FIELD: aviation.
SUBSTANCE: invention relates to anti-acing systems of aircrafts. Method for preventing the icing of the aircraft wing with the use of a laser anti-icing system is to generate directed beam (9) of laser beams. In this case, the beams of laser beam (9) are directed parallel to leading edge (10) of the aircraft wing profile or in the direction in which the rays form acute angle (17) with leading edge (10), without irradiating the outer skin of the skin.
EFFECT: invention prevents icing of the surfaces of the aircraft wing without deformation of the surface and simplifies the construction.
5 cl, 4 dwg
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