发明名称 Turbo air compressor
摘要 A method for operating an air-conditioning system (10) for an aircraft including receiving an available power level (25) from a control system of the aircraft, forwarding air from a first compressed air source (12;101) to an aircraft cabin (20) and forwarding air from a second compressed air source (22;103) to the aircraft cabin (20) if the available power level (25) exceeds a threshold value.
申请公布号 EP2591999(A2) 申请公布日期 2013.05.15
申请号 EP20120192142 申请日期 2012.11.09
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 BRUNO, LOUIS J.;ZYWIAK, THOMAS M.
分类号 B64D13/02;B64D13/06 主分类号 B64D13/02
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