MATHEMATICAL MODELLING OF SURFACE ROUGHNESS ON MACHINING OF AA6061-BORONCARBIDE COMPOSITE IN EDM THROUGH RSM. K.R. Thangadurai 1 * and A.

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International Journal of Mechanical and Materials Engineering (IJMME), Vol. 7 (2012), No. 3, 197-202. MATHEMATICAL MODELLING OF SURFACE ROUGHNESS ON MACHINING OF AA6061-BORONCARBIDE COMPOSITE IN EDM THROUGH RSM K.R. Thangadurai 1 * and A. Asha 2 1 Department of Mechanical Engineering, Jayaram College of Engineering and Technology, Tiruchirapalli 621 014, India. 2 Department of Mechanical Engineering, Kamaraj College of Engineering and Technology, Virudhunagar 626 001, India. *Corresponding author s E-mail: kthangam2010@gmail.com Received 21 January 2012, Accepted 20 December 2012 ABSTRACT The aim of present study is to investigate the machinability evaluation of AA6061- wt.5% B 4 Cp metal matrix composite in EDM. For machining of composite, three machining parameters were considered such as current, pulse on and pulse off. After experimentation, a mathematical model for surface roughness was developed to correlate the influences of these machining parameters and surface roughness (Ra). The experiments were planned as per DOE method. From the obtained results, it was evidenced that the surface roughness is influenced more by current and pulse on. The best surface finish was obtained at minimum of pulse off value. The optimum machining parameters in favour of good surface roughness were estimated and verified with proposed optimized results. Keywords: AA6061 wt.5%b 4 Cp, Surface roughness, Design of experiment, Response surface methodology. NOMENCLATURE EDM electrical discharge machining MRR material removal rate (gram/min) TWR tool wear rate (gram/min) Ra surface roughness (µm) MMC metal matrix composite DOE design of experiment RSM response surface methodology SEM scanning electron microscope ANOVA analysis of variance 1. INTRODUCTION Metal matrix composite is combination of two constituents in which one being a metal and other l may be as reinforcement or ceramic. These composites are used in automobiles and aircraft for their appreciable properties (Garg et al., 2010). Electrical discharge machining is a proven non-traditional machining process for machining of intricate, composite and hard material parts (Ho and Newman, 2003). Kalaiselvan et al. (2011) were reported the fabrication procedure of AA6061 and boron carbide powder particulate through stir casting route and analyzed the micro structure and mechanical properties. The hybrid composite were developed through stir casting technique and it was machined in electric discharge machining to analyze its machinability (Ahamed et al., 2009). Al-Si matrix composites were developed through stir casting technique reinforced with aluminium nitride particles and found out that AIN particles contributed to the increase of hardness of the matrix (Wahab et al., 2009). Singh et al. (2004) have studied the effect of machining parameters during machining of as-cast Al-MMC with 10% SiCp reinforcement in EDM. Karthikeyan et al. (1999) have identified the influencing effects volume percentage of SiCp, current and pulse on on MRR, TWR, taper and Ra.The author was developed mathematical models were developed for MRR, EWR and Ra in the machining of Al/SiC composite through response surface methodology (Habib, 2009). Dhar et al. (2007) were evaluated the effect of machining parameters on MRR, TWR, Radial overcut on electric discharge machining of Al-4Cu-6Si alloy-10wt.% SiCp composites. The effect of machining parameters on MRR, TWR and Ra were studied while machining tungsten carbide by Luis et al. (2005). The optimized model for material removal rate was developed during machining of Ti6Al4Vin EDM through DOE and RSM technique by Rahman et al. (2010). Ali et al. (2011) were reported the influence of SiC powder concentration in dielectric fluid and electrical energy in micro electric discharge machining of titanium alloy and three EDM output responses such as MRR, EWR and Ra were also investigated by using Design Expert software methodology. Iqbal et al. (2010) have developed mathematical models for MRR, EWR and Ra were developed during machining of stainless steel AISI 304 in EDM milling through response surface. The aim of present paper is to develop a mathematical model for surface roughness in machining of AA6061- wt.5% B 4 C p MMC prepared through stir casting technique. For experimentation, three machining parameters viz current, pulse on and pulse off were considered for machining of composite in electric discharge machining. The optimized machining parameters were obtained through RSM technique. The adequacy of the developed model has been checked through analysis of variance (ANOVA). Finally, the optimum machining parameters were found out for getting better surface roughness. 197

