The modular wing aircraft comprises a fuselage, the two sides of the fuselage extend to form detachably-arranged composite wing modules, and each composite wing module comprises a wing body and a duct formed in the middle of the wing body; connecting mechanisms are arranged on the left side and the right side of the wing main body, and the fuselage and the other composite wing module are selectively 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 hybrid power module capable of providing lift force is arranged in the duct. The power unit of the aircraft is arranged in the wing of the module, so that the wing assembly and the power assembly are highly combined, and the integration degree of the aircraft is improved. The flight performance of the aircraft can be conveniently and rapidly adjusted through the modularized wing assembly, and when the performance requirement of the aircraft needs to be adjusted, only the corresponding composite wing module needs to be assembled according to the requirement.

    本发明涉及一种模块化机翼飞行器,包括机身,所述机身两侧均延伸有可拆卸设置的复合翼模块,复合翼模块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择一连接机身和另一复合翼模块;所述涵道连通机翼主体上下翼面,涵道内供一可提供升力的复合动力模块设置。本发明将飞机的动力单元设置在模块的机翼中,使机翼组件和动力组件高度结合,提升飞行器的集成化程度。模块化的机翼组件便于快速调整飞行器的飞行性能,在需要调整飞行器性能需求时,只需按要求组装相应的复合翼模块即可。


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    Titel :

    Modular wing aircraft


    Weitere Titelangaben:

    一种模块化机翼飞行器


    Beteiligte:
    XU XING (Autor:in) / LI ZHIHONG (Autor:in) / BING FUQIANG (Autor:in)

    Erscheinungsdatum :

    14.03.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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