| 发明名称 |
GAS TURBINE ENGINE FLOW DUCT HAVING INTEGRATED HEAT EXCHANGER |
| 摘要 |
A gas turbine engine flow duct comprising a flow duct disposed along an engine centerline of the gas turbine engine and defining a stream flow passage, and first and second rows of heat exchangers disposed along the engine centerline of the gas turbine engine and integrated in the flow duct in fluid communication with the stream flow passage of the flow duct. |
| 申请公布号 |
US2015047315(A1) |
申请公布日期 |
2015.02.19 |
| 申请号 |
US201314136262 |
申请日期 |
2013.12.20 |
| 申请人 |
Rolls-Royce North American Technologies, Inc. |
发明人 |
Snyder Douglas J. |
| 分类号 |
F02K3/115;F02C7/18 |
主分类号 |
F02K3/115 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine flow duct comprising:
a flow duct disposed along an engine centerline of the gas turbine engine and defining a stream flow passage; and first and second rows of heat exchangers disposed along the engine centerline of the gas turbine engine and integrated in the flow duct in fluid communication with the stream flow passage of the flow duct. |
| 地址 |
Indianapolis IN US |
