发明名称 |
Turbine nozzle segment and method of repairing same |
摘要 |
A method for repairing a turbine nozzle segment having at least two vanes disposed between outer and inner bands includes the steps of separating the nozzle segment into a first singlet containing a repairable vane and a second singlet containing a non-repairable vane, and joining the first singlet to a newly manufactured singlet having a configuration that is similar to the second singlet.
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申请公布号 |
US2003215329(A1) |
申请公布日期 |
2003.11.20 |
申请号 |
US20010828019 |
申请日期 |
2001.04.06 |
申请人 |
CADDELL JAMES W.;CALDWELL JAMES M. |
发明人 |
CADDELL JAMES W.;CALDWELL JAMES M. |
分类号 |
F01D9/04;B23P6/00;F01D5/00;F02C7/00;F04D29/00;(IPC1-7):F01D1/02 |
主分类号 |
F01D9/04 |
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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