Deformation Characteristics and Microstructure Analysis of Aluminum Alloy Component with Complex Shape by Cold Orbital Forming

: This work aimed to study the deformation characteristics and microstructure of AA6063 aluminum alloy component with complex shape manufactured by cold orbital forming processing. The material ﬂowing behavior was analyzed by Finite Element (FE) simulation and forming experiments were carried out using bar blank with different lengths. The microstructure of the boss zone cut from the formed samples was observed using scanning electron microscopy (SEM) and electron back-scatter diffraction (EBSD). FE simulation and experiment results both showed the aluminum base can be formed using cold orbital forming process. The distributions of the effective strain of the component with different blank lengths were almost the same, and the effective strain was bigger at the boss and the ﬂash as the forming ﬁnished. The material ﬂow is complex, especially in the boss, and the folding defect was observed at the root of the boss. The distribution of Mg 2 Si strengthening precipitate is more homogeneous in the matrix, has a different shape, and shows directivity at different position of boss zone. The grains are elongated, and the extent is different at different positions of the boss zone after cold orbital forming, and the crystal orientation discrepancy is smaller in the component main body and bigger in the boss zone. Subsequent forming process and blank optimization need to be further researched to improve forming quality.


Introduction
A lot of aluminum components with side branch and boss are applied more and more widely in the automobile and aerospace industries to decrease weight and increase strength. It is difficult to form the complex shape, and the forming load is large when using a conventional forging process. Therefore, an innovative method to manufacture the aluminum alloy component with complex shape using cold orbital forming process was proposed.
Cold orbital forming is a continuous metal plasticity forming process with local loading that can produce complex components. During cold orbital forming process, the punch partially contacts with the blank, which reduces the contact area between the punch and the blank, thereby decomposing the entire deformation process of the blank into continuous small deformations; thus, the forming load is greatly reduced under the same process conditions [1], and the metal fluidity is superior [2].
At present, some researchers made great efforts to study the theory, equipment, and application of cold rotary forming owing to its many advantages. Standring et al. [3] summarized the change of the angle of inclination along the tool axis during the entire deformation and developed an advanced orbital forging system without skidding or slipping, and they also calculated four types of punch paths (circular, straight line, spiral, and planet). Gu et al. [4] studied the static and dynamic performance of a 6300 KN cold orbital forging machine. Feng et al. [5] studied the influence of eccentricity on movements of orbital head with inner and outer eccentric sleeves in orbital forging. Loyda [6] explored the influence of the processing parameters on the microstructural evolution during hot orbital forging of a nickel-based superalloy disc. Hetzel et al. [7] combined local short term preheat treatment with preform to improve material flow in cold orbital forming. Grosman et al. [8] proposed an incremental deformation method for orbital forming of components with a complex upper surface. Samolyk [9] presented cold orbital forging of aluminum alloy bevel gears using FE simulation and verified by experiment. Sheu et al. [10] performed the die stress analysis of the orbital forging process to prevent the die failure and product defects. Qin [11] revealed contact mechanisms between the dies and the workpiece through modeling and simulation. Zhuang et al [12] studied the effect of key factors on the final step during cold orbital forging of a spur bevel gear. Jiang [13] concluded that the hot rotary forging could remarkably promote formability of Ti-6Al-4V alloy component by observing the microstructure and texture of rotary forged sample. Hua and Han [14] revealed the contact pressure response in a complicated metal forming technology of cold orbital forming by FE methods and explored the effects of friction coefficient on the metal flow and materials forming limit.
Moreover, Han et al. [15][16][17][18][19] researched cold orbital forming of complex nonrotating components and proposed a method for accurately designing the nonrotating punch based on the punch motion equation. Milutinovic et al. [20] analyzed and compared mechanical properties of a nonaxisymmetric steel U-cross joint component manufactured by cold orbital forging and conventional hot forging and found that the component formed by orbital forging showed better mechanical properties than the component manufactured by conventional forging. Also, cold orbital forging can be utilized for riveting assembly, such as the assembly of wheel hub bearing [21,22] and artificial joints production [23]. Recently, a novel orbital forming process called ultrasonic orbital microforming (UOM) was developed to form metal components whose dimensions were smaller than 1 mm [24,25].
Although cold orbital forming of complex nonrotating components were researched in recent years, there are few reports about deformation characteristics or the potential forming defects analysis and microstructure during cold orbital forming of the nonrotating component with side branch and boss. In this paper, which involves a complex AA6063 aluminum alloy component with side branch and boss structure for electric pruning scissors as shown in Figure 1, the cold orbital forming scheme for manufacturing the aluminum alloy component with complex shape was designed using a bar as the blank, then the FE model was established and the forming characteristics were analyzed. Subsequently, the forming experiment was carried out at T630 rotary forging press using three bar blanks with the same diameter and different length. FE simulation results and experimental results were compared to verify the feasibility of FE model. The precipitates and microstructure of the boss zone cut from the formed samples were observed using scanning electron microscopy (SEM) and electron back-scatter diffraction (EBSD) to understand more about the forming characteristics of an aluminum alloy component with complex shape using cold orbital forming processing. Metals 2021, 11, x FOR PEER REVIEW 3 of 16

