发明名称 |
Gas turbine engine with air and fuel cooling system |
摘要 |
A gas turbine engine is provided with a first heat exchanger associated with a cooling air flow to deliver cooling air to a turbine section. A second heat exchanger is associated with a fuel supply line for delivering fuel into a combustion section. An intermediate fluid cools air at the first heat exchanger and heats fuel at the second heat exchanger.
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申请公布号 |
US8127547(B2) |
申请公布日期 |
2012.03.06 |
申请号 |
US20070759315 |
申请日期 |
2007.06.07 |
申请人 |
NORRIS JAMES W.;BERRYANN ANDREW P.;UNITED TECHNOLOGIES CORPORATION |
发明人 |
NORRIS JAMES W.;BERRYANN ANDREW P. |
分类号 |
F02C1/00 |
主分类号 |
F02C1/00 |
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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