| 发明名称 |
Process for repairing turbine components |
| 摘要 |
<p>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.</p> |
| 申请公布号 |
EP1486286(A2) |
申请公布日期 |
2004.12.15 |
| 申请号 |
EP20040253494 |
申请日期 |
2004.06.11 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
SUBRAMANIAN, PAZHAYANNUR RAMANATHAN;CRETEGNY, LAURENT;RUDD, JAMES ANTHONY |
| 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):B23P6/00 |
主分类号 |
F01D25/00 |
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