XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:30am] (PIC) [1–17] [PREPRINTER stage] Original Article An investigative study on the performance of twist roll machine in a continuous cold strip rolling mill Proc IMechE Part C: J Mechanical Engineering Science 0(0) 1–17 ! IMechE 2012 Reprints and permissions: sagepub.co.uk/journalsPermissions.nav DOI: 10.1177/0954406212469149 pic.sagepub.com Amir Mostashfi1, Mahmoud Kadkhodaei1, Mehrdad Poursina2 and Saeid R Bakhshi3 Abstract In many modern continuous production lines of steel sheets, a twist roll machine is used to change the strip direction for shortening the production line. A twist roll machine typically consists of a cylindrical body on which some guide rollers are mounted in rows to gradually change the traveling direction of the strip when passes over the guide rollers. In this article, quality of the sheets after exiting an industrial twist roll machine is first investigated. The amount and distribution of wear on the guide rollers are also assessed by measuring and comparing diameter at different sections of selected worn and new guide rollers. The specific wear rate as well as friction coefficient for guide rollers made of two different popular polymers is measured by pin-on-disk wear tests. Details of the strip path on the twist roll machine as well as contact between the strip and all the guide rollers are specified, and stress distribution in strip and the guide rollers is studied by finite element analysis. Effects of the guide rollers material and arrangement, the bridle rolls tension, and width and thickness of the strip on the amount and distribution of wear on the guide rollers as well as the elasto-plastic response of the strip are studied. The results are utilized to propose techniques for reducing defects on the sheet and the guide rollers, and finite element simulations show the effectiveness of these techniques. Keywords Twist roll, continuous rolling, wear, guide roller, strip defect Date received: 26 June 2012; accepted: 25 October 2012 Introduction In recent years, continuation of movement from one piece of equipment to another one has been investigated in various manners as a factor of rationalization for manufacture of steel sheets. However, since it involves various problems regarding the installation area and other aspects to array a number of pieces of equipment in a linear manner, in order to enable arrangement of the equipment in a small area, it is contemplated to change the traveling direction of the sheet. This is also necessary for achieving continuation of movement between existing pieces of equipment.1 One of the important equipment in most of the continuous production lines of steel sheet is twist roll machine, using which the traveling direction of the strip is changed to reduce the length of the production line. Figure 1 shows a schematic of this machine. The strip generally enters a twist roll machine (TRM) from above and begins to rotate by passing over some guide rollers, which are mounted in rows on the cylindrical body of the machine. The strip exits from below the TRM while its direction is changed by 90 . In 1918, Rosen2 presented the first mechanism for rotation of sheet in rolling mills. This mechanism, based on which many similar machines have been so far proposed, consisted of a cylindrical body containing steel balls to guide the strip motion. However, it was used just in a few industries because it made much noise and caused damages to the sheet due to its concentrated contact with the balls. Later, in 1986, Hashimito et al.1 founded the current roller-type twist roll, which has been widely used in steel production 1 Department of Mechanical Engineering, Isfahan University of Technology, Isfahan, Iran 2 Department of Mechanical Engineering, Faculty of Engineering, University of Isfahan, Isfahan, Iran 3 Department of Materials Engineering, Malek-Ashtar University of Technology, Isfahan, Iran Corresponding author: Mahmoud Kadkhodaei, Department of Mechanical Engineering, Isfahan University of Technology, Isfahan 84156-83111, Iran. Email: [email protected] Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:30am] (PIC) [1–17] [PREPRINTER stage] 2 Proc IMechE Part C: J Mechanical Engineering Science 0(0) companies. The guide rollers are usually made of polymer, among which polyamide 66 (PA66) and polyamide 11 (PA11) are the most common materials. When a TRM is utilized in a rolling mill, any improper adjustment in the sheet tension, contact between the strip and the guide rollers, arrangement of the guide rollers, or their material may cause imperfections such as formation of crossbow in the sheet or indented lines on its surface, and excessive or uneven wear on the guide rollers. A lot of modifications are thus tried in practice to reduce these damages, and no comprehensive technique is reported so far due to the complexity of the machine as well as changes in the sheet properties such as width, thickness, and