Materials
In this paper, the material of the complex component is AA6063 aluminum alloy, which belongs to Al-Mg-Si deformed aluminum alloy, has good physical properties, and is used widely in various engineering fields to develop lightweight industrial products [26,27]. Its chemical composition (wt. %) is as follows: Si-0.2~0.6%, Mg-0.45~0.9%, Fe-0.35%, Mn-0.1%, Cr-0.1%, Zn-0.1%, Ti-0.1%, Cu-0.1%, and Al-for the remainder. The yield strength and tensile strength are 80 MPa and 150 MPa, respectively. Young's modulus and Poisson's ratio are 68.9 GPa and 0.33 GPa, respectively. The constitutive equation of the material treated after full annealing (O state) was obtained by carrying out tensile test and fitting experimental data and is expressed as follows [27]: 21 (1) Figure 2 shows the 3D solid model of the forging for the aluminum alloy component with complex shape in question. It can be divided into two main structural parts; namely, an approximate cylinder and a half-cone, a side branch and the boss on the half-cone. The boss plays a significant role during assembly of the base and two blades. The component is a nonrotating complex part with a total length of 75.7 mm, and the length and diameter of the left cylinder end are 14 mm and 28 mm, respectively. The thickness and maximum length of the side branch are 3.7 mm and 7 mm, respectively. The height and diameter of the boss on the bottom right end are 4.5 mm and 15.5 mm, respectively. Cold orbital forming process of the aluminum alloy component with complex shape is proposed according to its structural characteristics.

Materials
In this paper, the material of the complex component is AA6063 aluminum alloy, which belongs to Al-Mg-Si deformed aluminum alloy, has good physical properties, and is used widely in various engineering fields to develop lightweight industrial products [26,27]. Its chemical composition (wt. %) is as follows: Si-0.2~0.6%, Mg-0.45~0.9%, Fe-0.35%, Mn-0.1%, Cr-0.1%, Zn-0.1%, Ti-0.1%, Cu-0.1%, and Al-for the remainder. The yield strength and tensile strength are 80 MPa and 150 MPa, respectively. Young's modulus and Poisson's ratio are 68.9 GPa and 0.33 GPa, respectively. The constitutive equation of the material treated after full annealing (O state) was obtained by carrying out tensile test and fitting experimental data and is expressed as follows [27]: 21 (1) Figure 2 shows the 3D solid model of the forging for the aluminum alloy component with complex shape in question. It can be divided into two main structural parts; namely, an approximate cylinder and a half-cone, a side branch and the boss on the half-cone. The boss plays a significant role during assembly of the base and two blades. The component is a nonrotating complex part with a total length of 75.7 mm, and the length and diameter of the left cylinder end are 14 mm and 28 mm, respectively. The thickness and maximum length of the side branch are 3.7 mm and 7 mm, respectively. The height and diameter of the boss on the bottom right end are 4.5 mm and 15.5 mm, respectively. Cold orbital forming process of the aluminum alloy component with complex shape is proposed according to its structural characteristics.

Materials
In this paper, the material of the complex component is AA6063 aluminum alloy, which belongs to Al-Mg-Si deformed aluminum alloy, has good physical properties, and is used widely in various engineering fields to develop lightweight industrial products [26,27]. Its chemical composition (wt. %) is as follows: Si-0.2~0.6%, Mg-0.45~0.9%, Fe-0.35%, Mn-0.1%, Cr-0.1%, Zn-0.1%, Ti-0.1%, Cu-0.1%, and Al-for the remainder. The yield strength and tensile strength are 80 MPa and 150 MPa, respectively. Young's modulus and Poisson's ratio are 68.9 GPa and 0.33 GPa, respectively. The constitutive equation of the material treated after full annealing (O state) was obtained by carrying out tensile test and fitting experimental data and is expressed as follows [27]: Figure 2 shows the 3D solid model of the forging for the aluminum alloy component with complex shape in question. It can be divided into two main structural parts; namely, an approximate cylinder and a half-cone, a side branch and the boss on the half-cone. The boss plays a significant role during assembly of the base and two blades. The component is a nonrotating complex part with a total length of 75.7 mm, and the length and diameter of the left cylinder end are 14 mm and 28 mm, respectively. The thickness and maximum length of the side branch are 3.7 mm and 7 mm, respectively. The height and diameter of the boss on the bottom right end are 4.5 mm and 15.5 mm, respectively. Cold orbital forming process of the aluminum alloy component with complex shape is proposed according to its structural characteristics.   be divided into orbital forming stages and the shaping stage. During the orbital forming stage, the rocking punch takes a rocking motion at angular velocity ω around a vertical axis at a fixed incline angle γ (usually between 1 • and 3 • ), and meanwhile, the lower die feeds upward vertically at a fixed speed v. The blank deforms under the pressure of the rocking punch and the lower cavity and flows into the die cavities until the required shape is formed. During the shaping stage, the rocking punch still performs the rocking motion, but the lower die stops feeding and remains stationary to make the component form with superior quality.  Figure 3 shows the schematic diagram of cold orbital forming of the aluminum alloy component with complex shape. As shown in Figure 3, the whole forming process can be divided into orbital forming stages and the shaping stage. During the orbital forming stage, the rocking punch takes a rocking motion at angular velocity ω around a vertical axis at a fixed incline angle γ (usually between 1° and 3°), and meanwhile, the lower die feeds upward vertically at a fixed speed v. The blank deforms under the pressure of the rocking punch and the lower cavity and flows into the die cavities until the required shape is formed. During the shaping stage, the rocking punch still performs the rocking motion, but the lower die stops feeding and remains stationary to make the component form with superior quality. According to Figure 2, the shape of the base is similar to a short shaft, thus, a bar is chosen as the blank. Considering the complex shape of pruning scissor base, especially the lateral branch with flattened and thin structure, the flash with a thickness of 1.36 mm was designed, and the volume of the blank was determined to be ~30-40% larger than the volume of component. The diameter of the blank was determined to be about 30 mm because the left end of the component was a cylinder with a diameter of ~28 mm. Thus, the length of bar blank can be decided according to the constancy of volume. Here, three types of bar blank with different lengths were designed, and their values were 55 mm, 58 mm, and 60 mm, respectively.

