发明名称 Supplemental oil cooler airflow for gas turbine engine
摘要 A gas turbine engine is provided with an oil cooler which receives cooling air from a turbo fan. At times when the turbo fan is operating at lower speeds, the volume of cooling air is also lowered. At such times, a supplemental airflow is provided over heat exchangers in the oil cooler. The supplemental airflow includes a supplemental airflow fan and valve for selectively controlling the supplemental airflow over the heat exchangers.
申请公布号 US7454894(B2) 申请公布日期 2008.11.25
申请号 US20040006306 申请日期 2004.12.07
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 LARKIN MICHAEL J.;EILER DONALD C.
分类号 F02C7/06;F02K3/06 主分类号 F02C7/06
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