The invention provides an unmanned aerial vehicle with an adjustable rotor angle. The unmanned aerial vehicle comprises a fuselage, a central wing and a plurality of tail supporting rods, wherein a rotating power cabin is arranged at the front end of each tail supporting rod; each rotating power cabin comprises a first rotor wing assembly and a first movable assembly. Each first movable assembly comprises a driving device and a rotating piece. When the unmanned aerial vehicle needs to achieve vertical take-off and landing and hovering, the first rotor wing assemblies rotate by a certain angle, so that the first rotor wing assemblies provide power in the vertical direction for vertical take-off and landing or hovering of the unmanned aerial vehicle, and when the unmanned aerial vehicle does not need to achieve vertical take-off and landing or hovering, the first rotor wing assemblies rotate to the initial position and provides power in the horizontal direction for the unmanned aerial vehicle. The angle of the rotor wings is adjustable, and power in different directions is provided for the unmanned aerial vehicle.

    本发明提供的旋翼角度可调的无人机包括机身、中央翼与若干尾撑杆,每一尾撑杆的前端布置有旋转动力舱;旋转动力舱包括第一旋翼组件与第一活动组件第一活动组件包括驱动装置、转动件。无人机需实现垂直起降和悬停时,第一旋翼组件转动一定角度,从而使第一旋翼件为无人机的垂直起降或悬停提供垂直方向的动力,当无人机不需进行垂直起降或悬停时,第一旋翼组件转动至初始位置,为无人机提供水平方向的动力,使旋翼角度可调,为无人机提供不同方向的动力。


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    Titel :

    Unmanned aerial vehicle with adjustable rotor angle


    Weitere Titelangaben:

    一种旋翼角度可调的无人机


    Beteiligte:
    HE JUN (Autor:in) / GONG ZHENG (Autor:in)

    Erscheinungsdatum :

    2021-11-19


    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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