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International Journal on Mechanical Engineering and Robotics (IJMER)

________________________________________________________________________________________________

Optimization Machining Conditions on Composite Materials Using Fuzzy Logic

1C. Dhavamani, 2A.B.K.Rajan, 3P. Sivakumar

1,3Dept. of Aeronautical Engineering, Mahendra Engineering College, Tiruchengode, Namakkal Dist, Tamilnadu, India.

2Department of Mechanical Engineering, Jawahar Engineering College, Chennai,Tamilnadu, India.

Abstract— Automotive, aircraft and train companies need to replace steel and cast iron in mechanical components with lighter high strength alloys like Al metal matrix composites (MMC).Experiments were carried out on Radial Drilling Machine. A plan of experiments, based on the techniques of Taguchi was performed. In this study drilling of Aluminium Silicon Carbide (Al/SiC) was investigated. The objective of this research is to study the effect of cutting speed, feed, and volume fraction, diameter of cut machining time on metal removal rate, specific energy, surface roughness, and flank wear. The experiments were conducted using L27 orthogonal array.

This paper deals with the use of Taguchi Technique with fuzzy logic to optimize drilling process in Al/SiC composites with multiple quality characteristics. The influence of each parameter on the responses is established using analysis of variances (ANOVA) at 5% level of significance. It is found that % of Vol SiC, Cutting Speed, Feed Rate, diameter of drill and machining time contribute significantly to the multiple performance characteristic index. The five responses at optimal parameter setting have been reported.

Keywords: Composite materials; drilling processes; Fuzzy Logic; ANOVA

I. INTRODUCTION

Metal Matrix Composites have found considerable applications in automotive, aircraft and manufacture of sea vehicles industries due to their improved strength, high specific strength/stiffness, microbiological attacks and increased wear resistance over unreinforced alloys.

As a consequence of the widening range of applications of MMC, the machining of these materials has become a very important subject for research. The particles used in the MMCs are harder than most of the cutting tool materials.

Fuzzy logic has great capability to capture human commonsense reasoning, decision-making and other aspects of human cognition. The classes of certain objects in the real world do not have precisely defined criteria of membership. Fuzzy set was introduced by Zadeh (1965) to deal such problems and is defined as a class of objects with a continuum of grades of

membership. Klir & Yuan (1998) sated that fuzzy logic involves a fuzzy interference engine and a fuzzification- defuzzification module. El-Sonbaty et al (2004) investigated the influence of cutting speed, feed, drill size and fiber volume fraction on the thrust force, torque and surface roughness in the drilling processes of fiber reinforced epoxy composite materials. However, in various machining operations like EDM (Lin & Lin 2005), milling and turning operations grey relational relation is used. This fuzzification of data is then defuzzified by the aggregation of these rules and converting the fuzzy quantity to a precise quantity.

Basheer et al (2008) presented an experimental work on the analysis of machined surface quality on Al/SiC composites leading to an artificial neural network-based (ANN) model to predict the surface roughness. The predicted roughness of machined surfaces based on the ANN model was found to be in very good agreement with the unexposed experimental data set. Palanikumar (2010) and Palanikumar et al (2012) used the grey relational analysis to predict the efficient drilling process parameter for surface roughness and delamination. Latha

& Senthilkumar (2009a, 2009b, 2010) analyzed the thrust force and surface roughness in drilling operation.

Fuzzy rule-based model has been developed to predict the thrust force. Response surface model has been developed and comparison between fuzzy based model and response surface model has been carried out.

However, very few researchers have used the Grey- Fuzzy technique for analyzing the influenced process parameter on drilling.

II. EXPERIMENTAL WORKS

In this work, LM25 –based Aluminium alloy (7 Si 0.33Mg 0.3Mn 0.5Fe 0.1Cu 0.1Ni 0.2Ti) reinforced with green bonded Silicon particles of size 25 micrometer with different volume fractions (10%, 15%, 20% in weight percentage) manufactured through stir casting route is used for experimentation.

The experiment was repeated for the various cutting conditions like % volume of SiC, feed, speed, depth of

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cut and time of machining. The variables used in this study are given in the Table 1.

