发明名称 METHOD OF REPAIRING TURBINE COMPONENTS
摘要 PROBLEM TO BE SOLVED: To provide a method to repair damaged components of a turbine. SOLUTION: The method to repair damaged components of the turbine consists of three processes, the first process to cover the surface of any turbine component including a damaged part with a preliminary molding of solder, the second process to fix the preliminary molding of solder to the surface, and the third process to heat the turbine component to the proper temperature for formation of a brazed joint between the solder and the turbine component. The invention also includes a repaired turbine component according to this method. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2005003003(A) 申请公布日期 2005.01.06
申请号 JP20040175051 申请日期 2004.06.14
申请人 GENERAL ELECTRIC CO 发明人 SUBRAMANIAN PAZHAYANNUR RAMANATHAN;RUUD JAMES ANTHONY;CRETEGNY LAURENT
分类号 F01D25/00;B23K1/00;B23K1/008;B23K1/19;B23K1/20;B23K11/00;B23K31/00;B23K31/02;B23P6/00;F01D19/02;F01D25/28;F02C7/00;(IPC1-7):F02C7/00 主分类号 F01D25/00
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