Deformation Analysis Method for Aeronautical Thin Walled Structures with Automated Riveting
The assembly variation of Aeronautical Thin Walled Structure (ATWS) with automated riveting is inevitable.The deformations of drilling,riveting and releasing are ralated to the final assembly variation.This paper represents a new method for deformation analysis of ATWS with automated riveting.Drilling deformation is modeled by the relationship among deflexion,strain and stress,riveting deformation is modeled by uilibrium equation,and releseaing deformation is modeled by releasing force.The comparison between computing result and expriment proves that the purposed deformation analysis method can solve the problem for ATWS automated riveting efficiently.
Deformation Aeronautical Thin-Walled Structures Automated Riveting Error
Hui Cheng Yuan Li Kaifu Zhang Feng Guo
The Ministry of Education Key Lab of Contemporary Design and Integrated Manufacturing Technical, Nor AVIC Xian Aircraft Industry(Group)Company LTD.
国际会议
香港
英文
1526-1530
2012-12-11(万方平台首次上网日期,不代表论文的发表时间)