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).


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    Title :

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM


    Additional title:

    REGELSYSTEM FÜR FLUGZEUGKLIMATISIERUNG
    SYSTÈME DE CONTRÔLE DE CLIMATISATION D'UN AÉRONEF


    Contributors:

    Publication date :

    2019-01-23


    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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