| 摘要 |
A system aircraft braking and taxiing comprising an electric motor (104) coupled to a first transmission (112), a first clutch (106) for selectively engaging the first transmission (112) to a propulsion transmission (108) and a brake clamping system (116), wherein, in response to engagement with the propulsion transmission (108), the electric motor (104) drives an aircraft wheel (114), wherein, in response to engagement with an actuator ram, the electric motor (104) drives the brake clamping system (116) to apply force to an aircraft brake disk stack. |
