A compressing device for use in an environmental control system includes at least one turbine (44) configured to provide energy by expanding one or more medium. The one or more mediums provided at an outlet of the at least one turbine form a heat sink within the environmental control system. A compressor (42) is configured to receive energy from the one or more mediums expanded across the at least one turbine. During a first mode of the compressing device, energy derived from a first medium (A1) of the one or more mediums is used to compress a second medium (A2) at the compressor and during a second mode of the compressing device, energy derived from both the first medium and a third medium (A3) of the one or more mediums is used to compress a second medium at the compressor.


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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 :

    2024-03-06


    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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