The invention relates to the technical field of aero-engine
turbine rear casings, in particular to a clamp tool and an inner runner crack repairing and
deformation control method. The clamp tool comprises a supporting mechanism, an expansion mechanism, a pressing ring mechanism and a center shaft; the center shaft sequentially penetrates through the supporting mechanism, the expansion mechanism and the ring pressing mechanism. The expansion mechanism is arranged above the supporting mechanism, and the ring pressing mechanism is arranged above the expansion mechanism; the method comprises the steps of pre-
welding treatment, deformation
simulation of an inner runner workpiece, clamping of the inner runner workpiece,
welding repair and post-
welding quality and size inspection. According to the method, simplified
simulation analysis is conducted on workpiece welding before welding, the deformation trend and the main deformation or
residual stress area of the part are rapidly judged, the welding clamp tool is designed to achieve pre-deformation before welding and rigid fixing of the mounting edge, post-
welding deformation can be effectively reduced, size out-of-tolerance is prevented, the
rejection rate is reduced, and the repair cost is saved; and the post-weld heat treatment or vibration destressing procedure is omitted, the part
machining time is shortened, and the repairing efficiency is improved.