The invention relates to the technical field of aero-engine
titanium alloy rotor blade repair, in particular to a
stress regulation and control method for improving fatigue strength of a
titanium alloy rotor blade after
welding repair, which comprises the following steps: vacuum heat treatment, self-adaptive
machining, first vibration finishing,
laser shock
peening,
shot peening and second vibration finishing. Performing vacuum heat treatment on the blade subjected to
electron beam
welding repair; a
machining program is compiled,
machining is conducted on the patch repairing area, and the blade with the profile size meeting the use requirement is obtained; and after the first time of vibration finishing,
laser strengthening equipment is used for carrying out
laser strengthening on the blade area needing to be strengthened, shot blasting is carried out, then second time of vibration finishing is carried out, and the
stress regulation and control method is completed. The
vibration fatigue strength of the repaired blade is improved by 30% compared with that of a
welding heating treatment process, the service life of the blade is effectively prolonged, the use
performance requirement of parts is met, the maintenance and part replacement cost of an aero-engine is reduced, and the method has large
economic benefits.