Cold Orbital Forming Scheme of Aluminum Alloy Compoent with Complex Shape
To make the bar maintain a stable position in the lower die during the forming process, the lower die must be deep enough. The structure of the rocking punch should be as simple as possible to reduce the design and production difficulties of the rocking punch. Because the cavity forming the top part of the forging is too shallow and the shape of the top part is much more complex than that of the bottom part, the top part of the forging is arranged to be formed by the rocking punch while the bottom part with boss is arranged to be formed by the lower die in this paper, as shown in Figure 3. According to Figure 2, the shape of the base is similar to a short shaft, thus, a bar is chosen as the blank. Considering the complex shape of pruning scissor base, especially the lateral branch with flattened and thin structure, the flash with a thickness of 1.36 mm was designed, and the volume of the blank was determined to be~30-40% larger than the volume of component. The diameter of the blank was determined to be about 30 mm because the left end of the component was a cylinder with a diameter of~28 mm. Thus, the length of bar blank can be decided according to the constancy of volume. Here, three types of bar blank with different lengths were designed, and their values were 55 mm, 58 mm, and 60 mm, respectively.
To make the bar maintain a stable position in the lower die during the forming process, the lower die must be deep enough. The structure of the rocking punch should be as simple as possible to reduce the design and production difficulties of the rocking punch. Because the cavity forming the top part of the forging is too shallow and the shape of the top part is much more complex than that of the bottom part, the top part of the forging is arranged to be formed by the rocking punch while the bottom part with boss is arranged to be formed by the lower die in this paper, as shown in Figure 3.
It is worth noting that the top part of the component is non-axisymmetric, different from the conventional rocking punch design method for axisymmetric components; the corresponding rocking punch is also non-axisymmetric. Moreover, the rocking punch performs a complex rocking motion during the formation process; thus, designing the non-axisymmetric rocking punch is a key issue. To deal with this problem, a novel method of designing the rocking punch that can form the non-axisymmetric component in cold orbital forming was developed by Han [15]. According to the design, the instantaneous geometric relation of contact surface between the non-axisymmetric component and the corresponding rocking punch was calculated and the complex non-axisymmetric rocking punch for cold orbital forming of the aluminum alloy component was designed accurately. Next, the lower die can be modeled using a reverse engineering method according to the geometric dimensions of the component using CAD software. Figure 4 shows the 3D solid models of the rocking punch and lower die built using Geomagic Wrap software (Geomagic Wrap 2015 Geomagic, Morrisville, NC, USA) and UG software (UG NX 8.5 Siemens PLM software, Munich, Germany). In addition, all angles of the models are rounded to avoid the mesh distortion in the FE simulation. It is worth noting that the top part of the component is non-axisymmetric, different from the conventional rocking punch design method for axisymmetric components; the corresponding rocking punch is also non-axisymmetric. Moreover, the rocking punch performs a complex rocking motion during the formation process; thus, designing the nonaxisymmetric rocking punch is a key issue. To deal with this problem, a novel method of designing the rocking punch that can form the non-axisymmetric component in cold orbital forming was developed by Han [15]. According to the design, the instantaneous geometric relation of contact surface between the non-axisymmetric component and the corresponding rocking punch was calculated and the complex non-axisymmetric rocking punch for cold orbital forming of the aluminum alloy component was designed accurately. Next, the lower die can be modeled using a reverse engineering method according to the geometric dimensions of the component using CAD software. Figure 4 shows the 3D solid models of the rocking punch and lower die built using Geomagic Wrap software (Geomagic Wrap 2015 Geomagic, Morrisville, USA) and UG software ( UG NX 8.5 Siemens PLM software, Munich, Germany). In addition, all angles of the models are rounded to avoid the mesh distortion in the FE simulation.

