Compared with the tradtional manual drilling technology

the application of automatic drilling technology in aircraft assembly has become an inevitable trend. In order to improve the efficiency and quality of drilling

the automatic drilling equipment is used in the assembly of certain aircraft parts. The experiments and analysis were carried out for the technical problems encountered in the application of the automatic drilling equipment and the processing parameters such as pressure

speed and feed rate were determined

the problem of low rigidity of parts was solved

the date processing flow was optimized

and the optimized process flow was introduced.