IL1401 | Reciprocating diesel engine development and production technologies, including specially designed software, the following— | |
| aDevelopment and production technology, including specially dsigned software, for reciprocating diesel engine ground vehicle propulsion systems having all of the following characteristics—
| D |
| 1a box volume of 1.2m3 or less; 2an overall power output of more than 750 kW based on 80/1269/EEC, ISO 2534 or national equivalents; 3a power density of more than 700 kW/m3 of box volume.
| |
| bDevelopment and production technology for solid or dry film cylinder wall lubrication permitting operation at temperatures in excess of 723 K (450°C) measured on the cylinder wall at the top limit of travel of the top ring of the piston
| D |
| In this entry the “box volume” means the product of three dimensions at right angles to each other measured in the following way— Length: the length of the crankshaft from front flange to flywheel face; Width: the greatest of the following: - a
the outside dimension from valve cover to valve cover; - b
the dimension of the outside edges of the cylinder heads; or - c
the diameter of the flywheel housing;
Height: the greater of the following: - a
the dimension of the crankshaft centreline to the top plane of the valve cover (or cylinder head) plus 2 times the stroke; or - b
the diameter of the flywheel housing.
| |
IL1416 | Vessels (including ships and surface-effect vehicles), water-screw propellers and hub assemblies, water-screw propeller systems, moisture and particulate separator systems and specially designed components, the following— | |
| aHydrofoil vessels with automatically controlled foil systems which are capable of speeds of above 40 knots in rough water (Sea State Five)
| S, I |
| bSurface-effect vehicles, namely hovercraft, air cushion vehicles (both sidewall and skirted varieties) and all variations of vehicles using the wing-in-ground effect for positive lift
| C |
| cSmall waterplane area twin-hull (SWATH) vessels having underwater hulls whose cross-sectional area varies along the longitudinal axis between points two major diameters from the bow and two major diameters from the stern
| C |
| dShips and vessels fitted with any of the following—
| |
| 1equipment specified in Group 1, in entry IL1485 in this Group or in entry IL1501, IL1502 or IL1510 in Group 3F
| S, I |
| | S, I |
| | |
| 3closed ventilation systems designed into the vessel which are designed to maintain air purity and positive pressure regardless of the conditions external to the vessel except where those closed ventilation systems are specially designed for and incorporated in the vessel’s medical facilities only
| C |
| eWater-screw propellers and hub assemblies, the following—
| |
| 1supercavitating propellers rated at greater than 10,000 hp
| C |
| 2controllable-pitch propellers and hub assemblies rated at above 40,000 hp capacity
| C |
| fWater-screw propeller systems, the following—
| |
| 1contrarotating propeller systems rated at greater than 20,000 hp
| C |
| 2ventilated, base-ventilated and super-ventilated propeller systems
| C |
| 3systems employing pre-swirl and post-swirl techniques for smoothing the flow into a propeller so as to improve propulsive efficiency of—
| C |
| iSWATH vessels, hydrofoil vessels, and surface-effect vehicles, or
| C |
| iiother vessels whose propeller rotation speed is above 200 rpm, or having propellers with a rating exceeding 50,000 hp per shaft
| C |
| gMoisture and particulate separator systems which are capable of removing 99.9 per cent of particles larger than 2 micrometers in diameter with a maximum pressure loss of 1.6 kPa (16 millibar) for gas turbine engine air inlets
| C |
| ggTechnology for moisture and particulate separator systems specified in head (g) above only the following—
| |
| 1technology for preventing water leakage around the filter stages
| D |
| 2technology for integrating the components of such a system
| D |
| hSpecially designed components for vessels covered by heads (a), (b) and (c) above, the following—
| |
| 1advanced hull forms which incorporate any of the following—
| |
| istepped hull for hydrofoil vessels
| C |
| iihulls for air cushion vehicles with trapezoidal platforms
| C |
| iiihulls for surface-effect vehicles with catamaran-like sidewalls
| C |
| ivhulls for wing-in-ground effect vehicles
| C |
| vunderwater hulls and struts for SWATH vessels
| C |
| 2fully submerged subcavitating or supercavitating hydrofoils
| C |
| 3lightweight structural components for SWATH vessels, hydrofoil vessels and surface-effect vehicles, constructed using anisotropic, orthotropic or sandwich construction methods
| C |
| In this subhead— - 1.
“Anisotropic construction methods” means the use of fibre reinforcing members aligned so that the load-carrying ability of the structure can be primarily orientated in the direction of expected stress. - 2.
