发明名称 |
DEVICE FOR COOLING OIL FOR A TURBINE ENGINE |
摘要 |
The invention relates to a device (11) for cooling oil for a turbine engine, such as an aircraft turbofan or turboprop, characterised in that it comprises a duct (12) for circulating a flow of cold air (F1); means for injecting oil (16) into the duct; and means (19) for extracting the oil mixed with the flow of cold air (F1), located in the duct (12), downstream from the injection means (16). |
申请公布号 |
WO2015004394(A1) |
申请公布日期 |
2015.01.15 |
申请号 |
WO2014FR51775 |
申请日期 |
2014.07.10 |
申请人 |
SNECMA |
发明人 |
MULLER, JEAN-LOUIS;MOUTON, PIERRE, CHARLES |
分类号 |
F01D25/12;F02C7/06;F02C7/14 |
主分类号 |
F01D25/12 |
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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