发明名称 Air cooling system with liquid to air heat exchanger
摘要 An air cooling system includes a heat exchanger (12), an inlet duct (42), an outlet duct (46), and an outlet header (34). The inlet duct (42) is fluidly connected to the heat exchanger (12) and is configured to direct relatively warm air (24) from a cabin (14) of an aircraft (10) into the heat exchanger (12). The outlet duct (46) is fluidly connected to the heat exchanger (12) and configured to direct relatively cool air (26) out of the heat exchanger (12) and back to the cabin (14). The outlet header (34) is located between the heat exchanger (12) and the outlet duct (46). The outlet header (34) has a shape configured to collect water (32) from the cool air (26).
申请公布号 EP2479108(A2) 申请公布日期 2012.07.25
申请号 EP20110195111 申请日期 2011.12.22
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 ARMY, STEVEN D.;MCCOLGAN, CHARLES J.
分类号 B64D13/00;B64D13/06 主分类号 B64D13/00
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