| 发明名称 |
ENGINE WITH NOSE CONE HEAT EXCHANGER AND RADIALLY OUTER DISCHARGE |
| 摘要 |
A gas turbine engine has a nose cone, a fan for delivering air into a bypass duct as bypass flow, and into a core engine to be delivered to a compressor. The nose cone includes a vent to receive air and deliver the air across a heat exchanger, which receives a fluid to be cooled. The air from the vents is delivered to an outlet downstream of the heat exchanger, such that a majority of the air being delivered to the outlet becomes part of the bypass flow. |
| 申请公布号 |
US2017122207(A1) |
申请公布日期 |
2017.05.04 |
| 申请号 |
US201514932066 |
申请日期 |
2015.11.04 |
| 申请人 |
United Technologies Corporation |
发明人 |
Suciu Gabriel L.;Chandler Jesse M. |
| 分类号 |
F02C7/14;F01D5/12;F02C7/18;F01D9/04;F02K3/06;F02C3/04 |
主分类号 |
F02C7/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
a nose cone; a fan for delivering air into a bypass duct as bypass flow, and into a core engine, to be delivered to a compressor; and said nose cone including a vent to receive air and deliver said air across a heat exchanger, said heat exchanger receiving a fluid to be cooled, and the air from the vents being delivered to an outlet downstream of the heat exchanger, such that a majority of the air being delivered to said outlet becomes part of the bypass flow. |
| 地址 |
Hartford CT US |
