发明名称 High efficiency aircraft cabin air supply cooling system
摘要 A thermal management system for an aircraft is provided. The aircraft includes a primary air conditioning system which compresses and cools outside air to create inside air. The inside air pressurizes the internal volume of the aircraft and ventilates a first object in the internal volume. An exhaust exhausts a portion of the inside air to allow more outside air to be drawn into the aircraft. A cooler cools a coolant which in turn controls temperature of at least two objects in the internal volume.
申请公布号 US2005051668(A1) 申请公布日期 2005.03.10
申请号 US20030658001 申请日期 2003.09.09
申请人 ATKEY WARREN A.;FITERMAN CHARLES J. 发明人 ATKEY WARREN A.;FITERMAN CHARLES J.
分类号 B64D13/06;(IPC1-7):B64C27/22 主分类号 B64D13/06
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