Variable stroke fatigue test for aircraft landing gears

The fixed stroke fatigue test cannot simulate the real loading conditions of the landing gear, and the variable stroke fatigue test has increasingly become mainstream. A modular test device for fatigue tests for aircraft landing gears was designed, and the automatic control of the buffer stroke was realized with ectopic displacement control technology effectively. The horizontal loading cylinder could follow the wheel axis actively with the displacement active control technology. The follow-up loading along the vertical direction was realized by constructing a polar coordinate system and making the loading line automatic alignment. A split-type dummy wheel was designed to improve the loading accuracy, and a booster cylinder was designed to realize the control loading of high pressure combined with the hydraulic control system. The test results show that the technical scheme meets the design requirements, and the fatigue test was completed successfully. The device for landing gear variable stroke fatigue testing is appropriate for other landing gear static/fatigue tests.