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

    2020-09-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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