The invention discloses a multi-stage rotor
assembly method based on four-in-one-axis cooperative regulation and control, and belongs to the technical field of aero-engine manufacturing. The four-in-one is a combination of a rotation axis, a geometric axis, an
inertia main shaft and a
mass center axis. The multi-stage rotor assembling method is realized through the following steps of S1, obtaining rotor size characteristics, geometric errors,
mass center coordinates and the
inertia main shaft; s2, establishing a
geometric error representation model of the single-stage rotor; s3, establishing an error
transfer model of multi-stage rotor
assembly; s4, calculating end surface
centroid and
centroid coordinates of each stage of rotor after
assembly; s5, fitting the rotation axis, the geometric axis and the
mass center axis; s6, solving an
inertia tensor matrix under the assembly coordinate
system; s7, calculating an inertia main shaft inclination angle under the assembly coordinate
system; and S8, four-axis-in-one assembling regulation and control are carried out. The problem that vibration exceeds the standard under the ultrahigh rotating speed due to low manufacturing precision of an aero-engine rotor can be solved.