“Orthotropic construction methods” means the means of stiffening plates, in which the structural members are at right angles to each other. - 3.
“Sandwich construction methods” means the use of structural members or plates which are fabricated and permanently affixed in layers to enhance their strength and reduce their weight.
| |
| 4flexible skirts, seals and fingers for surface-effect vehicles
| C |
| 5systems for automatically controlling the stability of SWATH vessels, hydrofoil vessels or surface-effect vehicles
| C |
| 6power transmission shaft systems which incorporate composite material components, for SWATH vessels, hydrofoil vessels or surface-effect vehicles
| C |
| 7lightweight, high capacity (K factor greater than 150) gearing (planetary, cross-connect and multiple input/output gears and bearings) for SWATH vessels, hydrofoil vessels and surface-effect vehicles
| C |
| 8water-cooled electrical propulsion machinery (motor and generator), including AC-AC synchronous and AC-DC systems, sectored-disc and concentric-drum rotors for DC homopolar machines, for SWATH vessels, hydrofoil vessels and surace-effect vehicles
| C |
| 9superconducting electrical propulsion machinery for SWATH vessels, hydrofoil vessels and surface-effect vehicles
| C |
| 10lift fans for surface-effect vehicles, rated at greater than 400 hp
| C |
| 11waterjet propulsor systems rated at 3,000 input hp or greater for hydrofoil vessels and surface-effect vehicles
| C |
PL7009 | Other vessels (including ships), the following: and specially designed components therefor— | |
| aVessels having special structural features for landing personnel and/or vehicles on a beach
| I |
| bVessels capable of supporting helicopter operations and maintenance
| I |
| cVessels capable of submerging
| I |
| dVessels not elsewhere specified in this Part of this Schedule of below 100 tonnes GRT including inflatable craft in an inflated or uninflated state except light vessels, fire floats and dredgers
| I |
| eShips with decks and platforms specially strengthened to receive weapons
| S, L, I |
IL1417 | Submersible systems including those incorporated in a submersible vehicle, the following: and specially designed components therefor— | |
| aAutomatically-controlled atmosphere-regeneration systems specially designed or modified for submersible vehicles which, in a single chemical-reaction cycle, ensure carbon dioxide removal and oxygen renewal
| C |
| bSystems specially designed or modified for the automated control of the motion of a submersible vehicle using navigation data and having closed-loop servo-control(s) so as to–
| |
| 1enable the vehicle to move within ten metres of a predetermined point in the water column
| C |
| 2maintain the position of the vehicle within ten metres of a predetermined point in the water column
| C |
| | |
| 3maintain the position of the vehicle within ten metres while following a cable on or under the sea bed
| C |
| | |
| cUnderwater vision systems, the following—
| |
| 1television systems (comprising camera, lights, monitor and signal transmission equipment) specially designed or modified for remote operation with a submersible vehicle, having a limiting resolution, when measured in the air, more than 500 lines, using IEEE Standard 208/1960 or any equivalent standard
| C |
| 2systems specially designed or modified for remote operation with a submersible vehicle employing techniques to minimize the effects of back-scatter, such as range-gated illuminators
| C |
| except television cameras used merely through a porthole. | |
| dRemotely controlled articulated manipulators specially designed or modified for use with submersible vehicles and having any of the following characteristics—
| |
| 1systems which control the manipulator using information from sensors which measure force or torque applied to an external object, distance from an external object, or tactile sense between the manipulator and an external object
| C |
| except systems where force or torque are only measured and then displayed to the operator. | |
| 2controlled by proportional master-slave techniques or by using a dedicated stored-programme computer
| C |
| | |
| 3capable of exerting a force of 250 Newtons or more or a torque of 250 Newton-metres or more and using titanium based alloys or fibrous and filamentary composite materials in their structural members
| C |
| ePhotographic cameras and associated equipment specially designed or modified for use underwater, having a film format of 35 mm or larger, and capable of any of the following—
| |
| 1film advancement of more than 5 frames per second
| C |
| 2annotating the film with data provided by a source external to the camera
| C |
| 3taking more than 250 full frame exposures without changing the film
| C |
| 4autofocusing specially designed or modified for use underwater
| C |
| | |
| 5operating at depths of more than 1,000 metres
| C |
| fLight systems specially designed or modified for use under water, the following— 1stroboscopic lights capable of—
| |
| ilight output energy of more than 150 joules per flash
| C |
| | |
| iiflash rates of more than 5 flashes per second at a light output energy of more than 10 joules per flash
| C |
| 2other lights and associated equipment, capable of operating at depths of more than 1,000 metres
| C |
| In this entry “limiting resolution” in television is a measure of resolution usually expressed in terms of the maximum number of lines per picture height discriminated on a test chart. | |
IL1418 | Deep submergence vehicles, manned or unmanned, tethered or untethered, capable of operating at depths exceeding 1,000 metres, and specially designed or modified associated systems, equipment, components and materials therefor, including the following— | C |
| apressure housings or pressure hulls; bpropulsion motors and thrusters; chull penetrators or connectors.
