 Original Article
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Investigation of TwoDimensional Ultrasonic Surface Burnishing Process on 7075T6 Aluminum
Chinese Journal of Mechanical Engineering volume 34, Article number: 19 (2021)
Abstract
A novel twodimensional ultrasonic surface burnishing process (2DUSBP) is proposed. 7075T6 aluminum samples are processed by a customdesigned 2DUSBP setup. Parameter optimization of 2DUSBP is conducted to determine the best processing strategy of 7075T6 aluminum. A uniform design method is utilized to optimize the 2DUSBP process. U_{13}(13^{3}) and U_{7}(7^{2}) tables are established to conduct parameter optimization. Burnishing depth, spindle speed, and feed rate are taken as the control parameters. The surface roughness and Vickers hardness are taken as the evaluation indicators. It establishes the active control models for surface quality. Dry wear tests are conducted to compare the wearresistance of the 2DUSBP treated sample and the original sample. Results show that the machining quality of 2DUSBP is best under 0.24 mm burnishing depth, 5000 r/min spindle speed, and 25 mm/min feed rate. The surface roughness S_{a} of the sample is reduced from 2517.758 to 50.878 nm, and the hardness of the sample surface is improved from 167 to 252 HV. Under the lower load, the wear mechanism of the 2DUSBP treated sample is mainly abrasive wear accompanied by delamination wear, while the wear mechanism of the original sample is mainly delamination wear. Under the higher load, the accumulation of frictional heat on the sample surface transforms the wear mechanisms of the original and the 2DUSBP treated samples into thermal wear.
1 Introduction
7075T6 aluminum is widely used in automobiles, aerospace, and other fields due to its low density, high processability, high specific elastic modulus, and high specific strength [1,2,3]. Aluminum is an excellent structure material, but its surface performance is not very well, whose wearresistance needs to be improved for broader industry applications [4,5,6]. Gradient nanostructure is recognized as an effective surface structure to improve the wearresistance of metal [7,8,9,10,11]. There are many methods to machine the gradient nanostructure on the material surface, such as laser shot peening [12], high energy shot peening [13], surface mechanical attrition treatment [14], and wirebrush [15]. Nonetheless, the methods mentioned above have disadvantages, which are easy to produce microcracks, unsatisfactory surface roughness, and thinner gradient nanostructure. Surface burnishing can realize continuous and controlled machining to produce gradient nanostructure with uniform thickness and smooth surfaces [16,17,18].
Researchers have achieved many research results in the field of surface burnishing. Lin et al. [19] found that surface burnishing can improve the comprehensive properties of the material surface, including hardness, surface roughness, and residual compressive stress. Rotella et al. [20] found that surface burnishing always improves the wear resistance of the components when cryogenic cooling and coated tools were employed. Bozdana et al. [21] introduced the ultrasonic field into the cryoburnishing process to machine Ti6Al4V, improved the surface hardness and the residual compressive stress of the sample with ideal surface roughness.
In the previous work of the research group, numerical simulation methods were introduced to investigate the varieties of grain sizes in the ultrasonicassisted surface burnishing process and reveal the relevant mechanism. The gradient nanostructure layer was machined on 7075aluminum samples by ultrasonicassisted surface burnishing process. The introduction of ultrasonic vibration increases the thickness of the gradient nanostructure [22, 23]. Nevertheless, ultrasonicassisted surface burnishing process has a higher coefficient of friction (COF) than surface burnishing process, which not conducive to surface roughness [24]. In the machining process, the twodimensional vibration can further optimize the cycle of stress loading, lessen the fluctuation of the machining force, and reduce COF. However, up to date, seldom researches have been committed to exploring the plane twodimensional ultrasonic surface burnishing process (2DUSBP). Material surface integrity is sensitive to 2DUSBP processing parameters. At present, the setting of processing parameters mainly depends on experience, resulting in large fluctuations in processing quality and low consistency. In order to improve the stability of the machining process, it is necessary to conduct an indepth study on the influence of related processing parameters in the machining process.
