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


    Publication date :

    2021-01-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



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