🇬🇧 United Kingdom

8501538110

Of an output not exceeding 150 kW, for use in civil aircraft

Details

Parent HS6
850153 Electric motors; AC motors, multi-phase, of an output exceeding 75kW

Related United Kingdom Codes

8501535010 Electric drive for motor vehicles, with an output of not more than 315 kW: - with an AC or DC motor with or without transmission, - with or without power electronics
8501535020 AC traction motor of the Interior Permanent Magnet Synchronous Motor (IPMSM) type with:<br> <br>-a torque output of 200 Nm or more, but not more than 400 Nm,<br> <br>-a power output of 50 kW or more, but not more than 200 kW ,<br> <br>-a rotation speed of no more than 15 000 rpm,<br>for use in the manufacture of electric vehicles
8501535030 Permanent magnet synchronous traction motor, with: -a continuous power of 110 kW or more but not more than 180 kW, -a liquid cooled system, -a total length of 500 mm or more but not more than 650 mm, -a total width of 600 mm or more but not more than 700 mm, -a total height of 550 mm or more but not more than 650 mm, -weighing of not more than 350 kg, -3 suspension points
8501535040 Permanent magnet traction AC motor, with: -a continuous power of 110 kW or more but not more than 150 kW, -a liquid cooled system, -a total length of 460 mm or more but not more than 590 mm, -a total width of 450 mm or more but not more than 580 mm, -a total height of 490 mm or more but not more than 590 mm, -a weight of not more than 310 kg, -4 mounting points
8501535050 Asynchronous traction motor, with: -a continuous power of 140 kW or more but not more than 180 kW, -a liquid cooled system, -a total length of 580 mm or more but not more than 730 mm, -a total width of 550 mm or more but not more than 670 mm, -a total height of 510 mm or more but not more than 630 mm, -with a weight of not more than 390 kg, -with or without reduction gear, -with or without starter generator, -2 mounting points, for use in the manufacture of the electric drive of hybrid buses
8501535090 Other
8501538110 Of an output not exceeding 150 kW, for use in civil aircraft
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