2. MATERIAL AND METHODOLOGY AA6061 wt.5%b 4 Cp MMC was machined using ELECTRA PLUS EDM machine. Figure 1 shows the microstructure of specimen before machining and dispersion of boron carbide particle in the aluminium matrix. Parameters Table 1 Experimental setting. Description Work piece material AA6061 wt.5%b 4 Cp Work piece size 18mm x 18mm x 84 mm Electrode material 14mm Dia x 150 mm height Dielectric fluid Kerosene Electrode polarity Negative Applied voltage 200 Volts. Flushing type Jet flushing Flushing pressure 2.2 kg/cm 2 Machining 20 minutes Surface roughness (Ra) is measured after machining the work piece by using the Surftest (SJ-210 MITUTOYO make) with a cut-off length 0.8mm over the three sampling lengths and the speed of indenter was 0.5 mm/s. The inventor type was diamond. Ra is surface roughness in µm. 2.1. Theory of the experimental design In the present experimental study, three independent machining parameters viz current, pulse on and pulse off were considered for experimentation. The experiments were conducted as per Box-Behnken design (BBD). Table 2 The levels and codification of machining parameters. Machining parameter Coding Level -1 Level 0 Level 1 Current A A 10 12.50 15 on- μs B 500 1250 2000 off - μs C 50 125 200 2.2. Response surface modelling Response Surface Methodology is a technique for formulating mathematical models and analysing the influencing parameters on output performance. In the present work RSM is utilized for developing mathematical model for surface roughness in EDM process. To study the effects of the EDM parameters, a higher order polynomial quadratic equation was developed. Table 3 Plan for Box Behnken Design matrix : Different machining parameters and results. Exp No Current (A) Amps on µs (B) off µs (C) Ra µm 1 1 0 1 7.436 2 1-1 0 7.231 3 0-1 1 6.132 4-1 1 0 5.891 5 0-1 -1 6.112 6 0 0 0 6.543 7-1 -1 0 5.243 8 0 0 0 6.252 9 0 0 0 6.253 10 1 0-1 7.775 11 0 1 1 6.688 12 0 0 0 6.251 13 1 1 0 7.747 14 0 0 0 6.252 15-1 0 1 5.546 16-1 0-1 5.559 17 0 1-1 6.789 In the general form of response surface is described by the below mentioned equation. ( 1) Figure 1 Microstructure of AA6061 wt.5% B 4 Cp composite before machining. The machining parameters were varied into three levels, coded as -1,0 and +1.The experimental design consists of 17 runs as given in Table 1. The levels and codification of machining parameters are given in the Table 2. And the Table 3 shows the details of Box Behnken Design matrix and its results. Where, Y is surface roughness (Ra) and Xi (A, B, C) are the coded machining parameters. The term β 0,β ii and β ij are the second order coefficients. The response surface methodology was used to indicate the relationship between the three response variables and machining parameters as given below form. Y = F (A, B, C) (2) 198

Where Y is the function of three machining parameters viz current (A), pulse on (B) and pulse off (C). The equation (3) can be rewritten as follows. Y = βo + β 1 A 1 + β 2 B 2 + β 3 C 3 + β 12 A 1 B 2 + β 13 A 1 C 3 + β 23 B 2 C 3 + β 11 A 1 2 + β 22 B 2 2 + β 33 C 3 2 (3) Where: A 1, B 2 and C 3 are the machining parameters current, pulse on and pulse off respectively. β O is a constant value. β 1, β 2 and β 3 are co efficient value of the linear effect. β 12, β 13, β 23 are the co efficient value of interaction effect. β 11, β 22, β 33 are the second order coefficient value. The Design Expert 7.0 software was utilized for experimentation, modelling and optimization. 2.3 The mathematical model for Ra As mentioned in equation 4, a mathematical model has been developed to correlate machining parameters and surface roughness. The final equation of actual factors Ra=4.80944-0.25927*A + 5.33278E-004*B+1.58278E- 003*C-1.76000E-005*A*B - 4.34667E-004*A*C- 5.37778E - 007*B*C + 0.029324*A 2 + 6.13778E - 008*B 2 +1.52044E - 005* C 2 (4) 3. RESULTS AND DISCUSSION 3.1 ANOVA results for surface roughness From the ANOVA table, as the model F value is 80.09, the model is significant. There is only 0.01 % chance that a model F-value this large could occur due to noise.values of Prob > F less than 0.0500 indicate model terms are significant. From the ANOVA table 4, it is understood that Current A, on B, A 2 are significantly affect the model. And probability values greater than 0.1000 indicate the model terms are not significant. It is aslo observed that the Lack of Fit F value of 0.36 implies the Lack of Fit is not significant relative to the pure error.there is a 78.54% chance that a Lack of Fit F value this large could occur due to noise. Non-significant lack