The modular wing combined aircraft comprises at least two aircraft bodies arranged side by side, composite wing modules are detachably connected to the two sides of each aircraft body, and each composite wing module 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 the machine body is selectively connected with the other composite wing module 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 design of a plurality of airframes expands the airframe space of the aircraft while improving the flight performance of the aircraft, and greatly improves the cargo carrying capacity of the aircraft. The hybrid power module can be designed into a lift fan module and a tiltable power module, and lift and thrust required by different flight modes can be provided for the aircraft.

    本发明涉及一种模块化机翼组合飞行器,包括至少两个并排设置的机体,每个机体两侧均可拆卸地连接复合翼模块,所述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将机体和另一复合翼模块择一连接;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。多个机体的设计在提升飞行器飞行性能的同时,拓展飞行器的机体空间,大大提升了飞行器的载货能力。复合动力模块可设计成升力风扇模块和可倾转动力模块,可为飞行器提供不同飞行模式所需的升力和推力。


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    Titel :

    Modular wing combined aircraft


    Weitere Titelangaben:

    一种模块化机翼组合飞行器


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

    Erscheinungsdatum :

    2023-03-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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