1 Introduction
Extruded lightweight alloy profiles are widely used in aerospace, transportation, and other fields due to their light weight, high strength and rigidity [1-4]. The traditional method for producing curved profiles involves extruding straight profiles first and then using subsequent bending processes such as stretch bending, press bending, roll bending, and push bending [5-8]. However, these methods often reslult in defects such as wrinkling, spring-back, cross-sectional distortion, and changes in wall thickness during the bending process [9-12], requiring repeated corrections to the formed components. To address the issues of lengthy processing steps and multiple forming defects associated with traditional bending methods, the one-step bending process has emerged as an effective method for producing high-precision curved components using a shorter processing route. It has also become a popular research direction in recent years for forming curved profiles.
Considerable researches have been conducted on the one-step bending process. One approach involves the core die to control the curvature by adjusting the position of the guiding device. MÜLLER et al [13, 14] added a disk as a guiding tool at the outlet and adjusted its position to achieve one-step extrusion bending for Z-profile and tube profiles. The results showed that the curvature of the bend was determined by the initial position of the disk, and the device reduced the residual stress of the profiles caused by thermal deformation. Moreover, installing the bending device at the exit of the extrusion die significantly reduced the residual stress. KLEINER et al [15] proposed a forming process in which external forces were used to force the extruded profiles to bend. This process added a feeding device onto the basis of normal extrusion, and the device applied external forces to induce bending after the profiles were extruded. Another method involves controlling the extrusion shape by changing the flow velocity inside the billet. By creating a flow velocity difference at the mouth of the core die, the profiles can naturally bend during extrusion, effectively avoiding spring-back in the bending profiles. ZHOU et al [16, 17] used a differential velocity extrusion process (DVSE) to extrude arc profiles laterally by loading the billet ends with different extrusion velocities, making use of the billet’s internal asymmetric flow. This effectively overcame the flaws of conventional bending processes, improved material utilization, and increased hardness, yield strength, and ultimate tensile strength by 134.8%, 354% and 116.8%, respectively. However, the mentioned methods require specific tooling designs, which can be complex and limit mass production to some extent.
In this study, a novel extrusion process for self-bending of complex profiles is proposed. By modifying the die structure, the extrusion process induces uneven internal flow behavior in the billet, allowing for the bending of the profiles during extrusion. Previous research has focused on the bending of solid rods, with WANG et al [18] identifying staggered amount and extrusion ratio as key parameters affecting curvature variation and demonstrating strong fiber texture in extruded rods. Meanwhile, ZHANG et al [19] derived the variable of eccentricity through theoretical deduction to verify the relationship between staggered extrusion theory and practice, validating the feasibility of the process. However, research on the bending of complex profiles using this process is still in the experimental stage. Building upon previous findings, this study explores the principle of bending complex profiles using the staggered extrusion process and investigates the curvature variation of profiles by utilizing die geometries with different eccentricities. Additionally, the research contributes to understanding the resulting microstructural changes and mechanical properties after staggered extrusion deformation.
2 Materials and methods
2.1 Process principle
Staggered extrusion is a bending profile forming process in which the cross-section of the traditional convex mold extrusion direction is changed from a rectangle to a stepped structure. During the loading process, due to the force of the biased load on the billet, the billet exhibits flow diversion behavior. A part of the billet flows towards the gap and fills the space between the convex mold and the sleeve, while another part fills the core mold cavity. The billet as a whole flows downward and is extruded from the core mold cavity to form the desired shape. Staggered extrusion causes deformation of the billet and leads to biased stress distribution within the billet. There is a flow inconsistency at the core mold cavity, resulting in a gradient difference in flow velocity distribution and a linear change in velocity distribution. The extruded profile exhibits certain bending characteristics, which is the principle of staggered extrusion forming. Figure 1 shows the complete process of staggered extrusion. The device includes the convex mold (the height difference between the vertical directions of the left and right convex molds is referred to as the mismatch value h, and the horizontal difference is referred to as the eccentricity value e), billet, split core mold, sleeve, base, etc. The split core mold is adopted for easy removal of the bent profile after extrusion. To prevent the core mold from breaking during extrusion due to excessive pressure, an appropriate sizing belt is set on the core mold to reduce the pressure during extrusion. Then, the core mold, billet, and convex mold are aligned and placed into the sleeve, and heated to the specified temperature. For convenience, in this study the eccentricity value of e=10 mm is defined as SEE1, e=20 mm as SEE2, and e=30 mm as SEE3.
