in UTC time in the format: YYYY-MM-DD T HH:MM:SS Z with italic letters denoting fixed characters e.g. ‘2002-05-30T09:30:10Z’
value with an integral data type, no leading zeros, e.g. ‘1800’
fractional number with exactly X digits after the decimal sign (‘.’) and no leading zeros e.g. for ‘double, 2’: ‘2345.67’; for ‘double, 4’: ‘45.6780’
physical unit of the parameter
Input parameters ‘Tyre’
Parameter name | Param ID | Type | Unit | Description/Reference |
---|---|---|---|---|
Manufacturer | P230 | token | ||
Model | P231 | token | Trade name of manufacturer | |
[F1CertificationNumber | P232 | token | ] | |
Date | P233 | date | Date and time when the component hash is created. | |
AppVersion | P234 | token | Version number identifying the evaluation tool | |
RRCDeclared | P046 | double, 4 | [N/N] | |
FzISO | P047 | integer | [N] | |
[F1Dimension | P108 | string | [-] | Allowed values (non-exhaustive): ‘ 9.00 R20 ’ , ‘ 9 R22.5 ’ , ‘ 9.5 R17.5 ’ , ‘ 10 R17.5 ’ , ‘ 10 R22.5 ’ , ‘ 10.00 R20 ’ , ‘ 11 R22.5 ’ , ‘ 11.00 R20 ’ , ‘ 11.00 R22.5 ’ , ‘ 12 R22.5 ’ , ‘ 12.00 R20 ’ , ‘ 12.00 R24 ’ , ‘ 12.5 R20 ’ , ‘ 13 R22.5 ’ , ‘ 14.00 R20 ’ , ‘ 14.5 R20 ’ , ‘ 16.00 R20 ’ , ‘ 205/75 R17.5 ’ , ‘ 215/75 R17.5 ’ , ‘ 225/70 R17.5 ’ , ‘ 225/75 R17.5 ’ , ‘ 235/75 R17.5 ’ , ‘ 245/70 R17.5 ’ , ‘ 245/70 R19.5 ’ , ‘ 255/70 R22.5 ’ , ‘ 265/70 R17.5 ’ , ‘ 265/70 R19.5 ’ , ‘ 275/70 R22.5 ’ , ‘ 275/80 R22.5 ’ , ‘ 285/60 R22.5 ’ , ‘ 285/70 R19.5 ’ , ‘ 295/55 R22.5 ’ , ‘ 295/60 R22.5 ’ , ‘ 295/80 R22.5 ’ , ‘ 305/60 R22.5 ’ , ‘ 305/70 R19.5 ’ , ‘ 305/70 R22.5 ’ , ‘ 305/75 R24.5 ’ , ‘ 315/45 R22.5 ’ , ‘ 315/60 R22.5 ’ , ‘ 315/70 R22.5 ’ , ‘ 315/80 R22.5 ’ , ‘ 325/95 R24 ’ , ‘ 335/80 R20 ’ , ‘ 355/50 R22.5 ’ , ‘ 365/70 R22.5 ’ , ‘ 365/80 R20 ’ , ‘ 365/85 R20 ’ , ‘ 375/45 R22.5 ’ , ‘ 375/50 R22.5 ’ , ‘ 375/90 R22.5 ’ , ‘ 385/55 R22.5 ’ , ‘ 385/65 R22.5 ’ , ‘ 395/85 R20 ’ , ‘ 425/65 R22.5 ’ , ‘ 495/45 R22.5 ’ , ‘ 525/65 R20.5 ’] |
eX*YYYY/YYYY*ZZZZ/ZZZZ*T*0000*00
Section 1 | Section 2 | Section 3 | Additional letter to section 3 | Section 4 | Section 5 |
---|---|---|---|---|---|
Indication of country issuing the certificate | HDV CO 2 certification Regulation (2017/2400) | Latest amending Regulation (ZZZZ/ZZZZ) | T = Tyre | Base certification number 0000 | Extension 00] |
This Annex sets out the requirements for the verification testing procedure which is the test procedure for verifying the CO 2 emissions of new heavy-duty vehicles.
