An environmental control system of an aircraft including 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. The environmental control system additionally includes a first compressing device (40a) and a second compressing device (40b). The second compressing device is arranged in fluid communication with the first compressing device and the outlet. An inlet of the second compressing device is directly connected to an outlet of the first compressing device, and the first compressing device is driven by energy extracted from the first medium. The first medium is a flow of bleed air.


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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 :

    2022-02-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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