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COOLING SYSTEM CONFIGURATIONS FOR AN AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM
COOLING SYSTEM CONFIGURATIONS FOR AN AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM
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机译:具有混合动力系统的飞机的冷却系统配置
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摘要
A cooling system for an engine of an aircraft of a having hybrid-electric propulsion system including a nacelle body including a bottom cooling air intake disposed below a propeller hub for supplying air to an oil-air cooler, wherein the bottom cooling air intake includes a splitter dividing the bottom cooling air intake into a first channel and a second channel.
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