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


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

    Erscheinungsdatum :

    01.11.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60W CONJOINT CONTROL OF VEHICLE SUB-UNITS OF DIFFERENT TYPE OR DIFFERENT FUNCTION , Gemeinsame Steuerung oder Regelung von Fahrzeug-Unteraggregaten verschiedenen Typs oder verschiedener Funktion / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    HYBRID AIRCRAFT PROPULSION POWER PLANTS

    DUBREUIL JEAN / ULLYOTT RICHARD | Europäisches Patentamt | 2020

    Freier Zugriff

    Hybrid aircraft propulsion power plants

    DUBREUIL JEAN / ULLYOTT RICHARD | Europäisches Patentamt | 2021

    Freier Zugriff

    HYBRID AIRCRAFT PROPULSION POWER PLANTS

    DUBREUIL JEAN / ULLYOTT RICHARD | Europäisches Patentamt | 2020

    Freier Zugriff

    HYBRID AIRCRAFT PROPULSION POWER PLANTS

    DUBREUIL JEAN / ULLYOTT RICHARD | Europäisches Patentamt | 2020

    Freier Zugriff

    HYBRID AIRCRAFT PROPULSION POWER PLANTS

    DUBREUIL JEAN / ULLYOTT RICHARD | Europäisches Patentamt | 2020

    Freier Zugriff