发明名称 |
Methods and systems for gas turbine engine bleed scoops |
摘要 |
A gas turbine engine includes a compressor including a casing and a stator assembly. The casing extends around the stator assembly, the stator assembly including a plurality of stator vanes, and a plurality of bleed scoops. Adjacent stator vanes define a static high-pressure region, the bleed scoops formed at least partially within the high pressure region.
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申请公布号 |
US2003033815(A1) |
申请公布日期 |
2003.02.20 |
申请号 |
US20010932585 |
申请日期 |
2001.08.17 |
申请人 |
PROCTOR ROBERT;MONTGOMERY JULIUS JOHN;EPSTEIN MICHAEL JAY;BARBE ROGER OWEN;SAM HAI BUU;OGZEWALLA JAMES BERNAR;KEMP ANDREW DAVID;DOLORESCO BRYAN KEITH |
发明人 |
PROCTOR ROBERT;MONTGOMERY JULIUS JOHN;EPSTEIN MICHAEL JAY;BARBE ROGER OWEN;SAM HAI BUU;OGZEWALLA JAMES BERNAR;KEMP ANDREW DAVID;DOLORESCO BRYAN KEITH |
分类号 |
F01D9/04;F01D17/10;F02C6/08;F04D29/54;(IPC1-7):F02C6/08 |
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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