In the present study, the uniform design method is proposed to optimize the processing parameters of 2DUSBP. The surface roughness S_{a} and Vickers hardness of samples are characterized by a white light interferometer and Vickers hardness tester, respectively. Subsequently, active control models of surface roughness S_{a} and Vickers hardness are established based on uniform design tables. The dry wear properties of the sample machined based on the optimized processing parameters are characterized by a scanning electron microscope (SEM) and a confocal laser scanning microscope (CLSM), then the corresponding mechanisms are discussed.
2 Uniform Design and Experiment
2.1 Experiment Material and Processing Equipment
The detailed compositions of the 7075T6 aluminum (30 mm ×50 mm ×10 mm) in the experiment are listed in Table 1. The surface roughness S_{a} of the sample used in this experiment is 2517.7 nm, and the surface Vickers hardness is 167 HV.
The schematic diagram and photo of the 2DUSBP setup are shown in Figure 1. Figure 1(a) shows the customerdesigned burnishing tool, where eleven balls are evenly distributed in the circumferential direction of the lower end. Under the action of the downward pressure, the balls make pure rolling contact with the sample, causing plastic flow on the surface and reducing scratches. Figure 1(b) shows the twodimensional ultrasonic vibration platform that directly applies twodimensional ultrasonic vibration to the sample with a vibration frequency of 20 kHz and an amplitude of 9 μm, resulting in the reduction of the machining force between the tool and the sample. Figure 1(c) shows the photo of the 2DUSBP device that was installed on an XK714 CNC milling machine, of which the displacement accuracy is 1 μm, to precisely control the machining process according to the program. The essence of 2DUSBP is the surface plastic deformation caused by the impact and rolling contact between the burnishing ball and the machined surface. The surface peaks undergo plastic flow to fill the free valleys, resulting in reducing the surface roughness. Plastic deformation activates dislocation movement and dislocation proliferation, which changes the surface microstructure (dislocations, grains, phase structure) and increases the hardness.
2.2 Uniform Design Method
In order that the mapping relationship between processing parameters and surface quality is considered comprehensively, active control models of surface quality were established based on uniform design [25, 26]. Burnishing depth, spindle speed, and feed rate were introduced as control parameters. Meanwhile, the surface roughness S_{a}, measured by the white light interferometer with a measurement range of 500×500 μm, and Vickers hardness, measured by the HV1000 hardness tester under 50 g load and 10 s loading time, were used evaluation indicators. Three samples were machined for each set of parameters, and five measurement points were taken for each sample. Then, the average value was taken as evaluation indicators. Table 2 lists the available range of 2DUSBP processing parameters. A U_{13}(13^{3}) uniform design table, listed in Table 3, was established according to Table 2.
After 2DUSBP the sample, acetone was used to remove the oil on the sample surface. The surface roughness S_{a} and the Vickers hardness were characterized, whose preliminary regression equations were established based on the characterization results. In order to select the optimal processing parameters more accurately, a U_{7}(7^{2}) uniform design table, listed in Table 4, was further established based on the preliminary regression equations.
2.3 Wear Test
Dry wear tests were conducted to compare the wear behavior of the original sample and the 2DUSBP treated sample by a CETR UMT3 ballondisc tribometer. The upper sample was a GCr15 steel ball with a diameter of 8 mm and hardness of 65 HRC. Three parallel dry wear experiments of each sample were conducted under 5 N, 15 N, 25 N, and 35 N loads, respectively. During testing, the frequency, reciprocating stroke, and test time were set at 2 Hz, 5 mm, and 1200 s, respectively. The wear scars were characterized by SEM and CLSM.
3 Results
3.1 Establish Regression Equation
In order to avoid that largevalue parameter annihilate smallvalue parameter information, the values of the three parameters were linearly transformed, whose result is shown in Eqs. (1), (2), (3), respectively. The measurement results of the surface roughness S_{a} and the Vickers hardness are shown in Table 3. Figure 2 shows the experimental results of the U_{13}(13^{3}) uniform design table.
Based on Table 3, the results were fitted to establish a surface roughness regression equation and a hardness regression equation.
