Bistable wing of a water-air amphibious vehicle
A bistable, aircraft technology, applied in the field of aircraft wings, can solve problems such as inability to improve aerodynamic performance
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[0012] The technical solutions of the present invention will be further described below with reference to the accompanying drawings and specific embodiments.
[0013] see figure 1 and figure 2 It is stated that a bistable wing of an amphibious aircraft includes a wing rib 1 and a bistable structure; the longitudinal section of the wing rib 1 adopts a NACA supercritical airfoil, and the leading edge and the rear of the wing rib 1 An elastic rod 3 is connected between the edges; the bistable structure includes a quadrilateral link mechanism 2-1 and two pneumatic muscle actuators 2-2; a pneumatic link mechanism 2-1 is installed between the opposite corners The muscle driver 2-2, one vertex of the quadrilateral link mechanism 2-1 is mounted on the wing rib 1, the other vertex of the quadrilateral linkage mechanism 2-1 opposite to the one vertex is mounted on the elastic rod 3, and the two The pneumatic muscle actuators 2-2 are located in the same vertical plane and arranged ver...
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