| 摘要 |
An aircraft air-conditioning system (10) comprises an air-conditioning unit (12) which is designed to provide cooled process air. A process air line (14) is designed to conduct cooled process air provided by the air-conditioning unit (12) into an working area (16) of an aircraft cabin. A cooler (20) is designed to supply cooling energy to a device to be cooled which is provided in the working area (16) of the aircraft cabin. Finally, the aircraft air-conditioning system (10) comprises a heat transfer arrangement (24) which is designed to transfer waste heat generated by the cooler (20) to process air flowing through the process air line (14). |
