The invention discloses a power
recovery type tester for a high-pressure large-flow
fuel pump, belongs to the technical field of aero-engine
fuel pump tests, and solves the problem of large
energy loss caused by the fact that redundant power of a tester is converted into heat dissipation. According to the technical scheme, the device mainly comprises a
hydraulic motor, a generator, a safety overflow valve, an
oil tank assembly and a refrigerating unit, one end of the
oil tank assembly is connected with the refrigerating unit, the other end of the
oil tank assembly is connected with a low-pressure
oil supply pump, the low-pressure
oil supply pump is connected with a tested piece, and one end of the tested piece is externally connected with a driving motor. One end of the
control system is connected with a power supply
system, the other end of the
control system is connected with a safety overflow valve and a
hydraulic motor, the
hydraulic motor is connected with a generator, the generator is connected with an SMM converter
system and an AEF
active front end, the SMM converter
system and the AEF
active front end are matched to control a load system, and the generator is connected with a refrigerating unit. The invention is mainly used for reducing the energy dissipation and the installed power of the system.