The invention relates to an aircraft fuel dual-pipe balanced pressure refueling device and a control method thereof, comprising a refueling system and a control system, the refueling system including a pipeline centrifugal pump, a ball valve, a joint valve, a pressure sensor, a pressure flow controller, a safety valve, a pressure flow The controller is connected to the No. 1 branch and the No. 2 branch. Both the No. 1 branch and the No. 2 branch include fuel filters, flow meters, electro-hydraulic valves, refueling hoses and refueling connectors in series. The No. 1 branch also includes A Venturi tube is installed, and the control system includes a conversion power supply, an electrical control box, a quantitative controller, and a display operation interface. The control system is electrically connected to a pipeline centrifugal pump, a pressure sensor, a flow meter, and an electro-hydraulic valve. The invention can realize double-pipe balance pressure refueling function, and can ensure the constant pressure of the refueling port and the safety of refueling. At the same time, the invention can monitor the flow rate and realize the automatic end of refueling. The invention has convenient operation, high refueling efficiency and precision.