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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    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 :

    22.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM

    BRUNO LOUIS J / HO TONY / COUTIN AIDEN | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM

    Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM

    Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM

    BRUNO LOUIS J / HIPSKY HAROLD W / ARMY JR DONALD E et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM

    ZHU YONGHUA / THIBAUD CATHERINE / LE CAM MATHIEU et al. | Europäisches Patentamt | 2024

    Freier Zugriff