Aircraft engine systems include a core assembly having at least a burner section and a fuel cell configured to generate electrical power. A cryogenic fuel source is configured to supply a fuel through a fuel supply line to each of the burner section and the fuel cell for reaction to generate the electrical power. A system controller is configured to direct fuel to each of the combustor section and the fuel cell. The controller determines if an amount of fuel in the fuel supply line is in excess of that necessary for operation of the core assembly and, based on a determination that excess fuel is present, the controller is configured to direct at least a portion of the excess fuel from the fuel supply line to the fuel cell to generate the electrical power.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HYBRID ELECTRIC HYDROGEN ENGINE FOR AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    11.01.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02D CONTROLLING COMBUSTION ENGINES , Steuern oder Regeln von Brennkraftmaschinen



    HYBRID ELECTRIC HYDROGEN ENGINE FOR AIRCRAFT

    TERWILLIGER NEIL J / STAUBACH JOSEPH B | Europäisches Patentamt | 2024

    Freier Zugriff

    Hybrid electric hydrogen engine for aircraft

    TERWILLIGER NEIL J / STAUBACH JOSEPH B | Europäisches Patentamt | 2024

    Freier Zugriff

    Hybrid electric hydrogen engine for aircraft

    TERWILLIGER NEIL J / STAUBACH JOSEPH B | Europäisches Patentamt | 2024

    Freier Zugriff

    HYBRID ELECTRIC HYDROGEN ENGINE FOR AIRCRAFT

    TERWILLIGER NEIL J / STAUBACH JOSEPH B | Europäisches Patentamt | 2024

    Freier Zugriff

    HYBRID ELECTRIC AIRCRAFT ENGINE

    ZATORSKI DAREK TOMASZ / HIGGINS CRAIG WILLIAM | Europäisches Patentamt | 2022

    Freier Zugriff