The surface roughness regression equation is given as:
The hardness regression equation is given as:
3.2 Dry Wear Test
Figure 3 shows the average of COF at the steady stage in dry wear tests. Under various loads, COF of the 2DUSBP treated sample is smaller than that of the original sample, and COF of the two has a similar trend with the increase of load. With the increase of the load, COF of the 2DUSBP treated sample decreased from 0.42 to 0.38 and stabilized around 0.38, while COF of the original sample decreased from 0.45 to 0.41 and stabilized around 0.41. The coefficient of variation, interquartile range of both decreased with the load increased. Under the same load, the coefficient of variation and interquartile range of the original sample are smaller than those of the 2DUSBP treated sample.
Figure 4 shows the crosssection of the wear scars measured by CLSM. Figure 5 shows the crosssection size of the wear scars (the maximum wear scar area, the maximum wear scar depth, and the maximum wear scar width) of the original sample and the 2DUSBP treated sample. Three samples were selected under the same test parameters, and the maximum size of each wear scar was recorded. Under the lower load (5 N, 15 N, and 25 N), the wear scar size of the original sample is larger than that of the 2DUSBP treated sample. Under the higher load (35 N), the wear scar size is close to the original sample and the 2DUSBP treated sample. The wear scar size of the 2DUSBP treated sample increased approximately linearly under the lower load. Similar trends existed in the original sample. When the load is 35 N, the increase rate of both wear scar sizes suddenly increases. Figure 6 shows the wear weight loss of the original sample and the 2DUSBP treated sample measured by electronic balance. Under the lower load, the wear weight loss of the 2DUSBP treated sample is less than that of the original sample, and the gap between the two increases with the increase of the load. Under the higher load, the original sample and the 2DUSBP treated sample have similar wear weight loss.
Figure 7 shows the wear scar morphologies of the original sample and the 2DUSBP treated sample by SEM. Figures 7(a), 7(c), 7(e) show that a large number of ploughlike wear marks parallel to the sliding direction due to abrasive wear on the surface of the 2DUSBP treated sample, accompanied by irregular peeling areas caused by delamination wear. As the load increases, the degree of abrasive wear increases first and then decreases. Figure 7(g) shows that under 35 N load, the 2DUSBP treated sample has a smoother wear scar, a smearing phenomenon caused by thermal wear. Figure 8 also shows that under the 5 N load, the wear scar of the 2DUSBP treated sample is mainly caused by abrasive wear accompanied by delamination wear. Meanwhile, under the 35 N load, the wear scar is mainly caused by thermal wear and accompanied by delamination wear. Figures 7(b), 7(d), and 7(f) show that under the load of 5 N, 15 N, and 25 N, many irregular peeling areas appear on the surface of the original sample due to delamination wear. Figure 7(h) shows that under the 35 N load, the surface wear scar of the original sample is mainly caused by thermal wear.
4 Discussion
4.1 Parameter Optimization
Regression equations based on uniform design cannot be extrapolated, to the extent that the extremum can only be found in the regression equation domain. According to the regression Eq. (4), BD=7, SS=17, and FR=5 are regarded as the extremum of the U_{13}(13^{3}) surface roughness regression equation, which differs from the actual extreme value of only 0.39%. According to the regression Eq. (5), BD=11, SS=25, and FR=5 are regarded as extremum of the U_{13}(13^{3}) hardness regression equation, which differs from the actual extreme value of only 0.05%.
Figure 9 and Figure 10 show that the U_{13}(13^{3}) hardness regression equation and the U_{13}(13^{3}) surface roughness regression equation at FR = 4, 5, and 6. When FR is in the range of 4‒6, there is only a slight difference in the shape and size of the hardness model and the surface roughness model. Both models are insensitive to changes near FR = 5 and more sensitive to BD and SS. It can be considered that FR and BD, SS have no interactivity near FR = 5. Considering the hardness and surface roughness comprehensively, the surface machining quality of the material is close to the optimum value when FR = 5. Furthermore, Figure 9 shows that there is a strong interaction between SS and BD, where it have two better regions, which are BD = 7‒12, SS = 1‒3, and BD = 7‒11, SS = 22‒25. Figure 10 shows that BD has a more significant effect on S_{a}, with better results at BD = 5‒10, SS=5‒25. In order to establish more accurate regression equations. Take BD = [7, 8, 9, 10, 11], SS = [17, 18, 19, 20, 21, 22, 23, 24, 25], FR=5, then solve regression Eqs. (4), (5). The solution results are shown in Tables 4 and 5.
