FIELD: devices for fuel combustion.
SUBSTANCE: invention relates to ceramic tile for lining of combustion chamber of, in particular, gas turbines. Ceramic tile for lining of combustion chambers of, in particular, gas turbines comprises base layer, made from ceramic material, e.g. alumina or alumina-mullite, and coating, which is applied, at least on one side of base layer; coating is multilayer ceramic coating, containing at least one external layer made from alumina or ceramic material containing alumina, and at least one intermediate layer located between outer layer and base layer and made from ceramic material, contained mullite and preferably mullite or alumina-mullite.
EFFECT: invention provides higher resistance of tiles to high temperatures, corrosion and mechanical loads.
11 cl, 1 dwg
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