| |
IL1425 | Floating docks, and software and technology therefor, the following— - a
Floating docks specially designed for use at remote locations (i.e. without support from shore bases) incorporating all of the following facilities— - 1
welding and pipe fitting repair shop(s); - 2
electrical and electronic repair shop(s); - 3
mechanical repair or metal working machine shop(s)
| |
| | C |
| bFloating docks specially equipped to permit the operation, maintenance or repair of nuclear reactors
| C |
| cFloating docks having both the following characteristics— 1a lifting capacity of more than 36,364 tonnes; 2larger than 120 metres in length and 30 metres in width, measured between the pontoons.
| |
| dSpecially designed software for computer-controlled pumping and flooding systems for the above floating docks, to permit the docking of listing vessels
| C |
| eTechnology, the following—
| |
| 1for that portion of the design of a floating dock specified in head (a) above which relates to the incorporation of the three types of facilities specified in that head
| D |
| 2for design, production and use of onboard floating dock facilities specified in head (b) above which permit the operation, maintenance and repair of nuclear reactors
| D |
IL1431 | Marine gas turbine engines (marine propulsion or shipboard power generation engines), whether originally designed as such or adapted for such use, and specially designed components therefor | C |
| Note: for the purpose of this entry “shipboard power generation” does not include offshore platform applications. | |
IL1460 | Aircraft and helicopters, aero-engines and aircraft and helicopter equipment, and technology therefor, the following— | |
| aAircraft and helicopters, except those which do not contain equipment specified in Group 1 or in the entries IL1485 or IL1501 in Groups 3E and 3F and which are of types which are in bona fide normal civil use
| C |
| bTechnology for aircraft and helicopter airframes, for aircraft propellers, and for aircraft and helicopter airframe, aircraft-propeller and helicopter-rotor-systems components, and specially designed ODMA software therefor, the following—
| |
| 1design technology using computer-aided aerodynamic analyses for integration of the fuselage, propulsion system and lifting and control surfaces to optimize aerodynamic performance throughout the flight regime of an aircraft
| D |
| 2technology for the design of active flight control, the following—
| |
| itechnology for configuration design for inter-connecting multiple microelectronic processing elements (on-board computers) to achieve high-speed data transfer and high-speed data integration for control law implementation
| D |
| iitechnology for control law compensation for sensor location and dynamic airframe loads, namely compensation for sensor vibration environment and for variation of sensor location from centre of gravity
| D |
| iiitechnology for electronic management of systems reducdancy and data redundancy for fault detection, fault tolerance and fault isolation
| D |
| | |
| ivtechnology for design of flight controls which permit in-flight reconfiguration of force and moment controls
| D |
| 3design technology for integration of flight control, navigation and propulsion control data into a flight management system for flight path optimzation
| D |
| 4design technology for protection of avionic and electrical sub-systems against electromagnetic pulse (EMP) and electromagnetic interference (EMI) hazards from sources external to the aircraft, the following—
| |
| itechnology for design of shielding systems
| D |
| iitechnology for the configuration design of hardened electrical circuits and sub-systems
| D |
| iiitechnology for determination of hardening criteria for the above
| D |
| 5technology for the design, production and reconstruction of adhesively bonded airframe structural members designed to withstand operational temperatures in excess of 120°C
| D |
| | |
| 6technology for the design and production of propeller blades constructed wholly or partly of composite materials, and specially designed hubs therefor
| D |
| | |
| 7technology for the design and production of digital electronic synchrophasers specially designed for propellers; technology for the design of digital electronic controls for propellers; and technology for the production of digital electronic controls for the propeller blades and hubs described in sub-head (b)(6) above
| D |
| 8technology for the design and production of active laminar flow control lifting surfaces including design data used to substantiate the design approach
| D |
| 9technology for the development of helicopter multi-axis fly-by-light or fly-by-wire controllers which combine the functions of at least two of the following into one controlling element
| D |
| | |
| 10technology for the development of circulation controlled anti-torque or directional control systems for helicopters
| D |
| | |
| 11technology for the development of helicopter rotor blades incorporating variable geometry airfoils utilizing trailer edge flaps or tabs or pivotted nose droop, which can be controlled in position in flight
| D |
| 12technology for the development of active control of helicopter blades and other surfaces used to generate aerodynamic forces and moments
| D |
| Note: “Active control” (of helicopter blades and other surfaces used to generate aerodynamic forces and moments) functions to prevent undesirable helicopter vibrations, structural loads or helicopter rotor dynamic behaviour by autonomously processing outputs from multiple sensors and then providing necessary preventive commands to effect automatic control.
