A fluid cooling system of an aircraft includes a compressor (42), a condenser (44), an expansion device (56), a turbine (46), and an evaporator (48) fluidly coupled to form a closed loop through which a cooling medium circulates. The expansion device is positioned such that an inlet of the expansion device receives a flow of the cooling medium from the condenser and an outlet of the expansion device delivers the flow of cooling medium to the turbine. Within the evaporator, the cooling medium is arranged in thermal communication with a medium of an environmental control system of the aircraft.


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    Titel :

    VAPOR COMPRESSION SYSTEM FOR AEROSPACE APPLICATIONS


    Weitere Titelangaben:

    DAMPFKOMPRESSIONSSYSTEM FÜR LUFT- UND RAUMFAHRTANWENDUNGEN
    SYSTÈME DE COMPRESSION DE VAPEUR POUR APPLICATIONS AÉROSPATIALES


    Beteiligte:
    COUTIN AIDEN (Autor:in)

    Erscheinungsdatum :

    2023-11-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    VAPOR COMPRESSION SYSTEM FOR AEROSPACE APPLICATIONS

    COUTIN AIDEN | Europäisches Patentamt | 2023

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