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


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ELECTRICAL CONNECTION FOR AN ELECTRIC MACHINE IN AN AIRCRAFT TURBOMACHINE



    Erscheinungsdatum :

    2022-12-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Electrical connection for an electric machine in an aircraft turbomachine

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

    Freier Zugriff

    ELECTRIC CONNECTION OF AN ELECTRIC MACHINE IN AN AIRCRAFT TURBOMACHINE

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

    Freier Zugriff

    Electric connection of an electric machine in an aircraft turbomachine

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

    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