The invention relates to an electric de-icing/anti-icing device for a turbojet engine/turbo-prop nacelle element for an element of an aircraft to be protected from ice, comprising: - a heating assembly comprising two heating stages positioned in the nacelle element to be protected from ice; - an electricity supply circuit delivering a primary voltage to the first stage of the heating assembly, and comprising: an electricity source; a de-icing/anti-icing circuit (13) connected to the heating assembly and supplied with voltage by said electricity supply source. The de-icing/anti-icing device according to the invention is remarkable in that it further comprises means (25, 29) for delivering a complementary voltage supplying the second stage of the heating assembly.


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    Title :

    Electric de-icing device for turbojet engine nacelle


    Contributors:

    Publication date :

    2015-09-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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