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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    Titel :

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM


    Weitere Titelangaben:

    FLUGZEUGKLIMAREGELUNGSSYSTEM
    SYSTÈME DE RÉGLAGE ENVIRONNEMENTAL D'UN AÉRONEF


    Beteiligte:
    BRUNO LOUIS J (Autor:in) / HO TONY (Autor:in) / COUTIN AIDEN (Autor:in)

    Erscheinungsdatum :

    2024-03-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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