A folding self-locking device for UAV wings
A technology of wing folding and self-locking device, which is applied to the fuselage, aircraft parts, aircraft control and other directions, can solve the problems of not reducing the load capacity of the wing surface, increasing the design requirements of the wing surface folding, and reducing the field area of the UAV. To achieve the effect of simple structure, good load characteristics and low weight
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[0023] The present invention will be further described below in conjunction with specific embodiments. The exemplary embodiments and descriptions of the present invention are used to explain the present invention, but not as a limitation to the present invention.
[0024] The working principle of the present invention is set forth in detail below: the fixed wing 21 and the foldable wing 22 are hinged together by a rotating shaft, the mounting plate 1 is fixedly installed on the fixed wing 21, and the fixed plate 4 is fixedly installed on the foldable machine on wing 22.
[0025] When unfolded after being folded, the small motor 10 simultaneously drives the small spur gear 8 and the small helical gear 7 to move. At this time, the helical gear 5 is driven to rotate on the rotating circle 303 of the locking plate 3. The gear 5 drives the locking plate 3 to rotate through the top wire 6, and then drives the fixed plate 4 to rotate. When the helical gear 5 rotates to 180 degrees, t...
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