The invention relates to the technical field of aeroengines, in particular to a method for
welding a
combustor liner and tile pads of an aeroengine. The method for
welding the
combustor liner and thetile pads of the aeroengine comprises floating tile blocks and studs, and the floating tile blocks and the studs use
forging pieces as raw materials, and the
welding technological steps of the floating tile blocks and the studs are as follows: (1)
machining; (2) surface treatment; (3) clamping; (4)
stud welding; (5) gripping and repairing; and (6) inspection. By adopting the method disclosed by the invention, the studs are welded to the floating tile blocks by adopting a
argon arc welding way, and the verticality deviation of the studs is larger; meanwhile, the phenomenon of incomplete fusionin a central area on which the studs are connected with the floating tile blocks possibly occurs so as to affect the welding strength and low welding and positioning precision of the studs; by adopting an overall
machining way, the
metal cutting quantity is large, so that a material utilization ratio of the materials is low, and a
machining period is long; and moreover, in a machining and cuttingprocess, high-temperature
cutting heat deformation easily occurs, and a destressing heat treatment procedures are required after machining, so that the problems of the production cost and the periodsare further increased.