Table 4 shows that when BD=7, S_{a} grows slowly with the increases of SS. When BD=7, SS=25, the predicted value of S_{a} is only 7.89% larger than the extremum. Table 5 shows that when SS=25, the hardness decreases slowly with the decrease of BD. When BD=7, SS=25, the hardness prediction value is only 8.06% smaller than the extremum. Considering surface roughness and hardness comprehensively, BD=7, SS=25, and FR=5 are the better parameters of surface machining quality. A new U_{7}(7^{2}) uniform design table was established with BD=7, SS=25, and FR=5 to find the optimal combination of test conditions further. Table 6 lists the U_{7}(7^{2}) uniform design table. Figure 11 shows the U_{7}(7^{2}) uniform design experiment results.
Based on Table 6, the results were fitted to establish a surface roughness regression equation and a hardness regression equation.
The surface roughness regression equation is given as:
The hardness regression equation is given as:
Table 7 shows the significance analysis for two regression equations. The coefficient of determination R^{2} of the surface roughness regression equation is 0.997. The sum of squares of S_{a} regression explains 99.7% of the total sum of squares of the model, and the equation fits well. The significance of Eq. (6) is less than onethousandth, and the model confidence is high. From the results of Table 7, the coefficient of determination R^{2} of the hardness regression equation is 0.810. The sum of squared regressions of hardness explains that 81.0% of the total square sum of the models, and the degree of equation fitting is within the acceptance range. The significance of Eq. (7) is 3.6%, and the model confidence is high.
Figures 12 and 13 show the U_{7}(7^{2}) surface roughness regression equation and the U_{7}(7^{2}) hardness regression equation. When BD=8, SS=25, the two are close to the extremum, whose extremums are R=74.155 nm, V =253.06 HV. Therefore, the processing quality of 2DUSBP is best under 0.24 mm burnishing depth, 5000 r/min spindle speed, and 25 mm/min feed rate.
Figure 14 shows the 3D profile of the 7075T6 aluminum surface before and after 2DUSBP. After 2DUSBP, surface roughness S_{a} of the sample is reduced from 2517.758 nm to 50.878 nm, and the Vickers hardness is improved from 167 to 252 HV. The original texture of the sample surface disappeared, and the surface became flat.
4.2 Wear Behavior
When the friction pairs slide relative to each other, the two surfaces are subject to tangential resistance (friction) at the contact point due to mechanical engagement and molecular attraction. Therefore, the frictional resistance during dry wear comprises two parts: the adhesion resistance and the plough resistance, of which adhesion resistance dominates. According to the modified adhesionplough friction theory, the friction force comprises adhesion force and plough force [27].
where T is the shear stress, A is the actual contact area, τ_{b} is the shear strength of the adhesion point, P_{e} is the plough force, S is the ploughed area, and p_{e} is the plough force per unit area.
2DUSBP increases the surface hardness and smooths the sample surface, reducing the actual contact area between the friction pairs and the ploughed area. Therefore, COF of the 2DUSBP treated sample is lower than the original sample. Figure 3(a) shows that COF decreases with increasing load, which is because of the nonlinear relationship between actual contact area and the load. Figure 3(b) shows that under each load, the coefficient of variation and the interquartile range of COF of the original sample is smaller than the 2DUSBP treated sample. Dry wear is a pulsating process in which sticking and sliding occur alternately, so COF inevitably undergoes a significant fluctuation phenomenon, the stickslip phenomenon [28]. COF is calculated by averaging the period. Therefore, in order to study the discrete characteristics of COF, it is necessary to study the discrete characteristics of the friction force and the loading force.