The verification testing procedure consists of an on-road test to verify the CO 2 emissions of new vehicles after production. It shall be carried out by the vehicle manufacturer and verified by the approval authority that granted the licence to operate the simulation tool.
During the verification testing procedure the torque and speed at the driven wheels, the engine speed, the fuel consumption, the engaged gear of the vehicle and the other relevant parameters listed in point 6.1.6 shall be measured. The measured data shall be used as input to the simulation tool, which uses the vehicle-related input data and the input information from the determination of the CO 2 emissions and fuel consumption of the vehicle. For the verification testing procedure simulation, the instantaneously measured wheel torque and the rotational speed of the wheels as well as the engine speed shall be used as input, as described in Figure 1 instead of the vehicle speed, in accordance with point 6.1.6. The fan power during the verification testing procedure shall be calculated in accordance with the measured fan speed. The measured fuel consumption shall be within the tolerances set out in point 7 and compared to the fuel consumption simulated with the verification data set to pass the verification testing procedure.
As part of the verification testing procedure, the correctness of the vehicle input data set from the certification of CO 2 emissions and fuel consumption related properties of the components, separate technical units and systems shall also be reviewed to check the data and the data handling process. The correctness of the input data relating to components, separate technical units and systems relevant for air drag and for rolling resistance of the vehicle shall be verified in accordance with point 6.1.1.
For the purposes of this Annex the following definitions shall apply:
‘verification test relevant data set’ means a set of input data for components, separate technical units and systems and input information used for CO 2 determination of a verification testing procedure relevant vehicle;
‘verification testing procedure relevant vehicle’ means a new vehicle for which a value of CO 2 emissions and fuel consumption was determined and declared in accordance with Article 9;
‘ corrected actual mass of the vehicle ’ means the corrected actual mass of the vehicle in accordance with point 2(4) of Annex III;
‘ actual mass of the vehicle ’ is as defined in Article 2(6) of Regulation (EU) No 1230/2012;
‘ actual mass of the vehicle with payload ’ means the actual mass of the vehicle with the superstructure and with the payload applied in the verification testing procedure;
‘ wheel power ’ means the total power at the driven wheels of a vehicle to overcome all driving resistances at the wheel, computed in the simulation tool from the measured torque and rotational speed of the driven wheels;
‘ control area network signal ’ or ‘ CAN signal ’ means a signal from the connection with the vehicle electronic control unit as referred to in paragraph 2.1.5 of Appendix 1 to Annex II to Regulation (EU) No 582/2011;
‘ urban driving ’ means the total distance driven during the fuel consumption measurement at speeds below 50 km/h;
‘ rural driving ’ means the total distance driven during the fuel consumption measurement at speeds from 50 km/h to 70 km/h;
‘ motorway driving ’ means the total distance driven in the fuel consumption measurement at speeds above 70 km/h;
‘crosstalk’ means the signal at the main output of a sensor (M y ), produced by a measurand (F z ) acting on the sensor, which is different from the measurand assigned to this output; the coordinate system assignment is defined in accordance with ISO 4130.
The number of new vehicles to be tested per year of production ensures that the relevant variations of components, separate technical units or systems used are covered by the verification testing procedure. The vehicle selection for the verification test shall be based on following requirements:
The vehicles for verification test shall be selected out of the vehicles from the production line for which a value of CO 2 emissions and fuel consumption has been determined and declared in accordance with Article 9. The components, separate technical units or systems mounted in or on the vehicle shall be out of series production and shall correspond to those mounted at production date of the vehicle.
The vehicle selection shall be made by the approval authority that granted the licence to operate the simulation tool based on proposals from the vehicle manufacturer.
Only vehicles with one driven axle shall be selected for verification test.
