An environmental control system (ECS) for an aircraft includes a primary heat exchanger, a compressor including an inlet fluidically connected to the primary heat exchanger, a turbine operatively connected to the compressor, and a cryogenic fluid heat exchanger fluidically connected to the primary heat exchanger.


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    Titel :

    CRYOGENIC FLUID HEAT EXCHANGER SYSTEM FOR AN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM (ECS)


    Beteiligte:
    EMERSON SEAN C (Autor:in) / QUARTARONE GIUSI (Autor:in) / TURNEY JOSEPH (Autor:in) / RANJAN RAM (Autor:in) / ZAVAGLIO ERICA (Autor:in) / BENZI FEDERICO MATTIA (Autor:in) / LENTS CHARLES E (Autor:in)

    Erscheinungsdatum :

    16.03.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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