Journal of Welding Science

In this research, the influence of friction stir welding parameters (tool traverse speed ranging from 50 to 150 mm/min, and tool rotational speed ranging from 300 to 1100 rpm) was investigated on the microstructure and mechanical properties of AA5052 aluminum/PP-Z30S polypropylene joint. Results showed that joint formation was accompanied by the formation of mechanical locks in the shape of anchor-like aluminum pieces. Decreasing the heat input (either by increasing the tool traverse speed or decreasing the tool rotational speed) resulted in the formation of larger anchors. The results of tensile-shear test showed that increasing the tool traverse speed from 50 to 100 mm/min led to an enhancement in the fracture load (by ~10%), while at higher traverse speeds, the fracture load decreased (from 235 to 181 N) due to the formation of defects and voids at the joint interface. An increase in the tool rotational speed from 300 to 900 rpm resulted in a superior fracture load (by 70%) due to the formation of anchors perpendicular to the polymer surface with greater penetration depth.

In this research, the effect of nickel powder as an interlayer and the tool penetration depth on the microstructure and mechanical properties of lap joints between aluminum 1050 (top sheet) and pure copper (bottom sheet), both with a thickness of 2 mm, was investigated. Nickel powder was added through a machined groove with a width and depth of 1 mm at the base of the aluminum sheet. Friction stir lap welding was performed using a hot work steel tool with a shoulder diameter of 16 mm, a pin diameter of 4 mm, a pin height of 2.1 mm, a rotational speed of 950 rpm, a feed rate of 85 mm/min, a tool tilt angle of 2°, and varying tool penetration depths of 0, 0.05, and 0.1 mm. The results revealed that in the sample with a 0 mm penetration depth, due to insufficient heat generation, defects such as tunnel voids were formed. Increasing the penetration depth to 0.05 mm resulted in the formation of uniform and thin intermetallic layers, including Al3Ni2, Al7Cu4Ni, and Cu3.8Ni at the interface, which enhanced joint quality and increased tensile strength to 185.2 MPa with a fracture strain of 8.7%. In the sample with a 0.1 mm penetration depth, thicker and less uniform intermetallic layers were formed, which, despite locally increasing hardness, led to a decrease in tensile strength and fracture strain to 136.6 MPa and 6.7%, respectively. This study demonstrates that under the conditions of this research, a tool penetration depth of 0.05 mm provides the optimal conditions for FSLW of aluminum-copper alloys using nickel powder.

In this research, the mechanical and microstructural properties of AISI 316L sheets welded by RSW method using copper interlayer were investigated. In this regard, two types of connections were made, one without the use of an interlayer and the other with the use of a copper interlayer in different currents. In order to choose the optimal current for both types of connections, tensile tests were first performed, and microstructural, microhardness, elemental evaluation and failure mode tests were conducted on the selected samples. According to the obtained results, by increasing the electric current, the heat input in the welding pool is sufficiently high and the microstructural and mechanical properties of the welding zone were improved(Conversion of coarse grain to fine grain). Also, due to the optimality of the electric current in both samples with and without the interface layer, both samples had environmental failure, which indicates the high strength of the interface and their welding point. Changes in the chemical composition in different welding zones were insignificant and the distribution of elements was uniform in all zones. Also, the hardness changes from the base metal to the center of the welding zone were in the order of welding zone > base metal > heat-affected zone, which was consistent with the results obtained from the microstructural investigations. According to the results obtained for both cases with and without the use of an interface layer, the resistance spot welding method showed a successful connection for both types of cases.