It is recommended to include in each verification test relevant data set engine, axle and transmission with highest sales numbers per manufacturer. The components, separate technical units or systems may be tested all in one vehicle or in different vehicles, under the condition that each component is covered by minimum one verification test on one vehicle.
Vehicles which use standard values for CO 2 certification of their components, separate technical units or systems instead of measured values for the transmission and for the axle losses shall not be selected for the verification test as long as vehicles complying with the requirements in points a) to c) and using measured loss maps for these components, separate technical units or systems in the CO 2 certification, are produced.
The minimum number of different vehicles with different combinations of verification test relevant data sets to be tested by verification test per year shall be based on the sales numbers of the vehicle manufacturer as set out in Table 1:
Table 1 | |
Determination of the minimum number of vehicles to be tested by the vehicle manufacturer | |
Number of vehicles to be tested | Verification testing procedure relevant vehicles produced/year |
---|---|
1 | 1- 25 000 |
2 | 25 001 - 50 000 |
3 | 50 001 - 75 000 |
4 | 75 001 - 100 000 |
5 | more than 100 000 |
The vehicle manufacturer shall finalize the verification test within a period of 10 months after the date of selection of the vehicle for the verification test.
Each vehicle for the verification test shall be in series conditions as typically delivered to the customer. No changes in hardware such as lubricants or in the software such as auxiliary controllers are allowed.
Run in of the vehicle is not mandatory. If the total mileage of the test vehicle is less than 15 000 km, an evolution coefficient for the test result shall be applied as defined in point 7. The total mileage of the test vehicle shall be the odometer reading at start of the fuel consumption measurement. The maximum mileage for the verification testing procedure shall be 20 000 km.
All lubricants shall be in line with the series configuration of the vehicle.
For the fuel consumption measurement as described in point 6.1.5, reference fuel as set out in point 3.2 of Annex V shall be used.
The fuel tank shall be full at start of the fuel consumption measurement run.
All laboratory reference measurement equipment, used for calibration and verification, shall be traceable to national (international) standards. The calibration laboratory shall comply with the requirements of ISO 9000 series and either ISO/TS 16949 or ISO/IEC 17025.
The direct torque at all driven axles shall be measured with one of the following measurement systems fulfilling the requirements listed in Table 2:
hub torque meter;
rim torque meter;
half-shaft torque meter.
The calibrated range shall be at least 10 000 Nm; the measurement range shall cover the entire range of torque occurring during the verification testing procedure of the tested vehicle.
The drift shall be measured during the verification test described in point 6 by zeroing the torque measurement system in accordance with point 6.1.5 after the pre-conditioning phase by lifting the axle and measuring the torque at lifted axle directly after the verification test again.
For a valid test result a maximum drift of the torque measurement system over the verification testing procedure of 150 Nm (sum of both wheels) shall be proven.
The vehicle speed shall be used for possible plausibility checks of the gear signal later on and shall be based on the CAN signal.
The engaged gear does not need to be measured but shall be calculated by the simulation tool based on measured engine speed, the vehicle speed and the tyre dimensions and transmission ratios of the vehicle in accordance with point 7. The gear position may be provided also from the CAN signal to check possible deviations from the gear position calculated by the simulation tool. In case of deviations of the gear position in more than 5 % of the test duration, the reasons for the deviation shall be investigated and reported by the vehicle manufacturer. The input data on gear position shall be used in the simulation tool to compute the gear dependent losses in the gear box. The engine speed shall be taken by the simulation tool from the input data as defined in point 5.4.
The signal from the connection with the vehicle electronic control unit via the open on-board diagnostic interface shall be used to measure the engine speed. Alternative measurement systems are allowed if they fulfil the requirements set out in Table 2.
The measurement system for the rotational speed of left and right wheel at the driven axle for the assessment of the power demand at the wheels as input to the simulation tool for the verification test simulation shall fulfil the requirements set out in Table 2.
The CAN signal for the fan speed may be used, if available. Alternatively an external sensor fulfilling the requirements set out in Table 2 may be used.
