An environmental control system (ECS) pack (100) is provided including a primary heat exchanger (102) and a secondary heat exchanger (104). An air cycle machine (106) is arranged in fluid communication with at least one of the primary and second heat exchanger (102, 104). The air cycle machine (106) includes a compressor (110) and a plurality of turbines (112, 114, 116). Discharged cabin air is supplied to at least one of the plurality of turbines (112, 114, 116) to operate the compressor (110).
AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
REGELSYSTEM FÜR FLUGZEUGKLIMATISIERUNG
SYSTÈME DE CONTRÔLE DE CLIMATISATION D'UN AÉRONEF
2019-01-23
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |