An unmanned aerial vehicle is disclosed, which comprises a fuselage, vehicle arm assemblies and rotor wing power assemblies, wherein the fuselage comprises a shell internally provided with a containing cavity, the vehicle arm assemblies are rotationally connected to vehicle arm hinge parts formed on the wall face of the shell, and the rotor wing power assemblies are arranged on the vehicle arm assemblies. The unmanned aerial vehicle is light in structure, the bearing capacity of the unmanned aerial vehicle can be improved, the waste weight of the unmanned aerial vehicle is prevented from beingincreased, the bearing capacity is improved, the endurance time is prolonged, the occupied space is effectively reduced through the foldable structure, the space utilization rate is high, storage isconvenient, and transportation is facilitated.

    本发明公开一种无人机,包括机身、机臂组件和旋翼动力组件,所述的机身包括内部有容纳腔的壳体,所述的机臂组件转动连接在壳体的壁面成形出的机臂铰接部上,所述的旋翼动力组件设置在机臂组件上。本发明所述的无人机结构轻型,能够提高无人机的承载能力,避免增加无人机的废重,提高承载能力、延长续航时间,可折叠的结构有效减小占用体积,空间利用率高,方便收纳,有利于运输。


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    Titel :

    Unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机


    Beteiligte:
    LI JI (Autor:in) / WANG LIGUANG (Autor:in)

    Erscheinungsdatum :

    2020-07-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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