89 CHAPTER - 5 EN Series Steels Surface finish and surface hardness of the components play vital role in quality of products/components, in general and failure resistance, in particular. One of the finishing process involving surface plastic deformation that introduce compressive residual stresses and thereby improve fatigue resistance is “Burnishing”. Even though the burnishing process is widely employed, its process parameters were not systematically studied till date and not fully established for various important structural materials. The burnishing process parameters include force, speed, feed, and number of tool passes. In the present study, the data obtained from systematically conducted burnishing experiments are correlated with theoretical design using Taguchi method in case of EN series steels (EN 8, EN 24 and EN 31). The surface characterization employed includes optical microscopy, micro hardness and magnitude of residual stress. The study revealed a oneto-one correlation between burnishing depth, increase in average micro hardness and magnitude of compressive residual stresses and a peak in all these three at intermittent extent of burnishing (either after first or second pass) in all the three alloy steels. One of the characterization of materials that was study in the present thesis pertained to alloy steels. Alloy steels are defined as a steels alloyed with variety of elements in total amounts ranging from 90 1% to 50% by weight to improve their mechanical properties. These are classified as low alloy and high alloy steels. The steels with alloy contains lower than 4-5% are considered as low alloy steels while those higher than 8% alloying elements are called high alloy steels. The commonly employed elements in these steels include Mn (most common), Ni, Cr, Mo, V, Si and Boron, less commonly used alloying elements include Al, Co, Cu, Ce, Nb, Ti, W, Sn and Zr. These steels find wide range of applications such as turbine blades in jet engines, space crafts and components for nuclear reactors and also find applications in electrical motors and transformers. Some of the commonly used alloy steels and their equivalent grades are given in Table 5.1. The standard chemical composition of EN series steels are given in table 5.2. Table 5.1: Alloy designations of select Engineering Materials Equivalent Grades Internal Standard BS DIN IS EN SAE/AISI EN18 530A40 37Cr4 40Cr1 EN18 5140 EN24 817M40 34CrNiMo6 40NiCr4Mo3 EN24 4340 EN19C 709M40 - 40Cr4Mo3 EN19C 4140, 4142 EN19 709M40 42Cr4Mo2 40Cr4Mo3 EN19 4140, 4142 EN18D 530A40 37Cr4 40Cr1 EN18D 5140 EN18C 530A40 37Cr4 40Cr1 EN18C 5140 EN353 815M17 - 15NiCr1Mo12 EN353 - EN18A 530A40 37Cr4 40Cr1 EN18A 5140 EN354 820M17 - 15NIVCr1Mo15 EN354 4320 27C15 - 28Mn6 27C15 - 1527 20MnCr5 - 20MnCr5 20MnCr1 - - 150M28 - 20Mn2 EN14A 1524 - 16MnCr5 17Mn1Cr95 - 5120 20Mn2 16MnCr5 91 15Cr3 523A14 15Cr3 15Cr65 EN206 5015 - - - - - EN18B 530A40 37Cr4 40Cr1 EN18B 5140 SCM420 708M20 - - - - SAE8620 805M20 - 20NiCrMo2 EN362 SAE8620 FILESTEEL Table 5.2: Chemical composition of EN series steels C Mn Si S P Cr Ni Mo EN 8 0.35 - 0.45 0.60 -1.0 0.10 0.35 0.05 max 0.05 max - - - EN 8D 0.40 -0.45 0.7 - 0.9 0.05 - .35 0.06 max 0.06 max - - - EN 9 0.50 - 0.60 0.5 - 0.8 0.05 - .35 0.04 max 0.04 max - - - EN 15 0.30 - 0.40 1.3 - 1.7 0.10 - .35 0.04 max 0.04 max - - - EN 16 0.30 - 0.40 1.3 - 1.8 0.10 - .35 0.04 0.04 - - 0.2 - 0.3 EN 18 0.35 - 0.45 0.6 - 0.95 0.10 - .35 0.04 0.04 0.85 - 1.15 - - EN 19 0.35 - 0.45 0.5 - 0.8 0.10 - .35 0.04 0.04 0.90 - 1.4 - 0.2 - 0.4 EN 24 0.35 - 0.45 0.45 - 0.7 0.10 - .35 0.04 0.04 0.90 - 1.4 