FIELD: aircrafts.
SUBSTANCE: invention relates to in-flight refueling systems for aircraft. The air refueling system contains refueling control system and auto-stabilized refueling device, which consists of two parts. The first part is a fixed stator formed by a nozzle (1), on which a protective shield (2) is fixed, and a contact cone (3) located at the end of the nozzle and facing the receiving aircraft. The second part is a movable rotor made with the possibility of rotation around the stator, including self-rotation under the action of an incoming air flow. The rotor is formed by three parallel platforms (4, 7, 10) located on a common shaft formed by a nozzle along the axis of the stator.
EFFECT: increase in system stabilization and simplification of the control process during docking is achieved.
1 cl, 2 dwg.
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