FIELD: aircrafts.
SUBSTANCE: invention relates to means of protecting surfaces of structures against icing and can be used in electric pulse and vibration-pulse anti-icing systems of aircraft. Electric pulse system for removal of ice formation from skin of aircraft aggregates includes at least two inductors connected to source of pulse current and attached to brackets in inner cavity of aircraft unit. At that, the first bracket is rigidly connected to one part of the skin, and the second bracket is connected to the opposite skin part and is located opposite to the first bracket. Axis of the inductor attached to the first bracket is an extension of the axis of the inductor attached to the second bracket.
EFFECT: increased efficiency of device operation due to increased efficiency at simultaneous increase of aircraft device service life.
1 cl, 3 dwg
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