The invention discloses a rotor unmanned aerial vehicle capable of being assembled and disassembled, and belongs to the field of unmanned aerial vehicles. The rotor unmanned aerial vehicle comprises a main machine body and a plurality of machine arms uniformly arranged on the circumferential side wall of the main machine body; each machine arm comprises a main arm and an auxiliary arm, a connecting plate is arranged at the root of each main arm, anti-falling sliding blocks are arranged on each connecting plate, a plurality of anti-falling sliding grooves matched with the anti-falling sliding blocks are formed in the circumferential side wall of the main machine body, the anti-falling sliding grooves are formed in the axial direction of the main machine body, and the anti-falling sliding grooves extend to the top surface of the main machine body; an inserting groove extending in the axial direction of each main arm is formed in the end face of the tip of the main arm, an inserting rod matched with each inserting groove is arranged at the root of the corresponding auxiliary arm, and a power assembly is fixedly mounted at the tip of each auxiliary arm. The connecting plates are fixed to the main machine body through first locking structures, and the auxiliary arms are fixed to the main arms through second locking structures. The unmanned aerial vehicle is simple in structure, reasonable in design, capable of making machine arms of the unmanned aerial vehicle disassembled, capable of reducing the transportation size, capable of being rapidly assembled and convenient to use.

    本发明公开了一种可组装可拆卸的旋翼无人机,属于无人机领域,包括主机体以及多个均匀布置在主机体的周向侧壁上的机臂;机臂包括主臂和副臂,主臂的根部设置有连接板,连接板上均设置有防脱滑块,主机体的周向侧壁上设置有多个与防脱滑块相适配的防脱滑槽,防脱滑槽沿主机体的轴向方向布置,且防脱滑槽延伸至主机体的顶面;主臂的梢部的端面设置有沿主臂的轴向方向延伸的插槽,副臂的根部设置有与插槽相适配的插杆,副臂的梢部固定安装有动力组件;连接板通过第一锁紧结构与主机体固定,副臂通过第二锁紧结构与主臂固定。本发明结构简单、设计合理,能够使无人机的机臂进行拆卸,从而降低运输尺寸,并且能够快速组装,方便使用。


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    Title :

    Rotor unmanned aerial vehicle capable of being assembled and disassembled


    Additional title:

    一种可组装可拆卸的旋翼无人机


    Contributors:
    ZHANG LI (author) / AI JIANLIANG (author)

    Publication date :

    2021-04-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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