Leading edge of anti-bird strike aircraft empennage with single inclined plate
A tail, swash plate technology, applied in the directions of wings, aircraft stability, wing shape, etc., can solve the problems of heavy structure, complicated processing and maintenance, etc., and achieve the effect of improving stiffness and anti-bird strike performance.
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[0037] This embodiment is used for the anti-bird strike aircraft empennage leading edge of a certain type of aircraft, including empennage leading edge skin 1, single inclined plate 6, multiple ribs 7, front beam web 9 and two front beam edge strips 8, in:
[0038] The plurality of ribs 7 are fixed on the surface of the front edge side of the front beam web 9 along the span direction, and are perpendicular to the front beam web 9; the distance between the ribs is 200-300mm, so as to take into account the structural weight and structure stiffness. The single-slope plate 6 is fixed on the folded edge of the upper hypotenuse of each rib, and an included angle α of 50-60° is formed between the surface of the single-slope plate and the surface of the front beam web; the rib The flanging of the straight edge is fixed on the surface of the front beam web 9 by rivets. The leading edge skin 1 of the empennage covers and is fixed on the surfaces of the monoslope plate 6 and the front ...
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