| 发明名称 |
CENTRIFUGAL COMPRESSOR WITH AXIAL IMPELLER EXIT |
| 摘要 |
<p>A gas turbine engine includes a centrifugal compressor having an improved impeller structure. The impeller structure includes a near axial discharge configuration thus reducing the overall size of the envelop surrounding the compressor assembly. The impeller structure may have axial exit vanes.</p> |
| 申请公布号 |
WO2014149099(A1) |
申请公布日期 |
2014.09.25 |
| 申请号 |
WO2013US75501 |
申请日期 |
2013.12.16 |
| 申请人 |
ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC. |
发明人 |
BRYAN, WILLIAM, B. |
| 分类号 |
F04D17/02;F01D5/28;F02C3/08;F04D29/28;F04D29/30 |
主分类号 |
F04D17/02 |
| 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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