发明名称 REPAIR OF GAS TURBINE BLADE TIP WITHOUT RECOATING THE REPAIRED BLADE TIP
摘要 <p>REPAIR OF GAS TURBINE BLADE TIP WITHOUT RECOATING THE REPAIRED BLADE TIP 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.</p>
申请公布号 SG144158(A1) 申请公布日期 2008.07.29
申请号 SG20080045874 申请日期 2005.12.21
申请人 GENERAL ELECTRIC COMPANY 发明人 GORMAN, MARK DANIEL;GROSSKLAUS, JR., WARREN DAVIS
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