期刊文献+
共找到4篇文章
< 1 >
每页显示 20 50 100
Comparative study on forming limit prediction of AA7075-T6 sheet with M−K model and Lou−Huh criterion 被引量:12
1
作者 Guo-jiang DONG Zhi-wei CHEN +1 位作者 Zhuo-yun YANG Bo-cheng FAN 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2020年第6期1463-1477,共15页
In order to effectively predict the fracture of AA7075-T6 sheet, the forming limit curves of AA7075-T6 high-strength sheet were drawn according to Morciniak Kuczyski (M K) model and Lou Huh criterion, respectively. Th... In order to effectively predict the fracture of AA7075-T6 sheet, the forming limit curves of AA7075-T6 high-strength sheet were drawn according to Morciniak Kuczyski (M K) model and Lou Huh criterion, respectively. The errors between the predicted values of the two theoretical prediction models and experimental values were calculated by error analysis. The forming limit curves were verified by the punch stretch test to evaluate the prediction accuracy of M K model and Lou Huh criterion. The error analysis results show that the mean error of Lou Huh criterion with the optimal parameters for all tensile specimens is 25.04%, while the mean error of M K model for all tensile specimens is 74.24%. The prediction accuracy of Lou Huh criterion in predicting the fracture of AA7075-T6 sheet is higher. The punch stretch test results show that the forming limit curve drawn by Lou Huh criterion can effectively predict the fracture of AA7075-T6 sheet, but the prediction accuracy of M K model is relatively poor. 展开更多
关键词 ductile fracture criterion M K model forming limit diagram aa7075-T6 sheet
下载PDF
Effect of deep cryogenic treatment on the microstructural,mechanical and ballistic properties of AA7075-T6 aluminum alloy 被引量:1
2
作者 S.Dharani kumar U.Magarajan +1 位作者 Saurabh S Kumar Rodríguez-Millan M 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2023年第12期101-110,共10页
The study focused on investigating the effect of Deep Cryogenic Treatment(DCT)on the mechanical and ballistic properties of AA7075-T6 aluminum alloy.The microstructure,microhardness,tensile strength,and impact strengt... The study focused on investigating the effect of Deep Cryogenic Treatment(DCT)on the mechanical and ballistic properties of AA7075-T6 aluminum alloy.The microstructure,microhardness,tensile strength,and impact strength of the Base Material(BM)and DCT-treated 7075 samples were analyzed through metallographic analysis and mechanical tests.The microstructure of the DCT-treated 7075 samples revealed fine grains and a distribution of secondary phase particles.The tensile strength,impact strength,and microhardness of DCT-treated samples increased by 7.41%,4%,and 9.68%,respectively,compared to the BM samples.The fractography analysis of the tensile samples showed cleavage facets,microvoids,and dimples in both the samples.The ballistic behavior of the BM and DCT target plates were studied by impacting hard steel core projectiles at a velocity of 750±10 m/s.The target plates failed due to petaling and ductile hole enlargement,and the depth of penetration(DOP)of the DCT target was less than that of the BM target,indicating a higher ballistic resistance.The post-ballistic microstructure examination of the target plates showed the formation of an Adiabatic Shear Band(ASB)without any cracks.It was concluded that the DCT treatment improved the mechanical and ballistic properties of the aluminum alloy due to grain refinement and high dislocation density. 展开更多
关键词 Deep cryogenic treatment aa7075-T6 Mechanical properties BALLISTIC Adiabatic shear band
下载PDF
铝合金搅拌摩擦焊缝和母材疲劳裂纹扩展行为 被引量:6
3
作者 秦红珊 杨新岐 《航空材料学报》 EI CAS CSCD 北大核心 2017年第5期41-47,共7页
对7075-T6和LC4CS两种铝合金搅拌摩擦焊缝的疲劳裂纹扩展(da/d N)行为进行实验研究,并与7075-T6母材疲劳性能进行对比分析。结果表明:沿焊缝中心、前进和后退边方向,7075-T6搅拌摩擦焊疲劳裂纹扩展速率da/d N均低于LC4CS的da/d N;但沿... 对7075-T6和LC4CS两种铝合金搅拌摩擦焊缝的疲劳裂纹扩展(da/d N)行为进行实验研究,并与7075-T6母材疲劳性能进行对比分析。结果表明:沿焊缝中心、前进和后退边方向,7075-T6搅拌摩擦焊疲劳裂纹扩展速率da/d N均低于LC4CS的da/d N;但沿垂直于焊缝方向两者da/d N基本一致;同种材料焊缝中心da/d N为最低,其次是后退边和前进边,而沿垂直焊缝方向da/d N为最高;7075-T6焊缝中心da/d N与其母材比较,低载荷ΔK下焊缝中心的da/d N较低、但高ΔK下母材的da/d N较低;在前进边、后退边和母材区域疲劳裂纹断口形貌明显不同,在母材区域可以观察到典型的疲劳条纹特征;但沿焊缝中心(焊核)的疲劳裂纹断口,没有任何疲劳条纹特征;7075-T6搅拌摩擦焊缝比LC4CS焊缝具有更好的抗疲劳裂纹扩展阻力,在高ΔK载荷下搅拌摩擦焊核区细小等轴晶粒不能提高疲劳裂纹扩展阻力。 展开更多
关键词 搅拌摩擦焊 7075-T6和LC4CS铝合金 疲劳裂纹扩展 疲劳断口
下载PDF
AA7075-T6铝合金电阻点焊工艺参数优化研究
4
作者 邱飒蔚 蒋家传 +3 位作者 叶拓 张越 雷贝 王涛 《材料导报》 EI CAS CSCD 北大核心 2024年第17期254-261,共8页
轻量化结构设计在保证了结构强度的前提下降低了整车质量,减少了能量消耗,成为汽车工业和航空航天的研究重点。本工作通过建立正交实验获取AA7075-T6铝合金的最佳焊接工艺参数。对接头进行拉伸剪切实验、金相观察和显微硬度测试,并对最... 轻量化结构设计在保证了结构强度的前提下降低了整车质量,减少了能量消耗,成为汽车工业和航空航天的研究重点。本工作通过建立正交实验获取AA7075-T6铝合金的最佳焊接工艺参数。对接头进行拉伸剪切实验、金相观察和显微硬度测试,并对最优参数组合进行数值模拟,以研究焊接工艺参数对接头质量的影响。结果表明:当焊接时间为60 ms、焊接电流为17 kA、电极压力为0.22 MPa时,点焊接头的综合力学性能最好;焊接参数对电阻点焊接头力学性能的影响顺序为焊接时间>焊接电流>电极压力。焊接过程数值模拟得到的熔核尺寸与实验结果一致。焊接过程发生飞溅和熔核存在缩孔缺陷,导致接头的力学性能较差,失效模式为界面断裂。由于焊接过程接头显微组织发生变化,接头显微硬度变化呈“W”形。 展开更多
关键词 aa7075-T6铝合金 电阻点焊(RSW) 工艺参数 显微硬度 数值模拟
下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部