| 发明名称 |
METHOD AND ASSEMBLY FOR REDUCING SECONDARY HEAT IN A GAS TURBINE ENGINE |
| 摘要 |
A turbine section (28) includes a rotor assembly (62) which includes an internal cooling passage (160,162). A segmented seal (102) is adjacent the rotor assembly (62) and includes a fluid passage that is in fluid communication with the internal cooling passage (160,162). |
| 申请公布号 |
EP3000966(A1) |
申请公布日期 |
2016.03.30 |
| 申请号 |
EP20150186522 |
申请日期 |
2015.09.23 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCUI, GABRIEL L.;MERRY, BRIAN D.;HILL, JAMES D.;ZELESKY, MARK F. |
| 分类号 |
F01D5/06;F01D5/18;F01D11/00 |
主分类号 |
F01D5/06 |
| 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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