The application belongs to the technical field of aircraft in-flight refueling, and particularly relates to a test
simulation system and method for
fuel delivery characteristics of a refueling pod, comprising: a ground controller, a steel
fuel tank of a refueling aircraft, an in-flight refueling pump set, a
fuel delivery pipeline, a negative pressure
fuel tank of a
receiver aircraft, a flight environment pressure
simulation box, a ram
turbine pump of the refueling pod, an electro-hydraulic
proportional valve, a high-speed
hydraulic motor, a refueling hose, a refueling and receiving
assembly, a pressure regulating valve, a receiving flow regulating valve and a receiving flow sensor. The ground controller adjusts the rotating speed of the ram
turbine pump of the refueling pod directly connected with the
hydraulic motor through the electro-hydraulic
proportional valve according to the command of a pressure regulating controller of the refueling pod, so that the pressure regulating
process simulation of the refueling pod is realized. The ground test controller changes the opening degree of the regulating valve to simulate the change of the receiving flow, so that the
verification of the
fuel delivery characteristics of the refueling pod under different receiving flows is realized. The negative pressure
fuel tank of the
receiver aircraft is provided with an oil
discharge pump, so that the
continuous simulation of the receiving process is realized.