发明名称 TURBO AIR COMPRESSOR
摘要 A method for operating an air-conditioning system for an aircraft including receiving an available power level from a control system of the aircraft, forwarding air from a first compressed air source to an aircraft cabin and forwarding air from a second compressed air source to the aircraft cabin if the available power level exceeds a threshold value.
申请公布号 US2013118190(A1) 申请公布日期 2013.05.16
申请号 US201113294906 申请日期 2011.11.11
申请人 BRUNO LOUIS J.;ZYWIAK THOMAS M.;HAMILTON SUNDSTRAND CORPORATION 发明人 BRUNO LOUIS J.;ZYWIAK THOMAS M.
分类号 F25B9/00 主分类号 F25B9/00
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