The invention provides a torsion wing with a tension-torsion coupling characteristic based on cell element stacking, and relates to the technical field of wings, the torsion wing comprises a wing root, a linear motor, a cantilever structure, a driving straight rod, a wing rib and a wing tail end; the two ends of the cantilever structure are fixedly connected with the wing root and the wing tail end correspondingly, the linear motor is fixedly connected with the wing root, one end of the driving straight rod is in transmission connection with the driving end of the linear motor, the other end of the driving straight rod is rotationally connected with the wing tail end, and the cantilever structure is formed by stacking a plurality of cell elements with the tension-shear coupling deformation characteristic. The linear motor can drive the cantilever structure to twist when driving the straight rod to move in the length direction of the straight rod. The invention has a continuous configuration variable function, gives consideration to the bearing capacity of the wing, can remarkably improve the section torsion capacity under the action of tension, and can continuously regulate and control the torsion angle, change the effective attack angle of each section of the wing in the spanwise direction and adjust the aerodynamic load distributed in the spanwise direction of the wing surface, thereby improving the aerodynamic efficiency of the wing.

    本发明提供一种基于胞元堆叠的具备拉扭耦合特性的扭转机翼,涉及机翼技术领域,包括机翼根部、直线电机、悬臂结构、驱动直杆、翼肋和机翼末端;悬臂结构的两端分别与机翼根部以及机翼末端固定连接,直线电机与机翼根部固定连接,驱动直杆的一端与直线电机的驱动端传动连接,另一端和机翼末端转动连接,悬臂结构由多个具有拉剪耦合变形特性的胞元堆叠而成,直线电机驱动直杆沿着自身长度方向移动时能够带动悬臂结构扭转。本发明具有连续构型可变功能,兼顾机翼承载能力的同时,能够在拉力作用下显著提升其截面扭转能力,可以连续地调控其扭转角度,改变机翼沿展向各剖面的有效迎角,调整翼面展向分布的气动载荷,从而改善机翼气动效率。


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    Title :

    Twisting wing with tension-torsion coupling characteristic based on cell element stacking


    Additional title:

    一种基于胞元堆叠的具备拉扭耦合特性的扭转机翼


    Contributors:
    ZHANG JIAYING (author) / CHEN WEI (author) / ZHU XUEREN (author) / HUANG KE (author)

    Publication date :

    2024-06-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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