Purpose
The actuator is intended for driving aircraft landing gear when manoeuvring on the ground without starting engine taxiing thrust.
Technical characteristics:
■ | Nominal power of traction wheel modules | 2х50 kW |
■ | Maximum power of traction wheel modules (short-time) | 2х75 kW |
■ | Maximum torque on the main wheels | 2х4,7 kN•m |
■ | Maximum traction force | 2 kN |
■ | Maximum taxiing speed | 40 km/h |
■ | Maximum starting acceleration | 0.45 m/s2 |
■ | Electric actuator weight | 125 kg |
■ | Traction motor type | converter-fed with permanent magnets |
■ | Nominal rotation speed | 15,000 rpm |
■ | Weight | 30 kg |
■ | Cooling type (antifreeze) | liquid |