Aircraft refuelling device including a fuel circulation pipe of which the downstream end is equipped with a wing coupling for connecting it to an inlet orifice of a fuel tank of the aircraft. The wing coupling includes a body which defines a fuel circulation duct at the end of the pipe, a sensor for measuring the value of a parameter indicative of a flow of fuel passing through the wing coupling, and at least one battery electrically powering the sensor. The sensor and the electrical power supply battery are housed in two half-shells mounted together around the body of the wing coupling.


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    Title :

    DISPOSITIF D'AVITAILLEMENT D'UN AÉRONEF ET PROCÉDÉ DE FABRICATION D'UN ACCROCHEUR D'AILE POUR UN TEL DISPOSITIF


    Additional title:

    AIRCRAFT REFUELLING DEVICE AND METHOD FOR MANUFACTURING A WING COUPLING FOR SUCH A DEVICE
    FLUGZEUGBETANKUNGSVORRICHTUNG UND VERFAHREN ZUR HERSTELLUNG EINER FLÜGELKOPPLUNG FÜR SOLCH EINE VORRICHTUNG


    Contributors:
    BECK CLAUDE (author)

    Publication date :

    2022-11-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    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 / B67D Ausschenken, Abgeben oder Überleiten von Flüssigkeiten, soweit nicht anderweitig vorgesehen , DISPENSING, DELIVERING, OR TRANSFERRING LIQUIDS, NOT OTHERWISE PROVIDED FOR