| 发明名称 |
Method and apparatus for enhancing compressor performance |
| 摘要 |
The present invention provides a non-axisymmetric flow member disposed in a duct of a gas turbine engine. The flow member narrows the area aft of a vane to reduce the cross sectional area through which a wake from the vane traverses. |
| 申请公布号 |
US2012014776(A1) |
申请公布日期 |
2012.01.19 |
| 申请号 |
US20070789688 |
申请日期 |
2007.04.25 |
| 申请人 |
FULAYTER ROY;WELLBORN STEVE |
发明人 |
FULAYTER ROY;WELLBORN STEVE |
| 分类号 |
F01D9/02 |
主分类号 |
F01D9/02 |
| 代理机构 |
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代理人 |
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