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2.2 Experimental plan
The experimental material used was commercially available extruded AZ31 magnesium alloy with the chemical composition shown in Table 1. The billets used in the study were cylindrical with a diameter of 40 mm and a height of 50 mm. The extrusion ratio was calculated to be 11.01, and the extrusion speed was set at 1 mm/s. For easy specimen retrieval, a split-core mold was used, with water-based graphite as a lubricant. First, the sleeve was evenly divided into four sections and labeled accordingly. The boundary of the split-core mold was marked at the top of the staggered stem. Graphite was applied to the surface of the core mold, aligning the boundary of the core mold with the horizontal marks on the sleeve. Next, the billet and staggered stem were placed inside the extrusion cylinder. The top of the staggered stem was marked corresponding with the direction of the core mold. A caution line was marked on the punch to prevent collision with the core mold and ensure safety. The extrusion direction was also marked on the sleeve. The assembly is then placed in a resistance furnace and heated to 350 ℃ for 30 min for preheating. Afterward, the assembly was taken out for the staggered extrusion forming process. To preserve the microstructure, the extruded curved samples were cut and water-quenched after the experiment.
Al | Zn | Mn | Fe | Cu | Zr | Mg |
---|---|---|---|---|---|---|
2.50 | 0.70 | 0.22 | 0.05 | 0.06 | 0.09 | Balance |
2.3 Microstructure testing
In order to investigate the influence of shear behavior of the staggered stem on the microstructure and structural changes of the bent profiles, samples were cut from typical sections of the extruded profiles for observation and analysis. The size of the cut samples was 3 mm×3 mm× 2.5 mm. The preparation of the samples involved grinding with silicon carbide sandpaper (80#, 400#, 1000#, 2000#, 3000#, 5000#). The surfaces were then polished using 1 µm diamond polishing suspension and water-based lubricant. After polishing, the surface was etched using a mixed solution of 1 mL acetic acid, 1 mL nitric acid, 1 g oxalic acid, and 150 mL water for 3 s. The microstructure was observed using a metallographic microscope. Electrolytic polishing using phosphoric acid (60 mL) and alcohol (100 mL) was performed on the samples. Electron backscatter diffraction (EBSD) testing is conducted on the TD-ED direction of the profiles, using a working voltage of 20 kV and an electrolysis time of 120 s.
2.4 Mechanical properties testing
To test the strength and ductility of the magnesium alloy, mechanical properties were generally tested along the direction of extrusion, which was the flow direction of the extruded profiles. In this study, due to the bent shape of the profiles, samples were taken along the reverse direction of the bending tangent as much as possible, to account for shape limitations. To ensure the accuracy of the experimental data, each test was performed 5 times. Tensile tests were conducted at room temperature, with a test speed of 1 mm/min. Before testing, the sample surfaces were polished with sandpaper to remove surface oxides and defects, ensuring a smooth surface. The tensile strength, yield strength, and elongation at fracture of the samples were obtained. The fracture morphology of the tensile samples at room temperature is observed using a Quanta 200F Field Emission Scanning Electron Microscope to determine the fracture type and clarify the fracture mechanism.
3 Results and discussion
3.1 Curvature feature
The clearance between the convex mold and the deformity of the billet are the two primary factors that determine the curvature of the bent component. Therefore, the curvature of the bent component obtained under different conditions is measured and calculated. The two endpoints of the bent component obtained under different conditions are placed on the same horizontal line. By connecting these two endpoints to form a straight line, equidistant points are selected on the line. Assuming that the bending height of both endpoints is 0 mm, the curvature radius of each point is measured. Taking 13 equidistant points as an example, as shown in Figure 2(a), the curvature radius of each point is calculated, as shown in Figure 2(b). Three bent components with equal horizontal lengths are chosen for curvature measurement. The maximum bending heights of the bent components are (18.1±0.5) mm, (17.2±0.5) mm, and (8±0.5) mm, respectively. As the eccentricity increases, the bending height of the bent component also increases. The greater the eccentricity, the more pronounced the change in the bending height.
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3.2 Mechanical properties
Figure 3 presents the engineering stress-strain curves for the initial billet and extruded profiles obtained from room temperature tensile tests conducted parallel to the axial direction. After the SE process, compared to the billet, the elongation (EL) increased to 10.5%, 12.1%, 15.9%, respectively, and the tensile strength improved to 250, 270 and 235 MPa. As mentioned earlier, DRX occurred during misalignment extrusion, resulting in grain refinement. The significant increase in tensile strength and elongation compared to the billet indicates the strengthening effect of grain refinement on the properties of material. In SEE1, both the yield strength and elongation are lower than those in SEE2. This can be attributed to changes in grain size at different parameters. The larger grain size corresponds to lower yield strength and tensile strength, which is consistent with the Hall-Petch formula. The changes of grain size and microstructure on mechanical properties need to be further analyzed.
