An environmental control system of an aircraft including a plurality of inlets for receiving a plurality of mediums including a first medium, a second medium, and a third medium 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 and a second compressing device. 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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft environmental control system


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

    Erscheinungsdatum :

    24.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F25B Kältemaschinen, Kälteanlagen oder Kälteverfahren , REFRIGERATION MACHINES, PLANTS, OR SYSTEMS / 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

    BRUNO LOUIS J / HO TONY / COUTIN AIDEN | Europäisches Patentamt | 2024

    Freier Zugriff