The invention discloses an aircraft wing structure, relates to the technical field of airplanes, and solves the problems of long takeoff run-up distance, slow rising speed and the like of an existing aircraft. A plurality of air holes are distributed in the upper plate surfaces of the wings, and the airplane is provided with an air suction pump. By adding the air holes in the upper plate surface of the aircraft wing and sucking air through the air suction pump, the air flow velocity of the upper plate surface of the wing is increased when the aircraft takes off, the purpose of rapid rising is achieved, the take-off run-up distance is successfully reduced, the lifting speed is increased, and wide-range application and popularization can be achieved.

    本发明公开了一种飞机机翼结构,涉及飞机技术领域,解决了现有飞机起飞助跑距离长、升高速度慢等问题。所述的机翼上板面分布有许多气孔,所述的飞机装有吸气泵。本发明通过增加飞机机翼上板面气孔,气孔通过吸气泵吸气,使飞机起飞时机翼上板面气流流速增大,达到快速上升的目的,成功减小起飞助跑距离,提高了起升速度,可大范围推广使用。


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    Titel :

    Rapidly-lifted aircraft wing structure


    Weitere Titelangaben:

    一种快速起升的飞机机翼结构


    Beteiligte:
    DANG JIHONG (Autor:in)

    Erscheinungsdatum :

    2024-05-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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