1.30 - 1.8 0.2 - 0.4 EN 25 0.27 - 0.35 0.5 - 0.7 0.10 - .35 0.04 0.04 0.50 - 0.80 2.3 - 2.8 0.4 - 0.7 EN 31 0.90 - 1.2 0.3 - 0.75 0.10 - .35 0.04 0.04 1.0 - 1.6 - - EN 36B 0.12 - 0.18 0.30 - 0.60 0.10 - .35 0.04 0.04 0.60 - 1.1 3.0 - 3.75 EN 36C 0.12 - 0.18 0.3 - 0.6 0.10 - .35 0.04 0.04 0.60 - 1.1 3.0 - 3.75 0.10 - 0.25 EN 41B 0.35 - 0.45 0.6 max 0.10 - .45 0.04 0.04 1.5 - 1.8 0.40 max 0.10 - 0.25 EN 42 0.70 - 0.85 0.55 - 0.75 0.10 - .40 0.04 0.04 - - - EN 45A 0.55 - 0.65 0.7 - 1.0 1.70 - 2.0 0.04 0.04 - - - EN 47 0.45 - 0.55 0.5 - 0.8 0.50 max 0.04 0.04 0.80 - 1.2 - - EN 48A 0.50 - 0.60 0.6 - 0.9 1.35 - 1.65 0.04 0.04 0.55 - 0.85 - - EN 353 0.20 max 0.5 - 1.0 0.35 max 0.04 0.04 0.75 - 1.25 1.0 - 1.5 0.08 - 0.15 EN 354 0.20 max 0.5 - 1.0 0.35 max 0.04 0.04 0.75 - 1.25 1.5 - 2.0 0.1 -0 .2 5.1. Experimental Details In order to establish the clear picture of burnishing process, a series of experiments were conducted on metals which find wide range of industrial applications, such as EN 8, EN 24 and EN 31 alloy steels. In these experiments, the work pieces were burnished after turning on lathe, keeping the roller burnishing tool fixed in the lathe tool dynamometer. The dynamometer is employed to measure three force 92 components, along x, y and z directions (force in z direction is taken as burnishing force). 5.1.1. Materials The work piece materials are EN 8, EN 24 and EN 31 (alloy steels) and the nominal composition of the experimental materials is given in Table 5.3. All the three alloy steels are in quenched (hardened) and tempered condition. Table 5.3: Chemical composition of the experimental materials Material Composition, in Wt. % C Si Mn Cr Ni S P EN 8 0.41 0.204 0.70 - - 0.02 0.026 EN 24 0.37 0.265 0.64 1.1 0.225 0.023 0.025 EN 31 1.01 0.30 0.78 0.76 - 0.024 0.028 5.2. Results and Discussion 5.2.1. Surface roughness The values of surface finish, a direct measurement of surface roughness before and after burnishing as a function of burnishing speed and burnishing feed are given in Table 5.4 and 5.5, respectively. The optimal forces for EN 8, EN 24 and EN 31 are 210N, 170N and 200N respectively. The feed for all materials is taken as 0.032 mm/rev From these data (data in Tables 5.4 and 5.5 and Figs. 5.1 and 5.2) optimal speed and feed values which result in highest increase in surface finish are determined and the same are given in Table 5.6. The 93 variation in the extent of improvement in the surface finish for EN series steels obtained in the present investigation (for that matter, for any other material) depends upon microstructural features and the levels of hardness and/or strength (in the present case microhardness values). Table 5.4: Comparison of surface finish values before and after burnishing for a 30 mm diameter work piece of alloy steels as a function of burnishing speed. Burnishing Material speed (m/min) EN 8 EN 24 EN 31 Surface finish before burnishing Ra (µm) Surface finish after % increase in burnishing Ra (µm) surface finish First Second Third First Second Third pass pass pass pass pass pass 51 1.32 0.10 0.11 0.17 92.42 91.66 87.121 34 1.62 0.43 0.38 0.23 91.98 76.54 85.80 22 1.39 0.33 0.34 0.19 76.26 75.54 86.34 14 1.31 1.04 0.92 0.35 20.61 29.77 73.28 9 1.32 0.24 0.19 0.22 81.81 85.60 83.33 51 2.00 0.25 0.27 0.56 87.50 86.50 72.00 34 3.88 0.36 0.15 0.26 90.72 96.13 93.30 22 3.92 0.18 0.17 0.27 95.41 95.66 93.11 14 3.48 0.48 0.62 0.90 86.20 82.18 74.14 9 3.71 0.53 0.51 0.92 85.72 86.25 75.20 51 0.99 0.62 0.38 0.92 37.37 61.61 07.07 34 0.81 0.11 0.13 0.18 86.45 84.00 77.77 22 0.98 0.28 0.20 0.12 71.43 79.60 87.75 14 1.18 