Establishment of FE Models
To analyze the forming characteristics during cold orbital forming of the aluminum alloy component with complex shape, corresponding 3D FE models were developed using Deform-3D software ( Ver11.0 SFTC, Columbus, Ohio, USA), as shown in Figure 5.
Firstly, the 3D model of the bar blank, the rocking punch, and the lower die built in UG software were imported into Deform-3D software. Then, the deformed bar blank was defined as the deformed body and was discretized into about 31,680 nodes and 150,200 tetrahedral elements, and an automatic remeshing technique was adopted during simulation. The elastic deformation is negligible, and the rocking punch and the lower die are regarded as the rigid body. The rocking punch is set to make a circular rocking motion around the vertical axis and the value is 25.12 rad/s, while the lower die feeds upward at a constant speed and the value is 4 mm/s during the orbital forming stage and 0 during shaping stage. According to the location relation and movement relation among the rocking punch, the lower die, and the bar blank, the total simulation step was designed to be 741 and the step increment per step was controlled by time, whose value was prescribed to be 0.01, and the shaping time was defined as 1 s, so the total forming time is 7.41 s and the orbital forming time is 6.41 s.
In this paper, the component material is AA6063 aluminum alloy, and its constitutive equation expressed by Equation (1) and mechanical property shown in section 2.1 were imported into Deform-3D software in the simulation.

Establishment of FE Models
To analyze the forming characteristics during cold orbital forming of the aluminum alloy component with complex shape, corresponding 3D FE models were developed using Deform-3D software (Ver11.0 SFTC, Columbus, OH, USA), as shown in Figure 5. The frictional models between the blank and punches were a constant shear friction model, and the empirical friction factor of 0.2 was designed to simplify the complex contact condition [28]. The simulation parameters and their values during the simulation of cold orbital forming of the component with complex shape are shown in Table 1.   Firstly, the 3D model of the bar blank, the rocking punch, and the lower die built in UG software were imported into Deform-3D software. Then, the deformed bar blank was defined as the deformed body and was discretized into about 31,680 nodes and 150,200 tetrahedral elements, and an automatic remeshing technique was adopted during simulation. The elastic deformation is negligible, and the rocking punch and the lower die are regarded as the rigid body. The rocking punch is set to make a circular rocking motion around the vertical axis and the value is 25.12 rad/s, while the lower die feeds upward at a constant speed and the value is 4 mm/s during the orbital forming stage and 0 Metals 2021, 11, 808 6 of 15 during shaping stage. According to the location relation and movement relation among the rocking punch, the lower die, and the bar blank, the total simulation step was designed to be 741 and the step increment per step was controlled by time, whose value was prescribed to be 0.01, and the shaping time was defined as 1 s, so the total forming time is 7.41 s and the orbital forming time is 6.41 s.
In this paper, the component material is AA6063 aluminum alloy, and its constitutive equation expressed by Equation (1) and mechanical property shown in Section 2.1 were imported into Deform-3D software in the simulation.
The frictional models between the blank and punches were a constant shear friction model, and the empirical friction factor of 0.2 was designed to simplify the complex contact condition [28]. The simulation parameters and their values during the simulation of cold orbital forming of the component with complex shape are shown in Table 1.

Cold Orbital Forming Experiment
To verify the reliability of the FE simulation, cold orbital forming experiments of aluminum alloy component with complex shape were performed. Firstly, three different bar blanks of the same dimensions as the 3D FE model, Φ30 mm × 55 mm, Φ30 mm × 58 mm and Φ30 mm × 60 mm, were manufactured using AA6063 aluminum alloy, respectively. Then, the rocking punch and the lower die were manufactured using LD (7Cr7Mo2V2Si) cold tool steel, as shown in Figure 6, and MoS 2 lubricant was used to decrease the friction between the tools and blank during forming. Next, cold orbital forming experiments were conducted using T630 rotary forging machine (Schmid Co., Lyss, Switzerland, as shown in Figure 7.
The frictional models between the blank and punches were a constant shear friction model, and the empirical friction factor of 0.2 was designed to simplify the complex contact condition [28]. The simulation parameters and their values during the simulation of cold orbital forming of the component with complex shape are shown in Table 1.

Cold Orbital Forming Experiment
To verify the reliability of the FE simulation, cold orbital forming experiments of aluminum alloy component with complex shape were performed. Firstly, three different bar blanks of the same dimensions as the 3D FE model, Ф30 mm × 55 mm, Ф30 mm × 58 mm and Ф30 mm × 60 mm, were manufactured using AA6063 aluminum alloy, respectively. Then, the rocking punch and the lower die were manufactured using LD (7Cr7Mo2V2Si) cold tool steel, as shown in Figure 6, and MoS2 lubricant was used to decrease the friction between the tools and blank during forming. Next, cold orbital forming experiments were conducted using T630 rotary forging machine (Schmid Co., Lyss,Switzerland, as shown in Figure 7.

Analysis of Microstructure
In this paper, the microstructure analysis was carried out only for the boss zone on the bottom part of the formed component. Samples were cut by wire-electrode from the initial bar blank and the boss of the formed component was used for microstructure observation. These samples were first ground using sandpaper with different mesh number in turn, polished with 9, 3, and 1 μm diamond solution for 10 minutes, and finally, polished with 40 nm silicon dioxide OPS solution for 10 minutes. The microstructures were observed by SEM using Quanta FEG 450 EBSD (FEI, Eindhoven, Netherlands) at 20 kV and EDAX (EDAX Inc., Mahwah, NJ, USA)

FE Simulation Analysis
3.1.1. Forming shape Figure 8 shows the forming shape of the top and bottom part of the AA6063 aluminum alloy component during cold orbital forming scheme as the blank dimensions are Ф30 mm × 55 mm, Ф30 mm × 58 mm, and Ф30 mm × 60 mm, respectively. In Figure 8, the shapes of the component and some subtle structures are visible, such as the side branch, the boss, and two grooves, which can all be well-formed for the three kinds of blanks with different length. Further, the smaller the blank length, the smaller the flash. When the length of the blank is 55 mm, the formed component has the minimum flash size.

