A fuel system for a gas turbine engine comprises an injector disposed to inject fuel and air into a combustor of the gas turbine engine. In a first embodiment, the fuel system further comprises an air separation module configured to supply oxygen-enriched air into the combustor via the injector for combustion. In a second embodiment, the fuel system further comprises a barbotage system and a heating element. The barbotage system is configured to feed hydrogen to the injector, and the heating element is configured to pre-heat the fuel.


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    Titel :

    Enhanced APU operability


    Beteiligte:

    Erscheinungsdatum :

    2019-09-03


    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



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    Inter-operability

    Armitt, J. A. / Institution of Mechanical Engineers; Railway Division | British Library Conference Proceedings | 1996


    Enhanced diesel fuel low temperature operability. Additive developments

    Brown,G.I. / Gaskill,G.P. / Exxon Chemical,Abingdon,GB | Kraftfahrwesen | 1990