FIELD: glass.
SUBSTANCE: invention relates to anti-icing glass used in aviation, on seacraft, or on railway transport. The technical result is achieved by the anti-icing glass or a part thereof located fully in the installed position on one side of the plane of symmetry of the body of an aerial, water or land-based vehicle, containing a transparent conductive layer of heterogeneous thickness, ensuring the differentiated heating power over the entire surface of the multilayer glass so as to direct maximum power to the part of the surface with maximal heat losses.
EFFECT: possibility of reducing the energy for managing icing and reducing the weight of the electricity-generating means due to the provided intentional heterogeneous heating of the glass.
6 cl, 2 dwg
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