发明名称 |
Verfahren zur Aufbereitung und Verfahren zur Herstellung einer Turbinenschaufel |
摘要 |
A method of reconditioning a rotating blade (1) with a shroud (8) following the operation in a gas turbine, comprises the application of a barrier (14) placed on the edge of the shroud (8) facing the edge of a shroud (8) of an adjacent blade having creep deformation. The barrier (14) prevents hot gas ingestion into a shroud cavity (10). It is pre-fabricated or built-up layer-by-layer by means of welding or laser cladding or other known methods. Additionally, the mass of the shroud (8) is reduced in order to re-establish the initial mass of the shroud. A thermal barrier coating (15) is additionally applied to the surfaces of the shroud (8) that are exposed to the hot gas of the turbine. The method significantly increases the lifetime of the blade (1). <IMAGE> |
申请公布号 |
DE602004003757(T2) |
申请公布日期 |
2007.10.11 |
申请号 |
DE20046003757T |
申请日期 |
2004.07.14 |
申请人 |
ALSTOM TECHNOLOGY LTD. |
发明人 |
BOEGLI, ANDREAS;RITCHIE, JAMES GEORGE;SLOWIK, SLAWOMIR;STUESSI, HEINRICH |
分类号 |
F01D5/00;F01D5/22 |
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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