Table 8 shows the statistical results of the friction force and loading force collected during the dry wear process. For the friction force, the interquartile range of the 2DUSBP treated sample is more extensive than the original sample, but the coefficient of variation has no distinct tendency for the two. The interquartile range represents the degree of concentration of the data, and the coefficient of variation represents the degree of dispersion. Compared to the 2DUSBP treated sample, the data near the average of the original sample is more concentrated, while the data far from the average is more divergent. Figure 15 shows the microtopography of the crosssection of the original sample and the 2DUSBP treated sample by a KEYENCE optical microscope. The surface grain of the original sample is coarse. After 2DUSBP, the surface grain has obvious plastic deformation and grain refinement, significantly improving the surface hardness. Previous research by the research group shows that the grains on the surface of 7075T6 aluminum can be refined to 15 nm [23]. The 2DUSBP treated sample keep nanocrystalline/ultrafine crystals on the surface, whose chemical activity is higher than the original sample surface. Because of the formation and shearing of the adhesive node during the dry wear process, the 2DUSBP treated sample is more prone to adhesion, resulting in that its friction force is less concentrated than the original sample. The wear mechanism of the original sample is mainly delamination wear, and the generation and expansion of cracks can absorb and release friction energy. Therefore, the data near the average of the original sample is more concentrated, while the data far from the average is more divergent. For the loading force, the interquartile range and the coefficient of variation of the 2DUSBP treated sample is more extensive than the original sample. During the sliding of the upper sample, the peak hardness of the contact point of the 2DUSBP treated sample is higher than the original sample. Therefore, the loading force of the 2DUSBP treated sample is highly volatile. The volatility of the friction coefficient results from the combination of friction force and loading force volatility.
Figures 4 and 5 show that when the load is 5‒25 N, the wear scar size of the 2DUSBP treated sample is proportional to the load. This linear relationship has been reported in abrasive wear [28, 29]. Because the wear mechanism of the original sample is delamination wear, there is no such linear relationship. Under the load of 35 N, the linear relationship of the 2DUSBP treated sample is destroyed, and the wear scar size of the 2DUSBP treated sample and the original sample are close. It is because the wear mechanism of the two has changed.
Figures 7(a), (c) shows that for the 2DUSBP treated sample, the wear mechanism under 5 N, and 25 N load is mainly abrasive wear accompanied by delamination wear. The abrasive particles are pressed into the friction surface by the normal force to form an indentation on the friction surface. Subsequently, under the action of the tangential force, the abrasive particles advance to shear, plow, and cut the friction surface. Figures 7(e), (g) show that as the load increases, the abrasive wear phenomenon gradually weakens, hardly observed at the 35 N load. As the load increases, the temperature at the friction zone gradually increases, softening the upper sample and the friction surface. The increase in the temperature of the friction pair reduces the hardness of the abrasive particles, improves the ductility of the friction surface, and reduces the degree of abrasive wear. At 35 N load, thermal wear causes the surface to “smear”, transfers and rubs off surface particles [30].
Figures 7(b), (d), (f) show that the delamination wear, generated thin and long lamellar wear debris, causes irregular detachment areas on the surface of the original sample. When the friction pairs slide against each other, the rough peak on the soft surface is easily deformed and broken under the cyclic load to form a smooth surface. During the dry wear process, the shear deformation accumulates, causing dislocation accumulation at a certain depth below the surface, which leads to the formation of cracks or voids. The crack extends in a direction parallel to the surface. When the crack propagates to a critical length, the material between the crack and the surface will peel off in the form of flaky wear debris. Figure 7(h) shows that the wear mechanism is a combination of thermal wear and delamination wear, which is similar to the mechanism of Figure 7(g) and not repeated here.
The wear mechanisms between the 2DUSBP treated sample and the original sample are different because 2DUSBP changed the mechanical properties and microstructure of the 7075T6 aluminum surface. Figure 14 shows that 2DUSBP improves the threedimensional profile of the sample surface, making the material surface smoother. The coarse grains and large roughness of the original sample surface caused significant discontinuities in composition and morphology, which constituted the source of stress concentration and caused the surface to experience higher stress cycles. 2DUSBP improves the uniformity of the sample surface and reduces stress concentration. Under the lower load, 2DUSBP improves the surface quality of the sample, resulting in reduced wear weight loss and reduced wear scar size. However, under the higher load, a large amount of heat is generated between the friction pairs, changing the microstructure and mechanical properties of the sample surface. Therefore, the difference in weight loss and wear scar size between the original sample and the 2DUSBP treated sample under the higher load is smaller than the difference between the two under the lower load.
