检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
机构地区:[1]上海交通大学上海市复杂薄板结构数字化制造重点实验室,上海200240 [2]上海飞机制造有限公司航空制造技术研究所,上海200436
出 处:《上海交通大学学报》2016年第4期595-600,607,共7页Journal of Shanghai Jiaotong University
基 金:国家自然科学基金(51275292);国家商飞制造工程技术研究中心创新基金(SAMC13-JS-15-026)资助
摘 要:利用主应力法推导了铆接壁板所受压力的力学公式,将壁板等效为厚壁圆筒,根据空间轴对称问题求解方法,得出铆接孔孔壁处径向和周向残余应力的表达式,理论分析结果可以合理解释镦头高度和钉孔直径对孔壁处残余应力的影响规律:随着镦头高度和钉孔直径的变化,孔壁各处径向残余应力的变化并不明显,而周向残余应力的变化十分显著;镦头高度和孔径尺寸的增加使周向残余压应力的绝对值下降,甚至出现残余压应力转变为残余拉应力的情况.对于孔壁处残余应力沿板厚方向的分布,采用有限元方法进行分析.结果表明,上、下壁板间应力存在突变,下壁板孔壁处残余应力呈"C"型分布.得出铝锂合金材料在自动钻铆过程中相关工艺参数的合理取值.Residual stress induced by riveting process is critical to the fatigue life of riveted structures.In this paper,the principal stress method was employed to calculate the pressure on the surface of rivet hole and the stress between upset head and sheet.The radial and circumferential residual stresses were solved by using the spatial axisymmetric elastoplasticity theory,where the sheets were equivalent to a thickwalled cylinder.The change of residual stresses caused by various process parameters was explained by the analytical results reasonably.The results show that the circumferential residual stress decreases with the increase of the upset head height and the rivet hole diameter.However,the radial residual stress is approximately independent of the two parameters.The distribution of residual stress on the surface of rivet hole along the thickness direction was investigated by using the finite element method.The results indicate that the residual stress on the faying surface is discontinuous.A C-shaped distribution of residual stress was introduced into the surface of rivet hole in the lower sheet.Reasonable process parameters were given for the Al-Li alloy sheets in the automatic drilling riveting process.
分 类 号:V261[航空宇航科学与技术—航空宇航制造工程]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:216.73.216.249