The invention provides a deformable wing, an aircraft and a deformation control method, the deformable wing comprises a combined wing and a combined wing connecting structure, the combined wing is mounted on a fuselage through the combined wing connecting structure, and the combined wing is expanded and contracted. By means of the special combined wing structure, continuous wing configuration deformation of the whole shape of the aircraft is achieved, and the aircraft adapts to ultra-wide-range flight working conditions and different flight tasks.

    本发明提出一种可变形机翼、飞行器及变形控制方法,包括组合翼和组合翼连接结构,组合翼通过组合翼连接结构安装在机身上,并实现组合翼展开和收缩。本发明通过特殊的组合翼结构,实现飞行器整体形态连续的机翼构型变形,适应超宽域飞行工况及不同的飞行任务。


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    Title :

    Deformable wing, aircraft and deformation control method


    Additional title:

    一种可变形机翼、飞行器及变形控制方法


    Contributors:
    ZHANG YINING (author) / ZHOU LIN (author) / XIE HAOPIN (author) / TU SHENGJIA (author) / YOON SUNG AH (author)

    Publication date :

    2022-12-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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