Table 1 Selected Input variables and output Sl

No

Input

Variables Variations Output 1 % Vol of

SiC

10, 15, 20 (%)

1.Metal Removal Rate 2.Surface Roughness 3.Flank Wear 4. Specific Energy 2 Cutting

Speed

400, 1000, 1500 ( m/min)

3 Feed Rate 0.12, 0.22, 0.40 ( mm/rev)

4 Dia of Drill 4, 7, 10 ( mm) 5 Machining

Time

2, 4, 6 ( min)

The Metal Removal Rate (MRR), Flankwear (Tw), Specific Energy (Es) and Surface Roughness (Ra) are considered as response for this study. The factors and their levels considered in this study are shown in Table 2 Table 2 Machining parameters and their levels Symbol Machining

parameters

Unit Level 1

Level 2

Level 3

A % Vol of

SiC

% 10 15 25

B Cutting

Speed

m/min 400 1000 1500

C Feed mm/rev 0.12 0.22 0.40

D Dia of Drill mm 4 7 10

E Machining

Time

min 2 4 6

III. OPTIMIZATION STEPS USING FUZZY LOGIC

A fuzzy logic unit consists of a fuzzifier, membership functions, a fuzzy rule base, an inference engine and a defuzzfier. In the system of fuzzy reasoning, the fuzzifier primarily uses membership functions to fuzzify the S/N ratios. A Membership Function (MF) is a curve to determine how each input value is mapped to a membership value (or degree of membership) between 0 and 1. Next, the inference engine performs a fuzzy interface so as to generate a fuzzy value according to the membership function and fuzzy rules. Finally, the defuzzifier converts the fuzzy value into a non-fuzzy value called multi-response performance index (MRPI).In this study, the membership function adopts the trapezoidal membership function that has a flat top and a truncated triangle curve. In fuzzy logic, if–then rule statements are used to formulate the conditional statements. In the following, the concept of fuzzy reasoning is described briefly based on the two-input- one-output fuzzy logic unit, where x1 and x2 are the two inputs and y is the output.

Rule 1: if x1 is A1 and x2 is B1 then y is C1 else Rule 2: if x1 is A2 and x2 is B2 then y is C2 else _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ Rule n: if x1 is An and x2 is Bn then y is Cn.

Ai, Bi, and Ci are fuzzy subsets defined by the corresponding membership functions, i.e., μAiBi and μCi. In this work, to obtain fuzzy sets, trapezoidal membership function was used for fuzzification, In fuzzification, numerical input and output values are converted into linguistic terms such as low , medium and high etc., The value of membership function ranges between 0 and 1, and it shows how much a variable matches a fuzzy set.

IV. RESULTS AND DISCUSSION

Membership functions and their ranges of input parameters were shown in Figure 1. A total of 27 rules were formed as shown in Figure 2. In this study , spindle speed , feed rate, drilling diameter , machining time and

% volume of silicon carbide were considered as input parameters. Flank wear, specific energy, surface roughness and metal removal rate were considered as output parameters.

Figure 1 Membership Function

Figure 2 Fuzzy rules with specific energy

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Figure 3 Fuzzy rules without specific energy

Figure 4 Fuzzy logic reasoning procedure for the Test results

TABLE 3 Fuzzy rule table MRPI Machining rate

Small Middle large

Overcut Small Very small Small middle Middle Small Middle large Large Middle Large Very large Nine fuzzy rules (Table 3) are derived directly based on the information that larger is the S/N ratio and the better is the performance characteristics. By taking the max - min compositional operation, the fuzzy reasoning of these rules fetches a fuzzy output. Supposing that x1 and x2 are the two input values of the fuzzy logic unit, the membership function of the output of fuzzy reasoning can be expressed as in Equation (1).

μC0 (y) = (μA1 (x1) ΛμB1 (x2) ΛμC1 (y)) V..(μAn (x1) ΛμBn (x2) Λ μCn (y)) (1) where Λ is the minimum operation and, V is the maximum operation.

 

 

0

0 0

C

C

y y

y

y

(2)

A defuzzification method, called the centroid method, is taken on here to transform the fuzzy inference output into a non-fuzzy value, called MRPI. Based on the above discussion, the larger is the MRPI, the better is the performance characteristic. Applying the fuzzy rules listed in Table 3 and the membership values for the fuzzy sets it is clear in Figure 4. The defuzzified output that gives the final Multi Performance Characteristics indices (MPCIs) value is calculated as 0.5 from the combined darkness area shown in the bottom of MPCIs column in Figure 4. The MRPI value of the corresponding machining parameters is shown in the Table 4 .The effect of each machining parameters at different levels is calculated and summarized in the MRPI table (Table 5).

