journal article·2024-10-17

A new approach based on a concurrent cooling method during GTAW and DC-LSND welding to mitigate residual stresses in Al 6061-T6

Hamed Hemmatpour, M. A. Mohtadi-Bonab

Publisher page

Abstract

Welding often induces residual stresses and undesired distortion in components. The negative impacts of these detrimental residual stresses have prompted researchers to explore methods for preventing or mitigating these stresses. Altering the temperature history can influence residual stress, and employing cold or heating techniques during welding has the potential to reduce harmful residual stress. In this study, the dynamically controlled low-stress no-distortion (DC-LSND) method with TIG welding was utilized to reduce the residual stresses in Al alloy 6061-T6. The methodology was simulated using Abaqus software, and the simulation results were validated with experimental data. The Al alloy served as the base metal, alloy (ER-4043) as the filler, and dry ice as the coolant. In the finite element analysis, the longitudinal residual stress at the center of the weld line in TIG welding was calculated to be 77 MPa. In the DC-LSND welding method, this value approached zero. Experimental measurements revealed residual stresses in the center of the welding line to be 183 MPa in conventional welding and 130 MPa in DC-LSND welding. According to the DC-LSND results, a 100% reduction in residual stresses was achieved in the finite element method. In the experimental test, a reduction of approximately 30% in residual stress was observed. The method developed in this research is recommended for application in welding metals and alloys where phase changes do not occur.
Source: openalex_inverted_index · Quality: baseline

Research context

OpenAlex topics: Welding Techniques and Residual Stresses · Advanced Welding Techniques Analysis · Non-Destructive Testing Techniques

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Department of Mechanical Engineering, Amirkabir University of Technology, Tehran, Iran

Department of Mechanical Engineering, University of Bonab, Bonab, Iran

Funding

Amirkabir University of Technology · University of Bonab

References (25)

Show source-provided references
1. 10.1016/j.matdes.2021.10992410.1016/j.matdes.2021.109924 ↗
2. 10.1016/j.prostr.2020.12.00610.1016/j.prostr.2020.12.006 ↗
3. 10.1016/j.actamat.2009.07.05510.1016/j.actamat.2009.07.055 ↗
4. 10.1016/j.engfailanal.2020.10478710.1016/j.engfailanal.2020.104787 ↗
5. 10.1080/01694243.2021.188436010.1080/01694243.2021.1884360 ↗
6. 10.3390/met1204065410.3390/met12040654 ↗
7. 10.3390/ma1215243610.3390/ma12152436 ↗
8. 10.1016/j.cma.2004.03.00710.1016/j.cma.2004.03.007 ↗
9. 10.1080/0950711970945441110.1080/09507119709454411 ↗
10. 10.1115/1.254070810.1115/1.2540708 ↗
11. 10.3390/met1211183110.3390/met12111831 ↗
12. 10.1016/j.matdes.2017.11.01610.1016/j.matdes.2017.11.016 ↗
13. 10.1080/01694243.2018.153915810.1080/01694243.2018.1539158 ↗
14. 10.1080/01694243.2019.165359310.1080/01694243.2019.1653593 ↗
15. 10.1016/j.matdes.2013.02.08110.1016/j.matdes.2013.02.081 ↗
16. 10.1080/13621718.2016.118086110.1080/13621718.2016.1180861 ↗
17. van der Aa EM. Local cooling during welding: prediction and control of residual stresses and buckling distortion [PhD thesis]. Delft The Netherlands: Department of Materials Science Delft University of Technology; 2007.
18. 10.1016/j.msea.2009.11.04410.1016/j.msea.2009.11.044 ↗
19. ASTM. Standard test method for determining residual stresses by the hole-drilling strain gage method in E837-13a; 2013.
20. 10.1016/j.commatsci.2007.12.00610.1016/j.commatsci.2007.12.006 ↗
21. 10.1177/1464420722110847110.1177/14644207221108471 ↗
22. Bagshaw N Olden E Bertaso D. Numerical simulation and experimental validation of low stress no distortion (LSND) welding in 304 stainless steel – report 780/2003. The Welding Institute (TWI); 2003.
23. 10.3390/ma1518645110.3390/ma15186451 ↗
24. 10.1007/s12666-018-1401-110.1007/s12666-018-1401-1 ↗
25. 10.1080/13621718.2018.156447310.1080/13621718.2018.1564473 ↗