FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft refuelling systems. Aircraft fuelling hardware comprises the system of pipelines, fuel tanks, first valves, pressure or flow rate pickup, first valves drive and electronic control unit. Feed pipeline id connected with multiple pipelines feeding fuel into tanks via first valves. Said first valves allow the disconnection of every fuel tank from fuel feed pipeline and adjustment of parameters of the flow in valve channel by aforesaid drive. First valves comprise body to be set to several positions between completely open and completely closed states. Electronic control unit is adapted to adjustment of first valves channels with the use of data from pressure pickups or flow rate pickups. Tank refuelling process comprises fuel flow feed into fuel pipeline at preset rate, distribution of said preset flow rate between fuel tanks, evaluation of flow parameter by flow arte pickup or flow pressure pickup and adjustment of first valves channels by electronic control unit.
EFFECT: higher efficiency.
17 cl, 8 dwg