Plain carbon steels are widely utilized in various industrial applications primarily due to their low cost. However, these steels often fall short in terms of mechanical properties and wear resistance. The deposition of hard and wear-resistant coatings on these steels significantly enhances their performance and extends their range of applications. Colomonoy 6, is a nickel-based superalloy, enhance hardness, erosion resistance, wear resistance, and corrosion resistance on the applied surfaces. The study investigated the application of weld overlay using colomonoy 6 on a plain carbon steel, aimed to create a hard and wear-resistant surface. The overlaying processes were performed using plasma transfer arc welding and gas tungsten arc welding under identical conditions. Microstructural characteristics were examined through optical and electron microscopy, and Phase analysis was performed using X-ray diffraction technique. The wear behavior of the weld overlays was evaluated using pin-on-disc wear testing at three different temperatures: 25 °C, 300 °C, and 600 °C, using an alumina pin. The microstructural investigation revealed the formation of dendritic nickel-rich solid solutions and interdendritic carbide and boride phases within the overlays, contributing to improved hardness and wear properties. Results demonstrated that in both overlaying methods, the wear mechanism at room temperature was mild abrasive, whereas at 600 °C, it was plastic deformation, exhibiting a wear track depth of approximately 33-35 μm, and 50-55 μm, respectively. In both overlayed metals, an approximate Vickers hardness number of 600 was measured a 4-fold increase in hardness of substrate. This finding suggests that factors other than hardness, such as microstructural stability and phase distribution at elevated temperatures, play significant roles in wear performance.

In this study, the effect of friction stir welding on the microstructure and mechanical properties of Fe-24Ni-4Cr austenitic steel was investigated. For this purpose, a sheet with a thickness of 1 mm was subjected to friction stir welding using a WC-5%Co tool at a traverse speed of 100 mm/min and a tool rotational speed of 450 rpm. Electron backscatter diffraction (EBSD) analysis revealed that this process led to grain refinement and an increase in high-angle grain boundaries in the stir zone, attributed to dynamic recrystallization during welding. Phase maps indicated an increase in the BCC phase fraction in the stir zone compared to the base metal. Given the high strain rate and the presence of stabilizing elements, this phase was primarily strain-induced martensite. Mechanical property assessments showed a significant increase in the tensile strength of the stir zone (450 MPa) compared to the base metal (350 MPa). Moreover, the yield strength of the stir zone (388 MPa) was substantially higher than that of the base metal (145 MPa), which can be attributed to grain refinement, an increase in high-angle grain boundaries, a higher dislocation density, and martensite formation. However, the ductility of the stir zone decreased due to higher stress concentration and dislocation density in this region. These findings suggest that friction stir welding can be an effective method for enhancing the strength and hardness of austenitic steels, but process conditions must be carefully controlled to prevent reductions in toughness and ductility.

In this research, the ultrafine-grained (UFG) composite of AA2024 and AA5083 aluminum alloys was made by accumulative roll bonding (ARB) process and butt-welded by friction stir welding. Friction stir welding (FSW) is the best method for the joining of UFG strips. Microstructural investigations were performed by optical microscope and transmission electron microscope in the stir zone (SZ), thermo-mechanically affected zone (TMAZ) and heat affected zone (HAZ). The fine recrystallized structure with a grain size of about 900 nm was determined in the weldment. Due to the strengthening mechanisms of grain boundaries, nano-meter size precipitates and solid solution strengthening, the high strength of about 403 MPa was achieved. The presence of precipitates with homogeneous distribution in FSWed strips caused a high ductility of about 14% compared to the fabricated composite strips (6.9%). The high hardness of the SZ was caused by the formation of new equiaxed grains and fine precipitates, and also the decrease in the hardness of the HAZ was due to the dissolution and coarsening of T-phase precipitates.

