| 发明名称 |
REPARATUR VON TURBINENBAUTEILEN |
| 摘要 |
Physical vapor deposition is utilized to deposit repair material on Ti alloy turbine components. In a preferred embodiment, a damaged area (30) of an airfoil leading edge is machined to produce a base surface (50), and a backing element (52) is attached to the airfoil (26) to receive the repair material which can subsequently be machined to the appropriate profile. |
| 申请公布号 |
AT410530(T) |
申请公布日期 |
2008.10.15 |
| 申请号 |
AT20040254725T |
申请日期 |
2004.08.05 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
MEMMEN, ROBERT L.;NEAL, JAMES W. |
| 分类号 |
C23C14/32;F01D5/28;B23P6/00;C22C14/00;C23C14/02;C23C14/04;C23C14/14;C23C14/16;C23C14/30;C23C14/58;F01D5/00;F01D5/12;F01D5/30;F01D25/00;F02C7/00;F04D29/34;F04D29/38 |
主分类号 |
C23C14/32 |
| 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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