A foldable wing flapping wing coupled with the design configuration of the aircraft

2015 
The present invention discloses a foldable wing flapping wing coupled with the design configuration of the aircraft, flapping wing leading from the inside, the outer rod-like structure of three sections connected as a foldable lever by the flapping hinge, the flapping flight expand rectilinear rod drive flapping wing flapping up and down to generate lift and thrust, after landing flutter rod folded into a "U" shape, wherein the size of the aircraft significantly reduced; both fixed-wing structure of shell lightweight shell structure, flight expand positioned above the wing flapping, wing play the role of the lifting surface, effectively enhance the aerodynamic efficiency of the aircraft, and in the flutter lever folded in a "U" shape, followed by both sides of the shell structure composed of a solid tight Collapse surrounded by half-shell structure, the rods and the aircraft flutter folded in inside the other cover member, while reducing the space occupied by the aircraft, greatly enhance the overall safety of the aircraft, easy storage and transportation.
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