There is provided a fuel system (1) for an aircraft. The fuel system comprises a fuel tank (10) for storing fuel (102) during operation of the aircraft and a diffuser (11) disposed inside the fuel tank (10). The diffuser is configured such that it forms part of a flow path configured to connect a fuel source to the inside of the fuel tank. The diffuser (11) comprises a wall (111) which at least partially defines an internal space (113) of the diffuser; an opening (13) in the wall (111), which provides access to the internal space; and a blocking component (12a) configured to block the opening (13).


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    Title :

    FUEL TANK DIFFUSER


    Additional title:

    KRAFTSTOFFTANKDIFFUSOR
    DIFFUSEUR DE RÉSERVOIR DE CARBURANT


    Contributors:
    BONTE ERIC (author) / PETIT DAVID (author) / PEACHEY DANIEL (author)

    Publication date :

    2024-10-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60K Anordnung oder Einbau von Antriebseinheiten oder von Kraft- bzw. Drehmomentübertragungen in Fahrzeugen , ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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