发明名称 Repair of gas turbine blade tip without recoating the repaired blade tip
摘要 A damaged gas turbine blade which has previously been in service, and which is made of a base metal, is furnished. Any damaged material is removed from the damaged blade tip. The damaged blade tip is weld repaired with a nickel-base superalloy that is more resistant to oxidation resistance than is the base metal in the operating environment of the tip-repaired gas turbine blade. The method does not include any step of coating a lateral surface of the repaired blade tip with a non-ceramic coating after the step of weld repairing.
申请公布号 US7587818(B2) 申请公布日期 2009.09.15
申请号 US20040022185 申请日期 2004.12.23
申请人 GENERAL ELECTRIC COMPANY 发明人 GORMAN MARK DANIEL;GROSSKLAUS, JR. WARREN DAVIS
分类号 B23P6/00;B63H1/26;C21D1/00;C21D1/09;F04D29/44 主分类号 B23P6/00
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