The invention belongs to the technical field of aircraft
assembly and connection, and relates to an aircraft panel fixture clamping plate
assembly method, which comprises the following steps of: 1, in CATIA
software, determining two process OTP points according to two positioning holes in an angle seat, and converting an angle seat mounting surface into OTS data; 2, importing the coordinate values of the two process OTP points and OTS data into SA
software of a
laser tracker
operating system; step 3, establishing a coordinate
system based on a tool reference on the fixture, and roughly adjusting the angle seat in place by using two process OTP points; step 4, accurately adjusting the angle seat in place by using the OTS data of the angle seat, and installing a bolt for pre-positioning; and fifthly, the clamping plates are installed on the angle seats and firmly fixed through refined bolts. Sixthly, the OTP holes in the
cardboard are measured again through the
laser tracker, so that it is determined that the mounting position of the
cardboard meets the standard requirement; and step 7, in CATIA
software, extracting one plane of the card board as OTS data which can be identified by the
laser tracker, and rechecking and extracting the flatness of the plane by using the
laser tracker.