The invention provides a variable stiffness sliding composite flexible skin system and a using method, the system comprises a wing used for installing a tension control mechanism, a skin sliding end fixing mechanism, a slidable deformation skin structure and a driving device, the system comprises a connecting wall and a pair of middle rib plates, and the middle rib plates are fixed to the connecting wall; a gap for mounting a tension control mechanism is formed by the pair of middle rib plates; the tension control mechanism, the slidable deformation skin structure and the skin fixed end fixing structure are connected in sequence; the slidable deformation skin structure comprises a skin, one end of the skin is fixedly connected with the skin fixing end fixing structure, and the other end of the skin is movably connected with the tension control mechanism; the skin fixed end fixing structure is connected with the connecting wall through a driving device; the driving device can stretch out and draw back and is hinged between the connecting wall and the skin fixing end fixing structure, and when the skin needs to deform, the skin can stretch out along with the driving device to be bent; and the skin sliding end fixing mechanism is used for locking the skin when deformation of the skin is not needed, and is arranged on the middle rib plate. The continuous and smooth deformation requirement of the wing surface can be met, and the rigidity and bearing requirements during high-speed flight of an aircraft can also be met.

    本发明提出了一种变刚度滑动复合柔性蒙皮系统及使用方法,该系统包括:机翼,用于安装张力控制机构、蒙皮滑动端固定机构、可滑动变形蒙皮结构和驱动装置,包括:连接墙和一对中部肋板,中部肋板固定于连接墙,一对中部肋板形成安装张力控制机构的间隙;张力控制机构、可滑动变形蒙皮结构和蒙皮固定端固定结构,依次连接;可滑动变形蒙皮结构,包括蒙皮,其一端与蒙皮固定端固定结构固定连接,另一端与张力控制机构活动连接;蒙皮固定端固定结构,通过驱动装置与连接墙连接;驱动装置,可伸缩并铰接在连接墙和蒙皮固定端固定结构之间,当需要蒙皮变形时,蒙皮可随驱动装置伸出而实现弯曲;蒙皮滑动端固定机构,当不需要蒙皮变形时,其用于锁定蒙皮,设置于中部肋板上。本发明既能满足机翼表面的连续光滑的变形要求,又能满足飞行器高速飞行时的刚度和承载需求。


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    Title :

    Variable-stiffness sliding composite flexible skin system and using method


    Additional title:

    变刚度滑动复合柔性蒙皮系统及使用方法


    Contributors:
    ZHAO YINJUN (author) / WANG JIEYU (author) / TIAN YINGZHONG (author) / XI FENGFENG (author)

    Publication date :

    2024-08-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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