Leading edge capable of improving bird impact resistance of airplane
A technology for wing leading edge and bird strike, applied in wings, aircraft parts, motor vehicles, etc., can solve problems such as skin tearing, wing leading edge deformation, front beam structure damage, etc., and achieve bird strike resistance. Improve, increase the structural rigidity, protect the effect of the beam web
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[0030] This embodiment is a bird strike-resistant wing front edge for a certain type of aircraft, including the wing leading edge skin 4, additional skin 5, front beam 3, small front beam 2, multiple front ribs 6, multiple rear Rib 7 and two side ribs 2. among them:
[0031] The two side ribs 1 are respectively fixed on the upper surface of the two ends of the front beam 3. The small front beam 2 is located above the two side ribs, and the two ends of the small front beam are riveted to the inner surfaces of the two side ribs respectively. The rear ribs 7 are arranged between the upper surface of the front beam 3 and the lower surface of the small front beam 2, and the rear ribs are inclined to form a "V" or inverted shape between two adjacent rear ribs. "V"-shaped included angle; the angles of the included angles are all 60°. A plurality of front ribs 6 are uniformly distributed on the upper surface of the small front beam 2. The vertex of each front rib 6 and the vertex of ...
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