TABLE 4 Experimental data and corresponding SN ratios.

S.

No MRR (mm3/m in)

Surface Rough ness micron s

Flank Specif ic

SN Ratio of MRR

SN Ratio of

SN Ratio of Flank Wear

SN Ratio of Specifi c Energ y Wear Energ

y

Surfac e Rough ness mm

W/m m3/mi n

1 192 9.02 0.141 38.157 45.67 -19.10 17.02 -31.63 2 1078 12.09 0.232 58.393 60.65 -21.65 12.69 -35.33 3 4000 14.31 0.435 75.1 72.04 -23.11 7.23 -37.51 4 1470 7.56 0.343 34.283 63.35 -17.57 9.29 -30.70 5 5500 9.57 0.581 52.245 74.81 -19.62 4.72 -34.36 6 1600 8.6 0.352 41.568 64.08 -18.69 9.07 -32.38 7 4500 6.79 0.718 36.881 73.06 -16.64 2.88 -31.34 8 1320 6.53 0.579 31.973 62.41 -16.30 4.75 -30.10 9 7350 8.19 0.734 44.907 77.33 -18.27 2.69 -33.05 10 588 9.21 0.413 68.531 55.39 -19.29 7.68 -36.72 11 2200 7.56 0.261 66.895 66.85 -17.57 11.67 -36.51 12 640 11.38 0.542 81.881 56.12 -21.12 5.32 -38.26 13 3000 4.23 0.368 42.71 69.54 -12.53 8.68 -32.61 14 880 7.61 0.683 56.961 58.89 -17.63 3.31 -35.11 15 4900 8.78 0.996 74.658 73.80 -18.87 0.03 -37.46 16 720 5.4 0.815 40.211 57.15 -14.65 1.78 -32.09 17 4042 6.67 1.166 57.424 72.13 -16.48 -1.33 -35.18 18 15000 5.12 0.678 51.444 83.52 -14.19 3.38 -34.23 19 1200 5.9 0.56 90.228 61.58 -15.42 5.04 -39.11 20 352 8.75 1.118 112.29 50.93 -18.84 -0.97 -41.01 21 1960 6.54 0.651 102.52 65.85 -16.31 3.73 -40.22 22 480 5.47 1.212 71.697 53.62 -14.76 -1.67 -37.11 23 2695 4.38 0.778 71.321 68.61 -12.83 2.18 -37.06 24 10000 5.62 1.133 98.295 80.00 -14.99 -1.08 -39.85 25 2205 3.11 0.91 50.347 66.87 -9.86 0.82 -34.04

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26 8250 4.27 1.293 75.604 78.33 -12.61 -2.23 -37.57 27 2400 5.12 1.969 87.256 67.60 -14.19 -5.88 -38.82 -9.86 17.02 -30.10 -23.11 -5.88 -41.01 TABLE 5 MRPI values obtained based on the S/N ratio.

Exp.No SN Ratio of MRR

SN Ratio of Surface Roughness

SN Ratio of Flank Wear

SN Ratio of Specific Energy

MRPI

1 45.67 -19.10 17.02 -31.63 0.59 2 60.65 -21.65 12.69 -35.33 0.47

3 72.04 -23.11 7.23 -37.51 0.38

4 63.35 -17.57 9.29 -30.70 0.64

5 74.81 -19.62 4.72 -34.36 0.51

6 64.08 -18.69 9.07 -32.38 0.57

7 73.06 -16.64 2.88 -31.34 0.67

8 62.41 -16.30 4.75 -30.10 0.63

9 77.33 -18.27 2.69 -33.05 0.66

10 55.39 -19.29 7.68 -36.72 0.39 11 66.85 -17.57 11.67 -36.51 0.57 12 56.12 -21.12 5.32 -38.26 0.27 13 69.54 -12.53 8.68 -32.61 0.66 14 58.89 -17.63 3.31 -35.11 0.49 15 73.80 -18.87 0.03 -37.46 0.48 16 57.15 -14.65 1.78 -32.09 0.56 17 72.13 -16.48 -1.33 -35.18 0.47 18 83.52 -14.19 3.38 -34.23 0.65 19 61.58 -15.42 5.04 -39.11 0.40 20 50.93 -18.84 -0.97 -41.01 0.18 21 65.85 -16.31 3.73 -40.22 0.38 22 53.62 -14.76 -1.67 -37.11 0.33 23 68.61 -12.83 2.18 -37.06 0.58 24 80.00 -14.99 -1.08 -39.85 0.43

