A cryogenic fueled aircraft propulsion system comprises a gas turbine engine mounted to a wing by an engine pylon, and configured to receive cryogenic fuel, the gas turbine engine comprising a core compressor. The propulsion system further comprises a pre-heater configured to heat the fuel prior to delivery to the gas turbine engine. The pre-heater is located within the engine pylon, aft of the engine core compressor.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    CRYOGENIC FUELLED AIRCRAFT PROPULSION SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    10.07.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Hydrogen fuelled aircraft propulsion system

    WILLMOT MICHAEL C / HUNT WILLIAM J | Europäisches Patentamt | 2025

    Freier Zugriff

    Hydrogen-fuelled aircraft power system

    PALMER CHLOE JO / TACCONI JACOPO | Europäisches Patentamt | 2024

    Freier Zugriff

    HYDROGEN-FUELLED AIRCRAFT POWER SYSTEM

    PALMER CHLOE JO / TACCONI JACOPO | Europäisches Patentamt | 2023

    Freier Zugriff

    Rising interest in gas-fuelled propulsion

    Woodyard, D. | Tema Archiv | 1997


    Development of a liquid nitrogen fuelled cryogenic engine

    Clarke, H. / Dearman, P. / Aryes, M. et al. | Tema Archiv | 2009