发明名称 |
Compressor interstage seal |
摘要 |
<p>An interstage seal (24) for a gas turbine engine includes a seal pad (30) attached to a backing strip (28). A plurality of tab springs (32) are fixedly attached to the outboard side of the strip for engaging an inner band of the supporting stator sector. <IMAGE></p> |
申请公布号 |
EP0980963(A2) |
申请公布日期 |
2000.02.23 |
申请号 |
EP19990306482 |
申请日期 |
1999.08.17 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
SCHILLING, JAN CHRISTOPHER |
分类号 |
F04D29/08;F01D11/00;F04D17/10;(IPC1-7):F01D11/00 |
主分类号 |
F04D29/08 |
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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