The invention belongs to the technical field of unmanned aerial vehicle grabbing operation, and provides a grabbing operation system for an unmanned aerial vehicle platform, which comprises a connecting piece, a base, a plurality of elastic sheets, a plurality of elastic plates, a rope, a winding wheel and a control assembly, the upper ends of the elastic sheets are uniformly connected to the lower end of the base at intervals in the circumferential direction, and the elastic plates are connected among the elastic sheets; fixing blocks are connected to the edges of the lower ends of the elastic pieces, each fixing block is provided with a first through hole, one fixing block is provided with a second through hole, the second through hole is communicated with the first through hole in the fixing block, and a rope sequentially penetrates through the first through holes, surrounds the elastic pieces arranged in the circumferential direction in an array mode, penetrates through the second through holes and is tied to the winding wheel. The wire winding wheel is arranged on the base, and a control assembly is further arranged on the base and used for controlling forward rotation and reverse rotation of the wire winding wheel. The device has the advantages that the thin shell structure of the elastic sheet and the elastic plate is adopted, the rope is used for driving, and the device is light in self weight and large in loading capacity.

    本发明属于无人机抓持作业技术领域,提供了一种用于无人飞行平台的抓持作业系统,包括:连接件、底座、若干弹性片、若干弹性板、绳索、缠线轮、控制组件,弹性片的上端沿周向间隔均布地连接在底座的下端,弹性片间连接弹性板,弹性片下端边缘位置连接有固定块,每个固定块上均设有第一通孔,其中一个固定块上设有第二通孔,第二通孔与该固定块上的第一通孔相连通,绳索依次穿过第一通孔环绕周向阵列的若干弹性片,并穿过第二通孔系在缠线轮上,缠线轮设置在底座上,底座上还设置有控制组件,控制组件用于控制所述缠线轮的正转和反转。本发明的优点在于:采用弹性片和弹性板的薄壳结构,并利用绳索进行驱动,具有自重轻、负载力大的优点。


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    Title :

    Grabbing operation system for unmanned flying platform


    Additional title:

    一种用于无人飞行平台的抓持作业系统


    Contributors:
    LI HAILI (author) / LIANG LIN (author) / MIAO XINYU (author) / WANG BO (author) / ZHAO QIANCHEN (author) / ZHENG WEI (author) / CHEN QIANG (author) / SHEN XIAOWEI (author) / YU HONGFAN (author)

    Publication date :

    2023-06-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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