e Schematic diagram of FSP and different regions.

e Schematic diagram of FSP and different regions.

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Nowadays friction stir processing (FSP) has been used as a surface modification technology. The FSP improves the surface properties of the material by intense plastic deformation, mixing and breaking the base material through stirring action alongside the heat generated by friction to achieve dense and homogenized microstructure. Moreover, FSP is a...

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... applications of FSP include obtaining ultra-fine grains [43,44], surface hardening [45,46], hybrid reinforcement and in-situ surface composites [28,47], and fabrication of various MMCs [48,49]. Figure 1 shows a schematic diagram and the different zones formed during FSP. These zones are divided into four regions: stirring zone (SZ), thermomechanical affected zone (TMAZ), heat-affected zone (HAZ), and base material (BM) [50]. ...
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... focused on cooling method after FSP on AZ91 alloy. The Vickers hardness distribution of the processing area is shown in Fig. 10. The highest hardness was recorded for the jet nozzle cooling samples ranging from 90 to 100 HV0.1. At about 1 mm below the surface, the hardness decreased to 85e94 HV0.1. These results showed that the hardness of the material decreased with the increase of the grain size, which was consistent with the HallePetch ...
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... wear mechanism tended to be abrasive wear. Figure 11 displays the size of the fragments and wear debris was inconsistent. It is shown that fragments resulted from the processed samples was smaller than that from BM. ...
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... studied the influence of different TS on the tribological properties of Ti6Al4V. Figure 13 shows the wear surface morphology observed by SEM. The wear surface morphology of the BM was characterized by deep groove wear, Fig. 13(a). ...
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... studied the influence of different TS on the tribological properties of Ti6Al4V. Figure 13 shows the wear surface morphology observed by SEM. The wear surface morphology of the BM was characterized by deep groove wear, Fig. 13(a). Severe plough and irregular tear pits were observed, o u r n a l o f m a t e r i a l s r e s e a r c h a n d t e c h n o l o g y 2 0 2 2 ; 2 0 : 1 9 4 0 e1 9 7 5 indicating poor friction performance of the BM. The coefficient of friction (COF) was 0.56 and the wear rate reached the highest value (3.96 Â 10 À4 mm 3 /N.m). The authors ...
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... et al. [76] examined the corrosion behavior of pure titanium before and after FSP by using electrochemical impedance spectroscopy (EIS) in phosphate buffer solution, Fig. 14. All the workpieces showed imperfect depressed semicircles. It was observed that the FSP of pure titanium with three passes had the highest corrosion resistance compared with the BM and single-pass FSP. The possible reason behind this is that crystal grains were rapidly refined the and dynamically recrystallized. So, the increase in ...
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... et al. [77] investigated the corrosion properties of magnesium ZE41. Figure 15 shows the polarization curves obtained. Before FSP, the corrosion rate was 3.15 mm/year, while the corrosion rate was 3.01 mm/year after FSP. ...
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... et al. [78] conducted electrochemical corrosion tests on AE42 alloy under different FSP parameters, Fig. 16. When the grain size difference was slight, the proportion of oxide layer formed on the surface was not significantly different. For the samples with small particles, surface energy increased surface dissolution and corrosion rate. Because the oxide layer connected fine particles, the oxide layer became stronger and broader, and the ...
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... particles can be embedded into the BM in various strategies during FSP, Fig. 17 and Table 2. Figure 17(a) shows the simplest way by laying a layer on the surface of BM. As long as the preplaced layer is uniform everywhere, but within the FSP, the high-speed rotating tool will seriously affect the uniformity of the particles [56]. To overcome this effect, many researchers have tried to drill grooves or holes to ...
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... particles can be embedded into the BM in various strategies during FSP, Fig. 17 and Table 2. Figure 17(a) shows the simplest way by laying a layer on the surface of BM. As long as the preplaced layer is uniform everywhere, but within the FSP, the high-speed rotating tool will seriously affect the uniformity of the particles [56]. ...
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... 17(a) shows the simplest way by laying a layer on the surface of BM. As long as the preplaced layer is uniform everywhere, but within the FSP, the high-speed rotating tool will seriously affect the uniformity of the particles [56]. To overcome this effect, many researchers have tried to drill grooves or holes to introduce reinforcement particles, Fig. 17(bed). Drilling holes into the surface of the BM requires consideration of the holes size, depth, and spacing, which will affect whether the coating can be evenly distributed in the SZ and requires multiple FSP passes [99]. The formation of grooves on the surface of the BM is also a helpful way such as straight lines and curves, Fig. ...
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... particles, Fig. 17(bed). Drilling holes into the surface of the BM requires consideration of the holes size, depth, and spacing, which will affect whether the coating can be evenly distributed in the SZ and requires multiple FSP passes [99]. The formation of grooves on the surface of the BM is also a helpful way such as straight lines and curves, Fig. 17(e, f). Most of the articles investigated straight lines within FSP [100,101]. Most of the articles preferred to choose along the traverse direction. However, some authors recently chose the groove direction to be perpendicular to the traverse direction, ensuring that the coating material is not extruded and can better combine the ...
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... parameters of FSP directly affect the uniformity of nanoparticles distribution. The authors found that reinforcement nanoparticles were almost uniformly distributed throughout the SZ in all samples after FSP. Three different microstructure zones were observed: SZ, TMAZ, and HAZ, Fig. 18. They observed that different nanoparticles exhibit different grain refinement effects. In the absence of nanoparticles, the average grain size in SZ was 81.1 mm, while the grain sizes of the workpiece processed with BN, SiC, Al 2 O 3 , and VC were in a range of 3.5e5 ...
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... et al. [83] used FSP to prepare Ti6Al4V reinforcement particles for AZ31 magnesium-based alloy by changing the volume content of Ti6Al4V particles from 0 to 27%, Fig. 19. When the content of reinforcing particles increased, the grain size continued to decrease, and the grain structure refined more, Fig. 19(bed). It can be observed that Ti6Al4V particles were evenly distributed and firmly bonded to the matrix alloy and interface, without diffusion layer, reaction layer and porosity. They also reported ...
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... et al. [83] used FSP to prepare Ti6Al4V reinforcement particles for AZ31 magnesium-based alloy by changing the volume content of Ti6Al4V particles from 0 to 27%, Fig. 19. When the content of reinforcing particles increased, the grain size continued to decrease, and the grain structure refined more, Fig. 19(bed). It can be observed that Ti6Al4V particles were evenly distributed and firmly bonded to the matrix alloy and interface, without diffusion layer, reaction layer and porosity. They also reported that Ti6Al4V particles were beneficial in enhancing the composites and produced sufficient plastic flow before fracture. Wang et al. [107] ...
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... The Vickers hardness was measured at different regions, Fig. 31. The average indentation hardness of the base material was 61 HV0.1, and the hardness of the FSP sample without adding any enhanced particles increased to 70 HV0.1. By comparing Fig. 31(a, b), it was found that the TiB 2 particles had a more substantial strengthening effect and higher hardness in the SZ. When the mass fraction of TiB 2 ...
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... The Vickers hardness was measured at different regions, Fig. 31. The average indentation hardness of the base material was 61 HV0.1, and the hardness of the FSP sample without adding any enhanced particles increased to 70 HV0.1. By comparing Fig. 31(a, b), it was found that the TiB 2 particles had a more substantial strengthening effect and higher hardness in the SZ. When the mass fraction of TiB 2 particles increased to 30% (Fig. 31(a)), the average hardness value increased to 90 HV0.1 and When the mass fraction of Gr nanoparticles increased to 2% (Fig. 31(b)), the average hardness ...
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... hardness of the base material was 61 HV0.1, and the hardness of the FSP sample without adding any enhanced particles increased to 70 HV0.1. By comparing Fig. 31(a, b), it was found that the TiB 2 particles had a more substantial strengthening effect and higher hardness in the SZ. When the mass fraction of TiB 2 particles increased to 30% (Fig. 31(a)), the average hardness value increased to 90 HV0.1 and When the mass fraction of Gr nanoparticles increased to 2% (Fig. 31(b)), the average hardness value increased to 84 HV0.1. In the AA6061-Gr-TiB 2 hybrid nanocomposites, it was found that the hardness of 1 wt % Gr-20 wt% TiB 2 was increased 67% (to 102 HV0.1, Fig. 31(c). The ...
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... increased to 70 HV0.1. By comparing Fig. 31(a, b), it was found that the TiB 2 particles had a more substantial strengthening effect and higher hardness in the SZ. When the mass fraction of TiB 2 particles increased to 30% (Fig. 31(a)), the average hardness value increased to 90 HV0.1 and When the mass fraction of Gr nanoparticles increased to 2% (Fig. 31(b)), the average hardness value increased to 84 HV0.1. In the AA6061-Gr-TiB 2 hybrid nanocomposites, it was found that the hardness of 1 wt % Gr-20 wt% TiB 2 was increased 67% (to 102 HV0.1, Fig. 31(c). The increase in hardness was due to grain refinement. The other aspect was the addition of multi-reinforcement particles at the ...
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... increased to 30% (Fig. 31(a)), the average hardness value increased to 90 HV0.1 and When the mass fraction of Gr nanoparticles increased to 2% (Fig. 31(b)), the average hardness value increased to 84 HV0.1. In the AA6061-Gr-TiB 2 hybrid nanocomposites, it was found that the hardness of 1 wt % Gr-20 wt% TiB 2 was increased 67% (to 102 HV0.1, Fig. 31(c). The increase in hardness was due to grain refinement. The other aspect was the addition of multi-reinforcement particles at the appropriate proportion. At this ratio, the yield strength was also significantly increased, reaching 225 MPa, with an increase of 300% and a decrease of elongation of about ...