material in different companies and different production schedules of a rolling mill. Consequently, published researches are also generally just focused on wear characteristics of the guide rollers for selection of appropriate materials to minimize their wear rate. Unal et al.3 investigated dry sliding wear characteristics of some industrial polymers against steel counterface with the use of a pin-on-disc testing machine. They studied the influence of test speed as well as the applied pressure values on friction and wear behavior of PA66 and other industrial polymers. They reported that the friction coefficient decreases with increase in the amount of pressure and that the specific wear rate of PA66 is less than that of the other polymers. They also found that the specific wear rate shows a very little sensitivity to the applied pressure and test speed for PA66. Chen et al.4 investigated the effect of fiber reinforcement on the friction and wear behavior of PA66 running against itself using a twin-disc test rig. They showed that both the wear and friction properties of unreinforced PA66 can be improved considerably by filling it with 20 wt% PTFE. Further, Kukureka et al.5 found that one of the major benefits of fiber reinforcement, particularly by using glass, is that it reduces the coefficient of friction and hence allows the material to be used for heavier duties without exceeding the softening point of the matrix. This increase in duty, however, increases the specific wear rate leading to a shorter component life. Chen et al.6 studied the mechanical and tribological properties of PA/PPS blends. They found that the crystalline structure of PA66, PPS, and PA66/PPS blends changes due to sliding and tribochemical reactions occurred with the PA66 and the PA66 phases in blends. In this article, for the TRM of Mobarkeh Steel Company (MSC) in Iran, defects on the steel sheets caused by the machine are first studied. Also specific wear rate and its distribution on the guide rollers are evaluated through the measurement of the worn guide rollers diameter at different sections, and the obtained dimensions are compared with those in the new guide rollers. As PA66 and PA11 are two popular materials for the guide rollers in MSC, pin-on-disk tests are carried out to assess and compare the friction and wear behavior of these two materials. Pin specimens are fabricated from sheets crossing over the TRM, and specific wear rate as well as friction coefficient is determined for different applied normal loads and sliding velocities. Geometry of the whole machine together with the passing strip is created in CATIA to investigate exact path of the strip on the TRM as well as its contact with all the guide rollers. This helps to better understand the origin of uneven wear on the guide rollers as well as differences in the wear behavior of different guide-roller rows. Finite element simulations of travelling the strip over the TRM guide rollers for different operational conditions are done using ABAQUS/Explicit, and stress distribution in strip and the guide rollers is studied. Finite element (FE) results as well as the wear test findings are utilized to study the effect of material and arrangement of the guide rollers, the bridle rolls tension, and width and thicknesses of the strip on the guide rollers specific wear rate and its distribution as well as the defects on the strip. Based on these findings, practical Figure 1. A schematic of a twist roll machine. Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:30am] (PIC) [1–17] [PREPRINTER stage] Mostashfi et al. 3 techniques are systematically found to reduce damages to the sheet and the guide rollers in the studied TRM. Effectiveness of these techniques is shown in the finite element simulations indicating that the method proposed in this article can be considered as an organized troubleshooting procedure for a TRM. Defects of the TRM Investigating the TRM of Mobarakeh Steel Company, the following major damages to the sheet and the guide rollers are identified: Crossbow formation on the sheet Although the ingoing strip to the TRM is tried to have a flat and smooth cross section, its edges are slightly deformed at exit from the machine leading to crossbow formation as shown in Figure 2. Crossbow is a type of surface-to-surface length differential defect, and it is seen in practice that this defect declines with decrease in the sheet thickness. strip and the guide rollers to be non-uniform and different from the expected manner. This leads to more pronounced defects on the sheet. The amount of the bridle rolls tension, the cross-sectional dimensions of the sheet, and the guide roller materials mainly affect the wear rate. In MSC, the guide rollers are made of PA66 or PA11, and investigations show that these two polymers exhibit different wear behaviors for the same process conditions. Angular wear of guide rollers In some of the TRM guide rollers, wear pattern is not flat but rather angular. Angular