An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame.


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    Titel :

    Lightweight cabin pressure thrust recovery outflow valve


    Beteiligte:
    HORNER DARRELL (Autor:in) / MEYER ROSS F (Autor:in) / KANG ALBERT (Autor:in) / PRODROMIDES KEVIN (Autor:in) / FUHRMANN BARRETT (Autor:in) / SCHROEDER KARL (Autor:in) / MILLER BETH (Autor:in) / GENTILE DAVID P (Autor:in) / YADAV GOVIND (Autor:in)

    Erscheinungsdatum :

    12.01.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F24F Klimatisierung , AIR-CONDITIONING / F16K VALVES , Ventile



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