The invention discloses a hydraulic buffer type
electromagnetic drive rotor-static rub-
impact device and a test method, and relates to the technical field of aeroengine blade rub-
impact tests. The hydraulic buffer type
electromagnetic drive rotor-static rub-
impact device comprises a shell and an
electromagnetic coil arranged at the end of the shell; the hydraulic
damper sequentially penetrates through the
electromagnetic coil and the shell, the three-way
force sensor and the rub-impact head are sequentially arranged at the telescopic end of the hydraulic
damper, the permanent
magnet is arranged at the end, away from the shell, of the hydraulic
damper in a sleeving mode, and the
electromagnetic coil is arranged on the outer wall of the hydraulic damper in a sleeving mode, one end of the first spring is connected with the shell, the other end of the first spring is connected with the shell, the
PID controller is electrically connected with the three-way
force sensor and used for controlling the magnitude of current of the electromagnetic coil in real time, the rub-impact head extends out of the shell and is arranged to be away from the end of the electromagnetic coil, the hydraulic damper is arranged to provide constant abutting force for the rub-impact head, and the problem that the rub-impact head retracts is solved; the current of the electromagnetic coil can be controlled in real time through the
PID controller, so that the adsorption force of the electromagnetic coil to the permanent
magnet is adjusted, and the stability of the rub-impact force is ensured.