wear results in the sheet deviation to one side of its path, and hence more wear is made on the guide rollers of that side. Figure 4(a) and (b) shows the flat and angular wear of the guide rollers, respectively. Geometrical considerations of the TRM The TRM guide rollers are gradually worn during operation due to contact with the travelling strip. Beside the material waste, decrease in the guide rollers diameter due to wear causes the contact between the As shown in Figure 5, the studied TRM consists of 7 guide-roller rows, each of which contains 27 guide rollers. The traveling direction of steel sheet is changed by its movement in a spiral manner over these guide-roller rows. The method of numbering the guide rollers is shown in Figure 5. The components of TRM are modeled in CATIA to better understand configuration of the machine and the strip and to show how the strip rotates over the machine. Using this 3D model, it is possible to determine the area, length, and angle of contact between the sheet and the guide rollers. This angle, varying between 5 and 7.5 , is shown in Figure 6. The contact angle increases in initial and final guide-roller rows due to more asymmetrical contact between the strip and the guide rollers. Due to the guide rollers arrangement on the cylindrical body and also the existence of the bridle tension on the sheet, outer edges of the guide rollers have the longest contact with the sheet. As a result, the amount of wear in this edge is more Figure 2. Crossbow in the sheet. Figure 3. Indented lines on the strip surface. Indented lines on the sheet surface When the strip passes over the TRM guide rollers, longitudinal indented lines shown in Figure 3 appear on its surface. Investigation of this defect indicates that increase in the bridle rolls tension leads to more tense indentations on the sheet surface. Measurements in MSC show that the depth of these indented lines varies from 0.1 to 1 mm along the strip length. This defect causes severe decrease in the quality of the produced sheet. Excessive wear on the guide rollers Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:30am] (PIC) [1–17] [PREPRINTER stage] 4 Proc IMechE Part C: J Mechanical Engineering Science 0(0) than the other one causing the angular wear of the guide rollers (Figure 4(b)). Once the contact angle between the guide rollers of a row and the raveling strip is determined in the CATIA model, average of the angles can be calculated as the theoretical wear angle in that row. The actual wear angle can be evaluated in practice, too, by measuring the slope on the surface of the worn guide rollers. In Figure 7 the experimental measurements on PA11 guide rollers are compared with the theoretical wear angles derived from the CATIA model. Referring to Figure 5, number of the guide-roller rows begins from 1, for the first row at entry side, and ends to 7, for the last row at exit side. As it can be seen, a very good agreement exists between the experimental and the simulation results for the middle roller rows. Differences shown for the initial and the final rows mainly arise from the following sources: 1. The arrangement of the guide rollers is so that the initial and the final rows are subjected to less average contact pressure in comparison to the middle ones. It will be shown in section ‘Wear behavior of guide rollers in the TRM’ that decrease in the contact pressure would lead to increase in the amount of wear especially for PA11. 2. The sheet experiences some fluctuations in practice when passing over the initial and the final guide-roller rows. This may be considered as another reason for a less contact pressure acting on these rollers leading to more wear on them. Figure 4. Two wear patterns on the guide rollers: (a) flat wear and (b) angular wear. Accordingly, the CATIA model gives a theoretical wear angle in which only geometrical aspects of the contacts are taken into account. However, less contact pressure causes more wear rate than the theoretical predictions. Consequently, beside the geometrical details, effects of contact pressure and some other factors are studied in section ‘Wear behavior of guide Figure 5. A schematic of the TRM guide rollers showing the method of numbering the rows and the rollers of each row. TRM: twist roll machine. Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:31am] (PIC) [1–17] [PREPRINTER stage] Mostashfi et al. 5 rollers in the TRM’ to more practically investigate the wear behaviors of the guide rollers. It should be noted that deep groove ball bearing are usually employed as the hinge supports of the guide rollers in a TRM. As these bearings cannot compensate any misalignment, using self-aligning bearings is suggested to allow the guide rollers to adjust their orientation relative to the sheet surface leading to less angular wear of the guide rollers. Moreover, if some guide-roller rows are added between the rows with high wear, the number of locations where the sheets rotate over the guide rollers is increased. This leads to smaller contact angle between the sheets and the guide rollers, and hence less angular wear is achieved. Figure 7 shows that the guide-roller rows 1, 2, 6, and 7 experience more angular wear than the other ones. So, addition of one row between the rows 1 and 2 and another between the rows 6 and 7 may effectively decrease the amount of angular wear in the guide rollers. the tensions of the bridle rolls located before and after the TRM. 2. Due to the existence of the bridle rolls, entry and the exit edges of the sheet are so fixed that they cannot move and/or rotate transversely and vertically. In other words, the sheet is only free to move and/or rotate longitudinally. 3. The front edge of the sheet moves with the velocity of 2 m/s at exit from the TRM. 4. Since the weight of the sheet crossing from TRM is not negligible, the gravity acceleration is defined for the sheet. C3D8R (an 8-node linear brick element with reduced integration and hourglass control) element is used to Stress analysis of the Sheet To study the stress distribution in the sheet, finite element method (FEM) is employed using ABAQUS/Explicit. The contact of guide rollers with the traveling sheet is assumed to be surface-to-surface using penalty contact algorithm where the contact interaction is according to tangential scheme in ABAQUS. The boundary conditions are as follows: 1. A distributed tensile stress is applied to the entry as well as the exit edge of the sheet representing Figure 7. The angles of wear for different guide-roller rows. Figure 6. Illustration of the guide rollers angular contact. Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:31am] (PIC) [1–17] [PREPRINTER stage] 6 Proc IMechE Part C: J Mechanical Engineering Science 0(0) mesh the sheet body. It is important to use a sufficiently refined mesh to ensure that the FEM results are independent from the element size. A mesh is said to be converged when further mesh refinement produces a negligible change in the results. Figure 8 shows variations of the maximum effective stress generated in a sheet with 2.8 mm thickness and 900 mm width subjected to 15 MPa tensile stress for different numbers of the element. It can be seen that after around 500,000 elements the maximum effective stress converges to 238 MPa. All the upcoming FE results are obtained from a converged mesh. The steel sheet used in MSC is ST12 with the engineering stress–strain curve shown in Figure 9 for a simple tension test. This curve is fitted to the following equation and is converted to true stress–strain curve to define the material properties in the FE simulations. ¼ 560"0:174 MPa ð1Þ To study the conditions in which the highest amounts of stresses are applied to the strip, a sheet with 900 mm width and 2.8 mm thickness is Figure 8. Illustration of the mesh convergence for the maximum effective stress of a sheet with 2.8 mm thickness and 900 mm width subjected to 15 MPa tension. Figure 9. Engineering stress–strain curve for ST12 steel sheet.15 Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:31am] (PIC) [1–17] [PREPRINTER stage] Mostashfi et al. 7 considered to pass over the TRM. According to the practical production plan, three different tensions per unit cross section area of the sheet with the amounts of 12, 15, and 20 MPa acting by the bridle rolls are investigated since these are the only amounts applied in Mobarakeh Steel Company. Figure 10 illustrates the maximum equivalent stress in the sheet for these three amounts of the forward and backward tensions. Referring to Figure 9, the yield stress of ST12 is 236 MPa, and Figure 10 shows that the maximum effective stress in the sheet reaches 236 MPa when a 14 MPa tensile stress is applied by the bridle rolls. Consequently, permanent deformations will occur in the traveling strip if the bridle rolls tension exceeds around 14 MPa. These permanent deformations appear in the form of indented lines on the sheet surface in the contact areas of the strip with the guide rollers. In other words, to avoid creating these lines on the sheet, the bridle rolls tension must be less than 14 MPa. A similar investigation is done in Figures 11 and 12, where the maximum effective stress in the sheet is shown for two thicknesses of 1.5 and 2.8 mm at a constant width of 900 mm and for the sheet with different widths of 900 and 600 mm at a constant thickness of 2.8 mm, respectively. These two figures show that increase in the width and thickness of sheets generally leads to increase in the maximum generated effective stress in the sheets. Therefore, to prevent yielding of the sheet, the applied tensile stress by the bridle rolls must be reduced. In Table 1, the maximum allowable tensions per unit cross section in order to limit the maximum generated effective stress to the Figure 10. Maximum effective stress of the sheet with 900 mm width and 2.8 mm thickness at different tensions. Figure 11. Maximum effective stress for the sheet with 1.5 and 2.8 mm thicknesses and 900 mm width. Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:32am] (PIC) [1–17] [PREPRINTER stage] 8 Proc IMechE Part C: J Mechanical Engineering Science 0(0) Figure 12. Maximum effective stress for the sheet with 900 and 600 mm widths and 2.8 mm thickness. Table 1. Maximum allowable tensile stresses and carrying capacity applied by the bridle rolls to ST12. 600 mm 900 mm Thickness (mm) Width (mm) Maximum allowable tensile stress (MPa) Carrying capacity (kN) Maximum allowable tensile stress (MPa) Carrying capacity kN) 1.5 2.8 17.2 16 15.48 26.88 15 14 20.25 35.28 Figure 13. Stress distribution on the sheet surface with 900 mm width and 1.5 mm thickness for 15 MPa tension. yield stress of 236 MPa are shown for steel ST12 at different widths (600 and 900 mm) and thicknesses (1.5 and 2.8 mm). Moreover, the corresponding carrying capacities as the allowable tensile loads (multiplication of the stress by the width and the thickness of the sheet) of the bridle rolls are listed. As it is seen, although less tensile stresses are allowable for larger thicknesses and widths, increase in the cross section gives rise to increase in the amount of resultant carrying capacities. Figure 13 shows the effective stress distribution on a sheet with 900 mm width and 1.5 mm thickness at 15 MPa tension. Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:33am] (PIC) [1–17] [PREPRINTER stage] Mostashfi et al. 9 Figure 14. Maximum effective stress for sheets with different widths and thicknesses subjected to the currently applied tensions and the suggested ones by the bridle rolls. Figure 15. Variations of the effective stress through the sheet thickness. Figure 14 compares the allowable tensile stresses of the bridle rolls recommended in Table 1 with those currently applied in practice by the bridle rolls in MSC. By comparing the numbers for both the two thicknesses, it is found that the appearance of indented lines on the strips of MSC after being passed over the TRM is due to the fact that the applied bridle-roll tensions are greater than the amounts due to which the sheet begins to yield. In Figure 15, distribution of the effective stress is shown through the sheet thickness. It can be seen that the stress at the bottom and the top layers of the sheet is higher than that in its middle layer. According to Beheshti7 and Hira et al.,8 in such a situation, the sheet will deform to a bent configuration leading to the appearance of the crossbow defect. Williamson9 recommends sheet leveling in these conditions to prevent the formation of crossbow on the sheets. Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:33am] (PIC) [1–17] [PREPRINTER stage] 10 Proc IMechE Part C: J Mechanical Engineering Science 0(0) by the load cell shown in Figure 18. The specific wear rate k reported in this study is calculated according to the relation Wear behavior of guide rollers in the TRM To study the effects of velocity and applied normal load on specific wear rate of the guide rollers as well as to determine the friction coefficient of the guide rollers with ST12 sheet, pin-on-disc wear tests are performed for two conventional polymeric guide rollers: PA66 and PA11. A polyamide, commonly referred to as Nylon, is a polymer containing monomers of amides joined by peptide bonds. By varying CH2/ CONH ratio, several PAs with varying properties have been synthesized. This ratio is 10 for PA11 and is 5 for PA66.10 In Table 2, some properties of PA66 and PA11 are presented. For pin-on-disc wear testing, according to the standard provided in Rao et al.,12 discs with 60 mm diameter and 5 mm thickness made of the two polymers are prepared. The pin specimen is made of the ST12 steel sheet. In order to provide real contact conditions of the guide rollers with the sheet, the pin is required to be prepared so that the practical contact between the sheet surface and the polymeric disc maintain during the wear tests. Therefore, the pin is cut from a strip, which is passed over the TRM, so that its length is equal to the strip thicknesses and its upper and lower surfaces are those of the strip. To use such a short pin, a fixture is made to put the pin in a point-to-point contact with the disc. As shown in Figure 16, this fixture is made from a 5-mm diameter rod for connection to the wear testing device and a mounting plate to install the pin specimen on the fixture. For the pin specimen, the sheet shown in Figure 17 is used and is mounted on the fixture. Prior to installation, the pin specimen is bulged to provide point-to-point contact with the disc. According to wear test standards, the contact area is set to be 1 mm2. In Figures 18 and 19, the pin-on-disc wear testing device and disc specimens cut from the guide rollers using conventional turning are shown, respectively. To investigate the effect of normal pressure on specific wear rate and coefficient of friction, 9 tests with different forces from 10 to 110 N (according to the capacity of the