The invention discloses a circumferential contour prediction method based on
cutting force and deformation field space-
time correlation, and relates to the field of
aerospace, and the method comprises the following steps: 1, carrying out the spatial
discretization of a circumferential contour region of a target workpiece; step 2, establishing a lightweight structure
stiffness matrix; 3, constructing an elastic mechanism model and solving
delta-F mapping; 4, introducing the
time sequence correlation of the
cutting load into the elastic mechanism model; step 5, constructing a Boolean relationship between the
tool path and the workpiece envelope; step 6, fusing actual measurement process signals, and performing state correction; step 7, iterating the elastic model again by using the corrected load; and step 8, reconstructing full-field deformation based on
spatial correlation. According to the method, online prediction of the
station-level circumferential deformation field is achieved, the method can be used in the multi-procedure
machining process, deformation in-situ compensation of the procedure is achieved, a clamping positioning strategy of the next procedure is output, and the
manufacturing quality and the production efficiency are improved.