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 |