FIELD: protective coatings.
SUBSTANCE: invention relates to materials for protecting refractory-alloy parts of gas-turbine engines against high-temperature gas corrosion and proposes refractory coating containing SiO2, B2O3, Al2O3, BaO, CaO, MgO, TiO2, Cr2O3 and SiO2-based mineral complex compound composed of, wt %: SiO2 56,25-58.05, Al2O3 34.3-35.1, CaO 1.0-1.2, MgO 1.0-1.1, K2O 2.5-2.6, Na2O 0.6-0.7, TiO2 1.6-1.8, SO3 0.15-0.25, and Fe2O3 0.8-1.0 or SiO2 32,25-40.05, Al2O3 34.3-35.1, CaO 1.0-1.2, MgO 1.0-1.1, K2O 2.5-2.6, Na2O 0.6-0.7, TiO2 1.6-1.8, SO3 0.15-0.25, Fe2O3 0.8-1.0, and SiB4 18.0-21.0, which additionally contains N2O3, P2O5, polymethyphenylsiloxane, organosilicon resin, and xylene so that coating finally contains, wt %: SiO2 20,0-36.0, B2O3 4.0-5.0, Al2O3 5.0-6.0, CaO 2.0-4.0, MgO 0.5-1.5, TiO2 1.5-2.5, Cr2O3 15.0-17.0, SiO2-based mineral complex compound 20.0-36.0, Na2O 4.0-5.0, P2O5 1.0-2.0, polymethyphenylsiloxane 0.5-0.8, organosilicon resin 11.5-13.2, and xylene 9.0-11.0. Coating is formed at ambient temperatures.
EFFECT: increased temperature resistance and adhesiveness at working temperatures above 1000оС.
3 tbl
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Authors
Dates
2004-11-10—Published
2002-11-11—Filed