The invention discloses a fixed-wing aircraft assembly which comprises an aircraft body used for being connected with other parts. The wings are in a closed ring shape surrounding the fuselage; the wings are fixed to the fuselage in an axial symmetry mode with the central axis of the fuselage as the symmetry axis, and the wings are fixed to the middle of the fuselage in the extending direction. The power device at least comprises an engine used as a power source and a pneumatic thrust vectoring nozzle used for adjusting the posture of the fuselage, and the pneumatic thrust vectoring nozzle is controlled to spray air; the multiple power devices are distributed along the periphery of the wing, and the multiple power devices are fixed to the wing in an axial symmetry mode with the central axis of the fuselage as the symmetry axis; the controllability of the aircraft can be improved while the structural mass of the aircraft is well reduced.

    本发明公开了一种固定翼飞行器总成,包括机身,所述机身用于连接其它零部件;机翼,所述机翼呈环绕于机身的闭口环形;所述机翼以机身的中心轴线为对称轴呈轴对称的方式与机身形成固定,所述机翼固定于机身延伸方向的中部;动力装置,所述动力装置至少包括用于作为动力源的发动机和用于调整机身姿态的气动矢量喷管,所述气动矢量喷管被控制的喷气;所述动力装置为多个,多个所述动力装置沿机翼的周缘分布,多个所述动力装置以机身的中心轴线为对称轴呈轴对称的方式与机翼形成固定;能够在很好的实现减少飞机结构质量的同时,提高飞行器的操控性。


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    Titel :

    Fixed-wing aircraft assembly


    Weitere Titelangaben:

    固定翼飞行器总成


    Beteiligte:
    ZHANG HAO (Autor:in) / YU YANG (Autor:in) / YU TAO (Autor:in) / LIANG SIJIA (Autor:in) / YANG YALIN (Autor:in)

    Erscheinungsdatum :

    2023-04-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U



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