testing device)are conducted for both PA66 and PA11 disks. The weight loss measurement is done after the tests for a sliding distance of 500 m. The sliding speed is set to be 0.083 m/s in order to be sure that the tests are carried out in a steadystate manner. The friction coefficient is obtained through the calculation of frictional torque measured k¼ wv FN S ð2Þ Figure 16. Fixture made for pin grippage. Figure 17. Pin specimen. Table 2. Properties of PA66 and PA11 guide rollers.16 Property Thermal expansion (K) Young’s modulus (MPa) Shear modulus (MPa) Tensile strength (MPa) Elongation (%) Melting temperature ( C) PA11 PA66 110–120 106 K 70–100 106 K 1100–1400 1700–2000 450–500 1100–1200 47 80–85 280 120–300 190 260 Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:34am] (PIC) [1–17] [PREPRINTER stage] Mostashfi et al. Figure 18. Wear test machine. Figure 19. Disk specimens. 11 where wv, S, and FN are the wear volume (mm3), the sliding distance (m), and the applied normal load (N), respectively. The wear volume wv is determined by measuring the weight loss of the disc by using an analytical balance with the precision of 0.1 mg. Three repeated sliding tests are carried out for minimizing data scattering, and the reported friction coefficient and specific wear rate are the average values obtained from the three repeated tests. Variations of the specific wear rate and friction coefficient with the applied normal load for PA11 and PA66 under dry friction conditions are presented in Figures 20 and 21, respectively. The results reveal that the specific wear rate and friction coefficient of PA11 considerably decrease with increase in the applied load, whereas those of PA66 are almost independent from the applied load. Since different amounts of contact loads act on different guide rollers of a row and on different points of each guide roller, the behaviors shown in Figures 20 and 21 indicate that guide rollers made of PA66 will all show almost flat and equal wear throughout the TRM while this is not the case for guide rollers made of PA11. If PA11 guide rollers have to be employed in a TRM, increase in the contact forces leads to decrease in the specific wear rate of the rollers. However, increasing the contact forces needs the bridle rolls tension to be increased, while the tension is limited to the amount which leads to the yielding of the sheet. In other words, increase in the bridle rolls tension results in decreasing the guide rollers wear rate, on one hand, and increasing the risk of the sheet yielding, on the other hand. Consequently, an optimum amount of the bridle rolls tension should be applied to satisfy both the requirements. Figure 20. Effect of applied load on the specific wear rate of polymer discs under dry sliding conditions (sliding speed: 0.083 m/s). Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:34am] (PIC) [1–17] [PREPRINTER stage] 12 Proc IMechE Part C: J Mechanical Engineering Science 0(0) Figures 20 and 21 also show that the specific wear rate and friction coefficient of PA66 are generally less than those of PA11. These all indicate that the use of PA66 instead of PA11 will efficiently lead to more even wear as well as less wear rate of the guide roller, and these benefits give rise to suppression of the surface defects on the traveling strip over a TRM. To investigate the effect of speed on wear behavior of PA11 and PA66, different wear tests at different typical velocities are carried out with a fixed load of 6.93 kg and the sliding distance of 500 m. Variations of the specific wear rate and friction coefficient with speed are respectively shown in Figures 22 and 23. In general, the specific wear rates for PA11 and PA66 are obtained in order of 109 mm3/Nm. It is believed that Figure 21. Effect of applied load on friction coefficient under dry sliding conditions (sliding speed: 0.083 m/s). Figure 22. Variations of the specific wear rate with velocity for PA66 and PA11 polymers (sliding speed 500 m, applied load 6.93 kg). Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:35am] (PIC) [1–17] [PREPRINTER stage] Mostashfi et al. 13 these results are associated with the softening temperature of the polymers, which leads to surface plastic deformation under lower load values.13 Comparison of Figures 22 and 20 shows that the specific wear rate of PA66 and PA11 are not highly influenced by changes in the speed, and this is in agreement with the findings reported by Liu et al.14 Referring to Figure 23, there will be an average decrease of about 25% in the friction coefficient of PA11 against ST12 when the speed is nearly doubled. This is in agreement with the findings reported by Jia et al.13 and Wang and Li.11 This figure also shows that an average increase of around 20% is seen in the friction coefficient of PA66 against ST12 if the speed is nearly doubled, and this is in agreement with the results obtained by Wang and Li11 and Unal et al.3 However, comparison of Figures 23 and 21 indicates that