The fuel consumed shall be measured on-board with a measurement device reporting the total amount of fuel consumed in kilograms. The fuel measurement system shall be based on one of the following measurement methods:
Measurement of fuel mass. The fuel measuring device shall fulfil the accuracy requirements set out in Table 2 for the fuel mass measurement system.
Measurement of fuel volume together with correction for the thermal expansion of the fuel. The fuel volume measurement device and fuel temperature measurement device shall fulfil the accuracy requirements set out in Table 2 for the fuel volume measurement system. The fuel mass consumed shall be calculated in accordance with the following equations:
where:
=
Calculated fuel mass [kg]
=
Total number of samples in measurement.
=
Density of the fuel used for the verification test in (kg/m 3 ). The density shall be determined in accordance with Annex IX of the Regulation (EU) No 582/2011. If diesel fuel is used in the verification test, also the average value of the density interval for the reference fuels B7 in accordance with Annex IX of the Regulation (EU) No 582/2011 may be used.
=
Fuel temperature that corresponds to density ρ 0 for the reference fuel, as defined in Annex V [°C]
=
Density of the test fuel at sample i [kg/m 3 ]
=
Total fuel volume consumed at sample i [m 3 ]
=
Measured fuel temperature at sample i + 1 [°C]
=
Temperature correction factor (0,001 K – 1 ).
The following masses of the vehicle shall be measured with equipment fulfilling the requirements set out in Table 2:
actual mass of the vehicle;
actual mass of the vehicle with payload.
All data shall be recorded at least in 2 Hz frequency or at recommended frequency from the equipment maker, whichever is the higher value.
The input data for the simulation tool may be composed from different recorders. The following input data shall be provided from measurements:
torque at the driven wheels per wheel;
rotational speed at the driven wheels per wheel;
gear (optional);
engine speed;
fan speed;
vehicle speed;
fuel flow.
The torque and rotational speed at the wheels shall be recorded in one data-logging system. If different data-logging systems are used for the other signals, one common signal, such as vehicle speed, shall be recorded to ensure correct time alignment of the signals.
The accuracy requirements set out in Table 2 shall be met by all measurement equipment used. Any equipment not listed in Table 2 shall fulfil the accuracy requirements set out in Table 2 of Annex V.
Requirements of measurement systems
a Rise time means the difference in time between the 10 percent and 90 percent response of the final analyser reading (t90 – t10). | ||
b The accuracy shall be met for the integral fuel flow over 100 minutes. | ||
Measurement system | Accuracy | Rise time a |
---|---|---|
Balance for vehicle weight | 50 kg or < 0,5 % of max. calibration whichever is smaller | — |
Rotational speed wheels | < 0,5 % of max. calibration | ≤ 1 s |
Fuel mass flow for liquid fuels | < 1,0 % of reading or < 0,5 % of max. calibration whichever is larger | ≤ 2 s |
Fuel volume measurement system b | < 1,0 % of reading or < 0,5 % of max. calibration whichever is larger | ≤ 2 s |
Temperature of the fuel | ± 1 °C | ≤ 2 s |
Sensor for measuring the rotational speed cooling fan | 0,4 % of reading or 0,2 % of max. calibration of speed whichever is larger | ≤ 1 s |
Engine speed | As set out in Annex V | |
Wheel torque | For 10 kNm calibration: < 40 Nm accuracy < 20 Nm crosstalk | < 0,1 s |
The maximum calibration values shall be at least 1,1 times the maximum predicted value expected during all test runs for the respective measurement system. For the torque measurement system the maximum calibration may be limited to 10 kNm.
Accuracy given shall be met by the sum of all single accuracies in the case more than one scale is used.
The vehicle shall be taken from the series production and selected as set out in point 3.
The manufacturer's records file for the vehicle selected shall be used as basis for validating the input data. The vehicle identification number of the vehicle selected shall be the same as the vehicle identification number in the customer information file.
