The invention discloses a rotor unmanned aerial vehicle with a retractable unmanned aerial vehicle structure, and relates to the technical field of unmanned aerial vehicles, the rotor unmanned aerial vehicle comprises a fuselage, a bent frame is fixedly mounted on the outer surface of the fuselage, and a protective frame is fixedly mounted at the top of the bent frame; the retractable undercarriage is used for stably supporting the unmanned aerial vehicle; and a balance driving member. According to the rotor unmanned aerial vehicle with the retractable unmanned aerial vehicle structure, when the unmanned aerial vehicle lands, the supporting blocks make contact with the ground, and when the unmanned aerial vehicle lands, the supporting blocks are affected by the weight of the unmanned aerial vehicle and extrude the ground, so that when the obliquely-arranged supporting blocks make contact with the ground, the supporting blocks make contact with the ground; damping rods connected to the surfaces of positioning blocks are driven to rotate in clamping blocks through rotating rings according to the terrain influence, so that the contact angle between supporting blocks and the ground is adjusted when the unmanned aerial vehicle is parked, the supporting blocks arranged in multiple directions are attached to and matched with the ground at the moment, the unmanned aerial vehicle is parked stably, and the phenomenon that the unmanned aerial vehicle shakes during landing is avoided.

    本发明公开了一种具有可收缩无人机结构的旋翼无人机,本发明涉及无人机技术领域,包括机身,该机身的外表面固定安装有弯架,所述弯架的顶部固定安装有防护框;收缩起落架,该收缩起落架用于无人机平稳支撑;平衡驱动件。该具有可收缩无人机结构的旋翼无人机,通过无人机降落时,支撑块与地面接触,在无人机降落时支撑块受到无人机重量影响与地面产生挤压,使得倾斜设置的支撑块在与地面接触时,根据地形影响带动定位块表面连接的阻尼杆通过转环在卡接块内旋转,以便于无人机停放时调整支撑块与地面接触角度,此时多方位设置的支撑块均与地面贴合适配,以便于无人机稳定停放,避免无人机降落时出现晃动现象。


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    Title :

    Rotor wing unmanned aerial vehicle with retractable unmanned aerial vehicle structure


    Additional title:

    一种具有可收缩无人机结构的旋翼无人机


    Contributors:
    SHI KUN (author) / LIU FANG (author) / ZHAO JI (author) / ZHANG XU (author) / TIAN XIANGGUO (author)

    Publication date :

    2025-03-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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