An aircraft air conditioning system (10) comprises a process air line (12). A ram air channel (32) allowing a flow of ambient air therethrough. A heat exchanger unit (26) is disposed within the ram air channel (32) so as to thermally couple the process air to the ambient air flowing through the ram air channel (32). A water extractor (48) is disposed in the process air line (12) downstream of the heat exchanger unit (26) so as to extract water from the process air. A water supply system (58) supplies water extracted from the process air by means of the water extractor (48) into the ram air channel (32). A control arrangement (64) controls a fluid connection between the water extractor (48) and the ram air channel (32) in dependence on an operating state of the aircraft air conditioning system (10).
Aircraft air conditioning system and method of operating an aircraft air conditioning system
Flugzeugklimaanlage und Verfahren für den Betrieb einer Flugzeugklimaanlage
Système de conditionnement d'air pour aéronef et procédé de fonctionnement d'un système de conditionnement d'air pour aéronef
2015-05-06
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AIRCRAFT AIR CONDITIONING SYSTEM AND METHOD OF OPERATING AN AIRCRAFT AIR CONDITIONING SYSTEM
European Patent Office | 2020
|AIRCRAFT AIR CONDITIONING SYSTEM AND METHOD OF OPERATING AN AIRCRAFT AIR CONDITIONING SYSTEM
European Patent Office | 2023
|AIRCRAFT AIR CONDITIONING SYSTEM AND METHOD OF OPERATING AN AIRCRAFT AIR CONDITIONING SYSTEM
European Patent Office | 2020
|Aircraft air conditioning system and method of operating an aircraft air conditioning system
European Patent Office | 2017
|Aircraft air conditioning system and method of operating an aircraft air conditioning system
European Patent Office | 2017
|