Upon request by the approval authority that granted the licence to operate the simulation tool, the vehicle manufacturer shall provide, within 15 working days, the manufacturer's records file, the input information and input data necessary to run the simulation tool as well as the certificate of CO 2 emissions and fuel consumption related properties for all relevant components, separate technical units or systems.
The following checks shall be performed for the components, separate technical units and systems mounted on the vehicle:
Simulation tool data integrity: the integrity of the cryptographic hash of the manufacturer's records file in accordance with Article 9(3) re-calculated during the verification testing procedure with the hashing tool shall be verified by comparison with the cryptographic hash in the certificate of conformity;
Vehicle data: the vehicle identification number, axle configuration, selected auxiliaries and power take off technology shall match the selected vehicle;
Component, separate technical unit or system data: the certification number and the model type imprinted on the certificate of CO 2 emissions and fuel consumption related properties shall match the component, separate technical unit or system installed in the selected vehicle;
The hash of the simulation tool input data and the input information shall match the hash imprinted on the certificate of CO 2 emissions and fuel consumption related properties for the following components, separate technical units or systems:
engines;
transmissions;
torque converters;
other torque transferring components;
additional driveline components;
axles;
body or trailer air drag;
tyres.
If requested by the approval authority that granted the licence to operate the simulation tool, a verification of the corrected actual mass of the vehicle shall be included into the verification of input data.
For the verification of the mass, the mass in running order of the vehicle shall be verified in accordance with point 2 of Appendix 2 to Annex I to Regulation (EC) No 1230/2012.
In case of discrepancies in the certification number or the cryptographic hash of one or more files regarding the components, separate technical units or systems listed in subpoints (d)(i) to (vii) of point 6.1.1.1 the correct input data file fulfilling the checks in accordance with points 6.1.1.1 and 6.1.1.2 shall replace the incorrect data for all further actions. If no complete input data set with correct certificates of CO 2 emissions and fuel consumption related properties is available for the components, separate technical units or systems listed in subpoints (d)(i) to (vii) of point 6.1.1.1 the verification test shall end and the vehicle fails the verification testing procedure.
After the validation of input data in accordance with point 6.1.1, a run in phase up to maximum 15 000 km odometer reading may take place, with no need to use the reference fuel, if the odometer reading of the vehicle selected is below 15 000 km. In case of damage of any of the components, separate technical units or systems listed in point 6.1.1.1, the component, separate technical units or systems may be replaced by an equivalent component, separate technical units or systems with the same certification number. The replacement shall be documented in the test report.
All relevant components, separate technical units or systems shall be checked before the measurements to exclude unusual conditions, such as incorrect oil fill levels, plugged air filters or on-board diagnostic warnings.
All measurement systems shall be calibrated in accordance with the provisions of the equipment maker. If no provisions exist, the recommendations from the equipment maker shall be followed for calibration.
After the run in phase, the vehicle shall be equipped with the measurement systems set out in point 5.
Tractors of the vehicle groups defined in Table 1 of Annex I shall be tested with any type of semitrailer, providing the loading defined below can be applied.
Rigid lorries of the vehicle groups defined in Table 1 of Annex I shall be tested with trailer, if a trailer connection is mounted. Any body type or other device to carry the loading set out below can be applied.
The bodies of the vehicles may differ from the standard bodies set out in Table 1 of Annex I for the certification of CO 2 emissions and fuel consumption related properties of component, separate technical units or systems.
The vehicle payload shall be at minimum to a mass leading to a total test weight of 90 % of the maximum gross combined weight or gross vehicle weight for rigid lorries without trailer.
The tyre inflation pressure shall be in line with the recommendation of the manufacturer. The tyres of the semitrailer may differ from the standard tyres set out in Table 2 of Part B of Annex II to Regulation (EC) No 661/2009 for the CO 2 certification of tyres.
