An aeronautical turbogenerator for hybrid electric propulsion includes a heat engine and an electrical generator coupled mechanically to the heat engine and including a rotor and a stator, the rotor extending in an axial direction and including a common magnetized rotor yoke comprising a plurality of permanent magnets defining at least three axially distributed movable annular rings, the stator including a magnetic stator yoke comprising a plurality of electrical windings defining axially and/or circumferentially distributed stationary sectors, at least two stationary sectors, one of which covers axially at least two movable annular rings, being arranged angularly so as not to mutually coincide and thus deliver at least two distinct and independent voltage levels.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Turbogenerator for hybrid electric aeronautical propulsion



    Erscheinungsdatum :

    03.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    TURBOGENERATOR FOR HYBRID ELECTRIC AERONAUTICAL PROPULSION

    VIVE LOÏS PIERRE DENIS / VIGUIER CHRISTOPHE LUDOVIC JEAN-CLAUDE | Europäisches Patentamt | 2022

    Freier Zugriff

    HYBRID-ELECTRIC PROPULSION SYSTEM FOR AERONAUTICAL APPLICATIONS

    MARIOTTI GABRIELE | Europäisches Patentamt | 2025

    Freier Zugriff

    AERONAUTICAL PROPULSION SYSTEM HAVING ELECTRIC FANS

    MURROW KURT DAVID / ZATORSKI DAREK TOMASZ / FRANER MATTHEW TIMOTHY | Europäisches Patentamt | 2024

    Freier Zugriff

    AERONAUTICAL PROPULSION SYSTEM HAVING ELECTRIC FANS

    MURROW KURT DAVID / ZATORSKI DAREK TOMASZ / FRANER MATTHEW TIMOTHY | Europäisches Patentamt | 2025

    Freier Zugriff