The invention discloses a self-locking unmanned aerial vehicle articulated arm. The self-locking unmanned aerial vehicle articulated arm at least comprises a longitudinal middle shaft, a detachable side arm, movable side arms and radial lock bodies, the movable side arms comprise hollow shell-shaped middle shells, external lantern rings, internal mandrels and side arm bodies, the radial lock bodies comprise input assemblies, cone pulley assemblies, worm assemblies, worm gear assemblies and elastic lock cylinders, and the self-locking unmanned aerial vehicle articulated arm further comprises axial lock bodies, telescopic lock heads and adjusting assemblies.

    本申请公开一种自锁式无人机铰接臂,至少包括:纵置中轴、可拆侧臂、活动侧臂、径向锁体。所述铰接侧臂包括空心壳体状的中置壳体,还包括外置套环、内置芯轴、侧臂本体;所述径向锁体包括输入组件、锥轮组件、蜗杆组件、蜗轮组件、弹性锁芯。还包括轴向锁体、伸缩锁头、调节组件。


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    Titel :

    Angle adjusting method of self-locking unmanned aerial vehicle articulated arm


    Weitere Titelangaben:

    一种自锁式无人机铰接臂的角度调节方法


    Erscheinungsdatum :

    08.12.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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