发明名称 |
PROCESS FOR REPAIRING TURBINE COMPONENTS |
摘要 |
A process for repairing a turbine component comprises overlaying a preform of a brazing material onto a surface of the turbine component, wherein the surface comprises a damaged portion; securing the preform of a brazing material to the surface; and heating the turbine component to a temperature effective to form a brazed joint between the brazing material and the turbine component. Also disclosed is a repaired turbine component repaired by the process.
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申请公布号 |
US2006117562(A1) |
申请公布日期 |
2006.06.08 |
申请号 |
US20030459805 |
申请日期 |
2003.06.13 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
SUBRAMANIAN PAZHAYANNUR R.;RUUD JAMES A.;CRETEGNY LAURENT |
分类号 |
B23P6/00;F01D25/00;B23K1/00;B23K1/008;B23K1/19;B23K1/20;B23K11/00;B23K31/00;B23K31/02;F01D19/02;F01D25/28;F02C7/00 |
主分类号 |
B23P6/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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