Unlike conventional welding methods, joining titanium alloys to steels using ultrasonic welding does not result in the formation of brittle intermetallic compounds and high torsion, causing a reduction in the mechanical properties of the joint. Ultrasonic welding of the St12-CP.Ti samples was performed at constant parameters of 7 bars, 2 s and 1 kW and variable parameter of interlayer material (Cu, 70B and Zn). The investigation of samples by OM, SEM, shear-tensile and microhardness tests revealed that Zn and Cu samples had the lowest and highest bond densities, with 42.2 and 80.6 percent, respectively. The bond density and the strength of the sample with greater interlayer deformability have higher values. Due to the high plastic deformation capability of copper, the Cu sample has generated more heat and deformation at the joint interface than in the other samples. As a result, the microstructure underwent recrystallization and grain growth after enduring severe plastic deformation. Also, the highest hardness of the steel side equal to

In this study, 1 mm thick austenitic stainless steel 316L sheets were used for experimental testing. The experimental welding process was carried out using a Nd:YAG pulsed laser welding machine, and the welding simulation was performed using the SYSWELD software with a three-dimensional model for thermodynamic and mechanical analysis. The simulation results showed over 90% correlation with the experimental results. Analysis of experimental and numerical data revealed that at a constant voltage of 440 volts, decreasing the welding speed from 2 to 0.5 mm/s increased the overlap rate of pulses from 67% to 93% and the maximum average power density (EPPD) from 5963 to 21831 W/mm². Additionally, increasing the voltage from 440 to 480 volts at a constant speed of 1 mm/s raised the heat input from 114 to 138 J/mm and the weld depth from 0.56 to 0.66 mm. Due to the high cooling rate, the grain size of the weld metal became finer than the base metal (63% reduction in grain size). Two phases, austenite and ferrite, were observed in the weld metal, and the solidification mode was predicted to be FA.With an increase in welding speed from 0.5 mm/s to 2 mm/s at a constant voltage of 440 volts, the maximum tensile residual stress increased from 96 to 260 MPa due to reduced pulse overlap (from 93% to 67%), uneven heat distribution in the part, and the generation of thermal stresses. Furthermore, increasing the welding voltage from 440 to 480 volts at a constant speed of 1 mm/s caused the maximum tensile residual stress to rise from 124 to 152 MPa. The maximum hardness of the weld metal increased from 180 to 215 Vickers as the welding speed rose due to the prevention of carbon diffusion and an increased growth rate. However, with an increase in welding voltage and heat input (from 57 to 69 J/mm), the hardness decreased from 225 to 215 Vickers due to a reduction in thermal gradients and grain growth.

This research looks at how microstructure and mechanical properties change in resistance spot welds of QP980 advanced high-strength steel. It specifically focuses on the effects of zinc coating and how it influences weld nugget formation, mechanical properties, and fracture behavior. The study involved microscopic examinations, mechanical tests, and finite element simulations to determine the thermal history of different weld zones. A key finding was that rapid cooling during the welding process led to the formation of, metastable phases, such as martensite, in both the weld nugget and the heat-affected zone. A finite element model of the welding process was used to simulate heat distribution and analyze the microstructure in various weld regions. This model showed that reaching the peak temperature during four-pulse resistance spot welding is delayed. This delay, along with proper hold times, helps prevent the formation of voids. The simulated thermal history and the rapid heating/cooling conditions effectively predicted the evolution and transformation of the microstructure in different weld areas. It was found that the presence of a zinc coating, and the resulting reduction in electrical contact resistance, delayed the formation of the weld nugget at lower welding currents. However, at higher currents, the primary source of heat generation shifted from contact resistance to bulk resistance within the steel sheet. This led to larger weld nuggets in coated samples compared to uncoated ones. While uncoated samples showed higher weld nugget hardness (512 Vickers) and greater tensile-shear strength (with a maximum load-bearing capacity of 28.1 kN in uncoated samples versus 24 kN in coated samples), coated samples were able to achieve the critical weld nugget size for a change in fracture mode at lower welding currents (9 kA compared to 9.5 kA).

