An aircraft turbine engine includes a gas generator having a longitudinal axis (A), a fan which is located at an upstream end of the gas generator and which is configured to rotate about the axis, and an electric machine which has a generally annular shape. The electric machine is mounted coaxially downstream of the fan and has a rotor which is coupled in terms of rotation to the fan, and a stator which is connected to an electronic power circuit by at least one rigid electroconductive bar.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Electric connection of an electric machine in an aircraft turbomachine



    Erscheinungsdatum :

    2023-09-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



    ELECTRIC CONNECTION OF AN ELECTRIC MACHINE IN AN AIRCRAFT TURBOMACHINE

    MILLIER VINCENT FRANÇOIS GEORGES / GUILLOTEL LOÏC PAUL YVES | Europäisches Patentamt | 2023

    Freier Zugriff

    Electrical connection for an electric machine in an aircraft turbomachine

    MILLIER VINCENT FRANÇOIS GEORGES / GUILLOTEL LOÏC PAUL YVES | Europäisches Patentamt | 2024

    Freier Zugriff

    ELECTRICAL CONNECTION FOR AN ELECTRIC MACHINE IN AN AIRCRAFT TURBOMACHINE

    MILLIER VINCENT FRANÇOIS GEORGES / GUILLOTEL LOÏC PAUL YVES | Europäisches Patentamt | 2022

    Freier Zugriff

    Concentric turbomachine with electric machine

    HARVEY GILES E | Europäisches Patentamt | 2022

    Freier Zugriff

    Concentric turbomachine with electric machine

    HARVEY GILES E | Europäisches Patentamt | 2022

    Freier Zugriff