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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

    Download

    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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    Download

    Zugriff

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    Titel:

    Protective coating systems for gas turbine engine applications and methods for fabricating the same

    Beteiligte:

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

    Erscheinungsdatum:

    02.01.2024

    Medientyp:

    Patent

    Format:

    Elektronische Ressource

    Sprache:

    Englisch

    Klassifikation:

    IPC:  C23C Beschichten metallischer Werkstoffe , COATING METALLIC MATERIAL / 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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