An environmental control system of an aircraft includes a plurality of inlets (22, 24, 28) for receiving a plurality of mediums including a first medium (A1), a second medium (A2), and a third medium (A3) and an outlet for delivering a conditioned flow of the second medium to one or more loads of the aircraft. A ram air circuit (30) includes a ram air shell (32) having at least one heat exchanger positioned therein. At least one compressing device (40) is arranged in fluid communication with the ram air circuit and the outlet. The at least one compressing device includes at least one compressor (42) and at least one turbine (44) operably coupled via a shaft. A heat exchanger (34) is arranged in fluid communication with the at least one compressing device. The second medium output from the at least one compressing device is cooled by the third medium. The second medium is fresh air.


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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 :

    2024-01-31


    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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