All settings influencing the auxiliary energy demand shall be set to minimum reasonable energy consumption where applicable. The air conditioning shall be switched off and venting of the cabin shall be set lower than medium mass flow. Additional energy consumers not necessary to run the vehicle shall be switched off. External devices to provide energy on board, such as external batteries, are allowed only for running the extra measurement equipment for the verification testing procedure listed in Table 2 but shall not provide energy to serial vehicle equipment.
A particle filter regeneration may be initiated and shall be achieved before the verification test. If an initiated particle filter regeneration cannot be achieved before the verification test, the test is invalid and shall be repeated.
The route selected for the verification test shall fulfil the requirements set out in Table 3. The routes may include both public and private tracks.
No specific pre-conditioning of the vehicle is required.
Before the fuel consumption measurement starts, the vehicle shall be driven for warm up as set out in Table 3. The warm up phase shall not be considered in the evaluation of the verification test.
Zeroing of the torque measurement equipment shall follow the instruction of the equipment maker. It shall be ensured for zeroing, that the torque on the driven axle is zero. For zeroing, the vehicle shall be stopped directly after the warm up phase and zeroing shall be performed directly after the vehicle stop to minimise cool down effects. Zeroing shall be finished within less than 20 minutes.
The fuel consumption measurement shall start directly after the zeroing of the wheel-torque measurement equipment at vehicle stand still and engine idling. The vehicle shall be driven during the measurement in a driving style avoiding unnecessary braking of the vehicle, gas pedal pumping and aggressive cornering. The setting for the electronic control systems which is activated automatically at vehicle start shall be used, and gear shifts shall be performed by the automated system if applicable. If only manual settings for the electronic control systems are available, the settings leading to higher fuel consumption per kilometre shall be selected. The duration of the fuel consumption measurement shall be within the tolerances set out in Table 3. The fuel consumption measurement shall end also at vehicle stand still in idling condition directly before the measurement of the drift of the torque measurement equipment.
Directly after the fuel consumption measurement, the drift of the torque measurement equipment shall be recorded by measuring the torque at the same vehicle conditions as during the zeroing process. If the fuel consumption measurement does not end at zero vehicle speed, the vehicle shall be stopped for the drift measurement in moderate deceleration.
The boundary conditions to be met for a valid verification test are set in Table 3.
If the vehicle passes the verification test in accordance with point 7, the test shall be set valid even if the following conditions are not met:
undercut of minimum values for parameter No 1, 2, 6, 9 in Table 3,
exceedance of maximum values for parameter No 3, 4, 5, 7, 8, 10, 12 in Table 3.
Parameters for a valid verification test
a Or maximum vehicle speed if lower than 70 km/h | ||||
No | Parameter | Min. | Max. | Applicable for |
---|---|---|---|---|
1 | Warm up [minutes] | 60 | ||
2 | Average velocity at warm up [km/h] | 70 a | 100 | |
3 | Fuel consumption measurement duration [minutes] | 80 | 120 | |
4 | Distance based share urban driving | 2 % | 8 % | vehicle groups 4, 5, 9, 10 |
5 | Distance based share rural driving | 7 % | 13 % | |
6 | Distance based share motorway driving | 74 % | — | vehicle groups 4, 5, 9, 10 |
7 | Time share of idling at stand still | 5 % | ||
8 | Average ambient temperature | 5 °C | 30 °C | |
9 | Road condition dry | 100 % | ||
10 | Road condition snow or ice | 0 % | ||
11 | Seal level of the route [m] | 0 | 800 | |
12 | Duration of continuous idling at stand still [minutes] | 3 |
In case of extraordinary traffic conditions, the verification test shall be repeated.
The data recorded during the verification testing procedure shall be reported to the approval authority that granted the licence to operate the simulation tool as follows:
The data recorded shall be reported in a constant 2 Hz signals as set out in Table 1. The data recorded at higher frequencies than 2 Hz shall be converted into 2 Hz by averaging the time intervals around the 2 Hz nodes. In case of e.g. 10 Hz sampling, the first 2 Hz node is defined by the average from second 0,1 to 0,5, the second node is defined by the average from second 0,6 to 1,0. The time stamp for each node shall be the last time stamp per node, i.e. 0,5, 1,0, 1,5 etc.
