| 发明名称 |
TURBINE NOZZLE SEGMENT AND METHOD FOR REPAIRING A TURBINE NOZZLE SEGMENT |
| 摘要 |
<p>A turbine nozzle segment (119) includes a first band (118), an airfoil (120) extending from the first band and a support attached to the first band. The support may have a plurality of circumferentially spaced apart tabs (130).</p> |
| 申请公布号 |
CA2709932(A1) |
申请公布日期 |
2009.07.09 |
| 申请号 |
CA20082709932 |
申请日期 |
2008.12.08 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
MORGAN, CLIVE ANDREW;HEFFRON, TODD STEPHEN;FONSEKA, SANJEEWA THUSITHA;GRIFFITHS, PETER ROBERT |
| 分类号 |
F01D9/04;F01D5/00;F01D11/00;F02C7/28 |
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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