This study investigated the influence of resistance spot welding current intensity on the formation of liquid metal embrittlement (LME) cracks in galvanized advanced QP1180 steel. Galvanized steel sheets with a thickness of 1 mm were welded at currents of 6.5, 7, 7.5, and 8 kA. The results revealed that increasing the current significantly enlarged the weld nugget size, molten volume, electrode indentation, and the likelihood of LME crack formation. Microstructural analysis, elemental distribution, and crack characterization were conducted using optical and electron microscopy. The findings indicated that the weld zone microstructure primarily consisted of martensite, while the non-uniform distribution of zinc along grain boundaries facilitated the initiation and propagation of LME cracks. Cracks were predominantly observed at the periphery of the weld pool indentation and in the electrode-sheet contact area. This study demonstrates that controlling welding current intensity is a key factor in mitigating LME and improving the mechanical properties of joints in galvanized QP1180 steel. Optimizing welding parameters, particularly limiting current intensity, can prevent molten metal-induced cracking and enhance the durability and safety of automotive structures. Hardness profiling revealed peak hardness in the weld zone, followed by a gradual decrease toward the heat-affected zone (HAZ).

This study investigated the effects of pulsed current and constant current on the microstructure and mechanical properties of Hastelloy X superalloy welds produced by Gas Tungsten Arc Welding (GTAW), using ERNiCrMo-2 filler metal. Key microstructural parameters, such as elemental segregation, dendrite refinement, and weld metal uniformity, along with changes in weld strength and hardness, were examined and compared between the two welding modes. Microstructural evaluations were conducted using optical microscopy, Field Emission Scanning Electron Microscopy (FESEM), Energy Dispersive Spectroscopy (EDS), and X-ray Diffraction (XRD) for phase identification. Pulsed current welding resulted in a finer microstructure with more equiaxed dendrites, reduced elemental segregation, and a more uniform distribution of M₆C carbides. Furthermore, this process led to significant improvements in hardness, impact toughness, and tensile strength of the weld metal compared to constant current welding. Fracture analysis confirmed ductile fracture behavior in all specimens, consistent with the microstructural and mechanical findings. The results of this research highlight the importance of using pulsed current in GTAW as an effective method for controlling the microstructure and enhancing the mechanical properties of Hastelloy X alloy joints. 

The friction stir spot welding (FSSW) process is a solid-state welding technique recognized as one of the most significant advancements in metal joining over the past decade. In this study, the effects of rotational speed and tool contact time, with a unique design different from previous research, on the microstructure and mechanical properties of 5754 series aluminum alloy were investigated. The workpiece was clamped using a specialized fixture on a radial drilling machine, and welding operations were performed using a FSSW machine at different rotational speeds and various tool contact times. Subsequently, the microstructure, microhardness, and tensile-shear strength of the welded spot region were evaluated. The results showed that increasing the tool rotational speed and prolonging the tool contact time led to an improvement of approximately 105% in the tensile-shear strength. According to statistical analyses, the factors of rotational speed and tool contact time significantly affected the shear strength with a confidence level greater than 95%; however, statistical analyses revealed different results regarding the relationship between rotational speed, contact time, and hardness.

In this study, the Friction Stir Welding process was employed to repair artificial cracks and grooves in 7075 aluminum alloy. Samples with different groove depths (0.5, 1, 1.5, and 2 mm) were prepared and evaluated through experimental tests, metallographic analysis, tensile testing, and numerical simulation using Abaqus software. The results showed that the Friction Stir Welding successfully repaired the defects without creating voids or surface irregularities. Microstructural observations in the stir zone revealed that dynamic recrystallization led to the formation of fine and homogeneous grains, resulting in improved hardness and tensile strength. The specimen with a 1 mm groove depth exhibited the best mechanical performance, with a maximum hardness of approximately 109 HV and the highest tensile strength among all samples. Conversely, samples with 0.5 and 2 mm groove depths showed void formation and reduced strength due to insufficient or excessive heat input and uneven material flow. Both experimental and simulation results confirmed that a groove depth of 1 mm provides optimal conditions for defect repair in 7075 aluminum alloy.

