FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to anti-icing system at nacelle panel 22. Proposed method comprises the following stages: a) positioning device 35 arranged at outer skin 24 is used to position screen composed of resistive elements around opening or openings. b) appropriate means is used to apply the screen of resistive elements to area defined at step (a) to form anti-icing system. c) surface coat is applied on produced anti-icing system.
EFFECT: higher efficiency of deicing.
12 cl, 14 dwg
