发明名称 |
Seal apparatus |
摘要 |
A seal for a gas turbine engine comprises an internal abradable lining and two interconnecting flanges. The flanges form a U-shaped channel therebetween for the insertion of radially inwardly directed features on the inner ends of a plurality of stator vanes. One or both flanges support the abradable lining via a land.
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申请公布号 |
US2004169122(A1) |
申请公布日期 |
2004.09.02 |
申请号 |
US20030684491 |
申请日期 |
2003.10.15 |
申请人 |
DODD ALEC G.;BURFORD COLIN J. |
发明人 |
DODD ALEC G.;BURFORD COLIN J. |
分类号 |
F01D11/12;(IPC1-7):F16M1/00 |
主分类号 |
F01D11/12 |
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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