the effect of changes in the contact force on the variations of friction coefficient is more pronounced than that of changes in the velocity. Consequently, the friction coefficient may be assumed to be almost independent from the sliding velocity. Practical Interpretation of the experimental and numerical predictions The proposed results of the pin-on-disk wear test mainly show that the contact force is a very influencing parameter on the wear rate of the guide rollers. Increase in the contact pressure generally results in decrease in the amount of wear on PA11 and PA66, but it is seen that PA11 is more pressure-sensitive than PA66. Wear of the guide rollers evidently affect their diameter in practice. Accordingly, to more clearly compare the present experimental and numerical results, PA11 guide rollers are investigated after being in service for a continuous period of 6 months in Mobarakeh Steel Company, and their diameters are measured to study their specific wear rate after this working interval. Moreover, the contact forces acting on each guide roller in the TRM of MSC is determined with the use of the finite element simulation. Figure 24(a) and (b) shows the amount of the contact forces on all the guide rollers and diameter of the worn rollers measured after 6 months, respectively. Comparison of these two figures indicates the following findings: 1. According to Figure 24(a), the guide rollers of rows No. 3, No. 4, and then No. 5 are mostly subjected to the highest contact forces, respectively, and Figure 24(b) shows that the guide rollers of these rows have larger diameters than the other ones. In other words, the less wear rates occur on the guide rollers where the highest contact forces act and this in agreement with the findings shown in Figure 20. 2. The obtained contact forces for the sixth row show the highest variations among its guide rollers as the maximum load is around 24858.5 N on the first guide roller and the minimum load is around 13027.7 N on the ninth roller. According to Figure 20, it is expected that the most non-uniform wear patters exists among the guide rollers of this row, and Figure 24(b) approves it as the most varying diameters are obtained for these rollers. In contrary, the least variations of the contact forces are seen among the guide rollers of the fourth row, and hence the least variations in diameter of the worn rollers of this row are seen. Figure 23. Variations of friction coefficient with sliding velocity for PA66 and PA11 polymers (sliding speed 500 m, applied load 6.93 kg). Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:35am] (PIC) [1–17] [PREPRINTER stage] 14 Proc IMechE Part C: J Mechanical Engineering Science 0(0) Figure 24. Illustration of: (a) applied contact load on guide rollers, (b) diameters of the guide rollers after 6 months working of TRM. TRM: twist roll machine. Figure 24(a) and (b) and the above-mentioned results indicate that if PA11 guide rollers are employed in the studied TRM, adding a rollers row after the first one in the current configuration of the machine as well as adding a row before the last one will cause the contact loads distribution to be more uniform. This leads the guide rollers to experience almost the same amounts of the specific wear rate causing diameters of the worn rollers to be all closer to each other. However, inserting new guide-roller rows between the current rows of the studied TRM is a difficult task. Any change in the orientation or the thickness of the guide rollers is no practical too. Consequently, a more practical and easier technique is proposed and investigated in the subsequent section. A practical modification to the TRM Considering the limitations of some solutions proposed in the previous section, another technique for obtaining more even wear on the guide rollers is to use guide rollers with different initial diameters to assist in obtaining more uniformly distributed contact forces. In a guide-rollers row, if the diameter of the rollers with the highest contact forces is less Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:36am] (PIC) [1–17] [PREPRINTER stage] Mostashfi et al. 15 than that of the other ones in the same row, a less contact area is achieved leading to decrease in the contact stresses acting on these guide rollers. For instance, referring to Figure 24(a), variations of the contact force on the guide rollers of the first row shows general increase from the first roller to the last one. Accordingly, if a reverse order is maintained in the initial diameter of these guide rollers, a more uniform distribution is achieved for their contact forces. Considering this rule, after trying various distributions for the diameters in the finite element simulations, the results shown in Figure 25 are obtained. As it is seen, from the first guide roller to the last one in a row, an increasing order for the rows No. 1 to No. 3 and a decreasing order for the rows No. 5 to No. 7 is proposed for the diameters. However, as