FIELD: aviation; anti-icing devices.
SUBSTANCE: system for distribution and discharge of anti-icing fluid in aircraft skin contains layered skin of wing tip, having outer skin (1) and inner skin (2). Cavity (4) is formed between outer skin (1) and inner skin (2). Outer surface of the skin, both in its upper and lower parts, has zones (3) with staggered rows of holes connecting the outer surface of skin (1) and cavity (4), through which there is "sweating" of the AIF on the outer surface of skin (1). Polymer membrane (5) with capillary effect passes between skins.
EFFECT: increasing the efficiency of preventing ice formation on the outer surface of the aerodynamic contours of the aircraft wing tip.
1 cl, 3 dwg
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