发明名称 |
Method for repairing a turbine blade |
摘要 |
<p>The method involves attaching an end replacement piece (34) at an end area (30). The end replacement piece is provided with a form recess (42) in an area of its contact surface (36) for the end area. The end replacement piece is welded at the end area. Place or origin (38) of a crack formation is determined in the end area. The form recess is attached in the contact surface in a zone, which corresponds with the place of origin.</p> |
申请公布号 |
EP1914382(A1) |
申请公布日期 |
2008.04.23 |
申请号 |
EP20060022061 |
申请日期 |
2006.10.20 |
申请人 |
SIEMENS AKTIENGESELLSCHAFT |
发明人 |
AHMAD, FATHI;DANKERT, MICHAEL, DR. |
分类号 |
F01D5/00;B23P6/00;B23P6/04 |
主分类号 |
F01D5/00 |
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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