The invention discloses a co-rotating vertical take-off and landing membrane-wing aircraft. The aircraft comprises a fuselage, at least two rows of power spars are rotationally connected to the fuselage, and propellers are installed on the power spars. membrane wings rotationally connected with the fuselage are arranged between the adjacent power spars; folding angle adjusting mechanisms are arranged in the middles of the membrane wings; and the fuselage is provided with a linkage operation device which enables the membrane wings and the power spars to synchronously rotate relative to the fuselage. According to the co-rotating vertical take-off and landing membrane wing aircraft, the operation of switching between the lifting state and the flying state is simple, the speed range is large, and energy consumption is low.

    本发明公开了一种共转垂直起降膜翼飞机,包括机身,所述机身上转动连接有至少两排动力翼梁,各排动力翼梁上安装有螺旋桨;相邻动力翼梁之间设有与机身转动连接的膜翼;膜翼中部设有折叠角度调节机构;机身上设有使膜翼与动力翼梁相对机身同步旋转的联动操作装置。本发明提供的共转垂直起降膜翼飞机,在升降状态与进入飞行状态之间切换的操作简单,而且速度范围大,能耗低。


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    Titel :

    Co-rotating vertical take-off and landing membrane wing aircraft


    Weitere Titelangaben:

    共转垂直起降膜翼飞机


    Beteiligte:
    ZENG ZHAODA (Autor:in) / ZENG XIANYUE (Autor:in)

    Erscheinungsdatum :

    27.08.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge






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