Repair welding of nickel-based superalloy Inconel 939, which was under working conditions of 100,000 hours, was performed by gas tungsten arc welding using Inconel 617 filler metal. The main objective of this study is to investigate and analyze the challenges during welding such as irregular distribution of primary MC carbides and crack formation in the heat-affected zone, and also to investigate the effect of post-welding heat treatment cycle on the microstructure and hardness of different weld zones. During welding, a crack of 91 micrometers length was observed in the heat affected zone, which due to the presence of a liquation film and accumulation of carbides around the crack, the crack was categorized as a liquation crack. Then, due to post-welding heat treatment, improvement of microstructural characteristics and hardness of the weld zone, partial melted zone, and heat-affected zone was observed, which resulted in homogenization of the hardness profile of the weld. It was observed that post-welding heat treatment caused the crack formed during welding to grow and spread to reach a length of 386 micrometers, which was classified as a strain-aging crack due to its formation and growth during post-welding heat treatment. 

Nickel-based superalloys are among the most critical materials used in high-temperature components of gas turbines, where their replacement costs and potential turbine damage necessitate effective protection and repair strategies. Optimizing repair methods to enhance efficiency and reduce costs has therefore been a continuous focus. The aim of this study is to improve the repair process of Inconel 738LC superalloy by reducing the susceptibility to liquation cracking. Activated tungsten inert gas (A-TIG) welding was performed on Inconel 738LC using a welding current of 60 A. Titanium dioxide (TiO₂) powder was employed as an activating flux, and weldments with four flux concentrations were examined. The microstructure was characterized using optical microscopy and scanning electron microscopy. The results revealed that flux concentration had a significant influence on penetration depth, with a concentration of 1 g/mL producing the maximum effect. At this concentration, weld penetration increased by 68% and weld pool volume by 63%, while the heat-affected zone width decreased by 12%. Arc imaging and quantitative/qualitative analysis demonstrated a constricted and focused plasma arc column in the presence of TiO₂ flux. Microstructural examinations further revealed suppression of columnar dendrite growth. It was found that TiO₂ flux enhances weld penetration and pool volume by constricting the arc and activating a reversed Marangoni flow, while simultaneously reducing HAZ width. However, the increased weld pool volume also intensified contraction stresses, leading to liquation cracking in the weld with the largest pool volume.

In this study, the effects of welding current intensity (9 and 10 kA) and holding time (5 and 40 cycles) on the energy absorption and failure mode of a dissimilar joint between DP590 and HSLA440 steels in the resistance spot welding process were investigated. For this purpose, four parameter combinations were prepared, and a tensile–shear test was performed on each sample. The results showed that increasing the current from 9 to 10 kA at a holding time of 5 cycles led to an increase of about 1 kN in strength; however, at a hold time of 40 cycles, changing the current resulted in a decrease of approximately 1.6 kN in strength. Therefore, the role of current is limited and dependent on the saturation of the weld nugget diameter. In contrast, increasing the hold time from 5 to 40 cycles had the most significant effect, increasing the energy absorption by about 217 J. Failure mode analysis also revealed that samples with longer hold times predominantly exhibited pull-out failure (PF), absorbing significantly more energy compared to interfacial failure (IF). Overall, the results indicate that controlling cooling through increasing the holding time is the most effective factor in enhancing absorbed energy and altering the failure mode in DP590/HSLA440 joints.

In this research, the influence of various forge pressure values and also the chemical composition of different carbon steels on rotary friction welding of SS 304 to carbon steels has been investigated. The steel rods of AISI 1015, 1030, and 1045 have been RFWed to SS 304 using 20, 40, and 80 bar forge pressure. Results indicated the 40 bar forge pressure as the optimum value, and by applying pressures below this number, the material flow in the weld interface would be tackled, resulting in improper mechanical values. By exceeding the optimum forge pressure, most of the viscoplastic material inside the weld interface would be rejected from that area in the form of flash, causing the weld to be done at a relatively low temperature. Microstructural investigation has been done by optical and scanning electron microscopes. Results showed that the weld zone is extremely fine due to DRX, and in the interface, a pro-eutectoid ferrite layer is formed, which has an increasing width when the heat input increases. Tensile test results showed that the optimum weld specimen is the RFW of AISI 1030 to SS 304 using 40 bar forge pressure, 40 bar friction pressure, 5s friction time, and 1500 RPM rotational speed. This specimen has shown 116 % joint efficiency and 715 MPa ultimate tensile strength.

