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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Electric de-icing device for turbojet engine nacelle


    Beteiligte:

    Erscheinungsdatum :

    16.09.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Turbojet engine nacelle

    JORET JEAN PHILIPPE / VAUCHEL GUY BERNARD | Europäisches Patentamt | 2015

    Freier Zugriff

    DEVICE FOR DE-ICING AN AIRCRAFT TURBOJET ENGINE NACELLE AIR INTAKE LIP

    MAALIOUNE HAKIM / GONIDEC PATRICK / RAMI JEAN-PAUL | Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft turbojet engine nacelle

    KERBLER OLIVIER / METEZEAU FABRICE HENRI EMILE / GONIDEC PATRICK et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    AIRCRAFT TURBOJET ENGINE NACELLE

    KERBLER OLIVIER / METEZEAU FABRICE HENRI EMILE / GONIDEC PATRICK et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    DE-ICING DEVICE FOR AN AIR INTAKE OF AN AIRCRAFT TURBOJET ENGINE NACELLE

    LE DOCTE THIERRY JACQUES ALBERT | Europäisches Patentamt | 2022

    Freier Zugriff