Analysis of Microstructure
In this paper, the microstructure analysis was carried out only for the boss zone on the bottom part of the formed component. Samples were cut by wire-electrode from the initial bar blank and the boss of the formed component was used for microstructure observation. These samples were first ground using sandpaper with different mesh number in turn, polished with 9, 3, and 1 µm diamond solution for 10 minutes, and finally, polished with 40 nm silicon dioxide OPS solution for 10 minutes. The microstructures were observed by SEM using Quanta FEG 450 EBSD (FEI, Eindhoven, The Netherlands) at 20 kV and EDAX (EDAX Inc., Mahwah, NJ, USA).

Results and Discussions
3.1. FE Simulation Analysis 3.1.1. Forming Shape Figure 8 shows the forming shape of the top and bottom part of the AA6063 aluminum alloy component during cold orbital forming scheme as the blank dimensions are Φ30 mm × 55 mm, Φ30 mm × 58 mm, and Φ30 mm × 60 mm, respectively. In Figure 8, the shapes of the component and some subtle structures are visible, such as the side branch, the boss, and two grooves, which can all be well-formed for the three kinds of blanks with different length. Further, the smaller the blank length, the smaller the flash. When the length of the blank is 55 mm, the formed component has the minimum flash size.

Analysis of Microstructure
In this paper, the microstructure analysis was carried out only for the boss zone on the bottom part of the formed component. Samples were cut by wire-electrode from the initial bar blank and the boss of the formed component was used for microstructure observation. These samples were first ground using sandpaper with different mesh number in turn, polished with 9, 3, and 1 μm diamond solution for 10 minutes, and finally, polished with 40 nm silicon dioxide OPS solution for 10 minutes. The microstructures were observed by SEM using Quanta FEG 450 EBSD (FEI, Eindhoven, Netherlands) at 20 kV and EDAX (EDAX Inc., Mahwah, NJ, USA)

