| 摘要 |
<p>A system for cooling an aircraft zone includes a mixing chamber (18) which is connected to an air-conditioning assembly (12a, 12b) for making cool air available and/or to a recirculated-air conveying device (20a, 20b) for supplying recirculated air into the mixing chamber (18). The system (10) further includes an aircraft-side air-distribution system (23) which includes at least one line (32) connecting the mixing chamber (18) to the aircraft zone to be cooled and also at least one line (28a, 28b) that is connectable to an aircraft-external air-generating assembly (26a, 26b, 26c, 26d) in order to route air made available by the aircraft-external air-generating assembly (26a, 26b, 26c, 26d) into the aircraft-side air-distribution system (23). The system (10) further includes a detection device (34) for detecting a parameter indicating an operating state in the aircraft-side air-distribution system (23) and/or in the mixing chamber (18) and also a control unit (42) which is set up to receive and evaluate signals made available by the detection device (34) and, when the system (10) is connected to the aircraft-external air-generating assembly (26a, 26b, 26c, 26d), to control the operation of the aircraft-external air-generating assembly (26a, 26b, 26c, 26d) in a manner depending on the signals made available by the detection device (34).</p> |
