发明名称 Method for repairing a turbine nozzle segment
摘要 A method for repairing a turbine nozzle segment includes providing a turbine nozzle segment having an enclosure with an integral discourager, removing the enclosure and/or the discourager from the turbine nozzle segment and attaching a new enclosure ad/or discourager to the turbine nozzle segment.
申请公布号 US8296945(B2) 申请公布日期 2012.10.30
申请号 US20070967178 申请日期 2007.12.29
申请人 BROOMER MARK;CORREIA VICTOR HUGO SILVA;GENERAL ELECTRIC COMPANY 发明人 BROOMER MARK;CORREIA VICTOR HUGO SILVA
分类号 B23P6/00 主分类号 B23P6/00
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