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 (80) of the repaired blade tip (62) with a non-ceramic coating after the step of weld repairing.
申请公布号 CA2530247(C) 申请公布日期 2014.08.19
申请号 CA20052530247 申请日期 2005.12.15
申请人 GENERAL ELECTRIC COMPANY 发明人 GORMAN, MARK DANIEL;GROSSKLAUS, WARREN DAVIS, JR.
分类号 F01D5/28;B23P6/00;C22C19/05;C22F1/10 主分类号 F01D5/28
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