5 Conclusions

(1)
A novel highefficiency surface burnishing tool is proposed, combined with a twodimensional ultrasonic vibration platform to improve the surface properties of 7075T6 aluminum. U_{13}(13^{3}) and U_{7}(7^{2}) uniform design tables are established with burnishing depth, spindle speed and feed rate as control parameters, and surface roughness S_{a}, Vickers hardness as evaluation indicators. Based on the results of the uniform design tables, surface quality regression equations are established to optimize 2DUSBP processing parameters. The optimal machining strategy for 7075T6 is 0.24 mm burnishing depth, 5000 r/min spindle speed, and 25 mm/min feed rate.

(2)
2DUSBP reduced the surface roughness S_{a} of the 7075T6 aluminum from 2517.758 to 50.878 nm and increased the Vickers hardness of the 7075T6 aluminum surface from 167 to 252 HV. The original texture of the sample surface disappeared, the surface became flat, and the surface hardness increased. Therefore, under different loads, the friction coefficient of the 2DUSBP treated sample is smaller than the original sample.

(3)
Dry wear experiments show that under the lower load, the wear mechanism of the 2DUSBP treated sample is abrasive wear, and the original sample is delamination wear. The wear weight loss and the wear scar size of the 2DUSBP treated sample are much smaller than the original sample. 2DUSBP reduces the unevenness of the sample surface, refines the grains in the surface layer, and improves the surface hardness, making the sample has a better wearresistance. Under the higher load, the accumulation of frictional heat transforms the wear mechanism of the original sample and the 2DUSBP treated sample into thermal wear, which reduces the wear weight loss and the wear scar size gap between the two samples.
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Acknowledgements
The authors sincerely thank to Professor Mingxue Shen of East China Jiaotong University for his assistance during manuscript preparation.
Funding
Supported by National Natural Science Foundation of China (Grant Nos. 51675483, 51705028), Fundamental Research Funds for the Provincial Universities of Zhejiang (Grant No. RFA2019008), Foundations (Grant Nos. 61409230606, EM2015042003).
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ZP was in charge of the whole trial; ZZ wrote the manuscript; GY conducted the experiments; ZZ and QZ conceived and designed the research; CD and GP revised the manuscript. All authors read and approved the final manuscript.
Authors’ Information
Zhenyu Zhou, born in 1993, is currently a PhD candidate at Key Laboratory of Special Purpose Equipment and Advanced Processing Technology (Zhejiang University of Technology), Ministry of Education, China. He received his bachelor degree from Zhejiang University of Technology, China, in 2016. His research interests include surface engineering. Email: zhouzy@zjut.edu.cn.
Qiuyang Zheng, born in 1995, is currently a PhD candidate at Key Laboratory of Special Purpose Equipment and Advanced Processing Technology (Zhejiang University of Technology), Ministry of Education, China. He received his bachelor degree from Zhejiang University of Technology, China, in 2017. His research interests include surface engineering. Email: m15990049659@163.com.
Cong Ding, born in 1990, is currently an associate professor at School of Mechanical Engineering, Zhejiang University of Technology, China. She received her bachelor degree from China University of Mining and Technology, in 2014 and PhD degree from China University of Mining and Technology, in 2019. Her research interests include surface engineering and tribology. Email: dcong105@126.com.
Guanglei Yu, born in 1994, is currently a master candidate at Key Laboratory of Special Purpose Equipment and Advanced Processing Technology (Zhejiang University of Technology), Ministry of Education, China. Email: glyu33@zjut.edu.cn.
Guangjian Peng, born in 1986, is currently an associate professor at School of Mechanical Engineering, Zhejiang University of Technology, China. His research interests include micronano manufacturing. Email: penggj@zjut.edu.cn.
Zhongyu Piao, born in 1982, is currently an associate professor at School of Mechanical Engineering, Zhejiang University of Technology, China. His research interests include surface engineering and tribology. Email: piaozy@zjut.edu.cn.
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Zhou, Z., Zheng, Q., Ding, C. et al. Investigation of TwoDimensional Ultrasonic Surface Burnishing Process on 7075T6 Aluminum. Chin. J. Mech. Eng. 34, 19 (2021). https://doi.org/10.1186/s1003302100540z
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DOI: https://doi.org/10.1186/s1003302100540z