The invention discloses a retractable and foldable unmanned aerial vehicle rotor structure which comprises a folding wing and a retractable wing arm, the head end of the retractable wing arm is rotatably connected with a steering engine, and the folding wing is arranged above the tail end of the retractable wing arm. According to the retractable and foldable unmanned aerial vehicle rotor wing structure, by arranging the folding wings and the retractable wing arms, the size of an unmanned aerial vehicle is compressed to the maximum extent, all the components are independently driven through different power sources and do not interfere with one another, and the retractable and foldable unmanned aerial vehicle rotor wing structure is high in safety, convenient to carry and capable of adapting to more use environments.

    本发明公开了一种可收缩折叠的无人机旋翼结构,包括折叠机翼及伸缩翼臂,所述伸缩翼臂的首端与舵机转动连接,所述折叠机翼设置于所述伸缩翼臂的末端上方。本发明公开的一种可收缩折叠的无人机旋翼结构,通过设置折叠机翼和伸缩翼臂,最大限度地压缩了无人机的体积,各部件通过不同的动力源单独驱动,互不干涉,安全性高,便于携带,也能适应更多的使用环境。


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    Titel :

    Retractable and foldable unmanned aerial vehicle rotor wing structure


    Weitere Titelangaben:

    可收缩折叠的无人机旋翼结构


    Beteiligte:
    DENG TAO (Autor:in) / YANG YALIN (Autor:in) / TAN LIZI (Autor:in) / LIU ZHIHAO (Autor:in) / HE JIAWEI (Autor:in) / DU TONG (Autor:in)

    Erscheinungsdatum :

    2022-05-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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