The invention discloses a deformable rotor unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles, the deformable rotor unmanned aerial vehicle comprises a rotor unmanned aerial vehicle body, a guide mechanism, a buoyancy mechanism and a rope driving mechanism; wherein the guide mechanism is fixedly mounted on the unmanned rotorcraft body and is used for guiding the rope driving mechanism; the buoyancy mechanism is an air bag connected with the guide mechanism and is used for providing buoyancy for the rotor unmanned aerial vehicle body; the rope driving mechanism is used for changing the shape of the airbag. According to the deformable rotor unmanned aerial vehicle, the cruising ability of the rotor unmanned aerial vehicle can be effectively improved by arranging the buoyancy mechanism, the buoyancy mechanism can be tightly attached to the indoor wall face, and the concealment of the rotor unmanned aerial vehicle is enhanced.

    本发明公开了一种可变形的旋翼无人机,属于无人机技术领域,该可变形的旋翼无人机除包括旋翼无人机机体外,还包括导向机构、浮力机构以及绳索驱动机构;其中,导向机构固定安装于旋翼无人机机体,用于为绳索驱动机构导向;浮力机构为与导向机构相连的气囊,用于为旋翼无人机机体提供浮力;绳索驱动机构用于改变气囊的形状。该可变形的旋翼无人机通过设置浮力机构能够有效提升旋翼无人机的续航能力,而且浮力机构可以紧贴室内壁面,增强该旋翼无人机的隐蔽性。


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    Titel :

    Deformable rotor unmanned aerial vehicle


    Weitere Titelangaben:

    一种可变形的旋翼无人机


    Beteiligte:
    YU JIANQIAO (Autor:in) / ZHOU HONGMIAO (Autor:in) / LI JIAXUN (Autor:in) / NIU KANG (Autor:in) / LI ZIYUAN (Autor:in)

    Erscheinungsdatum :

    2022-12-16


    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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