期刊文献+
共找到3篇文章
< 1 >
每页显示 20 50 100
Numerical analysis of temperature profile and weld dimensions in laser + GMAW hybrid welding of aluminum alloy T-joint
1
作者 胥国祥 武传松 +1 位作者 秦国梁 王旭友 《China Welding》 EI CAS 2013年第3期51-55,共5页
The temperature fields in the transient state and weld dimensions in laser + gas metal arc welding (GMAW) hybrid welding of aluminum alloy T-joint for different welding conditions were calculated using the develope... The temperature fields in the transient state and weld dimensions in laser + gas metal arc welding (GMAW) hybrid welding of aluminum alloy T-joint for different welding conditions were calculated using the developed heat source model, and the effect of welding speed on them was analyzed. The results show that the temperature field for the first weld pass only shows the feature of GMAW and the one for the second weld pass has the characteristics of both laser welding and GMAW. Welding speed can affect greatly weld dimensions and temperature distribution. When welding speed reaches 3.5 m/min, the fusion zones of two weld passes are separated and the maximum peak temperature of thermal cycle on the workpiece surface decreases largely. 展开更多
关键词 hybrid welding aluminum alloy temperature field T-JOINT numerical simulation
在线阅读 下载PDF
Fatigue Crack Growth Behavior of Different Zones in an Annealed Automatic Gas Tungsten Arc Weld Joint of TA16 and TC4 Titanium Alloys
2
作者 SHAO Ling WU Sujun +3 位作者 PENG Wenya DATYE Amit JU Hongbo LIU Ying 《Journal of Wuhan University of Technology(Materials Science)》 SCIE EI CAS 2020年第6期1090-1097,共8页
Based on the investigated microstructure of different zones in the annealed automatic gas tungsten arc weld joint of TA16 and TC4 titanium alloys,the mechanical property of them was assessed under fatigue crack growth... Based on the investigated microstructure of different zones in the annealed automatic gas tungsten arc weld joint of TA16 and TC4 titanium alloys,the mechanical property of them was assessed under fatigue crack growth rate tests.For evaluation of fatigue crack growth rate,three points bending specimens were used.The correlation between the range of stress intensity factor and crack growth rate was determined in different zones of the annealed weld joint.Fatigue crack growth rates were obviously different in different zones of weld joint of dissimilar titanium alloys,due to their different microstructures.Scanning electron microscope examinations were conducted on the fracture surface in order to determine the relevant fracture mechanisms and crack growth mechanisms with respect to the details of microstructure. 展开更多
关键词 dissimilar titanium alloys joining weld joint microstructure fatigue crack growth rate FRACTURE
在线阅读 下载PDF
Numerical Analysis of Welding Residual Stress and Distortion in Laser+GMAW Hybrid Welding of Aluminum Alloy T-Joint 被引量:13
3
作者 Guoxiang XU Chuansong WU +1 位作者 Xuezhou MA Xuyou WANG 《Acta Metallurgica Sinica(English Letters)》 SCIE EI CAS CSCD 2013年第3期352-360,共9页
A 3-D finite element model is developed to predict the temperature field and thermally induced residual stress and distortion in laser+GMAW hybrid welding of 6061-T6 aluminum alloy T-joint. And the characteristics of... A 3-D finite element model is developed to predict the temperature field and thermally induced residual stress and distortion in laser+GMAW hybrid welding of 6061-T6 aluminum alloy T-joint. And the characteristics of residual stress distribution and deformation are numerically investigated. In the simulation, the heat source model takes into account the effect of joint geometric shape and welding torch slant on the heat flux distribution and a sequentially coupled thermo-mechanical method is used. The calculated results show that higher residual stress is distributed in and surround the weld zone. Its peak value is very close to the yield strength of base metal. Besides, a large deformation appears in the middle and rear part of the weldment. 展开更多
关键词 Hybrid welding Residual stress Welding distortion Aluminum alloy T-joint Numerical simulation
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部