发明名称 Gas turbine engine with supplemental oil cooler airflow
摘要 A gas turbine engine (10) is provided with an oil cooler which receives cooling air from a turbo fan (14). At times when the turbo fan (14) is operating at lower speeds, the volume of cooling air is also lowered. At such times, a supplemental airflow is provided over heat exchangers (38) in the oil cooler. The supplemental airflow includes a supplemental airflow fan (42) and valve (40) for selectively controlling the supplemental airflow over the heat exchangers (38).
申请公布号 EP1669551(A2) 申请公布日期 2006.06.14
申请号 EP20050257508 申请日期 2005.12.05
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 LARKIN, MICHAEL J.;EILER, DONALD C.
分类号 F01D25/12;F01D25/18;F02C7/18 主分类号 F01D25/12
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