| 发明名称 | Bore cavity thermal conditioning system | ||
| 摘要 | A gas turbine engine includes a rotor having at least one rotor bore cavity and a heat exchanger. The heat exchanger is fluidically connected to a conditioning air source and to the rotor bore cavity for flowing air from the conditioning air source to the rotor bore cavity. The heat exchanger is also fluidically connected to a hot fluid source and a cool fluid source for selectively heating and cooling conditioning air flowing to the rotor bore cavity. | ||
| 申请公布号 | US9188009(B2) | 申请公布日期 | 2015.11.17 |
| 申请号 | US201213663665 | 申请日期 | 2012.10.30 |
| 申请人 | United Technologies Corporation | 发明人 | Yilmaz Cagdas;Coderre Paul E. |
| 分类号 | F01D5/08;F02C7/12 | 主分类号 | F01D5/08 |
| 代理机构 | Kinney & Lange, P.A. | 代理人 | Kinney & Lange, P.A. |
| 主权项 | 1. A gas turbine engine comprising: a rotor comprising at least one rotor bore cavity; and a heat exchanger fluidically connected to a conditioning air source and to the rotor bore cavity for flowing air from the conditioning air source to the rotor bore cavity, wherein the heat exchanger is also fluidically connected to a hot fluid source and a cool fluid source for selectively heating and cooling conditioning air flowing to the rotor bore cavity. | ||
| 地址 | Hartford CT US | ||