The invention provides a double-tail-boom tail folding mechanism of an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle double-tail-boom tail folding mechanism comprises a double-tail-boom vehicle body, a tail wheel, a balance wing plate, two tail wheel tail booms and two tail wheel vertical booms capable of being telescopically locked. One end of the tail wheel tail boom is pivoted on the double-tail boom machine body, and the tail wheel is arranged at the other end of the tail wheel tail boom; the balance wing plate is pivoted between the two tail wheel tail booms, and a gyroscope balance piece is arranged on the balance wing plate, so that the inclination angle of the balance wing plate is the same as the dive angle of the unmanned aerial vehicle; the tail wheel vertical support is fixedly arranged on the double-tail-support machine body, and the extending end of the tail wheel vertical support is connected with the tail wheel tail support in a pivoted mode. The technical effect of reducing the landing skating distance of the unmanned aerial vehicle is achieved.

    本发明提供了一种无人机双尾撑折尾机构,涉及无人机的技术领域。无人机双尾撑折尾机构包括双尾撑机体、尾轮、平衡翼板、两个尾轮尾撑和两个可伸缩锁定的尾轮立撑;尾轮尾撑的一端枢接在双尾撑机体上,尾轮设置在尾轮尾撑的另一端;平衡翼板枢接在两个尾轮尾撑之间,且平衡翼板上设置有陀螺仪平衡件,以使平衡翼板的倾角与无人机的俯冲角相同;尾轮立撑固定设置在双尾撑机体上,且尾轮立撑的伸出端与尾轮尾撑枢接。达到了降低无人机降落滑跑距离的技术效果。


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    Title :

    Double-tail-boom tail folding mechanism of unmanned aerial vehicle


    Additional title:

    无人机双尾撑折尾机构


    Contributors:
    YAN ZIHUI (author) / FANG LIBO (author)

    Publication date :

    2022-04-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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