An air conditioning system for an aircraft is provided. The air conditioning system includes a first rotating component and a second rotating component. The first rotating component includes a compressor and a turbine. The compressor pressurizes a first medium. The first turbine receives a mixture of a second medium and a pressurized form of the first medium. The second rotating component includes a fan.


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    Titel :

    MIXING BLEED AND RAM AIR AT A TURBINE INLET OF A COMPRESSING DEVICE


    Weitere Titelangaben:

    MELANGE D'AIR DE PRELEVEMENT ET D'AIR DYNAMIQUE A L'ENTREE D'UNE TURBINE D'UN APPAREIL COMPRESSEUR


    Beteiligte:
    BRUNO LOUIS J (Autor:in) / HIPSKY HAROLD W (Autor:in)

    Erscheinungsdatum :

    2017-11-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F24F Klimatisierung , AIR-CONDITIONING / F25B Kältemaschinen, Kälteanlagen oder Kälteverfahren , REFRIGERATION MACHINES, PLANTS, OR SYSTEMS



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