Welding characteristics analysis and application on spacecraft of friction stir welded 2A14-T6 aluminum alloy
文献类型:期刊论文
作者 | Luo HT(骆海涛)6,7; Wu TK(武廷课)6,8; Fu J(富佳)6,7; Wang W(王巍)4,6; Chen N( 陈宁)4,6; Wang HN(王浩楠)4,6 |
刊名 | Materials |
出版日期 | 2019 |
卷号 | 12期号:3页码:1-17 |
ISSN号 | 1996-1944 |
关键词 | friction stir welding (FSW) finite element model (FEM) microstructure mechanical properties aerospace application |
产权排序 | 1 |
英文摘要 | According to the actual size parameters, the finite element model (FEM) of friction stir welding (FSW) was established, and the FEM was updated by experiments. The FSW of the 2A14- T6 high-strength aluminum alloy was simulated under a reasonable welding process parameter range, and the welding process parameters with good simulation effect were determined. The test was carried out under the same parameters, and the axial force of the FSW tool and temperature of the workpiece measuring point were collected. The comparison between the simulated data and the experimental data is reasonable, indicating the correctness of the FEM. The microstructure analysis of the welded joint shows that the grain size in the upper part of the weld nugget was smaller than that in the middle and lower parts, and there are obvious boundaries of grain size in each region of the joint. The hardness of the joint in the upper layer is higher than that in the middle and lower layers, and the minimum Vickers hardness value of the joint appears near the interface between the thermo-mechanically affected zone and the heat-affected zone on both sides of the weld. Tensile testing shows that the strength coefficient of the joint reaches 82.5% under this process parameter, and the sample breaks at the intersection of the material flow during stretching. After analyzing the final mechanical properties of the joint, we found that a degree of aerospace application can be achieved. Under this parameter, the welding test was carried out on the top cover of the rocket fuel tank. Firstly, melon valve welding, which is relatively difficult in welding conditions, was carried out, and a high-quality joint with good surface and no defects was obtained. |
WOS关键词 | MECHANICAL-PROPERTIES ; PROCESS PARAMETERS ; MICROSTRUCTURE ; JOINTS ; TEMPERATURE ; SIMULATION ; EVOLUTION ; 6061-T6 ; TORQUE |
资助项目 | National Natural Science Foundation of China[51505470] ; Youth Innovation Promotion Association, CAS ; JXS innovation fund, SIA |
WOS研究方向 | Materials Science |
语种 | 英语 |
WOS记录号 | WOS:000460768000149 |
源URL | [http://ir.sia.cn/handle/173321/24147] |
专题 | 沈阳自动化研究所_空间自动化技术研究室 |
通讯作者 | Luo HT(骆海涛) |
作者单位 | 1.Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, China 2.School of Mechanical Engineering, Shenyang Ligong University, Shenyang 110159, China 3.Institute of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819, China 4.Institute of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819, China 5.Institutes for Robotics and Intelligent Manufacturing, Chinese Academy of Sciences, Shenyang 110016, China 6.Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, China 7.Institutes for Robotics and Intelligent Manufacturing, Chinese Academy of Sciences, Shenyang 110016, China 8.School of Mechanical Engineering, Shenyang Ligong University, Shenyang 110159, China |
推荐引用方式 GB/T 7714 | Luo HT,Wu TK,Fu J,et al. Welding characteristics analysis and application on spacecraft of friction stir welded 2A14-T6 aluminum alloy[J]. Materials,2019,12(3):1-17. |
APA | Luo HT,Wu TK,Fu J,Wang W,Chen N,&Wang HN.(2019).Welding characteristics analysis and application on spacecraft of friction stir welded 2A14-T6 aluminum alloy.Materials,12(3),1-17. |
MLA | Luo HT,et al."Welding characteristics analysis and application on spacecraft of friction stir welded 2A14-T6 aluminum alloy".Materials 12.3(2019):1-17. |
入库方式: OAI收割
来源:沈阳自动化研究所
其他版本
除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。