发明名称 |
COOLED GAS TURBINE ENGINE MEMBER |
摘要 |
<p>A gas turbine engine is disclosed having a vane disposed in a flow path of a gas turbine engine component, for example a gas turbine engine compressor. The vane is in thermal contact with a heat tube that extends through a wall of the engine component and into a space in which a thermal fluid passes. The thermal fluid can be at a different temperature than the vane such that heat is transferred between the two. In one embodiment the vane forms part of an intercooler for a compressor of the gas turbine engine. The vane can have a fin disposed at the end of the heat tube to facilitate a heat transfer.</p> |
申请公布号 |
WO2012088493(A1) |
申请公布日期 |
2012.06.28 |
申请号 |
WO2011US67115 |
申请日期 |
2011.12.23 |
申请人 |
ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES INC.;CASWELL, MARK, OWEN |
发明人 |
CASWELL, MARK, OWEN |
分类号 |
F02K99/00 |
主分类号 |
F02K99/00 |
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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