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    METHODS AND MATERIALS FOR REPAIRING A THERMAL BARRIER COATING OF A GAS TURBINE COMPONENT

    New search for: KESHAVAN HRISHIKESH
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    A sprayable thermal barrier coating powder mixture (208) for a gas turbine engine (10) includes: a dry composition having a low surface area ceramic powder (214) having a median particle size distribution greater than 5 microns and less than 50 microns, and a high surface area ceramic powder (216) having a median particle size distribution smaller than 5 microns, wherein the low surface area ceramic powder (214) makes up at least 50% by weight of the dry composition of the sprayable thermal barrier coating powder mixture (208).

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    METHODS AND MATERIALS FOR REPAIRING A THERMAL BARRIER COATING OF A GAS TURBINE COMPONENT

    New search for: KESHAVAN HRISHIKESH
    New search for: SAHA ATANU
    New search for: WALLACE MARGEAUX
    New search for: NAGESH MAMATHA
    New search for: BEWLAY BERNARD PATRICK

    A sprayable thermal barrier coating powder mixture (208) for a gas turbine engine (10) includes: a dry composition having a low surface area ceramic powder (214) having a median particle size distribution greater than 5 microns and less than 50 microns, and a high surface area ceramic powder (216) having a median particle size distribution smaller than 5 microns, wherein the low surface area ceramic powder (214) makes up at least 50% by weight of the dry composition of the sprayable thermal barrier coating powder mixture (208).

    Access

    Download

    METHODS AND MATERIALS FOR REPAIRING A THERMAL BARRIER COATING OF A GAS TURBINE COMPONENT

    New search for: KESHAVAN HRISHIKESH
    New search for: SAHA ATANU
    New search for: WALLACE MARGEAUX
    New search for: NAGESH MAMATHA
    New search for: BEWLAY BERNARD PATRICK

    A sprayable thermal barrier coating powder mixture (208) for a gas turbine engine (10) includes: a dry composition having a low surface area ceramic powder (214) having a median particle size distribution greater than 5 microns and less than 50 microns, and a high surface area ceramic powder (216) having a median particle size distribution smaller than 5 microns, wherein the low surface area ceramic powder (214) makes up at least 50% by weight of the dry composition of the sprayable thermal barrier coating powder mixture (208).

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    Title:

    METHODS AND MATERIALS FOR REPAIRING A THERMAL BARRIER COATING OF A GAS TURBINE COMPONENT

    Additional title:

    VERFAHREN UND MATERIALIEN ZUR REPARATUR EINER WÄRMEDÄMMSCHICHT EINER GASTURBINENKOMPONENTE
    PROCÉDÉS ET MATÉRIAUX DE RÉPARATION D'UN REVÊTEMENT BARRIÈRE THERMIQUE D'UN COMPOSANT DE TURBINE À GAZ

    Contributors:

    KESHAVAN HRISHIKESH (author) / SAHA ATANU (author) / WALLACE MARGEAUX (author) / NAGESH MAMATHA (author) / KULKARNI AMBARISH JAYANT (author) / BEWLAY BERNARD PATRICK (author)

    Publication date:

    2022-06-08

    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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