of fit is good Table 5 shows the value of R 2 and adjusted R 2 are 99% and 99% respectively. This means that regression model of surface roughness provides perfect explanation of the relationship between the response for surface roughness and the independent variables of machining parameters. In the Table 4 shows the lack of fit term is nonsignificant, as it is desired. The Predicted R-Squared of 0.9554 is in reasonable agreement with the Adjusted R-Square of 0.9780. Adequate Precision measures the signal to noise ratio. A ratio greater than 4 is desirable. As the adequate signal ratio is 30.410 the model can be used to navigate the design space. Figure 2 The normal probability plot of Ra. Table 4 The ANOVA results of surface roughness. Source Sum of squares DF Mean square Table 5 R-squared values for surface roughness. Std. Dev. 0.110907007 R-Squared 0.990382474 Mean 6.452941176 Adjusted R-Squared C.V. % 1.718704763 Predicted R-Squared PRESS 0.399546375 Adequate Precision F value P value Prob>F Model 8.8665 9 0.9852 80.09 < 0.0001 A-Current 7.9003 1 7.9003 642.28 < 0.0001 B- on C- off 0.7182 1 0.7182 58.39 0.0001 0.0234 1 0.0234 1.91 0.21 A X B 0.0044 1 0.0044 0.35 0.5705 A X C 0.0266 1 0.0266 2.16 0.1851 B X C 0.0037 1 0.0037 0.30 0.6023 A^2 0.1414 1 0.1414 11.50 0.0116 B^2 0.0050 1 0.0050 0.41 0.5433 C^2 0.0308 1 0.0308 2.50 0.1576 Residual 0.0861 7 0.0123 Lack of Fit 0.0184 3 0.0061 0.36 0.7854 Pure Error 0.0678 4 0.0169 Cor Total 8.9527 16 0.978017082 0.955371265 30.41024588 199

Figure 2 shows the normal probability plot residulas for surface roughness. From the figure it is noticed that the residuals are falling on a straightline which means the errors are normally distributed. Further Figure 3 shows the comparision between observed value and the predicted value calcutalated from model. 3.2 Effect of current, pulse on and pulse off on Ra Figure 4 and Figure 5 shows 3D surface model and contour effect of current and pulse on on surface roughnessrespectively. From the model, the surface roughness value gradually increases with increase of current and pulse on inwhich current influence more on roughness than pulse off. The best surface roughness value is obtained at minimum current and pulse on vaule. Figure 5 Contour effect of current and pulse on for Ra. Figure 6 The 3D surface model of surface roughness with respect to current and pulse off. Figure 3 Predicted vs. Actual for Ra. Figure 4 The 3D surface model of surface roughess with respsect to current and pulse on. Figure 7 Contour effect of current and pulse off for surface roughness. 200

it was observed high in some place high crater size due to increase of high current and pulse on.it is concluded that pulse on and current has strong effect on the surface roughness value. Figure 8 The 3D surface model of surface roughness with respect to pulse on and pulse off. Figure 6 and Figure 7 shows 3D surface model and contour effect of current and pulse off surface roughness. It is observed from the model,the surface roughness value gradually increases with increase of current and there is no significant effect on surface roughness value. The best surface roughness is obtained in minimum current and minimum pulse off. Figure 8 and Figure 9 shows 3D surface model and contour effect of pulse on and pulse off on surface roughness value. Figure 10 Photograph of machined composite. Figure 11 SEM image of machined photograph. 4. OPTIMIZATION OF MANUFACTURING CONDITIONS The optimal manufacturing conditions for machining of AA 6061-wt. %5B 4 Cp MMC with the constraints of machining parametric range is to identify the optimum values of machining parameter (y) in order to surface roughness (Ra). The optimization problem can be computed by using design of expert software 7.0.0. The aim of multi response optimization is to minimize surface roughness while machining. The constraints used during the optimization are summarized in Table 6. Figure 9 Contour effect of pulse on and pulse off for surface roughness. The surface roughness value gradually increases with increase of current. There is no significant effect on surface roughness with the parameter of pulse off and pulse off influence is smaller than pulse on. The best surface roughness is obtained in minimum pulse on and pulse off. Figure 10 shows the photograph of machined composite after electric discharge machining. Figure11 depicts the SEM image of machined composite. In the SEM image, Table 6 The Constraints for optimization of machining conditions. Name Goal Lower limit Upper limit Current in range 10 15 on in range 500 2000 off in range 50 200 The optimized solutions were obtained based on the desirability level by using design expert software. 201

