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    PROTECTIVE COATING SYSTEMS FOR GAS TURBINE ENGINE APPLICATIONS AND METHODS FOR FABRICATING THE SAME

    Neue Suche nach: DOWNS JOHN
    Neue Suche nach: MEHR MEHRAD
    Neue Suche nach: JADIDIAN BAHRAM

    A protective coating system includes a turbine engine component substrate formed of a ceramic matrix composite material, an environmental barrier coating layer including a rare earth disilicate material formed directly on the substrate, and a thermal barrier coating layer including a porous rare earth monosilicate material having a metal silicate material infiltrated within at least a portion of the pores formed directly on the environmental barrier coating layer.

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    PROTECTIVE COATING SYSTEMS FOR GAS TURBINE ENGINE APPLICATIONS AND METHODS FOR FABRICATING THE SAME

    Neue Suche nach: DOWNS JOHN
    Neue Suche nach: MEHR MEHRAD
    Neue Suche nach: JADIDIAN BAHRAM

    A protective coating system includes a turbine engine component substrate formed of a ceramic matrix composite material, an environmental barrier coating layer including a rare earth disilicate material formed directly on the substrate, and a thermal barrier coating layer including a porous rare earth monosilicate material having a metal silicate material infiltrated within at least a portion of the pores formed directly on the environmental barrier coating layer.

    Zugriff

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    PROTECTIVE COATING SYSTEMS FOR GAS TURBINE ENGINE APPLICATIONS AND METHODS FOR FABRICATING THE SAME

    Neue Suche nach: DOWNS JOHN
    Neue Suche nach: MEHR MEHRAD
    Neue Suche nach: JADIDIAN BAHRAM

    A protective coating system includes a turbine engine component substrate formed of a ceramic matrix composite material, an environmental barrier coating layer including a rare earth disilicate material formed directly on the substrate, and a thermal barrier coating layer including a porous rare earth monosilicate material having a metal silicate material infiltrated within at least a portion of the pores formed directly on the environmental barrier coating layer.

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    Ähnliche Titel

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    Titel:

    PROTECTIVE COATING SYSTEMS FOR GAS TURBINE ENGINE APPLICATIONS AND METHODS FOR FABRICATING THE SAME

    Weitere Titelangaben:

    SCHUTZBESCHICHTUNGSSYSTEME FÜR GASTURBINENMOTORANWENDUNGEN UND HERSTELLUNGSVERFAHREN DAFÜR
    SYSTÈMES DE REVÊTEMENT PROTECTEUR POUR APPLICATIONS DE MOTEUR À TURBINE À GAZ ET LEURS PROCÉDÉS DE FABRICATION

    Beteiligte:

    DOWNS JOHN (Autor:in) / MEHR MEHRAD (Autor:in) / JADIDIAN BAHRAM (Autor:in)

    Erscheinungsdatum:

    20.03.2024

    Medientyp:

    Patent

    Format:

    Elektronische Ressource

    Sprache:

    Englisch

    Klassifikation:

    IPC:  C04B Kalk , LIME / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES

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