The present invention discloses an aircraft and a retrofit cryogenic fuel system. The aircraft has a turbine engine (500) having a bleed air output line (501), a cryogenic fuel system (502) having a cryogenic fuel tank (504) for storing cryogenic fuel and a supply line (506) operably coupling the tank to the turbine engine (500), and an on board inert gas generating system (OBIGGS) (510) fluidly coupled to the bleed air output (501) and having a nitrogen rich stream output line (512) and an oxygen rich stream output line (514).


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    Titel :

    Aircraft and a retrofit cryogenic fuel system


    Beteiligte:

    Erscheinungsdatum :

    2015-09-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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