A valve unit for an aircraft is provided. The valve unit includes valve assembly; and a servo controller coupled to the valve assembly and configured to control operation of the valve assembly. At least a portion of at least one of the valve assembly or servo controller is formed by a high temperature aluminum alloy.


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    Titel :

    High temperature aluminum valve components


    Weitere Titelangaben:

    Hochtemperatur-Aluminiumventilkomponenten
    Composants de soupape en aluminium haute température


    Beteiligte:
    HRDLICHKA AARON (Autor:in) / ADAMS ROBBIE JOSEPH (Autor:in) / HOPKINS RICH (Autor:in) / HOLTZ ERIC (Autor:in) / PATTERSON STEVE (Autor:in)

    Erscheinungsdatum :

    24.04.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS



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