An hybrid aircraft power plant, has: a gas turbine engine having a high-pressure spool including a high-pressure compressor, a high-pressure turbine, and a high-pressure shaft drivingly engaging the high-pressure turbine to the high-pressure compressor, a low-pressure spool including a low-pressure compressor, a low-pressure turbine, and a low-pressure shaft drivingly engaging the low-pressure turbine to the low-pressure compressor; an electric motor drivingly engaged to the low-pressure shaft; and a torque-transmitting device operatively connected to the HP-shaft and having an engaged configuration in which the torque-transmitting device drivingly engages the electric motor to the high-pressure shaft and a disengaged configuration in which the torque-transmitting device disconnects the electric motor from the high-pressure shaft.


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    Titel :

    HYBRID POWER PLANT FOR AIRCRAFT


    Weitere Titelangaben:

    GROUPE MOTOPROPULSEUR HYBRIDE POUR AERONEF


    Beteiligte:
    VALOIS PATRICK (Autor:in) / TURCOTTE HERVE (Autor:in) / FREER RICHARD (Autor:in) / TREMBLAY JONATAN (Autor:in) / LATULIPE ERIC (Autor:in)

    Erscheinungsdatum :

    25.07.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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