The invention discloses a foldable unmanned aerial vehicle wing based on multistable characteristics, which comprises a main wing, a folding structure, a flexible skin and a supporting piece fixed tothe vehicle body. The folding structure comprises a multistable composite cylindrical shell, a first memory alloy and two first stand columns. One end of the multistable composite cylindrical shell isfixed with the main wing; the other end of the multistable composite cylindrical shell is fixed with the supporting piece; the lower ends of the two first stand columns are fixed to the two oppositesides of the multistable composite cylindrical shell correspondingly. The two ends of the first memory alloy are fixed to the upper ends of the two first stand columns respectively, the two ends of the first memory alloy are electrically connected with heating circuits respectively, the folding structure is wrapped with the flexible skin, and the two ends of the flexible skin are fixed to the folding structure, the main wing and the supporting piece respectively. The foldable unmanned aerial vehicle wing based on the multistable characteristics has the advantages of being simple in folding structure, small in weight, stable in folding and unfolding state and the like.
本发明公开了一种基于多稳态特性的可折叠无人机机翼,包括主翼、折叠结构、柔性蒙皮以及与机身固定的支撑件,所述折叠结构包括多稳态复合材料圆柱壳、第一记忆合金和两个第一立柱,多稳态复合材料圆柱壳的一端与主翼固定,多稳态复合材料圆柱壳的另一端与支撑件固定,两个第一立柱的下端分别固定在多稳态复合材料圆柱壳的相对两侧,第一记忆合金的两端分别与两个第一立柱的上端固定,第一记忆合金的两端分别与加热电路电连接,柔性蒙皮包裹在折叠结构外部,柔性蒙皮两端分别与折叠结构与主翼和支撑件固定。本发明提供了一种基于多稳态特性的可折叠无人机机翼,具有折叠结构简单,重量小,折叠与展开状态稳定等优点。
Foldable unmanned aerial vehicle wing based on multistable characteristics
一种基于多稳态特性的可折叠无人机机翼
2020-07-17
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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