A hybrid aircraft propulsion system. The system comprises a gas turbine engine having a turbine system comprising first and second turbine sections. The gas turbine engine further comprises a first combustor provided upstream in core flow from the turbine system, and a second combustor provided between the first and second turbine sections. The hybrid aircraft propulsion system further comprises an energy storage system and an electric propulsion system electrically coupled to the energy storage system.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    12.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F16H Getriebe , GEARING



    HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM

    BACIC MARKO | Europäisches Patentamt | 2022

    Freier Zugriff

    HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM

    LATULIPE ERIC / FREER RICHARD | Europäisches Patentamt | 2020

    Freier Zugriff

    HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM

    LATULIPE ERIC / FREER RICHARD | Europäisches Patentamt | 2020

    Freier Zugriff

    HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM

    LATULIPE ERIC / FREER RICHARD | Europäisches Patentamt | 2020

    Freier Zugriff

    HYBRID-ELECTRIC PROPULSION SYSTEM FOR AIRCRAFT

    SRIDHAR ADIBHATLA / ROBERT CHARLES HON / MICHAEL THOMAS GANSLER | Europäisches Patentamt | 2019

    Freier Zugriff