An aircraft power plant has: a hybrid propulsion system having an electric motor, an output shaft drivingly connectable to a thrust generator, a combustion engine, a compressor, and a transmission having a first transmission drive path and a second transmission drive path selectively engageable to the first transmission drive path, the electric motor and the compressor in driving engagement with the first transmission drive path, the combustion engine and the output shaft in driving engagement with the second transmission drive path.


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    Titel :

    HYBRID AIRCRAFT PROPULSION POWER PLANTS


    Weitere Titelangaben:

    GROUPES MOTOPROPULSEURS D`AERONEF HYBRIDE


    Beteiligte:
    DUBREUIL JEAN (Autor:in) / ULLYOTT RICHARD (Autor:in)

    Erscheinungsdatum :

    29.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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