The application discloses a parameter optimization configuration method of a heavy-load three-coordinate
numerical control positioner, belongs to the technical field of
aerospace tooling equipment, and is used for solving the problems of scattered parameter selection of an existing positioner, easy parameter redundancy, and deformation out of tolerance under
heavy load. The scheme constructs a closed-
loop optimization process including basic
motion parameter threshold determination, multi-dimensional
verification of a three-shaft
ball screw transmission system, configuration of a roller linear rail and a hard rail combined structure,
servo drive
system matching, and finite element whole
machine deformation
verification. Differentiated load calculation and
verification rules are set for two types of positioners, namely, a straight column type and a
cantilever type. The method can realize the collaborative
adaptation of the
load bearing capacity,
motion accuracy and
structural rigidity of the positioner, greatly shortens the
design cycle, reduces the iteration cost, meets the application requirements of high-precision
pose adjustment of
aerospace large components, bears well, scientifically distributes stress, has high stability, has a large safety factor, and has strong overload capacity and
impact resistance.