0.23 0.19 0.21 80.51 83.90 82.20 9 0.77 0.20 0.22 0.70 74.02 71.43 09.09 94 Table 5.5 Comparison of surface finish values before and after burnishing for a 30 mm diameter work piece of alloy steels as a function of burnishing feed. Burnishing Material feed mm/rev Surface Surface finish after % increase in finish before burnishing Ra (µm) surface finish burnishing Ra (µm) 22 34 51 22 34 51 m/min m/min m/min m/min m/min m/min 0.111 1.32 0.75 1.11 0.67 43.18 15.90 49.24 0.095 1.62 0.33 1.08 0.92 79.63 33.33 43.21 0.063 1.31 0.57 0.77 1.09 56.48 41.22 16.80 0.032 1.32 0.19 0.43 0.10 85.60 67.42 92.42 0.111 2.00 0.25 0.37 1.70 87.5 81.50 15.00 0.095 3.88 0.54 0.22 0.97 86.08 94.32 75.00 0.063 3.92 0.42 0.32 2.18 89.28 90.45 44.39 0.032 1.8 0.18 0.36 0.25 90.00 80.00 86.11 0.111 0.99 0.33 0.19 0.75 66.66 80.80 24.24 0.095 0.81 0.34 0.13 0.44 58.02 83.95 45.68 0.063 0.98 0.72 0.20 0.51 26.53 79.59 47.95 0.032 1.18 0.28 0.11 0.62 76.27 90.67 47.45 EN 8 EN 24 EN 31 95 % increase in surface finish 100 90 80 st 1 pass nd 2 pass rd 3 pass 70 60 50 40 30 20 10 (a) EN 8 10 20 30 40 50 Speed, m/min % increase in surface finish 100 st 1 pass nd 2 pass rd 3 pass 90 80 70 (b) EN 24 60 10 20 30 40 50 Speed, m/min % increase in surface finish 100 st 1 pass nd 2 pass rd 3 pass 90 80 70 60 50 40 30 20 10 0 (c) EN 31 10 20 30 40 50 Speed, m/min Fig. 5.1: Variation of burnishing speed with % increase in surface finish for different passes in (a) EN 8 (b) EN 24 and (c) EN 31 alloy steels. 96 % increase in surface finish 100 22 m/min 34 m/min 51 m/min 90 80 70 60 50 40 30 20 10 0.02 (a) EN 8 0.04 0.06 0.08 0.10 0.12 Feed, mm/rev % increase in surface finish 100 90 80 22 m/min 34 m/min 51 m/min 70 60 50 (b) EN 24 40 0.02 0.04 0.06 0.08 0.10 0.12 Feed, mm/rev 100 % increase in surface finish 90 80 70 60 50 40 30 20 10 0 0.02 (c) EN 31 0.04 0.06 0.08 22 m/min 34 m/min 51 m/min 0.10 0.12 Feed, mm/rev Fig. 5.2: Variation of burnishing feed with % increase in surface finish at different speeds in (a) EN 8 (b) EN 24 and (c) EN 31 alloy steels. 97 Table 5.6 Optimal values of burnishing parameters for the alloy steels, EN 8, EN 24 and EN 31. Material Speed No of Force Feed Ra (m/min) passes (N) (mm/rev) (µm) EN 8 51 1 210 0.032 0.10 EN 24 34 2 170 0.095 0.15 EN 31 34 1 200 0.032 0.11 5.2.2. Microstructure Figure 5.3 to 5.5 shows the typical set of optical micrographs obtained from EN 8, En 24 and EN 31 alloy steels in the unburnished (Fig. 5.3a) and burnished (Fig. 5.3b for first pass, Fig. 5.3c for second pass, Fig. 5.3d for third pass) conditions. The optical micrographs (corresponding to surfaces from periphery to inner cross section of the cylindrical specimens) show similar structure with varied burnished depths for different burnishing conditions in all the three alloy sheets. These figures clearly show a distinct variation in the thickness of burnishing affected zone with each of the burnished pass. The variation in depth of these zones is measured from micrographs and the same are given in Fig. 5.6 and Table 5.7. These data clearly reveal that highest burnishing depth occurs at 1 st pass in EN 8 and EN 31 while the same occurs at 2nd pass in EN 24 alloy steel. It should be noted here that the highest depth of burnishing presumably provides maximum effectiveness in surface modification. The actual values of burnishing layer thickness are obtained experimentally. The variation of burnishing layer thickness which is different for different EN series 98 steels is a function of many microstructural and surface condition dependent properties. The principal reasons for such