Stressed-skin construction capable of implementing large area deformation
A large-area skinning technology, applied in the field of aircraft skinning, can solve problems such as limited deformability, increased resistance to skeleton deformation, and difficulty in co-deformation
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[0018] Below in conjunction with accompanying drawing and specific embodiment the present invention will be further described:
[0019] to combine figure 2 , the present embodiment is composed of skin overlapping structures 2 grid-like weaving, each skin overlapping structure 2 is close to no gap, and the side of the skin overlapping structure 2 is provided with a skin retractable structure 1. The skin overlapping structure is composed of a single skin overlapping, which is a multi-layer slideway structure and makes the multi-layer flexible skin completely overlap into one layer; the skin retractable structure is that the skin can be rolled in and out of the retractable structure, including rollers and the skin storage compartment, the skin overlapping structure connects the rollers.
[0020] In this embodiment, in order to realize large-area deformation, a braided structure is used to realize it. When the wing area needs to change greatly, this change is often in two direc...
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