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    THERMAL BARRIER COATING FOR CMAS RESISTANCE AND LOW THERMAL CONDUCTIVITY

    New search for: BOCHIECHIO MARIO P
    New search for: LITTON DAVID A
    New search for: MALONEY MICHAEL J

    A thermal barrier coating for a turbine engine component contains neodymia, optionally alumina, and zirconia. The thermal barrier coating has resistance to CMAS attack and a low thermal conductivity.

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    THERMAL BARRIER COATING FOR CMAS RESISTANCE AND LOW THERMAL CONDUCTIVITY

    New search for: BOCHIECHIO MARIO P
    New search for: LITTON DAVID A
    New search for: MALONEY MICHAEL J

    A thermal barrier coating for a turbine engine component contains neodymia, optionally alumina, and zirconia. The thermal barrier coating has resistance to CMAS attack and a low thermal conductivity.

    Access

    Download

    THERMAL BARRIER COATING FOR CMAS RESISTANCE AND LOW THERMAL CONDUCTIVITY

    New search for: BOCHIECHIO MARIO P
    New search for: LITTON DAVID A
    New search for: MALONEY MICHAEL J

    A thermal barrier coating for a turbine engine component contains neodymia, optionally alumina, and zirconia. The thermal barrier coating has resistance to CMAS attack and a low thermal conductivity.

    Access

    Download

    Access

    Download

    Page navigation

    Document information
    Similar titles

    Export, share and cite

    Document information
    Title:

    THERMAL BARRIER COATING FOR CMAS RESISTANCE AND LOW THERMAL CONDUCTIVITY

    Contributors:

    BOCHIECHIO MARIO P (author) / LITTON DAVID A (author) / MALONEY MICHAEL J (author)

    Publication date:

    2019-07-04

    Type of media:

    Patent

    Type of material:

    Electronic Resource

    Language:

    English

    Classification:

    IPC:  C04B Kalk , LIME / C23C Beschichten metallischer Werkstoffe , COATING METALLIC MATERIAL / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES

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