FIELD: engines and pumps.
SUBSTANCE: invention relates to materials which protect parts of gas turbine engines that made out of heat-resistant steels and nickel alloys against oxidation under action of high-temperature gas corrosion during operation. High-heat resistant cover, mas%: Al2O3 - 13.0-18.0, MgO - 1.0-2.5, CaO - 3.0-8.0, BaO - 5.0-9.0, TiO2 - 1.5-4.8, B2O3 - 3.5-7.6, Cr2O3 - 2.5-6.0, BaSi2O5 - 5.0-10.0, BaAl2Si2O8 - 2.0-6.5, mineral complex compound based on SiO2 - 2.5-6.0, SiO2 - the rest.
EFFECT: higher heat resistance, thermal fastness, wetting ability of the surface of samples and strength of adhesion of coating with substrate.
1 cl, 3 ex, 2 tbl
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Authors
Dates
2016-09-27—Published
2015-06-10—Filed