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Citations

... Friction Stir Welding (FSW) has been invented for more than three decades and quickly applied to the joining of many materials, [1][2][3][4][5] for example, aluminum alloys, 6-11 magnesium alloys, [11][12][13] steels, [14][15][16][17] titanium alloys, [18][19][20] and even dissimilar metals. [21][22][23][24][25][26] Based on FSW, different new processing technologies are developed, including friction stir processing, 27 friction stir spot welding, 28,29 friction stir additive manufacturing, [30][31][32] etc. Friction Stir Additive Manufacturing (FSAM) is a solid state technology. In FSAM, the problems occurring in solidification processes in general additive manufacturing technology with liquidsolid transformations can be avoided. ...
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... Also, the study of MMCs is constantly broadening due to the fact that such materials can be fabricated through the incorporation of a huge mix of reinforcements that are added to the matrix with the possibility of varying not only their type, but also their size, shape and content [3]. Further, it was observed that such variations tend to tune the final composite properties and provide the designer with innumerable options to come up with a material which suits the targeted application [4][5][6]. Amongst the innumerable types of reinforcement, ceramic reinforcements, in both micro and nano scales, have attracted the highest interest [7]. MMCs, due to the merging of the properties of the base alloy and the ceramic reinforcements, possess a superior combination of properties such as ductility coupled with improved toughness and reduced weight with high strength [8]. ...
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