The invention discloses a wing protection device and method for a biplane, and belongs to the field of wing protection of biplanes. The wing protection device comprises an upper wing protection frame, and a lower wing protection frame is arranged at the lower end of the upper wing protection frame; the first fixing cavity extends into the upper wing protection frame and the lower wing protection frame, clamping fixing plates are arranged on the two sides of the interior of the first fixing cavity correspondingly, and a plurality of fixing strips are longitudinally arranged at the upper ends and the lower ends of the two clamping fixing plates correspondingly. The problems that in the existing fixing process, large friction force can be generated, so that scratches are left on the surface of an aircraft wing, the aircraft wing gradually adapts to the appearance of the aircraft wing in the sliding process, and extrusion and fixing are continuously pushed and completed through the rebound resilience of an adaptive spring are solved; and the fixing can adapt to airplanes with different shapes and external sizes and the shapes of corresponding wings.

    本发明公开了一种双翼飞机机翼防护装置及防护方法,属于双翼飞机机翼防护领域。本发明的一种双翼飞机机翼防护装置及防护方法,包括上机翼保护框,所述上机翼保护框的下端设置有下机翼保护框;所述第一固定腔延伸至上机翼保护框和下机翼保护框的内部,所述第一固定腔内部的两侧均设置有加持固定板,两个所述加持固定板的上下两端均纵向设置有若干个固定条。本发明解决了现有固定的过程中会产生较大的摩擦力从而造成飞机机翼表面残留有划痕,滑动的过程中逐步适应飞机机翼的外形,并且通过适配弹簧的回弹性可持续的推动并完成挤压和固定,固定得以应对不同外形外部尺寸飞机以及对应的机翼的外形。


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    Titel :

    Wing protection device and protection method for biplane


    Weitere Titelangaben:

    一种双翼飞机机翼防护装置及防护方法


    Beteiligte:
    SUN FENGQIN (Autor:in) / ZHONG ZHIYONG (Autor:in) / TIAN YINQIAO (Autor:in) / TANG XUELIAN (Autor:in) / CUI ZHIHUA (Autor:in)

    Erscheinungsdatum :

    03.02.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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