An environmental control system of an aircraft with a power turbine includes a heat exchanger and a plenum attached to and in fluid communication with the heat exchanger. The plenum includes a housing with a first inlet fluidly connected to the power turbine, a second inlet fluidly connected to a source of ram air, and an outlet fluidly connected to the heat exchanger.


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    Titel :

    ECS DUAL ENTRY RAM INLET PLENUM


    Beteiligte:
    MCCORD PATRICK (Autor:in) / TOKAS CHRISTOPHER (Autor:in) / ARMY DONALD E (Autor:in)

    Erscheinungsdatum :

    25.07.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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