Sharkskin-imitating resistance-reducing wing
A technology imitating sharks and wings, applied in wings, heat-reducing structures, aircraft parts, etc., can solve problems such as flight resistance and achieve the effect of reducing resistance
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specific Embodiment approach 1
[0019] The drag-reducing wing of imitation shark skin of the present embodiment, combines figure 1 As shown, its composition includes: wings 2 respectively installed on both sides of the fuselage 1, a group of speed sensors 3 are installed on the surface of the fuselage 1, a skin layer 4 is attached to the surface of each wing 2, and the surface of the skin layer 4 has A group of arc-shaped protruding ribs 5, grooves 6 are formed between two adjacent protruding ribs 5; and the protruding ribs 5 are wound on the surface of the wing 2, and the cross section of each protruding rib 5 is elliptical shape or circle, the area of each raised rib 5 cross section is about 245-628mm 2 , the distance between the midpoints of the ellipse or circle where the cross-sections of two adjacent raised ribs 5 are located is 25-40mm;
[0020] Wherein, the skin layer 4 is composed of a shape-memory polymer matrix 7 and an elastic fiber body 8 disposed inside the shape-memory polymer matrix 7 .
specific Embodiment approach 2
[0021] The difference from Embodiment 1 is that in the sharkskin-like drag-reducing wing of this embodiment, the angle between the plane of the arc formed by each raised rib 5 and the central axis of the fuselage 1 is 20-80° .
specific Embodiment approach 3
[0022] Different from Embodiment 1 or Embodiment 2, in the sharkskin-like drag-reducing wing of this embodiment, the elastic fiber body 8 disposed inside the shape-memory polymer matrix 7 is in the shape of a spiral filament.
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