The invention discloses a flapping-wing aircraft wing capable of being quickly folded and stored. The flapping-wing aircraft wing comprises a root leading edge carbon tube, a tip leading edge carbon tube, a sliding quick release tube, a wing film, a main reinforcing rib, an auxiliary reinforcing rib, an inelastic line and transparent adhesive tapes. The root leading edge carbon tube and the tip leading edge carbon tube can be connected through a sliding quick release tube; the wing film is adhered to two leading edge rods through the transparent adhesive tapes; the sticking parts keep away from the movement range of a sliding sleeve; a main reinforcing rib and an auxiliary reinforcing rib are respectively arranged at the middle part and the outer part of the wing film; the two reinforcingribs are pasted to the wing film through the transparent adhesive tapes, the inelastic line penetrates through the two leading edge carbon tubes, one end of the inelastic line is stably fixed into theroot leading edge carbon tube, the other end of the inelastic line is stably fixed into the tip leading edge carbon tube, and when the sliding quick release tube completely moves to the root leadingedge carbon tube, the wing can rotate around the middle shaft to be folded by 180 degrees. The flapping-wing aircraft wing can be quickly folded and stored, and has the characteristics of being simplein structure, low in manufacturing difficulty and convenient to carry.

    本发明公开了一种可快速折叠收纳的扑翼飞行器机翼,包括根部前缘碳管、梢部前缘碳管、滑动快拆管、机翼薄膜、主加强筋、副加强筋、无弹力线和透明胶带。根部前缘碳管和梢部前缘碳管可通过滑动快拆管连接,机翼薄膜通过透明胶带粘贴至两根前缘杆上,粘贴部分避开滑动套管运动范围,在机翼薄膜的中部和外部分别布置主加强筋和副加强筋,两根加强筋用透明胶带粘贴至机翼薄膜上,无弹力线贯穿两根前缘碳管,其中一端稳定固定于根部前缘碳管内部,另一端稳定固定于梢部前缘碳管内部,当滑动快拆管完全移动至根部前缘碳管上时,机翼可绕中间轴旋转对折180度。本发明可实现扑翼飞行器机翼快速折叠收纳,具有结构简单、制作难度低、携行方便的特点。


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    Title :

    Flapping-wing aircraft wing capable of being quickly folded and stored


    Additional title:

    可快速折叠收纳的扑翼飞行器机翼


    Contributors:
    LI RENSHU (author) / HOU MINGSHUO (author) / LI QIAN (author) / LIU KUN (author) / MENG YU (author) / HUANG SHENGYAO (author) / YUAN HONGYU (author)

    Publication date :

    2020-07-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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