The invention provides a deformable wing capable of being digitally designed. The deformable wing capable of being digitally designed comprises a wing surface and a bistable structure composition unit. Wherein the wing surface is flexible; the wing surface is filled with the bistable structure composition unit, and the bistable structure composition unit has the zero Poisson's ratio characteristic, can be telescopically deformed in the vertical direction and can be assembled and reconstructed. The deformable wing capable of being digitally designed is adjustable in deformation, can bear aerodynamic loads before and after deformation, and has the characteristics of light weight, simplicity in preparation and the like.

    本发明提供了一种可数字化设计的可变形机翼。该可数字化设计的可变形机翼包括翼面和双稳态结构组成单元。其中,所述翼面呈柔性;所述双稳态结构组成单元填充于所述翼面内,所述双稳态结构组成单元具有零泊松比特性、在上下方向上可伸缩变形且可组装重构。本发明的可数字化设计的可变形机翼的变形可调控,且可承受变形前后的气动载荷,具有质轻、制备简单等特点。


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    Title :

    Deformable wing capable of being digitally designed


    Additional title:

    可数字化设计的可变形机翼


    Contributors:
    YIN SHA (author) / YANG YU (author) / WANG CHENGYU (author) / WANG ZHIGANG (author)

    Publication date :

    2022-11-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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