The invention discloses a deformation skin structure capable of realizing variable camber and thickness of a wing. The deformation skin structure comprises a deformation skin, a chordwise supporting structure, a spanwise stringer and a locking device, the deformed skin serves as the outer surface of the wing and wraps other structures in the deformed skin, the chordwise supporting structures are laid in the chordwise direction, the multiple chordwise supporting structures are arranged in the wing direction according to the spanwise length of the skin, the spanwise stringers are arranged between the chordwise supporting structures and fixedly connected with the skin, and the locking devices are laid between the chordwise supporting structures and fixedly connected with the wing. And fixedly connecting with the deformation skin. According to the invention, rapid deformation of the wing skin and the capability of flexibly adapting to different flight states can be realized, so that the performance and the application range of the deformed wing are improved.

    本发明公开了一种可实现机翼变弯度和厚度的变形蒙皮结构,包括:变形蒙皮、弦向支撑结构、展向长桁、锁扣装置;变形蒙皮作为机翼的外表面,将其他结构包裹其中,弦向支撑结构铺设在沿弦向方向上,根据蒙皮展向长度在机翼方向上布置多个,展向长桁设置在弦向支撑结构之间与蒙皮固定连接,锁扣装置铺设在弦向支撑结构之间,与变形蒙皮固定连接。本发明能够实现机翼蒙皮的快速变形和灵活适应不同飞行状态的能力,从而提升变形机翼的性能和应用广度。


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    Titel :

    Deformation skin structure capable of realizing variable camber and thickness of wing


    Weitere Titelangaben:

    一种可实现机翼变弯度和厚度的变形蒙皮结构


    Beteiligte:
    WU FUQIANG (Autor:in) / YANG BOHAN (Autor:in) / ZHAO QIJUN (Autor:in)

    Erscheinungsdatum :

    27.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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