An aircraft engine electric
oil pump center
plunger rod anti-disengaging clamping ring disassembling and assembling tool comprises a base, a cylinder body connecting lug and a pair of guide rods are arranged on the base, a lifting frame is arranged on the guide rods in a sliding and sleeving mode, a disassembling and assembling mechanism is arranged in the center of the lifting frame in a hanging mode, and the disassembling and assembling mechanism is located over the cylinder body connecting lug. The center
plunger rod is sleeved with the disassembling and assembling mechanism, and the disassembling and assembling mechanism is in threaded connection with the center
plunger rod. The disassembling and assembling mechanism comprises a lifting cylinder, the lower end of the lifting cylinder extends into the engine electric
oil pump, the center plunger rod is sleeved with the lifting cylinder, and the lifting cylinder is installed on the lifting frame in a suspended mode and synchronously ascends and descends along with the lifting frame. A cutter mounting base is arranged at the lower end of the lifting cylinder, and a cutter
assembly is detachably mounted on the cutter mounting base. The top face of the lifting cylinder is connected with a driving nut (54), and the driving nut (54) is in threaded connection with threads on the center plunger rod. According to the tool, the anti-disengaging clamping ring of the center plunger rod of the electric
oil pump of the engine can be rapidly disassembled and assembled, positioning is accurate, operation is easy, disassembling and assembling precision is high, and efficiency is high.