发明名称 |
Stator vane assembly for a gas turbine engine |
摘要 |
<p>A low-pressure compressor exit stator assembly for a gas turbine includes a multiple of vanes (26) mounted between a full hoop outer shroud (34) and an inner shroud (36). The outer shroud (34) and inner shroud (36) are mounted to the intermediate case structure (28). A seal (38) is located between the outer shroud (34) and a bleed duct structure (30) to accommodate thermal growth mismatch.</p> |
申请公布号 |
EP1544415(B1) |
申请公布日期 |
2012.12.12 |
申请号 |
EP20040257870 |
申请日期 |
2004.12.16 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SERVADIO, MICHAEL A.;RICHARDSON, R. BRIAN |
分类号 |
F02C9/18;F01D5/00;F01D9/02;F01D9/04;F01D25/00;F01D25/24;F04D29/54;F04D29/64 |
主分类号 |
F02C9/18 |
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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