The invention provides a flexible composite material skin and a preparation method thereof. The flexible composite material skin comprises a zero Poisson's ratio skeleton, a negative Poisson's ratio filler and an elastic surface layer, the zero-Poisson-ratio framework is provided with a plurality of filling areas; the negative Poisson's ratio filler is arranged in the filling area; the elastic surface layer is attached to the upper surface and/or the lower surface of the zero-Poisson-ratio framework with the negative-Poisson-ratio filler. According to the flexible composite material skin provided by the invention, the surface can be kept continuous, smooth and free of concave-convex fluctuation in the deformation process, and the stealth performance and aerodynamic performance of a corresponding aircraft structure prepared from the flexible composite material skin can be improved.

    本发明提供了一种柔性复合材料蒙皮及其制备方法,柔性复合材料蒙皮包括零泊松比骨架、负泊松比填充物以及弹性表层;零泊松比骨架具有多个填充区域;负泊松比填充物设于填充区域内;弹性表层贴覆于具有负泊松比填充物的零泊松比骨架的上表面和/或下表面。本发明提供的柔性复合材料蒙皮在变形过程中能够保持表面的连续、光滑且无凹凸起伏的现象,能够提高采用该柔性复合材料蒙皮制备的对应飞行器结构的隐身性能和气动性能。


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    Title :

    Flexible composite material skin and preparation method thereof


    Additional title:

    柔性复合材料蒙皮及其制备方法


    Contributors:
    WANG TINGTING (author) / GAO JUNPENG (author) / XU HU (author) / MA ZHAODAN (author) / ZHANG BAOYAN (author)

    Publication date :

    2025-04-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge



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