FIELD: heating.
SUBSTANCE: invention relates to heated transparent elements. The transparent element of an aircraft has a heating element for removing condensate, snow and ice from the outer surface of the transparent element. The heating element comprises a pair of spaced apart parallel buses, and the ends of the buses are offset relative to each other, and the coating which comprises several spaced apart segments of electrically conductive coatings electrically connected to the buses. The ratio of the main diagonal to the secondary diagonal is in the range from 1 to 1.25 in order to heat more uniformly the coating and the outer surface of the transparent element.
EFFECT: increased efficiency of heating.
15 cl, 9 dwg
