A system includes an inlet line configured to receive a medium flowing from a low-pressure location of an engine to a chamber, a plurality of heat exchangers configured to receive the medium from the inlet line, and a valve located upstream from the plurality of heat exchangers. The valve is configured to divide in parallel the medium across at least a first heat exchanger and a second heat exchanger of the plurality of heat exchangers. A recirculation air system is configured to supply a recirculation.


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    Titel :

    Recirculation system for parallel ram heat exchangers


    Beteiligte:
    BRUNO LOUIS J (Autor:in) / ZYWIAK THOMAS M (Autor:in) / KLINE ERIN G (Autor:in) / MILLOT CHRISTINA W (Autor:in) / ARMY JR DONALD E (Autor:in) / HIPSKY HAROLD W (Autor:in)

    Erscheinungsdatum :

    13.02.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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