The present application relates to a kind of thin-walled cabin section class part alignment method, belong to part
processing technical field, solve the problem that the precision of
machining reference cannot be ensured in prior art for the part with large shape
surface deformation and no
machining allowance.The method comprises: taking a point on the part as zero point O, and based on the zero point O, scanning the part, establishing theoretical three-dimensional coordinate
system XYZ in the three-dimensional model of the part;In three-dimensional model, construct plane ABC;Adjust the position of the part until the normal vector a of plane ABC coincides with the Z axis of theoretical three-dimensional coordinate
system XYZ;In three-dimensional model, construct new plane DEP, plane FGQ;In three-dimensional model, adjust the position of plane DEP, plane FGQ, so that the included angle β and γ between the normal vector b, c of plane DEP, plane FGQ and normal vector a are 90°.Realize that under the condition that the shape of the part is deformed relatively large, the part can be aligned more accurately.