The invention provides a long-
cantilever large-scale integral blade-disc blade one-step milling method and belongs to the technical field of aeroengines. The long-
cantilever large-scale integral blade-disc blade one-step milling method comprises the following steps of 1, cutter selection, 2, five-axis
processing anti-interference calculation, 3, five-axis
processing cutter locus design: 1), integral spiral cutter locus design and 2), blade root and channel cutter locus design, and 4, milling. The long-
cantilever large-scale integral blade-disc blade one-step milling method adopts an integral spiral
milling cutter locus mode, realizes precise milling of blades by one-step clamping, eliminates secondary clamping errors, prevents
butt joint milling gear marks and effectively control
processing deformation. A gradient cutter
handle is used, stretches into a cavity groove and carries out milling so that the overhanging length of the cutter is at most shortened by 4 times than that of the cutter with the same size, processing vibration is effectively controlled, blade surface vibratory lines are eliminated and part surface quality is improved by one grade. Through the long-cantilever large-scale integral blade-disc blade one-step milling method, the non-standard cutter is changed to form a standard cutter so that all
milling cutter standardization is realized, milling efficiency is greatly improved and
machining efficiency is improved by 33%.