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3.3 Fracture analysis
Figure 4 shows the fracture morphology and SEM characterization results, along with local magnified images, for the original billet and different eccentricities under staggered extrusion. In Figure 4(a), the original billet sample exhibits numerous intergranular fractures (indicated by yellow arrows) and intergranular steps. Additionally, transgranular fractures can be observed in the dimple area. Intergranular fractures and intergranular steps are characteristic of brittle fracture. Their occurrence is attributed to the increase in internal dislocations within the coarse grains during tension, where the internal slip bands have undergone a decrease in their strength and ductility, leading to crack propagation and transgranular fracture. On the other hand, misalignment extrusion achieves the goal of grain refinement through dynamic recrystallization. Furthermore, through the local magnified images in Figures 4(e) and (f)), it can be observed that there are a significant number of dimples (indicated by red arrows) within the fracture surface. Therefore, the alloy exhibits transgranular fracture during failure, indicating that misalignment extrusion promotes ductile fracture. The plastic deformation of the billet during extrusion enhances the strength and ductility of the magnesium alloy.
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3.4 Grain misorientation angles of boundary and grain size
To study the relationship between grain orientation and grain boundaries, Figure 5 shows the inverse pole figure (IPF) and the percentage of grain misorientation angles of boundary. The colors in the figure correspond to different grain orientations: red represents grains with (0001)//ED orientation, green represents grains with
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3.5 Twinning analysis
In order to illustrate the influence of
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3.6 Recrystallization mechanism
Through the analysis above, it is found that the microstructure of I-beam curved profiles changes during the forming process due to the different eccentricities of the misalignment extrusion die. Figures 7(a)-(c) show the volume fractions of recrystallized grains, subgrains, and deformed grains for three different parameters of misalignment extrusion. The blue color represents recrystallized grains, the yellow color represents subgrains, and the red color represents deformed grains. From Figure 7(d), it can be seen that at SEE1, the proportion of deformed grains is the highest at 61%, at SEE2 the recrystallized grains gradually increase to 28%, and at SEE3 the highest proportion of recrystallized grains is 58%. This indicates that as the eccentricity e increases during the misalignment extrusion process, the uneven deformation of the billet increases, leading to the generation of a large number of dislocation accumulations and the formation of subgrains. With the increase in the amount of deformation provided, the subgrains gradually transform into dynamically recrystallized grains. To further investigate dynamic recrystallization, the grains were further analyzed. From Figure 7(a), it can be observed that the deformed grain boundaries exhibit a “serrated” shape [24-26]. It is found that the deformed grains have a bow-out shape, and subgrains and recrystallization are found near them. which is a typical feature of DDRX mechanism. In Figure 7(b) under the SEE2 process, when the proportion of deformed grains decreases to 31%, it is found that recrystallization and subgrains occur near the deformed grains with a bulging shape, and the transformation from LABS to HABS dominates. This is the main characteristic of CDRX, indicating that the recrystallization process involves both CCRX and DDRX. As shown in Figure 7(c), a large number of twins are found, resulting in the misalignment of twin boundaries and the occurrence of twin-induced recrystallization (TDRX) process, leading to a significant increase in recrystallized grains.
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3.7 Kernel average misorientation
In order to investigate the relationship between heterogeneous deformation and dislocations during plastic deformation, KAM is called kernel average misorientation, which is a method to characterize the local mismatch angle in EBSD data analysis, as shown in Figures 8(a)-(c), where a higher KAM value is represented by a greater amount of green color, while lower values are represented by blue color. In Figure 8(a), the highest amount of green color indicates a higher KAM value, suggesting larger strains within the grains. The average misorientation angles were calculated to be 1.131, 0.729, and 0.379 for each case, respectively. At the same time, in SEE1, most of the grains were deformed grains, and the local deformation inhomogeneity caused severe dislocation accumulation and strain gradient. Figure 8(a) shows different grain colors indicating significant misorientation, leading to the accumulation of dislocations at grain boundaries, ultimately resulting in an increase in θKAM. In SEE2, the uneven deformation of the billet provided sufficient energy for the occurrence of continuous dynamic recrystallization. Additionally, the shear deformation of the billet consumed a large number of dislocations and reduced local strain concentration. As shown in Figure 8(c), in SEE3, most of the grains exhibit a blue color. This is because the peculiar structure of the die results in the longest reverse extrusion time, and the billet may undergo static recovery while providing energy through shear deformation. The opposite-sign dislocations within the grains offset each other, reducing local strain and decreasing the misorientation angles at grain boundaries, simultaneously reducing θKAM and increasing the alloy’s ductility. As shown in Eq. (1), GND represents the density of geometrically necessary dislocations (GND density), θKAM represents the average local misorientation within the EBSD scanning area, μ is the scanning step size, and in this chapter, a step size of 1 μm was used. b represents the Burgers vector, which in this chapter has a value of 0.286 nm. It can be observed that the distribution of GND follows a linear relationship with KAM values. The calculated values of GND were 7.91×1014/m2, 5.10×1014/m2 and 2.65×1014/m2, which correspond to the values of KAM.
