A fan blade includes a root including a front surface, a rear surface, a first side surface connected to the front surface and the rear surface, and a second side surface connected to the front surface and the rear surface. The front surface engages the first side surface and the second side surface by one or more blunted surfaces, and the rear surface engages the first side surface and the second side surface by one or more blunted surfaces. A blade extends from the root.


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    Titel :

    FAN BLADE ATTACHMENT OF GAS TURBINE ENGINE


    Weitere Titelangaben:

    LÜFTERSCHAUFELBEFESTIGUNG FÜR EINEN GASTURBINENMOTOR
    FIXATION DE PALE DE VENTILATEUR DE MOTEUR À TURBINE À GAZ


    Beteiligte:

    Erscheinungsdatum :

    02.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES




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