The present invention ensures explosion-proof performance without increasing the capacity for supplying nitrogen-enriched air in an aircraft fuel system having a ventilation function. An aircraft fuel system includes: fuel tanks; an NEA supply system; a left ventilation channel extending from a ventilation duct to a fuselage and leading into the tanks; and a right ventilation channel extending from a ventilation duct to the fuselage and leading into the tanks. The tank leading to the channel and the tank leading to the channel are separated by a central wall. The tanks communicate with each other through a fuel path, which allows, of fuel and gas, only the fuel to pass through, and float valves.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft fuel system and aircraft


    Beteiligte:

    Erscheinungsdatum :

    09.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Double-walled tube for aircraft fuel system, aircraft fuel system and aircraft

    ANTHONY BRYANT / COLLOT PHILIPPE / MILLIER JEROME | Europäisches Patentamt | 2025

    Freier Zugriff

    Aircraft fuel ventilation system and aircraft

    MAO DE'AI / SHAO LIANG / HUANG PING et al. | Europäisches Patentamt | 2024

    Freier Zugriff


    AIRCRAFT SYSTEM, AIRCRAFT FUEL SYSTEM AND METHOD

    THORNER CALLUM / JAMES DYLAN BENEDICT / SAVIN DAVID | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft system, aircraft fuel system and method

    CALLUM THORNER / DYLAN JAMES / DAVID SAVIN | Europäisches Patentamt | 2023

    Freier Zugriff