FE Simulation Analysis
3.1.1. Forming shape Figure 8 shows the forming shape of the top and bottom part of the AA6063 aluminum alloy component during cold orbital forming scheme as the blank dimensions are Ф30 mm × 55 mm, Ф30 mm × 58 mm, and Ф30 mm × 60 mm, respectively. In Figure 8, the shapes of the component and some subtle structures are visible, such as the side branch, the boss, and two grooves, which can all be well-formed for the three kinds of blanks with different length. Further, the smaller the blank length, the smaller the flash. When the length of the blank is 55 mm, the formed component has the minimum flash size.  To understand the shaping procedure and forming characteristics of the AA6063 aluminum alloy component with complex shape during cold orbital forming, the component with the length of 58 mm will next be used as an example to analyze in detail.  Figures 9 and 10, the side branch, the boss, and two grooves are gradually formed, and the side branch is finally formed as the flash expands around the component, as shown in Figures 9c-f and 10c-f, but oversize flash is produced at the end of the shaping, as shown in Figures 9f and 10f. To understand the shaping procedure and forming characteristics of the AA6063 234 aluminum alloy component with complex shape during cold orbital forming, the com-235 ponent with the length of 58 mm will next be used as an example to analyze in detail. 236 Figures 9 and 10 show the forming shape evolution of the top and bottom part of 237 the AA6063 aluminum alloy component with length of 58 mm under the different form-238 ing time during cold orbital forming scheme, respectively. In Figures 9 and 10, the side 239 branch, the boss, and two grooves are gradually formed, and the side branch is finally 240 formed as the flash expands around the component, as shown in Figures 9c-f and 10c-f, 241 but oversize flash is produced at the end of the shaping, as shown in Figures 9f and 10f.   Figure 11 shows the distribution of effective strain in the top and bottom part of the 253 AA6063 aluminum alloy component during cold orbital forming scheme as the blank 254 dimensions are Φ30 mm × 55 mm, Φ30 mm × 58 mm, and Φ30 mm × 60 mm, respective-255 ly. In Figure 11, the distribution features of the component with different blank length 256 are almost same. When the forming finished, the effective strain was bigger at the boss 257 and the flash, while the effective strain was smaller in the other zone. To understand the shaping procedure and forming characteristics of the AA6063 aluminum alloy component with complex shape during cold orbital forming, the component with the length of 58 mm will next be used as an example to analyze in detail. Figures 9 and 10 show the forming shape evolution of the top and bottom part of the AA6063 aluminum alloy component with length of 58 mm under the different forming time during cold orbital forming scheme, respectively. In Figures 9 and 10, the side branch, the boss, and two grooves are gradually formed, and the side branch is finally formed as the flash expands around the component, as shown in Figures 9c-f and 10c-f, but oversize flash is produced at the end of the shaping, as shown in Figures 9f and 10f.   Figure 11 shows the distribution of effective strain in the top and bottom part of the AA6063 aluminum alloy component during cold orbital forming scheme as the blank dimensions are Ф30 mm × 55 mm, Ф30 mm × 58 mm, and Ф30 mm × 60 mm, respectively. In Figure 11, the distribution features of the component with different blank length are almost same. When the forming finished, the effective strain was bigger at the boss and the flash, while the effective strain was smaller in the other zone.  Figure 11 shows the distribution of effective strain in the top and bottom part of the AA6063 aluminum alloy component during cold orbital forming scheme as the blank dimensions are Φ30 mm × 55 mm, Φ30 mm × 58 mm, and Φ30 mm × 60 mm, respectively. In Figure 11, the distribution features of the component with different blank length are almost same. When the forming finished, the effective strain was bigger at the boss and the flash, while the effective strain was smaller in the other zone.  Figure 12 gives the distribution of the velocity field with the forming time as the blank length of 58 mm during cold orbital forming. In Figure 12a,b, the material flows like a vortex around the central axis in the early part of the orbital forming stage. With the increase in forming time, the metal on the right side of the blank was forced into the boss cavity rapidly and diagonally downward, and the boss was gradually filled from the right to the left; moreover, the redundant metal of the right flows rapidly into the flash gutter, as shown in Figure 12c,d. At the end of the filling forming stage, the metal on the left side of the boss flows obliquely upward to fill out the cavity, and the metal above the boss flows vertically downward into the boss cavity at the same time. The redundant metal on the left flows rapidly into the flash gutter, as seen in Figure 12e. When the forming finished, the boss filled again and the metal velocity in the boss cavity tended to zero after shaping of 1 s. The shape of the forging meets the design requirements, as seen in Figure  12f.   Figure 12 gives the distribution of the velocity field with the forming time as the blank length of 58 mm during cold orbital forming. In Figure 12a,b, the material flows like a vortex around the central axis in the early part of the orbital forming stage. With the increase in forming time, the metal on the right side of the blank was forced into the boss cavity rapidly and diagonally downward, and the boss was gradually filled from the right to the left; moreover, the redundant metal of the right flows rapidly into the flash gutter, as shown in Figure 12c,d. At the end of the filling forming stage, the metal on the left side of the boss flows obliquely upward to fill out the cavity, and the metal above the boss flows vertically downward into the boss cavity at the same time. The redundant metal on the left flows rapidly into the flash gutter, as seen in Figure 12e. When the forming finished, the boss filled again and the metal velocity in the boss cavity tended to zero after shaping of 1 s. The shape of the forging meets the design requirements, as seen in Figure 12f.  Figure 12 gives the distribution of the velocity field with the forming time as the blank length of 58 mm during cold orbital forming. In Figure 12a,b, the material flows like a vortex around the central axis in the early part of the orbital forming stage. With the increase in forming time, the metal on the right side of the blank was forced into the boss cavity rapidly and diagonally downward, and the boss was gradually filled from the right to the left; moreover, the redundant metal of the right flows rapidly into the flash gutter, as shown in Figure 12c,d. At the end of the filling forming stage, the metal on the left side of the boss flows obliquely upward to fill out the cavity, and the metal above the boss flows vertically downward into the boss cavity at the same time. The redundant metal on the left flows rapidly into the flash gutter, as seen in Figure 12e. When the forming finished, the boss filled again and the metal velocity in the boss cavity tended to zero after shaping of 1 s. The shape of the forging meets the design requirements, as seen in Figure  12f.

Folding Defect Analysis
Folding is a common phenomenon that comes up in the forging, especially in the forging process of complex-shape aluminum, which can lead to source fatigue and affect the service performance of the component [29]. The material flow velocity of the boss is complex according to the analysis of flow velocity above, which may cause folding phenomena. So, taking the component with the length of 58 mm as an example, the boss was sectioned along its central axial section and the forming procedure was analyzed in detail, as shown in Figure 13. Figure 13 illustrates the formation of the folding defect when the blank length is 58 mm. In the late forming stage, when the rocking punch is pressed on the left half of the forging, the metal flows into the right of the forging horizontally, which resulted in underfilling phenomena of the boss filled in advance and forming a gap because the metal at the root of the boss is pressed into the right of the forging, as shown in Figure 13a,b. When the rocking punch revolves to the right half of the forging, the metal above the gap flows downward under pressure, and the metal on the right side of the gap flows back to the left (as shown in Figure 12d), thus the gap is filled again and a folding defect is formed, as shown in Figure 13c. During the subsequent forming process, the folding defect is repeatedly generated at the root of the boss during the same forming mechanism. The fold occurs again at the root of the boss when the rocking punch revolves every circle (0.25 s), as shown in Figure 13d-i. Finally, the folding defect forms many times. In summary, due to the severe flowback phenomena during the filling of the boss, the folding defect appears at the inside of the flowback, namely, the left root of the boss.

