A hybrid propulsion system includes a heat engine configured to drive a heat engine shaft. An electric motor is configured to drive an electric motor shaft. A transmission system includes at least one gearbox. The transmission system is configured to receive rotational input power from each of the heat engine shaft and the electric motor shaft and to convert the rotation input power to output power.


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    Titel :

    Architectures for hybrid-electric propulsion


    Beteiligte:
    LATULIPE ERIC (Autor:in) / THOMASSIN JEAN (Autor:in) / WANG XIAOQIN (Autor:in) / DUBREUIL JEAN (Autor:in) / DIONNE LUC (Autor:in) / JULIEN ANDRE (Autor:in)

    Erscheinungsdatum :

    27.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16H Getriebe , GEARING / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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