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Method for producing a gas turbine component and protective coating on a superalloy metal substrate, with a protective coating
Method for producing a gas turbine component and protective coating on a superalloy metal substrate, with a protective coating
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机译:在超合金金属基底上生产燃气轮机部件和保护涂层的方法,带有保护涂层
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摘要
Forming a thermal protection coating on a superalloy substrate comprises forming a bonding sublayer comprising an intermetallic compound of alpha-nickel-platinum and aluminum, and anchoring a ceramic coating to an alumina film on the sublayer. - An INDEPENDENT CLAIM is also included for a gas turbine part comprises a superalloy substrate, a bonding sublayer as above and an external ceramic coating anchored to an alumina film formed on the sublayer.
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