The wheel power shall be calculated from the measured wheel torque and rotational wheel speed. All values shall first be converted into 2 Hz signals in accordance with point (a). Then the wheel power for each driven wheel shall be calculated from the 2 Hz torque and speed signals as set out in the following equation:
where:
=
Index standing for left and right wheel of the driven axle
=
power at the left and right driven wheel time node (t) [kW]
=
rotational speed of driven the left and right driven wheel at time node (t) [rpm]
=
measured torque at the left and right driven wheel at time node (t) [Nm]
The wheel power input data for the verification test simulation with the simulation tool shall be the sum of the power of all driven wheels of the vehicle as set out in the following equation:
where:
=
total power at a driven wheel at time node (t) [kW]
=
number of driven wheels
Data reporting format for measured data for the simulation tool in the verification test
Quantity | Unit | Header input data | Comment |
---|---|---|---|
time node | [s] | <t> | |
vehicle speed | [km/h] | <v> | |
engine speed | [rpm] | <n_eng> | |
engine cooling fan speed | [rpm] | <n_fan> | |
torque left wheel | [Nm] | <tq_left> | |
torque right wheel | [Nm] | <tq_right> | |
wheel speed left | [rpm] | <n_wh_left> | |
wheel speed right | [rpm] | <n_wh_right> | |
gear | [-] | <gear> | optional signal for MT and AMT |
fuel flow | [g/h] | <fc> | for standard NCV (point 7.2) |
The simulated fuel consumption shall be compared to the measured fuel consumption using the simulation tool.
The input data and input information for the simulation tool for the verification test shall be the following:
The certified CO 2 emissions and fuel consumption related properties of the following components, separate technical units or systems:
engines;
transmissions;
torque converters;
other torque transferring components;
additional driveline components;
axles.
The input data set out in Table 4.
The power calculated by the simulation tool by the equations of longitudinal dynamics from the measured vehicle speed and road gradient course may be used for plausibility checks to test if the total simulated cycle work is similar to the measured value.
The simulation tool shall calculate the gears engaged during the verification test by calculating the engine speeds per gear at the actual vehicle speed and selecting the gear that provides the engine speed closest to the measured engine speed.
The measured wheel power shall replace in the verification test mode of the simulation tool the simulated power demand at the wheels. The measured engine speed and the gear defined in the verification test input data shall replace the corresponding simulation part. The standard fan power in the simulation tool shall be replaced by the fan power calculated from the measured fan speed in the simulation tool as follows:
where:
=
fan power to be used in the simulation for the verification test [kW]
=
measured rotational speed of the fan [1/s]
=
diameter of the fan [m]
=
generic parameters in the simulation tool:
=
7 320 W
=
1 200 rpm
=
810 mm
The steering pump, compressor and generator shall be attributed standard values in accordance with Annex IX.
All other simulation steps and data handling concerning axle, transmission and engine efficiency shall be identical to the application of the simulation tool to determine and declare the CO 2 emissions and fuel consumption of new vehicles.
The simulated fuel consumption value shall be the total fuel flow over the verification test relevant test distance, from the end of the zeroing after the warm up phase to the end of the test. The total verification test relevant test distance shall be calculated from the vehicle speed signal.
