The invention provides a fixed-wing aircraft, which takes a Karsi vertical coordinate system as a reference, takes a first plane formed by an X axis defined by the sailing direction of the fixed-wing aircraft and a Z axis defined by the gravity direction of the fixed-wing aircraft as a symmetry plane, and comprises an aircraft head, a fixed-wing aircraft body and a fixed-wing aircraft body, a fuselage; the main wing comprises a connecting part positioned at the rear part of the main wing, and the connecting part is used for connecting an air propulsion device; the air propulsion devices are connected with the main wings, each air propulsion device comprises an air guiding pipe, an air thruster and an air spraying pipe which are connected front and back in the X-axis direction, each air guiding pipe comprises an air inlet connected with the connecting part of the corresponding main wing, and the air inlets are used for guiding air into the air propulsion devices. According to the fixed-wing aircraft provided by the invention, the total lift force of the wings can be improved during cruising, and meanwhile, the maneuvering capability for supporting the fixed-wing aircraft to realize vertical/or short-distance take-off and landing and hovering is also provided.

    本发明提供了一种固定翼飞机,以卡氏垂直坐标系为参照,所述固定翼飞机以其航行方向所定义的X轴和重力方向所定义的Z轴共同构成的第一平面为对称面构置,包括:机头;机身;主机翼,所述主机翼包括位于主机翼后部的连接部,用于连接空气推进装置;与主机翼相连的至少一组空气推进装置,所述空气推进装置包括沿X轴方向前后相连接的引气管件、气体推力器和喷气管件,所述引气管件包括与主机翼连接部相连的进气口,所述进气口用于向空气推进装置导入空气。本发明所提供的固定翼飞机,不仅可以在巡航时提高机翼的总升力,同时还提供支持该固定翼飞机实现垂直/或短距起降和空中悬停的机动能力。


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    Titel :

    Fixed-wing aircraft


    Weitere Titelangaben:

    一种固定翼飞机


    Beteiligte:
    HUANG HE (Autor:in)

    Erscheinungsdatum :

    20.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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