Welding is one of the methods of surface repair of cast irons. In this study, surface repair of gray cast iron was first performed by gas metal arc welding method with ER70S-6 welding wire under inter-pulse current, heat input of 393 J/mm and dilution of 17%. Also, to compare the results, two samples were welded with ENi-CI and E6013 covered electrodes. Microstructural studies showed that the microstructure of the interface of the sample is composed of martensite with fine lathes and upper bainite. Despite the presence of cementite (Fe₃C) next to alpha iron (α-Fe) in the interface area, the formation of incomplete mixing zone with bainite lathes in the ferrite zone has led to increased toughness and prevented crack formation. The hardness of the ER70S-6 sample was similar to that of the E6013 sample at the interface, at about 809 Vickers, which is 334 Vickers higher than the hardness of the ENi-CI sample. The results of the open circuit potential and potentiodynamic polarization tests showed that the ER70-CI sample, with a corrosion potential and current of -653 mV and 6.8 μA/cm², had a higher polarization resistance and was more resistant to galvanic corrosion than the ENi-CI sample (-622 mV and 8.9 μA/cm²).

In this study, the metallurgical and mechanical properties of the interface obtained by explosive welding of 8-92 phosphor bronze to St37 carbon steel were investigated. The effects of explosive welding parameters such as explosive charge amount and stand-off distance on the shape and microstructure of the interface, mechanical properties and corrosion behavior were investigated. The results showed that with increasing stand-off distance and explosive charge amount, the velocity and angle of impact increased, and this phenomenon led to the interface transforming from a smooth to a wavy state and resulting in melted and separated regions. The results obtained from scanning electron microscope (SEM) images showed that with increasing stand-off distance and explosive charge amount and consequently increasing impact velocity, the length and height of the waves created at the interface increased. Energy dispersive X-ray spectroscopy (EDS) and X-ray diffraction (XRD) analysis showed that no intermetallic compounds were formed at the joint interface. The results of the microhardness test also indicated that the hardness around the joint interface increased by 25% due to plastic deformation and work hardening caused by the intense impact of the base and flying plates. By performing shear strength tests, it was found that in all samples, failure occurred in the phosohor bronze layer and no failure occurred due to separation of the samples from the interface. By performing tensile tests, it was found that the ultimate tensile strength increased from 430 to 488 MPa with increasing stand-off distance and explosive load. Polarization acquisition and impedance spectroscopy (EIS) tests showed that with increasing impact energy, the corrosion potential decreased and the corrosion current density increased significantly from 5.5 to 13.2 μA/cm².

The joining of dissimilar aluminum sheets is an important issue in the optimization of industrial joints due to the differences in physical, mechanical and metallurgical properties. In this study, the mechanical behavior and microstructural changes of bimetallic joints made of AA5052 and AA3105 alloys joined by two methods of TIG welding (TIG) and friction stir welding (FSW) were investigated and compared. First, preliminary experiments were carried out to optimize the parameters of the friction stir welding and TIG welding processes and to select appropriate levels of the process parameters. The results of mechanical experiments showed that in the FSW welded samples, the failure occurred mainly in the weld zone, but in the TIG welded samples, the failure occurred in the base metal. The tensile test results showed that the AA5052 sample had the highest tensile strength (273 MPa) and the highest elongation percentage (20%), and the F 3-5 welded sample with a strength of 89 MPa and 6% elongation performed worse than the T 3-5 welded sample and fractured in the weld area. The microhardness test results showed that the TIG welded sample had a higher hardness in the weld area than the FSW method due to the use of 5356 ER filler. Finally, by analyzing and comparing the results obtained from the tests related to the mechanical properties obtained from each method, it was found that the TIG method performed better than FSW in joining some alloys.