variation observed in the present study was not investigated in the present thesis as this requires detailed microstructural analysis involving transmission electron microscopy. (a) (b) (c) (d) Fig. 5.3: Optical micrographs of EN 8 showing the depth of burnishing in (a) Unburnished (b) Burnished – 1st pass (c) Burnished – 2nd pass (d) Burnished – 3rd pass conditions 99 (a) (b) (c) (d) Fig. 5.4: Optical micrographs of EN 24 showing the depth of burnishing in (a) Unburnished (b) Burnished – 1st pass (c) Burnished – 2nd pass (d) Burnished – 3rd pass conditions 100 (a) (b) (c) (d) Fig. 5.5: Optical micrographs of EN 31 showing the depth of burnishing in (a) Unburnished (b) Burnished – 1st pass (c) Burnished – 2nd pass (d) burnished – 3rd pass conditions 101 Burnishing layer thickness, m 800 EN 8 EN 24 EN 31 700 600 500 400 300 200 B B1 B2 B3 No of Passes Fig. 5.6: Correlation of burnishing layer thickness with burnishing parameters Table 5.7: Variation of burnishing burnishing zone for three alloy steels. layer thickness in the Burnishing Process BB B1 B2 B3 Material Characteristic EN 8 Burnishing layer thickness 260.0 475.0 425.0 350.0 EN 24 Burnishing layer thickness 250.0 350.0 450.0 430.0 EN 31 Burnishing layer thickness 400.0 650.0 700.0 675.0 [BB – Before burnishing, B1 – B3 – Burnished-3rd pass] Burnished-1st pass, B2 – Burnished-2nd pass and 5.2.3. Micro hardness The specimens polished to obtain microstructure were further used to determine the variation in micro hardness as a function of distance from the surface. The micro hardness values are found to be almost similar with no systematic variation with the burnishing distance. Hence, an average value of micro hardness is taken as a representative value for each of the experimental condition such as 102 unburnished, burnished-1st pass, burnished-2nd pass and burnished3rd pass. These data are summarized and given in Table 5.8 and are shown in Fig. 5.7. It is interesting to note that maximum burnished depth (as obtained from optical micrographs) also results in highest values of average micro hardness. The micro hardness variation depends on nature and magnitude of residua stresses that arise due to different extents of burnishing. It should be noted here that in all the three EN series steels highest micro hardness were obtained either at B1 or B2 (depending upon the extent of burnishing in each stage) and comparatively lower micro hardness values in B and B3, the first (B) for the lack of any surface modification and the later for the effects of flaking like microstructural degradation. Table 5.8: Variation of average micro hardness values in the burnishing zone for three alloy steels. Burnishing Process Material Characteristic BB B1 B2 B3 EN 8 Micro Hardness 251.2 303.5 279.4 294.3 EN 24 Micro Hardness 297.2 312.7 339.6 335.1 EN 31 Micro Hardness 196.1 251.6 254.1 223.9 [BB – Before burnishing, B1 – Burnished-1st pass, B2 – Burnished-2nd pass and B3 – Burnished-3rd pass] 103 400 350 B1 Micro hardness 300 250 B2 B3 B B1 B2 B3 B1 B2 B B3 B 200 150 100 50 0 EN 8 EN 24 EN 31 Fig. 5.7: Correlation of surface micro-hardness with burnishing parameters 5.2.4. Residual stress The residual stresses that are determined by XRD for EN series steels are given in Table 5.9 and the data are shown in Fig. 5.8 as a function of number of passes for the three alloy steels. The data in Fig. 5.8 show that the residual stresses gradually build up with burnishing and exhibit a peak in residual stresses at 1 st or 2nd burnishing pass. Unlike in EN 8 steel the other two alloy steels namely EN 24 and EN 31 show significant decrease in the magnitude of compressive residual stresses. The magnitude of compressive residual stress is also found to be strongly dependent on nature of alloy steel. The harder is the alloy steel; the highest is the magnitude of compressive residual stresses. 