Current A Table 7 Optimization results. on µs off µs Ra µm 10 500 200 5.3444 Desirability 0.606 5. CONFIRMATUIN OF EXPERIMENTS To check the accuracy of mathematical model given in equation (4), two trial experiments were conducted. The details of confirmation experiments are shown in Table 8. From the table 8, it is observed that the error is less than 5%. Current A Table 8 the details of confirmation experiments. on µs off µs Ra µm predicted Exp. % error 10 500 200 5.3444 5.2445 1.9 10 500 200 5.3444 5.5365 3.46 6. CONCLUSION The following conclusions were made for the mathematical modelling of surface roughness on machining of AA6061 wt.5%b 4 Cp MMC. 1. The obtained results evidence that the surface roughness has influenced by current and pulse on. But whereas it has not been significantly affected by pulse off. 2. In the overall observation the optimized minimum surface roughness values are current10 A, pulse on 500 µs and pulse off 200 µs. 3. The error between the predicted values and experimental values are within 5%. 4. In mathematical model, the surface roughness of experimental values exactly fit with predicted values of these response factors with 99% confident interval. 5. The developed mathematical model can be used by the manufacturers while selecting the machining parameters. ACKNOLOWLEDEMENT The authors wish to thank Dr. K. RAGHUKANDAN Professor and Head Department of Manufacturing Engineering, Annamalai university, Tamilnadu, India for providing valuable guidance and Electric Discharge Machine, and tools to carry out experiments in a successful way and also express sincere thanks to staff members of metallurgy lab for taking measurements of machined components. REFERENCES Ahamed, A.R., Ashokan, P. and Aravindan, S. 2009. EDM of hybrid Al-SiCp-B4C and Al-SiCp-Glass MMCs, International Journal of Advanced Manufacturing Technology 44: 520-528. Ali, M.Y., Atiqah, N. and Erniyati. 2011. Silicon carbide powder mixed micro electro discharge milling of titanium alloy, International Journal of Mechanical and Materials Engineering 6 (3): 338-342. Cochran, G. and Cox, G.M. 1997. Experimental Design, Asia Publishing House, New Delhi. Design Expert Software, Version7, 2005. Users guide, Technical manual, State-Ease Inc., Minneapolis, MN. Dhar, S., Purohit, R., Saini, N., Sharma, A. and Kumar, G.H. 2007. Mathematical modelling of electric discharge machining of cast Al-4Cu-6Si alloy-10 wt.% SiCp composites, Journal of Materials Processing Technology 194: 24-29. Garg, R.K., Singh, K.K., Sachdeva, A., Sharma, V.S., Ojha, K. and Singh, S. 2010. Review of research work in sinking EDM and WEDM on metal matrix composite materials, International Journal of Advanced Manufacturing Technology 50: 611-624. Habib, S.S. 2009. Study of the parameters in electrical discharge machining through response surface methodology approach, Applied Mathematical Modelling 33: 4397-4407. Ho, K.H. and Newman, S.T. 2003. State of the art electrical discharge machining, International Journal of Machine Tools & Manufacture 43:1287-1300. Iqbal, A.K.M.A. and Khan A.A. 2010. Modelling and analysis of MRR, EWR and Surface roughness in EDM milling through response surface methodology, American Journal of Engineering and Applied Sciences 3 (4): 611-619. Kalaiselvan, K., Murugan, N. and Parameswaran, S. 2011. Production and characterization of AA6061- B 4 Cp stir cat composite, Materials and Design 32: 4004-4009. Karthikeyan, R., Narayanan, P.R.L. and Naagarazan, R.S. 1999. Mathematical modelling for electric discharge machining of aluminium silicon carbide particulate composites, Journal of Materials Processing Technology 87: 59-63. Luis, C.J., Puertas, I. and Villa, G. 2005. Material removal rate and electrode wear study on the EDM of silicon carbide. Journal of Materials Processing Technology 164-165: 889-896. Montgomery, D.C. 1997. Design and Analysis of Experiments Fourth ed. Wiley, New York. Montgomery, D.C., Peck, E.A. and Vining G.G. 2003. Introduction to linear Regression Analysis, Third ED, Wiley, New York. Rahman, M.M., Khan, M.A.R., Kadirgama, K., Noor, M. and Baskar, R.A. 2010. Modeling of Material Removal on Machining of Ti-6Al-4V through EDM using Copper Tungsten Electrode and Positive Polarity, International Journal of Mechanical and Materials Engineering 1 (3):135-140. Singh, P.N., Raghukandan, K., Rathinasabapathi, M. and Pa, B.C. 2004. Electric discharge machining of Al- 10% SiCp as cast metal matrix composites, Journal of Materials Processing Technology 155:1653-1657. Wahab, M.N., Daud, A.R. and Ghazali, M.J. 2009. Preparation and characterization of stir castaluminium nitride reinforced aluminum metal matrix composites, International Journal of Mechanical and Materials Engineering 4 (2): 115-117. 202