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

    New search for: DOWNS JOHN
    New search for: MEHR MEHRAD
    New search for: 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

    New search for: DOWNS JOHN
    New search for: MEHR MEHRAD
    New search for: 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.

    Access

    Download

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

    New search for: DOWNS JOHN
    New search for: MEHR MEHRAD
    New search for: 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

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    Document information
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    Document information
    Title:

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

    Contributors:

    DOWNS JOHN (author) / MEHR MEHRAD (author) / JADIDIAN BAHRAM (author)

    Publication date:

    2024-01-02

    Type of media:

    Patent

    Type of material:

    Electronic Resource

    Language:

    English

    Classification:

    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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