An aircraft engine (12) configured to controllably shed ice during icing conditions is presented. The engine has a fan member (14) operating at a first angular velocity having a surface (18) divided into a first ice accumulating surface (20) configured to collect ice, and a first shadow surface (22) configured to resist the collection of ice. A first flange (16) is disposed between the first ice accumulating surface and the first shadow surface.


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    Titel :

    AIRCRAFT ENGINE WITH ICE SHEDDING SYSTEM


    Weitere Titelangaben:

    FLUGZEUGTRIEBWERK MIT EISABLÖSUNG
    MOTEUR D'AÉRONEF À DÉLESTAGE DE GLACE


    Beteiligte:

    Erscheinungsdatum :

    17.02.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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