| 发明名称 |
ACTIVE CLEARANCE CONTROL FOR GAS TURBINE ENGINE |
| 摘要 |
A gas turbine engine includes a conduit that is configured to direct a fluid to at least one manifold that is adjacent to a turbine section. A first intake is in fluid communication with the conduit. A second intake is in fluid communication with the conduit. A valve is configured to selectively direct a fluid from at least one of the first intake and the second intake. |
| 申请公布号 |
US2017074112(A1) |
申请公布日期 |
2017.03.16 |
| 申请号 |
US201515123940 |
申请日期 |
2015.03.23 |
| 申请人 |
United Technologies Corporation |
发明人 |
Philbrick Graham Ryan;Lagueux Ken |
| 分类号 |
F01D17/10;F01D25/24;F01D17/14;F02K3/06;F01D21/00 |
主分类号 |
F01D17/10 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
a conduit configured to direct a fluid to at least one manifold adjacent a turbine section; a first intake in fluid communication with the conduit; a second intake in fluid communication with the conduit; and a valve configured to selectively direct a fluid from at least one of the first intake and the second intake. |
| 地址 |
Farmington CT US |