The results from the simulation tool for the verification test shall be calculated as follows:
where:
=
Verification test work calculated by the simulation tool for the complete fuel consumption measurement phase [kWh]
=
Fuel consumption simulated by the simulation tool over the complete fuel consumption measurement phase [g/kWh]
=
Simulation rate [Hz]
=
Instantaneous fuel consumption simulated by the simulation tool over the test [g/s]
The measured fuel flow shall be integrated for the same time span as the simulated fuel consumption. The measured fuel consumption for the total test shall be calculated as follows:
where:
=
Fuel consumption measured by integrating fuel mass flow over the complete fuel consumption measurement phase [g/kWh]
=
Instantaneous fuel mass flow measured during the fuel consumption measurement phase [g/s]
=
Sampling rate [Hz]
=
Verification test work at the wheel calculated from the measured wheel torque and wheel rotational speeds over the complete fuel consumption measurement phase [kWh]
=
Positive power at the left (i = l) and right (i = 2) wheel calculated from the measured wheel torque and wheel rotational speeds at time step t where only power values greater zero are considered
=
instantaneously measured torque at the wheel ‘ i ’ in time step ‘ t ’ [Nm]
=
instantaneously measured rotational speed at the wheel ‘i’ in time step ‘t’ [min – 1 ]
The measured fuel consumption values shall be corrected for the net calorific value (NCV) as set out in point 3 of Annex V to calculate the verification test results.
where:
=
NCV of the fuel used in the verification test determined in accordance with point 3.2 of Annex V [MJ/kg]
=
Standard NCV in accordance with Table 4 of Annex V [MJ/kg]
=
Fuel consumption measured by integrating fuel mass over the complete fuel consumption measurement phase corrected for the test fuel NCV [g/kWh]
The vehicle shall pass the verification test if the ratio of corrected measured fuel consumption to simulated fuel consumption is below the tolerances set out in Table 5.
In the case of a shorter run-in phase than 15 000 km the influence on the fuel efficiency of the vehicle may be corrected with the following evolution coefficient:
where:
=
Fuel consumption measured and corrected of a shorter run-in phase
=
run-in distance [km]
=
Evolution coefficient of 0,98
For vehicle odometer reading above 15 000 km, no correction shall be applied.
The ratio of measured and simulated fuel consumption for the total verification test relevant trip shall be calculated as verification test ratio in accordance with the following equation:
Where:
=
Ratio of fuel consumption measured and simulated in the verification testing procedure
For a comparison with the declared CO 2 emissions of the vehicle in accordance with Article 9, the verified CO 2 emissions of the vehicle are determined as follows:
where:
=
verified CO 2 emissions of the vehicle in [g/t-km]
=
declared CO 2 emissions of the vehicle in [g/t-km]
If a first vehicle fails the tolerances for C VTP , two more tests may be performed on the same vehicle or two more similar vehicles may be tested on request of the vehicle manufacturer. For the evaluation of the pass criterion set out in Table 5, the averages of the verification testing procedure ratio from the up to three tests shall be used. If the pass criterion is not reached, the vehicle fails the verification testing procedure.
Pass fail criterion for the verification test
C VPT | |
---|---|
Pass criterion for the verification testing procedure | < 1,075 |
The test report shall be established by the vehicle manufacturer for each vehicle tested and shall include at least the following results of the verification test:
the row 41A is replaced by the following:
‘41A | Emissions (Euro VI) heavy duty vehicles/access to information | Regulation (EC) No 595/2009 Regulation (EU) No 582/2011 | X (9) | X (9) | X | X (9) | X (9) | X’ |
the following row 41B is inserted:
‘41B | CO2 simulation tool licence (heavy-duty vehicles) | Regulation (EC) 595/2009 Regulation (EU) 2017/2400 | X (16) | X’ |
‘46B | Rolling resistance determination | Regulation (EU) 2017/2400, Annex X’ |
Commission Regulation (EU) No 1230/2012 of 12 December 2012 implementing Regulation (EC) No 661/2009 of the European Parliament and of the Council with regard to type-approval requirements for masses and dimensions of motor vehicles and their trailers and amending Directive 2007/46/EC of the European Parliament and of the Council (OJ L 353, 21.12.2012, p. 31).
Regulation (EC) No 661/2009 of the European Parliament and of the Council of 13 July 2009 concerning type-approval requirements for the general safety of motor vehicles, their trailers and systems, components and separate technical units intended therefor (OJ L 200 31.7.2009, p. 1)
Specify the tolerance; to be within ± 3 % of the values declared by the manufacturer.
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