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

    Neue Suche nach: KESHAVAN HRISHIKESH
    Neue Suche nach: SAHA ATANU
    Neue Suche nach: WALLACE MARGEAUX
    Neue Suche nach: NAGESH MAMATHA
    Neue Suche nach: 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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    METHODS AND MATERIALS FOR REPAIRING A THERMAL BARRIER COATING OF A GAS TURBINE COMPONENT

    Neue Suche nach: KESHAVAN HRISHIKESH
    Neue Suche nach: SAHA ATANU
    Neue Suche nach: WALLACE MARGEAUX
    Neue Suche nach: NAGESH MAMATHA
    Neue Suche nach: 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).

    Zugriff

    Download

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

    Neue Suche nach: KESHAVAN HRISHIKESH
    Neue Suche nach: SAHA ATANU
    Neue Suche nach: WALLACE MARGEAUX
    Neue Suche nach: NAGESH MAMATHA
    Neue Suche nach: 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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    Titel:

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

    Weitere Titelangaben:

    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

    Beteiligte:

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

    Erscheinungsdatum:

    08.06.2022

    Medientyp:

    Patent

    Format:

    Elektronische Ressource

    Sprache:

    Englisch

    Klassifikation:

    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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