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 代理人
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