发明名称 Repair of gas turbine blade tip without recoating the repaired blade tip
摘要 A damaged gas turbine blade (40) 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 (50). The damaged blade tip (50) 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 (60). 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 SG123747(A1) 申请公布日期 2006.07.26
申请号 SG20050008275 申请日期 2005.12.21
申请人 GENERAL ELECTRIC COMPANY 发明人 GORMAN MARK DANIEL;GROSSKLAUS, WARREN DAVIS, JR.
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