发明名称 |
Protecting a surface of a nickel-base article with a corrosion-resistant aluminum-alloy layer |
摘要 |
<p>A surface of a nickel-base article such as an internal surface (36) of a gas turbine airfoil (22) is protected with a protective layer (40) of aluminum and at least one other element. To form the protective layer (40), a donor alloy is contacted to the protected surface of the article, and simultaneously the article and the donor alloy are heated to a coating temperature that is greater than about 0.7 of the absolute solidus temperature of the donor alloy but is such that the donor alloy remains in the form of a condensed phase contacting the protected surface of the article. The donor alloy is thereafter interdiffused into the protected surface of the article. <IMAGE></p> |
申请公布号 |
EP1199377(A2) |
申请公布日期 |
2002.04.24 |
申请号 |
EP20010308794 |
申请日期 |
2001.10.16 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
PFAENDTNER, JEFFREY ALLAN;RIGNEY, JOSEPH DAVID;WEIMER, MICHAEL JAMES |
分类号 |
C23C26/00;B22F7/04;C22C19/03;C22C21/00;C23C10/18;C23C10/26;C23C10/30;C23C10/48;C23C10/52;C23C10/56;C23C24/08;C23C28/00;(IPC1-7):C23C10/04;C23C10/28 |
主分类号 |
C23C26/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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