The invention discloses a wing-body-fused aircraft structure. The wing-body-fused aircraft structure comprises an aircraft body, wings, a power device and pulleys; the fuselage and the wings are of a wing body fusion structure; and the normal axial section of the wing, namely the wing section of the wing and the normal axial section of the fuselage are of symmetrical water-drop-shaped structures. The wings and the fuselage adopt a wing body fusion structure, and the sections of the wings and the fuselage are of symmetrical water drop-shaped structures, so that the wet area of the whole aircraft can be greatly reduced, the frictional resistance and the interference resistance among parts are reduced, the airfoil has the characteristic of high lift-drag ratio, and on the premise of uniform linear motion of the aircraft structure, the airfoil lift force is 0, and the airfoil lift force is 0. And the airfoil can approach a resistance-free effect, so that the aerodynamic efficiency of an aircraft is improved, and the aviation operation cost is reduced.

    本发明公开了一种翼身融合的飞机结构,包括机身、机翼、动力装置和滑轮;所述机身和机翼呈翼身融合结构;所述机翼的法向轴截面即机翼的翼型和所述机身的法向轴截面均呈对称的水滴状结构。本发明的机翼和机身采用翼身融合结构,并且机翼和机身的截面都呈对称的水滴状结构,可以大幅减小全机的湿面积,降低摩擦阻力和部件间的干扰阻力,具有升阻比高的特点,且飞机结构在匀速直线运动的前提下,翼型升力为0,翼型可接近无阻力的效果,从而提升飞机的空气动力效率,降低航空运营成本。


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    Titel :

    Aircraft structure with fused wing body


    Weitere Titelangaben:

    一种翼身融合的飞机结构


    Beteiligte:
    BAI YUCHENG (Autor:in)

    Erscheinungsdatum :

    27.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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