The invention belongs to the technical field of fuel accessories of aircraft engines, and relates to a hydraulic stability adjusting device composed of a piston damping and a variable throttle nozzle.The hydraulic stability adjusting device comprises a piston shell (1), a spring seat (2), a first damping spring ( 31), a second damping spring (32), a piston (4), a first piston spring seat (51), asecond piston spring seat (52), an adjustable spring seat (7), a support (81), a plug (82), a nozzle (10) and a throttle adjusting nail (11), wherein three pipelines are arranged outside the piston shell (1), the first pipeline is an oil inlet, the second pipeline is connected with an oil outlet of the nozzle (10), and the third pipeline is connected with the oil inlet of the nozzle (10); the piston shell (1) is provided with an oil circuit communicating with the two sides of the piston (4); the throttle adjusting nail (11) is installed in the nozzle (10); and the hydraulic stability adjustingdevice provided by the invention has a small volume, simple structure, high reliability, and can adjust hydraulic stability effectively.