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(A2) |
申请公布日期 |
2015.12.30 |
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 |
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代理人 |
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主权项 |
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地址 |
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