Torsion-adaptive wing structure for large flapping wings
A wing structure and self-adaptive technology, applied in the field of aircraft, can solve the problems of shortened service life of steering gear, increased wing root moment, increased wing weight, etc., to reduce impact force, improve energy utilization, and high reliability Effect
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[0028] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.
[0029] Such as figure 1 As shown, a kind of torsional adaptive wing suitable for large flapping wings provided by the example of the present invention includes a bent wing part and a twisted wing part, wherein the bent wing part includes a bent wing upper beam 11 and a bent wing lower beam 12. Wing ribs 13, bending section support rods 14 and wing connectors 15. In the example of the present invention, in order to facilitate the fixing between the wing spar and the wing ribs, the upper beam of the bent wing adopts a square high-strength carbon fiber structure, and the upper beam of the bent wing adopts a square high-strength carbon fiber structure. The lower beam of the bent wing can be a carbon fiber structure of any shape. Two wing ribs are arranged on the bent wing, and slot holes are arranged on the rib. During the flapping process of the w...
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