The invention discloses an unmanned aerial vehicle lock catch assembly, and relates to the technical field of unmanned aerial vehicles, the unmanned aerial vehicle lock catch assembly comprises a pressing buckle assembly, a fixing seat assembly and a folding piece clamping buckle part, the pressing buckle assembly comprises a clamping hook rotating shaft, a clamping hook, a clamping hook spring and a pressing buckle; the two ends of the pressing buckle are provided with an end buckling part and a side stirring part respectively, the pressing buckle is provided with a hinge hole, and the upper end of the pressing buckle is provided with mounting holes used for containing the clamping hook and the clamping hook spring. The clamping hook is hinged in the mounting hole through a clamping hook rotating shaft, and the clamping hook and the end buckling part are distributed at the two ends of the mounting hole; a fixing seat buckling part and a hinging end are arranged on the fixing seat assembly; the middle of the pressing buckle is installed at the hinged end, the clamping hook is buckled to the fixing base buckling part, and the end buckling part is buckled to the folding piece buckling part. The clamping hook and the end part clamping part are fixed and matched in a double-buckling manner, so that the reliability of the buckling structure of the lock catch assembly is ensured; the locking mode of the unmanned aerial vehicle locking assembly is quick and convenient to operate, and the problems that the folding mode is tedious and the unfolding and folding efficiency is low are solved.

    本发明公开了一种无人机锁扣组件,涉及无人机技术领域,包括压扣组件、固定座组件、折叠件卡扣部,压扣组件包括卡钩转轴、卡钩、卡钩弹簧、压扣;压扣的两端分别设置有端部卡扣部、侧部拨动部,压扣设置有铰接孔,压扣的上端设有用于放置卡钩、卡钩弹簧的安装孔;卡钩通过卡钩转轴铰接于安装孔内,卡钩、端部卡扣部分布于安装孔的两端;固定座组件上设置有固定座卡扣部、铰接端;压扣的中部安装于铰接端,卡钩卡扣于固定座卡扣部,端部卡扣部卡扣于折叠件卡扣部。采用卡钩、端部卡扣部进行双重卡扣形式固定配合,保证锁扣组件扣合结构的可靠性;无人机锁扣组件锁扣形式操作快捷方便,解决了折叠方式繁琐、展开折叠效率低的问题。


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    Titel :

    Unmanned aerial vehicle lock catch assembly


    Weitere Titelangaben:

    无人机锁扣组件


    Beteiligte:
    DING YONGXIANG (Autor:in) / CHEN WAN (Autor:in) / WEN SHUSHENG (Autor:in) / LI NING (Autor:in) / TANG CHAOFENG (Autor:in) / LIU SHAOYI (Autor:in) / WANG JIANGLIN (Autor:in) / MA RAN (Autor:in) / YAN SHAOXIA (Autor:in) / ZHUANG SUOZENG (Autor:in)

    Erscheinungsdatum :

    2022-03-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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