Folding Defect Analysis
Folding is a common phenomenon that comes up in the forging, especially in the forging process of complex-shape aluminum, which can lead to source fatigue and affect the service performance of the component [29]. The material flow velocity of the boss is complex according to the analysis of flow velocity above, which may cause folding phenomena. So, taking the component with the length of 58 mm as an example, the boss was sectioned along its central axial section and the forming procedure was analyzed in detail, as shown in Figure 13. Figure 13 illustrates the formation of the folding defect when the blank length is 58 mm. In the late forming stage, when the rocking punch is pressed on the left half of the forging, the metal flows into the right of the forging horizontally, which resulted in underfilling phenomena of the boss filled in advance and forming a gap because the metal at the root of the boss is pressed into the right of the forging, as shown in Figure 13a,b. When the rocking punch revolves to the right half of the forging, the metal above the gap flows downward under pressure, and the metal on the right side of the gap flows back to the left (as shown in Figure 12d), thus the gap is filled again and a folding defect is formed, as shown in Figure 13c. During the subsequent forming process, the folding defect is repeatedly generated at the root of the boss during the same forming mechanism. The fold occurs again at the root of the boss when the rocking punch revolves every circle (0.25 s), as shown in Figure 13d-i. Finally, the folding defect forms many times. In summary, due to the severe flowback phenomena during the filling of the boss, the folding defect appears at the inside of the flowback, namely, the left root of the boss.  Figure 14 displays the formed AA6063 aluminum alloy component with different blank lengths. In Figure 14, the forming shapes of the component with different blank lengths are almost the same, and all the subtle structures are fully filled at the end of the formation. Besides, the formed forgings have a big flash, and the smaller the blank length, the smaller the flash. The experimental forging shapes are the same as those shown in the FE simulation results in Figure 8.  Figure 14 displays the formed AA6063 aluminum alloy component with different blank lengths. In Figure 14, the forming shapes of the component with different blank lengths are almost the same, and all the subtle structures are fully filled at the end of the formation. Besides, the formed forgings have a big flash, and the smaller the blank length, the smaller the flash. The experimental forging shapes are the same as those shown in the FE simulation results in Figure 8.

Experimental Results Analysis
Moreover, the boss was sectioned along its central axial section and a metallographic sample was prepared, then the metal flow line was observed by Zesis Axio Scope optical microscopy. Figure 15 shows the enlarged graph of the boss of the sample under different bar blank lengths. In Figure 15, a few folding defects exist at the root of the boss, the phenomena may be caused by the different velocities of filling cavities, and the experimental results are the same as FE simulation results. Moreover, the boss was sectioned along its central axial section and a metallographic sample was prepared, then the metal flow line was observed by Zesis Axio Scope optical microscopy. Figure 15 shows the enlarged graph of the boss of the sample under different bar blank lengths. In Figure 15, a few folding defects exist at the root of the boss, the phenomena may be caused by the different velocities of filling cavities, and the experimental results are the same as FE simulation results.

Microstructure Analysis
According to the above analysis, the material flow velocity is complex in the boss zone; thus, the sample was cut along the longitudinal direction cross section of the boss from the product with blank length of 58 mm processed by cold orbital forming, and the metallographic sample was prepared to study the microstructural characteristics in different position of the boss zone in detail, as shown in Figure 16a. The microstructure observation positions were illustrated in Figure 16b, which was on RD × TD plane; position A is the middle zone in the right part of the formed component; position B is the junction between the middle zone in the right part of the formed component and boss; position D, C, and E are the boss regions with complex flow velocity, respectively. Moreover, the boss was sectioned along its central axial section and a metallographic sample was prepared, then the metal flow line was observed by Zesis Axio Scope optical microscopy. Figure 15 shows the enlarged graph of the boss of the sample under different bar blank lengths. In Figure 15, a few folding defects exist at the root of the boss, the phenomena may be caused by the different velocities of filling cavities, and the experimental results are the same as FE simulation results.

Microstructure Analysis
According to the above analysis, the material flow velocity is complex in the boss zone; thus, the sample was cut along the longitudinal direction cross section of the boss from the product with blank length of 58 mm processed by cold orbital forming, and the metallographic sample was prepared to study the microstructural characteristics in different position of the boss zone in detail, as shown in Figure 16a. The microstructure observation positions were illustrated in Figure 16b, which was on RD × TD plane; position A is the middle zone in the right part of the formed component; position B is the junction between the middle zone in the right part of the formed component and boss; position D, C, and E are the boss regions with complex flow velocity, respectively.

