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Combined Pump system for size reduction of thermal management heat exchangers and optimized ventilation to the aircraft cabin
Combined Pump system for size reduction of thermal management heat exchangers and optimized ventilation to the aircraft cabin
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机译:组合式泵系统可减小热管理热交换器的尺寸并优化机舱通风
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摘要
A compression pump (128) for an engine (100) is provided. The pump (128) may include a first impeller (136) operatively coupled to a main shaft (108) of the engine (100), a first inlet (144) configured to at least partially receive bypass airflow and a first outlet (148) configured to direct compressed air to a thermal management system (130).
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