it was discussed earlier according to Figure 24(a), the contact forces on the guide rollers of the fourth row have the least variations, and hence no change in the diameters of this row is suggested. The effect of this new arrangement of the diameters is seen in Figure 26(a) and (b) where the stress distribution on the traveling sheet is shown for the proposed and the current arrangements, respectively. It is seen that the sheet would be involved with more uniform contact stresses, in comparison to the current situation of TRM, if the proposed arrangement is applied. This gives rise to more uniform contact forces as well. Figure 27 compares the contact forces acting on the guide rollers in the current configuration of the machine with those obtained if the new arrangement is employed. As it is seen, less variations in the contact forces are seen when the proposed arrangement is replaced with the current one. Conclusion In this article, for an industrial twist roll machine, defects on the traveling sheets as well as the amount and distribution of wear on the guide rollers are investigated. Pin-on-disk wear tests are carried out to assess and compare specific wear rate as well as friction coefficient of two polymers PA66 and PA11 against ST12 at different conditions. The results show that the effect of the contact force on the wear rate and friction coefficient is higher than that of the sliding velocity. Moreover, PA66 has a smaller wear rate as well as friction coefficient and its wear behavior is not very sensitive to changes in the sliding velocity and contact force compared to PA11. As these two polymers are widely used in industrial twist roll machines, these results indicate the advantages of PA66 over PA11. Geometry of the machine and the strip is modeled in CATIA to better understand the origin of uneven wear on the guide rollers as well as differences in the wear behavior of different guideroller rows. Finite element simulations of the travelling strip and the guide rollers are done using ABAQUS/Explicit. It is shown that distribution of stress through the sheet thickness causes the formation of crossbow and that the sheet yields if high amounts of tension greater than some allowable numbers are applied by the bridle rolls. Yielding of the sheet will lead to the appearance of indented lines on its surface. Maximum applicable tensions before the sheet begins to yield are determined for different operational conditions of the studied TRM. Adding some roller rows between the existing ones is found to be beneficial in both suppressing the angular wear as well as obtaining more uniform wear rate of the guide rollers in each row. Employing self-aligning bearings Figure 25. The proposed variations of the initial diameters of guide rollers in the studied TRM. TRM: twist roll machine. Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d 16 [30.11.2012–10:36am] (PIC) [1–17] [PREPRINTER stage] Proc IMechE Part C: J Mechanical Engineering Science 0(0) Figure 26. Comparison of the effective stress distribution on the sheet for: (a) the proposed arrangement, (b) the current arrangement. Downloaded from pic.sagepub.com at PENNSYLVANIA STATE UNIV on September 13, 2016 XML Template (2012) K:/PIC/PIC 469149.3d [30.11.2012–10:38am] (PIC) [1–17] [PREPRINTER stage] Mostashfi et al. 17 Figure 27. Comparison between the rollers contact force in the proposed and the current arrangements. instead of deep groove ones as the supports of the guide rollers is also suggested to reduce the uneven wear of the rollers. If PA11 has to be used in a TRM, a practical technique to obtain more even wear on the guide rollers is to use different initial diameters for the rollers of each row. An arrangement according to the distribution of the contact forces on the guide rollers is proposed in this work, and the FE simulations show that this method effectively results in more even wear of the rollers. The present study can be considered as a comprehensive tool in optimization of the performance of a twist roll machine. Funding This research received no specific grant from any funding agency in the public, commercial, or not-for-profit sectors. 6. 7. 8. 9. 10. 11. Acknowledgment The technical personnel of Mobarkeh Steel Company are appreciated for their cooperation in collecting the experimental data and for their instructive discussions. 12. References 1. Hashimoto K, Nakano T, Arita K, et al. Apparatus for changing the traveling direction of a web-like material. Patent No. 4687125, USA, 1987. 2. Roesen O. Web feeding mechanism. Patent No. 1273926, USA, 1918. 3. Unal H, Sen U and Mimaroglu A. Dry sliding wear characteristics of some industrial polymers against steel counterface. J. Tribol Int 2004; 37: 727–732. 4. ChenYK, Kukureka SN, Hooke CJ, et al. Surface topography and wear mechanisms in polyamide 66 and its composites. J Mater Sci 1999; 35: 1269–1281. 5. Kukureka SN, Hooke CJ, Rao M, et al. 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