Microstructure Analysis
According to the above analysis, the material flow velocity is complex in the boss zone; thus, the sample was cut along the longitudinal direction cross section of the boss from the product with blank length of 58 mm processed by cold orbital forming, and the metallographic sample was prepared to study the microstructural characteristics in different position of the boss zone in detail, as shown in Figure 16a. The microstructure observation positions were illustrated in Figure 16b, which was on RD × TD plane; position A is the middle zone in the right part of the formed component; position B is the junction between the middle zone in the right part of the formed component and boss; position D, C, and E are the boss regions with complex flow velocity, respectively. Figure 17 shows the SEM micrographs of the AA6063 alloy in the blank before forming and in different observation position of the boss after forming, which revealed the precipitates' characteristics. As shown in Figure 17a, a lot of rod and particle like black precipitates can be observed in the initial blank; these precipitates should be Mg 2 Si strengthening phase, as referenced in previous studies [30,31]. The distribution of these phases is heterogeneous in the matrix. After the blank deformed, the shape of these rod-like Mg 2 Si strengthening phase in position A transformed into particles, and they are distributed the matrix in a homogeneous dispersion state, as shown in Figure 17b. The precipitated phases in positions B and D have obvious directivity, pointed to plus 30 • and minus 30 • along RD, respectively. Parts of the particle shape were elongated into short rod shapes, as seen in Figure 17c,e, while the inclined angle to the RD of the precipitated phases weaken in position C, as shown in Figure 17d. This is caused by the change of metal flow direction at the three positions B, C, and D inside the boss. In Figure 17f, distribution direction of the precipitated phases in position E is almost aligned with RD, which implies position E was subjected to a small deformation. These results agreed well with FE simulation results from Figure 12.  Figure 17 shows the SEM micrographs of the AA6063 alloy in the blank before forming and in different observation position of the boss after forming, which revealed the precipitates' characteristics. As shown in Figure 17a, a lot of rod and particle like black precipitates can be observed in the initial blank; these precipitates should be Mg2Si strengthening phase, as referenced in previous studies [30,31]. The distribution of these phases is heterogeneous in the matrix. After the blank deformed, the shape of these rodlike Mg2Si strengthening phase in position A transformed into particles, and they are distributed the matrix in a homogeneous dispersion state, as shown in Figure 17b. The precipitated phases in positions B and D have obvious directivity, pointed to plus 30° and minus 30° along RD, respectively. Parts of the particle shape were elongated into short rod shapes, as seen in Figure 17c,e, while the inclined angle to the RD of the precipitated phases weaken in position C, as shown in Figure 17d. This is caused by the change of metal flow direction at the three positions B, C, and D inside the boss. In Figure 17f, distribution direction of the precipitated phases in position E is almost aligned with RD, which implies position E was subjected to a small deformation. These results agreed well with FE simulation results from Figure 12.  Figure 18 shows the orientation maps (OMs) of the AA6063 alloy in the blank before forming and in the different observation positions of the boss after forming that were obtained by EBSD analysis. In the initial blank in Figure 18a, the microstructure shows ribbon-like fiber morphology in RD × TD plane, and the direction of their long axes is aligned with RD; also, the crystal orientation discrepancy is large. After cold orbital forming, the grains are elongated and are tilted from RD, as shown in Figure 18b-f. In position A in Figure 18b, the crystal orientation discrepancy becomes small compared with that of the initial blank, and the tilted angle is also smaller than that of the other position. In addition, the grains in positions B and D are elongated much more, which implies metal deformed more severely in these zones.  Figure 18 shows the orientation maps (OMs) of the AA6063 alloy in the blank before forming and in the different observation positions of the boss after forming that were obtained by EBSD analysis. In the initial blank in Figure 18a, the microstructure shows ribbon-like fiber morphology in RD × TD plane, and the direction of their long axes is aligned with RD; also, the crystal orientation discrepancy is large. After cold orbital forming, the grains are elongated and are tilted from RD, as shown in Figure 18b-f. In position A in Figure 18b, the crystal orientation discrepancy becomes small compared with that of the initial blank, and the tilted angle is also smaller than that of the other position. In addition, the grains in positions B and D are elongated much more, which implies metal deformed more severely in these zones.

Conclusions
In this paper, deformation characteristics and microstructures were studied by FE simulation, processing experiments, and SEM and EBSD examination during cold orbital forming of AA6063 aluminum alloy component with complex shape. It can be concluded that: (1) It is feasible to manufacture the AA6063 aluminum alloy component with complex shape using cold orbital forming processing. The shape of some subtle structures such as the boss and side branch can be formed well. The distribution features of the effective strain of the component with different blank lengths are almost the same, and the effective strain is bigger at the boss and the flash as the forming finished.
(2) The material flow is complex, especially in the boss, because the contact position between the rocking punch and the blank is changed with forming time under forming. The folding defect was observed at the root of the boss by FE simulation and experimental test. As such, future research should investigate optimizing the form processing and modifying the blank.
(3) After the blank deformed by cold orbital forming, the distributions of Mg2Si strengthening precipitates are more homogeneous in the matrix, and their shape changed from initially rod-like to particles in position A and short rod in the boss zone. Besides, these precipitated phases in the boss zone show obvious directivity due to the change of metal flow direction inside the boss.

Conclusions
In this paper, deformation characteristics and microstructures were studied by FE simulation, processing experiments, and SEM and EBSD examination during cold orbital forming of AA6063 aluminum alloy component with complex shape. It can be concluded that: (1) It is feasible to manufacture the AA6063 aluminum alloy component with complex shape using cold orbital forming processing. The shape of some subtle structures such as the boss and side branch can be formed well. The distribution features of the effective strain of the component with different blank lengths are almost the same, and the effective strain is bigger at the boss and the flash as the forming finished.
(2) The material flow is complex, especially in the boss, because the contact position between the rocking punch and the blank is changed with forming time under forming. The folding defect was observed at the root of the boss by FE simulation and experimental test. As such, future research should investigate optimizing the form processing and modifying the blank.
(3) After the blank deformed by cold orbital forming, the distributions of Mg 2 Si strengthening precipitates are more homogeneous in the matrix, and their shape changed from initially rod-like to particles in position A and short rod in the boss zone. Besides, these precipitated phases in the boss zone show obvious directivity due to the change of metal flow direction inside the boss.
(4) After cold orbital forming, the grains are elongated and the extent is different at different positions of boss zone. The crystal orientation discrepancy is smaller in the component main body and bigger in the boss zone. Besides, the elongated grains are tilted from RD.