FIELD: aviation.
SUBSTANCE: invention relates to a device for refueling an aircraft. Device (2) contains pipeline (40) for fuel supply, at far end (43) of which wing connector (42) is mounted for connection to an inlet of a fuel tank of the aircraft. The wing connector contains case (421) forming a channel for fuel passage at the end of the pipeline, sensor (501) for measuring a value of a parameter characterizing a fuel flow passing through this wing connector, and at least one battery (502) for electric energy supply to the sensor. The sensor and the battery are placed in two half-shells (500A, 500B) mounted around case (421) of wing connector (42).
EFFECT: increase in the reliability, and elimination of the need for modification of a structure of a case of a wing connector or its inner mechanisms.
13 cl, 16 dwg
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