发明名称 Aircraft air conditioning system and method of operating an aircraft air conditioning system
摘要 <p>A throttle (TCV C) varies the airflow through a first line (10). An electronic control unit (ECU) operates in first and/or second modes. In the first, when the flow is increased by the throttle (TCV H) in the bypass line (20), a reduction of flow is effected in the first line (10) by throttle (TCV C), and vice versa. In the second mode, throughput increase is caused in the bypass line (20) by throttle (TCV H) and throttle (TCV C) in the first line, or a reduction of throughput is caused by the throttle (TCV H) in the bypass line (20) and the throttle (TCV C) in the first line. An independent claim is included for the corresponding method of operation.</p>
申请公布号 EP1880939(A1) 申请公布日期 2008.01.23
申请号 EP20060016265 申请日期 2006.08.03
申请人 LIEBHERR-AEROSPACE LINDENBERG GMBH 发明人 VOEGEL, FRANZ MARTIN
分类号 B64D13/06 主分类号 B64D13/06
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