The invention relates to a tiltable power module wing which comprises a wing main body and a duct formed in the middle of the wing main body, connecting mechanisms are arranged on the left side and the right side of the wing main body, and a machine body and another tiltable power module wing are alternatively connected through the connecting mechanisms; the duct is communicated with the upper wing surface and the lower wing surface of the wing main body, and a tiltable power module capable of tilting by an angle to provide lift force/thrust is arranged in the duct. The wings with the lift force of the aircraft are combined with the power device for providing the lift force, the provided lift force is large, the lift force variety is rich, the structure is compact, and the compact design of the aircraft is facilitated. The upper wing surface and the lower wing surface of the wing main body can provide lift force when the aircraft cruises, the tiltable power module can provide lift force when the aircraft vertically takes off and lands, and the tiltable power module can also provide thrust when the aircraft cruises.

    本发明涉及一种可倾转动力模块机翼,包括机翼主体和开设在机翼主体中部的涵道,机翼主体左右两侧均设置连接机构并通过连接机构将机体和另一可倾转动力模块机翼择一连接;所述涵道连通机翼主体上下翼面,涵道内供一可倾转角度以提供升力/推力的可倾转动力模块设置。本发明将飞行器具有升力的机翼与提供升力的动力装置相结合,可提供的升力大、升力种类丰富,结构紧凑,便于飞行器的紧凑设计。机翼主体上下翼面可以在飞行器巡航时提供升力,可倾转动力模块可在飞行器垂直起降时提供升力,可倾转动力模块也可在飞行器巡航时提供推力。


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    Title :

    Tiltable power module wing


    Additional title:

    可倾转动力模块机翼


    Contributors:
    XU XING (author) / LI ZHIHONG (author) / BING FUQIANG (author)

    Publication date :

    2023-03-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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