FIELD: unmanned aerial vehicles.
SUBSTANCE: invention is related in particular to IAV wings, equipped with means to prevent icing. Aircraft wing contains upper and lower shaping walls made of polymer composite material. The wing also contains a screen, an inductor and a source of pulsed voltage connected to the inductor. The screen is located in the body of the upper shaping wall, being introduced into the body of the upper shaping wall in the process of its moulding. The inductor is fixed on the lower shaping wall from the side of its inner surface. When said source generates a voltage pulse, the inductor is able to act on the screen in the direction of the outer surface of the upper shaping wall.
EFFECT: reduction of the vertical size of the wing, reduction of the weight of the wing and simplification of its manufacturing technology are achieved.
10 cl, 2 dwg
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