The invention discloses a self-locking type unmanned aerial vehicle hinged arm which at least comprises a longitudinal middle shaft, a detachable side arm, movable side arms and a radial lock body. Each hinged side arm comprises a hollow shell-shaped middle shell, and further comprises an external lantern ring, an internal mandrel and a side arm body. The radial lock body comprises an input assembly, a cone pulley assembly, a worm assembly, a worm gear assembly and an elastic lock cylinder. The self-locking type unmanned aerial vehicle hinged arm further comprises an axial lock body, a telescopic lock head and an adjusting assembly.

    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 :

    Pre-adjusting method of self-locking type unmanned aerial vehicle hinged arm


    Weitere Titelangaben:

    一种自锁式无人机铰接臂的预调节方法


    Erscheinungsdatum :

    08.12.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




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