An electric architecture for a twin-engined, hybrid thermal/electric propulsion aircraft and, for each turboshaft which includes a high-voltage DC propulsive electric distribution network, a non-propulsive electric distribution network which is connected to loads of the aircraft, and an electric distribution network which is connected to loads of an electrified control system of the turboshaft engine, and wherein power supply sources are shared for these different networks.


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    Titel :

    Electric architecture for a hybrid thermal/electric propulsion aircraft and twin-engined aircraft comprising such an architecture


    Beteiligte:
    DELBOSC PHILIPPE (Autor:in) / DUPAYS CLEMENT (Autor:in) / LIENHARDT ANNE (Autor:in) / MICHAUD BENOIT (Autor:in) / GAUTIER CYRILLE (Autor:in) / GIMENO ANTHONY (Autor:in)

    Erscheinungsdatum :

    24.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



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