Invention Grant
US07861512B2 Turbofan bypass duct air cooled fluid cooler installation 有权
涡轮风扇旁路管风冷流体冷却器安装

Turbofan bypass duct air cooled fluid cooler installation
Abstract:
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.
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