铝蜂窝的电阻点焊工艺及其结构的压缩性能
[Abstract]:In this paper, based on the application requirement of honeycomb energy absorption structure, the fabrication process of aluminum honeycomb resistance spot welding is studied, and the specimen of square aluminum honeycomb structure unit is prepared. The axial quasi-static compressive properties of the sample are tested at different temperatures. Compared with the quasi static compression test results of adhesive aluminum honeycomb structure specimens of the same size, the performance characteristics of spot welded square aluminum honeycomb structural units were investigated. At the same time, the axial compression behavior of resistance spot welding aluminum honeycomb structure element was simulated by Abaqus finite element method, and the deformation of aluminum honeycomb panel and the stress distribution around the solder joint were observed and analyzed. The optimum technological parameters of aluminum honeycomb resistance spot welding (welding voltage 250V, welding time 1.4s, electrode pressure 60N) were determined by observing the microstructure of weld pool and measuring the shear force of solder joint. The shear force and positive tensile force of single solder joint were 66.5 N and 30.9 N respectively. The compression stress-strain curves of aluminum honeycomb element specimens are divided into four stages: linear elastic deformation, initial peak yield, stable yield platform and compaction. By changing the number of solder joints to prepare aluminum honeycomb with different solder joint spacing, the quasi-static compression test shows that the stable yield platform stress of aluminum honeycomb compression increases with the decrease of solder joint distance. However, the solder joint distance has no significant effect on the initial peak yield strength of aluminum honeycomb. The sensitivity of resistance spot welding aluminum honeycomb to ambient temperature is less, from -50 掳C to 100 掳C, the initial peak yield strength of resistance spot welding aluminum honeycomb decreases 9.02 and the initial peak yield strength of adhesive aluminum honeycomb decreases 38.97. Based on the observation of compression process and finite element simulation of aluminum honeycomb structural unit specimen by resistance spot welding, the initial yield stacking of honeycomb occurs at the end of the structure, and then expands in turn, and there is no obvious stress concentration near the solder joint of aluminum honeycomb structure.
【学位授予单位】:哈尔滨工业大学
【学位级别】:硕士
【学位授予年份】:2017
【分类号】:TG453.9
【参考文献】
相关期刊论文 前10条
1 王琦;童国权;李晓青;陈峰;马振武;杨钦鑫;;点焊钛合金蜂窝芯平压性能模拟研究[J];航空制造技术;2016年18期
2 黄江平;满剑锋;杨建中;叶耀坤;刘荣强;邓宗全;;铝蜂窝材料温度环境适应性试验研究[J];载人航天;2016年03期
3 柳敏静;武湛君;;复合材料蜂窝夹层结构在飞机中的应用[J];科技导报;2016年08期
4 程文礼;袁超;邱启艳;王清明;陈静;;航空用蜂窝夹层结构及制造工艺[J];航空制造技术;2015年07期
5 孙德强;罗显洲;方众望;张小强;高芬;赵建伟;;多层规则排列圆形铝蜂窝共面缓冲优化[J];包装工程;2014年19期
6 姜立标;习成;李金水;区廷杰;邝贺林;;铝蜂窝夹层材料在客车噪声控制的应用研究[J];汽车零部件;2014年03期
7 孙德强;孙玉瑾;郑波波;王庆庆;李文娥;王晨阳;孙建建;;正方形蜂窝芯材共面冲击力学性能[J];包装工程;2014年03期
8 孙德强;孙玉瑾;郑波波;王庆庆;李文娥;王晨阳;孙建建;张超;;六边形蜂窝芯异面类静态压缩力学行为的仿真分析[J];包装工程;2014年01期
9 胡玲玲;尤帆帆;;铝蜂窝的动态力学性能及影响因素[J];爆炸与冲击;2012年01期
10 梁森;陈花玲;;常见蜂窝胞元轴向承载能力研究[J];四川兵工学报;2011年01期
相关博士学位论文 前4条
1 彭明军;钎焊蜂窝铝板力学性能研究[D];昆明理工大学;2013年
2 孟黎清;飞机蜂窝结构动态冲击下的破坏机理及吸收能量分配机制[D];太原理工大学;2011年
3 芦颉;金属蜂窝夹芯结构的疲劳行为研究[D];哈尔滨工程大学;2011年
4 栾旭;金属蜂窝夹芯板疲劳和冲击力学性能研究[D];哈尔滨工业大学;2009年
相关硕士学位论文 前10条
1 贾培奇;蜂窝铝材料面内尺寸效应及应变率影响研究[D];太原理工大学;2016年
2 唐爽;铝蜂窝静动态压缩行为研究[D];中南大学;2014年
3 李欣;镁合金无损精密成型与蜂窝结构制备研究[D];西南交通大学;2014年
4 苏小丽;钛合金蜂窝芯制造技术研究[D];南京航空航天大学;2014年
5 杨宇;金属蜂窝夹层结构的力学性能分析[D];哈尔滨工业大学;2013年
6 徐天娇;六边形铝蜂窝力学行为的尺寸效应研究[D];太原理工大学;2013年
7 刘建华;夹层结构中蜂窝芯塌陷分析及改进工艺研究[D];天津大学;2013年
8 刘天宝;高强度铝蜂窝自动化组装工艺及设备的研究[D];重庆理工大学;2013年
9 张小波;复合材料蜂窝结构面外静、动力屈曲研究[D];华中科技大学;2013年
10 刘叶花;胞元结构参数对蜂窝铝芯力学性能的影响研究[D];湘潭大学;2012年
,本文编号:2219293
本文链接:https://www.wllwen.com/kejilunwen/jiagonggongyi/2219293.html