A cryogenic fueled aircraft propulsion system includes a core engine where fuel is mixed with compressed air and ignited to generate a high energy exhaust gas flow, a fuel system that is configured to supply the fuel to the core engine, a cryogenic fuel tank for storing fuel cryogenically in a liquid phase, a gas collection system where boil off gas from the fuel system is collected, a fuel cell system where a flow of collected boil off gas is utilized to generate electric power, and an electrical coupling where electric power generated by the fuel cell is communicated to location outside of the aircraft.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    CRYOGENIC FUEL BOIL OFF POWERED FUEL CELL


    Beteiligte:

    Erscheinungsdatum :

    01.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    CRYOGENIC FUEL BOIL OFF POWERED FUEL CELL

    TERWILLIGER NEIL J / MULDOON MARC J | Europäisches Patentamt | 2024

    Freier Zugriff

    Cryogenic fuel system with auxiliary power provided by boil-off gas

    GERSTLER WILLIAM DWIGHT / HUDY LAURA MICHELE / KALRA CHIRANJEEV | Europäisches Patentamt | 2016

    Freier Zugriff

    Cryogenic fuel system with auxiliary power provided by boil-off gas

    GERSTLER WILLIAM DWIGHT / HUDY LAURA MICHELE / KALRA CHIRANJEEV | Europäisches Patentamt | 2015

    Freier Zugriff

    Cryogenic Boil-Off Reduction System Testing

    W. D. Plachta / L. W. Johnson / R. J. Feller | NTIS | 2014


    Cryogenic Propellant Boil-Off Reduction Approaches

    Nast, Ted / Frank, David / Burns, K. | AIAA | 2011