A landing gear system includes an axle having an inner cavity and a wheel rotatably coupled with the axle. A drive shaft is mounted in the cavity to be rotatable about an axis. The landing gear system also includes a lever slidably mounted within the drive shaft and a clutch. The clutch has a first portion coupled to the rod and rotating with the drive shaft. A second portion of the clutch is fixedly coupled to the wheel. The lever selectively reciprocates along the axis between a first position and a second position to engage and disengage the clutch.

    一种起落架系统,包括具有内腔的轮轴和与轮轴可旋转地联接的轮。驱动轴安装在该腔中以围绕轴线可旋转。起落架系统还包括杆和离合器,该杆可滑动地安装在该驱动轴内。离合器具有第一部分,该第一部分联接到杆并且与驱动轴一起旋转。离合器的第二部分固定地联接到轮。杆沿着轴线在第一位置和第二位置之间选择性地往复运动,以接合和分离离合器。


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    Title :

    Clutch assembly for autonomous taxiing of aircraft


    Additional title:

    用于飞行器自主滑行的离合器组件


    Contributors:

    Publication date :

    2022-11-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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