An environmental control system of an aircraft includes a ram air circuit (30) including a ram air shell (32) having at least one heat exchanger (34, 36) positioned therein and a divider (56) arranged within the ram air shell to separate the ram air shell into a first region and a second region. The at least one heat exchanger is arranged within both the first region and the second region. A first medium (Al) is configured to flow through the first region and a second, distinct medium (A2) is configured to flow through the second region. The environmental control system additionally includes a dehumidification system arranged in fluid communication with the ram air circuit and a compression device (40) arranged in fluid communication with the ram air circuit and the dehumidification system.
AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM
FLUGZEUGKLIMAREGELUNGSSYSTEM
SYSTÈME DE RÉGLAGE ENVIRONNEMENTAL D'UN AÉRONEF
2022-02-02
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |