A torque link assembly for an aircraft landing gear, comprising: an upper torque link; a lower torque coupling; a knuckle pin arranged to pivotally couple the upper torque link and the lower torque link; an electric motor assembly; a sensor arranged to detect movement of the upper torque link or the lower torque link and to provide a control signal to an electric motor assembly in response to detecting the movement, where the electric motor assembly is configured to linearly translate the knuckle pin relative to one of the upper torque link or the lower torque link.
一种用于飞行器起落架的扭矩联结件组件,包括:上扭矩联结件;下扭矩联结件;关节销,布置成枢转地联接上扭矩联结件和下扭矩联结件;电动马达组件;传感器,布置成检测上扭矩联结件或下扭矩联结件的运动,并且响应于检测到该运动而将控制信号提供给电动马达组件,其中,电动马达组件构造成使关节销相对于上扭矩联结件或下扭矩联结件中的一个线性平移。
Aircraft landing gear torque coupling assembly
Patent
Elektronische Ressource