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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    Title :

    AIRCRAFT ENGINE WITH ICE SHEDDING SYSTEM


    Additional title:

    FLUGZEUGTRIEBWERK MIT EISABLÖSUNG
    MOTEUR D'AÉRONEF À DÉLESTAGE DE GLACE


    Contributors:

    Publication date :

    2021-02-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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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