104 Table 5.9: Compressive residual stresses for EN series steels Material EN 8 EN 24 EN 31 Principal Principal Direction Max Burnishing Stress Stress of shear condition (max) (min) Principal stress (MPa) (MPa) Stress * (MPa) BB -171 -331 14.4 80 286.9 B1 -223 -368 6.6 72.4 323 B2 -203 -369 4.6 83 323.4 B3 -205 -358 2.9 76.6 314.5 BB -208 -285 5.7 38.5 258.6 B1 -272 -667 11.4 197.4 582.7 B2 -293 -598 2.2 152.5 519.7 B3 -249 -628 10.8 189.4 549.4 BB -160 -317 8.1 78.8 311.7 B1 -208 -285 5.7 38.5 258.6 B2 -175 -275 6.3 49.8 241.8 B3 -171 -331 14.4 80 286.8 Equivalent stress (MPa) [BB – Before burnishing, B1 – Burnished-1st pass, B2 – Burnished-2nd pass and B3 – Burnished-3rd pass]; * Angle in degrees from the axial direction of the cylindrical sample Burnishing depth too revealed a systematic correlation with the average hardness of the alloy steel. According to the expected lines, softest alloy steel of the three exhibited the highest burnishing depth. Parameters chosen for XRD analysis are wave length: 2.291 A° and Bragg angle: 156°. 105 Compressive residual stress, MPa 300 EN 8 EN 24 EN 31 250 200 150 B B1 B2 B3 No of passes Fig. 5.8: Variation of magnitude of residual compressive stresses with burnishing pass in case of the three alloy steels. 5.3. Technological Implication Surface compressive residual stresses have been found to be beneficial for tensile mean stress controlled fatigue as well as creep. The same would be grossly detrimental to the conditions where compressive mean stress is in vogue. However, in most engineering applications the rotary parts grossly experience tensile loading conditions and compressive residual stresses are desirable and they effectively enhance fatigue resistance. Hence, burnishing is highly beneficial for most rotating structural components in improving their service life. Further studies are required to evaluate the effectiveness 106 of compressive residual stresses that result an industrial burnishing process by extending the present studies to at least high cycle fatigue loading. Such studies also need to address the progressive relaxation in the net compressive residual stresses with the extent of high cycle fatigue damage as occurs with number of such fatigue cycles. Such studies have not been attempted till date and should be of significant technological value in case of present low cost EN series alloy steels. 5.4. Conclusions 1. Burnishing results in significant surface finish depth of burnishing and increase in micro hardness and residual stresses. 2. The present systematic study reveals that the burnishing depth, increase in micro hardness or increase in magnitude of compressive residual stresses, is higher in case of softer alloy steels EN 8 and EN 24 as compared to the relatively harder EN 31 alloy steel. 3. In all the three alloy steels, higher extent of burnishing resulted in different extents of micro structural modification (as reflected by the magnitude of compressive residual stresses) and in general, showed a maximum at intermediate burnishing pass – First in case of EN 8, EN 31 and second in case of EN 24 steel. 4. The present study revealed one-to-one correlation between burnishing depth, increase in micro hardness and magnitude of compressive residual stresses.
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