| 发明名称 |
CENTRIFUGAL COMPRESSOR WITH BLEED FLOW SPLITTER FOR A GAS TURBINE ENGINE |
| 摘要 |
An impeller includes a plurality of vanes formed around a hub, each of the plurality of vanes defines an offset between a leading edge and a trailing edge.
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| 申请公布号 |
US2012102969(A1) |
申请公布日期 |
2012.05.03 |
| 申请号 |
US20100914947 |
申请日期 |
2010.10.28 |
| 申请人 |
WAGNER JOEL H.;MAGGE SHANKAR S.;SANTELER KEITH A. |
发明人 |
WAGNER JOEL H.;MAGGE SHANKAR S.;SANTELER KEITH A. |
| 分类号 |
F02C6/08;F04D29/28 |
主分类号 |
F02C6/08 |
| 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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