A twin-engine system includes a gas turbine engine comprising a core and a first output shaft drivable by the core. An electric engine has an electric motor configured to drive a second output shaft. A reduction gear box (RGB) has an RGB input drivingly engaged to both the first output shaft and the second output shaft. The RGB has an RGB output to provide rotational output to a rotatable load.


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    Titel :

    TWIN-ENGINE SYSTEM WITH ELECTRIC DRIVE


    Weitere Titelangaben:

    MOTEUR A DEUX CYLINDRES AVEC COMMANDE ELECTRIQUE


    Beteiligte:
    LEFEBVRE GUY (Autor:in)

    Erscheinungsdatum :

    2021-11-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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