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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    Title :

    ARCHITECTURES FOR HYBRID-ELECTRIC PROPULSION


    Additional title:

    ARCHITEKTUREN FÜR HYBRID-ELEKTRISCHEN ANTRIEB
    ARCHITECTURES DE PROPULSION HYBRIDE-ÉLECTRIQUE


    Contributors:
    LATULIPE ERIC (author) / THOMASSIN JEAN (author) / WANG XI (author) / DUBREUIL JEAN (author) / DIONNE LUC (author) / JULIEN ANDRE (author)

    Publication date :

    2025-03-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02B INTERNAL-COMBUSTION PISTON ENGINES , Brennkraftmaschinen mit innerer Verbrennung mit Verdrängerwirkung / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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