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.
DISPOSITIF D'AVITAILLEMENT D'UN AÉRONEF ET PROCÉDÉ DE FABRICATION D'UN ACCROCHEUR D'AILE POUR UN TEL DISPOSITIF
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
2022-11-09
Patent
Electronic Resource
French
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 |
European Patent Office | 2019
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