An aircraft engine is provided. The aircraft engine includes a compressor section having a compressor. A turbine section is downstream of the compressor section. The turbine section includes a turbine having turbine blades arranged in counter rotating stages. The aircraft engine further includes one or more fluid supply lines and a fuel cell assembly fluidly coupled to the one or more fluid supply lines for receiving one or more input fluids. The fuel cell assembly is in fluid communication with the turbine section to provide one or more output products to the turbine section. The aircraft engine further includes a heat exchanger in fluid communication with the turbine downstream of the counter rotating stages of turbine blades to receive exhaust gases from the turbine. The heat exchanger is thermally coupled to the one or more fluid supply lines of the fuel cell assembly.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Gas turbine engines with a fuel cell assembly


    Beteiligte:

    Erscheinungsdatum :

    10.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    TURBINE ENGINES HAVING HYDROGEN FUEL SYSTEMS

    HOLLEY BRIAN M / STAUBACH JOSEPH B / MULDOON MARC J et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Fuel cell engines

    Mench, Matthew M. | TIBKAT | 2008


    GAS TURBINE ENGINES HAVING CRYOGENIC FUEL SYSTEMS

    JOHNSON STEVEN B / MURPHY ANDREW J | Europäisches Patentamt | 2022

    Freier Zugriff

    Electrical wiring assembly for gas turbine engines

    WILLMOT MICHAEL / BROUGHTON PAUL / PEACE RICHARD et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    Fuel System Requirements for Small Gas Turbine Engines

    Moore, R. G. | SAE Technical Papers | 1974