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3.8 Schmid factor
The influences of internal material anisotropy can be more comprehensively explained by considering basal <a> slip, prismatic <a> slip, pyramidal <a> slip, and pyramidal <c+a> slip. Figure 9 illustrates the difficulty level of activation for different slip systems in various regions. From the observation of the figure, it can be seen that in SEE1, the Schmid factors for basal <a> slip, prismatic <a> slip, and pyramidal <c+a> slip are 0.281, 0.153 and 0.399, respectively. In SEE2, the Schmid factors for basal <a> slip, prismatic <a> slip, and pyramidal <c+a> slip are 0.299, 0.118 and 0.403, respectively. In SEE3, the Schmid factors for basal <a> slip, prismatic <a> slip, and pyramidal <c+a> slip are 0.243, 0.141 and 0.411, respectively. It is well known that the larger the SF value, the easier the slip is to open.
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From Figures 9(c), (f), (i), it can be observed that misalignment extrusion activates mainly basal <a> slip and pyramidal <c+a> slip, as HAN et al [27, 28] discovered that shear strain can promote the activation ofpyramidal <c+a> slip, thus altering the texture type of magnesium alloys. Decreased Schmid factors for basal slip were observed in the same alloy under misalignment extrusion, which is beneficial for improving the plasticity and strength enhancement of the extruded alloy. Additionally, the activation of pyramidal <c+a> slip contributes to the enhancement of plasticity. The presence of twins [29] in SEE3 indicates that twins can promote basal <a> slip and prismatic <a> slip, further confirming that twins can improve the performance of the alloy.
3.9 Pole figures and inverse pole figures
Figure 10 shows the pole figures and inverse pole figures for different eccentricities under misalignment extrusion. In Figure 10(a), for the SEE1 region, the pole figure exhibits a bimodal structure, with the c* axis of the grains parallel to the ED direction and a pole density of 10.98. XU et al [30-32] proposed that the introduction of shear strain during the extrusion process of magnesium alloys causes a deviation in the basal texture and suggested that this is due to the activation of pyramidal <c+a> slip, leading to texture type alterations. In Figure 10(b), the c* axis of the grains is parallel to the ED direction, with a maximum pole density of 12.68. The inverse pole figure also reveals a strong presence of the basal orientation, confirming the activation of basal slip as indicated by the Schmid factor. Additionally, due to lower shear strain values, some grains may undergo dynamic recrystallization. As for SEE3, it experiences the least shear stress, resulting in the highest degree of deformation for the grains. The newly formed grains maintain their original orientation, as shown in Figure 10(c), with a pole density of 23.34. Additionally, this region exhibits the highest texture strength, indicating that misalignment extrusion leads to heterogeneous deformation of the billet, resulting in an increase in pole density in the pole figures.
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4 Conclusions
Under the extrusion temperature of 350 ℃ and extrusion speed of 1 mm/s, AZ31 magnesium alloy I-beams with different eccentricities were extruded using misalignment convex molds. SEM testing, EBSD testing, and mechanical property testing were conducted, and the following conclusions were drawn from the results:
1) The SE process was able to extrude and significantly refine the grain size of the AZ31 magnesium alloy I-beams. The grain sizes of SEE1, SEE2, and SEE3 were measured to be 15.98, 12.28 and 20.32 µm, respectively, compared to an initial grain size of approximately 168 µm in the original billet. The uneven flow inside the billet caused by the shearing behavior of the SE mold structure led to a change in the grain size. Overall, the grain size was refined to less than 15% of its original size.
2) Analysis of the fracture surfaces and mechanical testing revealed that the fracture surfaces of the original billet were mainly cleavage planes, indicating brittle fracture. After the SE process, the fracture surfaces exhibited dimples, indicating ductile fracture. Compared to the billet, the tensile strength is increased to 250, 270,
235 MPa, and the engineering strain elongation is increased to 10.5%, 12.1%, 15.9%.
3) The variation in grain size under different eccentricities during the SE process is mainly attributed to different mechanisms, including continuous dynamic recrystallization (CDRX), discontinuous dynamic recrystallization (DDRX), and twinning-induced dynamic recrystallization (TDRX). These mechanisms result in stress concentration and increased dislocation density in some grains in SEE1, leading to poorer ductility. Additionally, in SEE3, a significant number of {1012} twinning features were observed, enhancing the ductility of the grains.
4) As the eccentricity increases, the bending height of the bent component also increases. The greater the eccentricity, the more pronounced the variation in bending height.
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