| |
| cHelicopter power transfer systems and technology therefor
| C |
| except— - i
helicopter power transfer systems for use in civil helicopters only, the following— - 1
those which have been in civil use in civil helicopters for more than eight years; - 2
those which do not contain, and were not fabricated utilizing, any of the technologies shown in Table 2 below; - 3
those for replacement in or servicing of specific, previously exported helicopters;
- ii
technological documents resulting from helicopter power transfer system performace and installation design studies; fabrication technology, or overhaul and refurbishing technology for specific helicopter power transfer systems in civil use in civil helicopters for more than eight years unless listed in Table 2 below.
Note: Documents resulting from helicopter power transfer system performance and installation design studies do not include documents containing technology for: computer-aided design (CAD); computer-aided design/manufacture (CAD/CAM); or parametric performance analysis, engine analysis and selection, or component design utilizing unpublished technical data.
| |
| dGas turbine engines and auxiliary power units (APUs) for use in aircraft or helicopters and technology therefor—
| C |
| except - i
those for use in civil aircraft or civil helicopters only, the following— - 1
jet, turboprop and turboshaft aircraft engines in civil use in civil aircraft or civil helcopters for more than eight years; - 2
gas turbine powered aircraft APUs in civil use in bona fide civil aircraft or civil helicopters for more than eight years;
- ii
technological documents resulting from aircraft performance and installation design studies; fabrication technology, or overhaul and refurbishing technology for specific gas turbine aero-engines or gas turbine powered aircraft APUs in civil use in civil aircraft or civil helicopters for more than twelve years, unless listed in Table 1 below.
Note: Aircraft performance and installation design studies does not include technology for: computer-aided design (CAD); computer-aided design/manufacturing (CAD/CAM); or parametric engine performance analysis, engine cycle analysis and selection, or component aerodynamic design utilizing unpublished technical data.
| |
| eSpecially designed components for gas turbine engines, APUs and helicopter power transfer systems specified in heads (c) and (d) above, the following—
| |
| 1embodying technologies listed in Tables 1 or 2 below
| C |
| | C |
| 3engine control system components
| C |
| 4gas turbine engine or APU rotor system components (including bearings)
| C |
| Notes: 1The period of civil use referred to in heads (c) and (d) above begins with the date that the particular engine or helicopter power transfer system (model and specifications) or its most recent modification was certified as airworthy for commercial service or commercial navigability under the standards and requirements of the government of the country in which it was manufactured: modification does not include minor safety or operational changes which do not significantly enhance the performance of a particular gas turbine aero-engine or improve its reliability. For the purposes of this entry: aA gas turbine aero-engine which is recertified as the result of incorporating any technology listed in Table 1 below is to be treated as a newly certified engine. Recertification which does not result from incorporation of such technology, or modifications which do not require recertification by national authorities, will not affect the period of civil use of the engine; bModification of a gas turbine APU by incorporation of any technology listed in Table 1 will cause it to be treated as a new APU. Other modifications will not affect the period of civil use of the APU. cModification of a helicopter power transfer system by incorporation of any technology listed in Table 2 will restart the period of civil use for the helicopter power transfer system as though it were newly certified in a helicopter. Other modifications will not affect the period of civil use of the helicopter power transfer system. 2This entry does not include gas turbine engines, APUs and helicopter power transfer systems for civil use and modifications (and technology therefore) certified or re-certified for civil use, as described in Note 1 prior to the 1st January 1979, other than: Helicopters over 4,530 kg empty weight, and power transmissions systems therefor. Note: Empty weight is understood to include normal installation and normal minimum crew, but does not include fuel or payload. Aero-engines, the following— - i
Piston engines; - ii
Jet engines of less than 2,625 kg thrust; - iii
Turboprop or turboshaft engines of less than 2,500 horsepower or with a residual thrust of less than 453 kg.
3Head (d) above does not include those engines which contain none of the technologies listed in Table 1 below for use in civil aircraft or civil helicopters.
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