发明名称 Turbofan bypass duct air cooled fluid cooler installation
摘要 A cooling apparatus for cooling a fluid in a bypass gas turbine engine comprises a heat exchanger disposed within a bypass duct and accommodated by a sub-passage defined by a flow divider affixed to an annular wall of the bypass duct. The sub-passage defines an open upstream end and an open downstream end to direct a portion of the bypass air flow to pass therethrough.
申请公布号 US2008053059(A1) 申请公布日期 2008.03.06
申请号 US20060511419 申请日期 2006.08.29
申请人 PRATT & WHITNEY CANADA CORP. 发明人 OLVER BRYAN;CIAMPA ALESSANDRO;MARRANO ROBERTO;TREPANIER RICHARD;LAMARRE SYLVAIN;BERNARD MARTIN;GERMAIN PATRICK
分类号 F02K3/02 主分类号 F02K3/02
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