A
turbine disc / blade tenon connection high-temperature combined
fatigue loading device comprises a low cycle load stress application mechanism, a force transmission pin, a force transmission main tension plate, a force transmission crown plate, a force transmission
round bar, a blade clamp, a rolling bearing, a hold-down bolt, a high cycle transmission plate, a high-frequency
heating cycle, and a vibration generator, wherein, the low cycle load stress application mechanism is connected with the force transmission main tension plate through the force transmission pin; the force transmission main tension plate is connected with the force transmission
round bar through the rolling bearing; the lower end of the force transmission crown plate is sleeved on the force transmission
round bar, and the upper end is connected with the
load bearing dummy club of the blade clamp through the rolling bearing; the blade clamp is connected with the blade of a
turbine through the hold-down bolt; the
turbine disc is connected with the low cycle load stress application mechanism through the force transmission pin; the high cycle transmission plate is connected with the blade clamp through the hold-down bolt; and the vibration generator is positioned on one side above a high cycle load transmission plate. The loading method is characterized in that the force application point of low cycle loads is moved backwards, thereby enabling small high cycle loads to be smoothly transferred to the tenon connection position, ensuring the
stress distribution along the tenon tooth is reasonable, and preventing combined loads from interfering with each other.