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.


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    Title :

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM


    Additional title:

    FLUGZEUGKLIMAREGELUNGSSYSTEM
    SYSTÈME DE RÉGLAGE ENVIRONNEMENTAL D'UN AÉRONEF


    Contributors:
    BRUNO LOUIS J (author) / HO TONY (author) / COUTIN AIDEN (author)

    Publication date :

    2022-02-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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