| 摘要 |
An air-conditioning system for an aircraft for the individual temperature control of regions (28, 30, 32, 34) of a cabin (28) of an aircraft, comprises a central air-conditioning device (2), which provides a pressurised and temperature-controlled central air flow. A part of the central air flow (6) is supplied to a first cabin region (28). A further part of the central air flow is heated in a heating device (16, 18, 20) or cooled in a cooling device (22, 24, 26) and supplied to another cabin region (30, 32, 34). Water is evaporated in the cooling device (22, 24, 26), in order to cool the air flow for supply to the cabin region (28, 30, 32, 34). |
