A rotor blade (2) for a gas turbine engine, comprising a blade tip 4. At least a portion of the blade tip (4) is provided with a wear-resistant coating (16), (18) comprising magnesium aluminate spinel. A corresponding method to coat a rotor blade tip (4) of a gas turbine engine with magnesium aluminate spinel. The use of magnesium aluminate spinel as a wear resistant coating.


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    Titel :

    Wear Resistant Coating and Use Thereof


    Weitere Titelangaben:

    Verschleißfeste Beschichtung und Verwendung davon
    Revêtement résistant à l'usure et son utilisation


    Beteiligte:
    HEWITT ANDREW (Autor:in) / HANCOCK MATTHEW (Autor:in)

    Erscheinungsdatum :

    2017-10-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / 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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