| 发明名称 |
GAS TURBINE ENGINE WITH ROTOR BORE HEATING |
| 摘要 |
A gas turbine engine has a compressor rotor with blades and a disk. A bore is defined radially inwardly of the disk. A combustor includes a burner nozzle. A tap taps air that has been combusted in the combustor section through a valve, and into the bore of the disk. A method is also disclosed. |
| 申请公布号 |
EP2959109(A4) |
申请公布日期 |
2016.06.01 |
| 申请号 |
EP20140797283 |
申请日期 |
2014.02.11 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SCHWARZ, FREDERICK M.;DUESLER, PAUL W. |
| 分类号 |
F01D5/08;F01D25/10;F02C9/16 |
主分类号 |
F01D5/08 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
