| 发明名称 |
Bleed deflector for a gas turbine engine |
| 摘要 |
The present invention relates to a bleed deflector for a gas turbine engine. The bleed deflector comprises an inlet portion for receiving bleed air from the engine, a perforated top plate for discharging the bleed air into a duct, and an aerodynamically shaped strut for positioning the perforated top plate above an inner wall of the duct to allow dilution air to flow beneath the top plate.
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| 申请公布号 |
US2003068223(A1) |
申请公布日期 |
2003.04.10 |
| 申请号 |
US20010971404 |
申请日期 |
2001.10.04 |
| 申请人 |
NIKKANEN JOHN P.;MIGLIARO EDWARD F.;ZYSMAN STEVEN H.;AVIS THOMAS B. |
发明人 |
NIKKANEN JOHN P.;MIGLIARO EDWARD F.;ZYSMAN STEVEN H.;AVIS THOMAS B. |
| 分类号 |
F01D25/00;F01D9/06;F02C9/18;F02K3/04;F02K3/075;(IPC1-7):F01D17/00 |
主分类号 |
F01D25/00 |
| 代理机构 |
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