发明名称 |
COOLING SYSTEMS FOR GAS TURBINE ENGINES |
摘要 |
An air-oil cooler for a gas turbine engine includes an air cooling structure and a lubricant channel. The lubricant channel extends between a lubricant inlet and a lubricant inlet and is bounded by the air cooling structure. The air cooling structure has an arcuate shape for circumferentially spanning a portion of a gas turbine engine core. |
申请公布号 |
EP3094845(A1) |
申请公布日期 |
2016.11.23 |
申请号 |
EP20140878605 |
申请日期 |
2014.12.22 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
WEINER, RICHARD ALAN |
分类号 |
F02C7/14;F01D25/12;F01D25/18;F02C7/06;F02C7/18 |
主分类号 |
F02C7/14 |
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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