The invention discloses a damping undercarriage convenient to replace and used for an intelligent unmanned aerial vehicle, which comprises an unmanned aerial vehicle body, and mounting frames are evenly and fixedly connected to the outer side of the unmanned aerial vehicle body; supporting leg mounting positions are evenly arranged at the bottom end of the unmanned aerial vehicle body, mounting plates are fixedly mounted at the bottom ends of second threaded holes through screws, supporting legs are conveniently replaced and detached, when needing to be used, the unmanned aerial vehicle is mounted to the bottom end of the unmanned aerial vehicle body through the mounting plates, the supporting legs are fixedly connected to the bottom ends of the mounting plates, and the supporting legs are conveniently replaced and detached. The supporting legs are slidably connected to the elastic telescopic legs, the bottom ends of the supporting legs are fixedly connected with first sliding blocks, the first sliding blocks are slidably connected to the inner sides of the elastic telescopic legs, and the bottom ends of the first sliding blocks are fixedly connected with first springs, so that when the unmanned aerial vehicle body lands, the inertia effect borne by the unmanned aerial vehicle body can be effectively reduced, and the use safety of the unmanned aerial vehicle body is protected; the damping undercarriage is simple in structure and convenient to use, and the supporting legs can be effectively replaced after the unmanned aerial vehicle body is used.

    本发明公开了一种便于更换的智能无人机用减震起落架,包括无人机主体,所述无人机主体的外侧均匀固定连接有安装架;通过在无人机主体的底端均匀设置有支腿安装处,在第二螺纹孔的底端通过螺丝固定安装有安装板,方便对支腿进行更换拆卸,在需要使用时,在通过安装板将其安装至无人机主体的底端,安装板的底端固定连接有支腿,支腿滑动连接于弹性伸缩腿,支腿的底端固定连接有第一滑块,第一滑块滑动连接于弹性伸缩腿的内侧,第一滑块的底端固定连接有第一弹簧,在无人机主体落地时,能有效减少无人机主体受到的惯性的作用,保护无人机主体的使用安全,本装置结构简单,使用方便,能有效在无人机主体使用后对支腿进行更换。


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    Titel :

    Damping undercarriage convenient to replace and used for intelligent unmanned aerial vehicle


    Weitere Titelangaben:

    一种便于更换的智能无人机用减震起落架


    Beteiligte:
    ZHANG HENG (Autor:in) / LIU HAO (Autor:in)

    Erscheinungsdatum :

    18.06.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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