The invention discloses an aero-engine rib plate type part repairing method, and belongs to the technical field of aero-engine part
performance recovery. The aero-engine rib plate type part repairingmethod comprises the following steps: S1, part inspection is conducted, specifically,
fluorescence inspection is conducted on rib plate type parts with cracks, and the positions and the lengths of thecracks are determined; S2, cracks are removed and polished, a through groove with the width
ranging from 1 mm to 1.5 mm is polished in the length direction of the cracks, grooves are formed in the two sides of the through groove in the length direction, and oxides on the surfaces of the grooves and the
peripheral surfaces of the grooves are removed; S3,
welding repair is conducted, and direct-current fast-frequency pulse
welding is adopted; S4, heat treatment for eliminating
welding stress is conducted; and S5, post-welding inspection is conducted, specifically,
fluorescence inspection and X-
ray inspection are conducted on each weld joint. The aero-engine rib plate type part repairing method is effective, reliable, high in
operability, stable in welding parameter and simple in process, and the problem of crack repairing of aero-engine rib plate type parts can be effectively solved.