南京航空航天大学学报2012，Vol.44Issue(z1)：9-14,6.
飞机总装自动化制孔预装配紧固件安装位置优化
Optimization of Tack Fastener Install Position for Automatics Drilling of Aircraft Final Assembly
摘要
Abstract
A finite element analysis (FEA) model is built for a case of typical location for middle-fuselage and middle-after fuselage section assembly. Then, the influence of pressure on interfacial clearance is analyzed based on the FEA model. Finally, the tack fastener install position is optimized by analyzing the effects of three different install positions on the inerfacial clearance.关键词
飞机装配/预装配紧固件/单向压紧/毛刺/有限元分析Key words
aircraft assembly/ tack fasteners/ one-side pressure/ burr/ finite element analysis分类
航空航天引用本文复制引用
曾长,王珉,陈文亮,余路,王宇波..飞机总装自动化制孔预装配紧固件安装位置优化[J].南京航空航天大学学报,2012,44(z1):9-14,6.基金项目
南京航空航天大学基本科研业务费专项科研(NS2010137)资助项目. （NS2010137）
