Variable aircraft flexible wing, variable stiffness skin structure and preparation method thereof
A technology of flexible wings and morphing aircraft, which is applied in the directions of wings, aircraft parts, transportation and packaging, etc. It can solve the problems of heavy mass, low efficiency, and long response time of drive units, achieve high elastic energy density, and overcome deformation The effect of slow, short response times
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[0030] The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.
[0031] see Figure 1 to Figure 3 , a variant aircraft flexible wing of the present invention, comprising: wing skeleton and variable stiffness skin unit 6 . The wing skeleton is formed by connecting the inner wing 1, the first cylindrical hinge 3, the second cylindrical hinge 4, and the outer wing 7 through the connecting shaft 5, and the variable stiffness skin unit 6 is fixed on both sides of the wing skeleton by fixing pins 2 and The wing skeleton is assembled into a complete skin structure. The specific connection relationship is as follows: the inner wing 1 is connected together with the first cylindrical hinge 3 through the connecting shaft 5, the first cylindrical hinge 3 is connected with the second cylindrical hinge 4 through the connecting shaft 5, and the second cylindrical hinge 4 is connected through the connecting shaft...
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