25 66.87 -9.86 0.82 -34.04 0.63

26 78.33 -12.61 -2.23 -37.57 0.56 27 67.60 -14.19 -5.88 -38.82 0.31

20 15 10 0.60 0.55 0.50 0.45 0.40

1500 1000

400 0.12 0.22 0.40

10 7 4 0.60 0.55 0.50 0.45 0.40

6 4 2

% Vol of Silica

Mean of Means

Cutting Speed in m/min Feed rate mm/rev

Dia of drill in mm machining time in min Main Effects Plot for Means

Data Means

Figure 5 MRPI graph TABLE 6 MRPI Table

Sym bol

FACT ORS

MRPI Level

1 Level 2 Level 3

Maxi mum A % Vol of

SiC 5.126 4.542 3.786 5.126 B Cutting

Speed 3.626 4.696 5.132 5.132

C Feed 4.86 4.462 4.132 4.86

D Diameter 3.931 4.695 4.828 4.828

of Drill

E Machinin

g Time 5.237 4.474 3.743 5.237 Total mean of MRPI = 4.485

The effect of each machining parameters at different levels is calculated and summarised in the MRPI table (Table 6). Table 6 depicts an optimal combination of process parameter for higher metal removal rate, lesser surface roughness, flank wear and specific energy with

% vol of SiC (level 1), machining speed (level 3), feed rate(level 1), diameter of drill (level 3) and machining time (level 1). The total mean of all 15 values are calculated and presented in Table 6. The MRPI graph is shown in Figure 5. Larger values of the MRPI in the graph (or in the MRPI table 5) indicate that the smaller is the variance of the performance characteristics around the desired value. Moreover, the relative importance between the machining parameters for the multiple performance characteristics still needs to be known so that the optimal combinations of the machining parameter levels can be determined more exactly.

A. Analysis of Variance (ANOVA)

The MRPI values, determined from the experimental values are statistically studied by ANOVA to investigate the effects of each machining parameter on the observed values and to clarify which machining parameters significantly affects the observed values. In addition, the F-test named after Fisher can also be used to determine which process parameters have a significant effect on the performance characteristics (Montgomery DC., 1997). Usually, the change of the process parameter has a significant effect on the performance characteristics when the F value is large. Table 7 shows the calculated F-values of the ANOVA for machining rate and overcut respectively to determine the relative significances of different control factors. From the calculated F value, it is observed that cutting speed and machining time have significant effect in metal removal rate and surface roughness. From the ANOVA test, it is also clear that cutting speed have a high percentage of contribution on different machining criteria compared to other parameters.

TABLE 7 Results of ANOVA

S Sym Bb bol

Factor Sum ofsquares

Degrees of freedo m

Mean square (variance)

F- value F0.05

Contribut ion (%) A

Percentag e volume of SiC

0.100303 2 0.050152 37.44 3.63 21.73

B Cutting

Speed 0.133446 2 0.066723 49.81 3.63 28.91 C Feed 0.029529 2 0.014765 11.02 3.63 6.3 D Diameter

of Drill 0.052074 2 0.026037 19.44 3.63 11.3 E Machinin

g Time 0.124021 2 0.062010 46.29 3.63 26.95

F Error 0.021435 16 0.001340 4.5

T Total 0.460808 26 100

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B. Validation

After identifying the optimal level of the process parameters, the last step is to predict and verify the improvement of the performance characteristic using the optimal level of the process parameters. The purpose of the confirmation test is to validate the conclusions drawn during the analysis phase. The predicted or estimated MRPI value using the optimal level of the process parameters can be calculated as per the Equation (3).

1

( )

q

m i m

i

   

 

(3)

Where ηm is the total mean of the MRPI, q is the number of significant parameters, ηi is the mean of the MRPI at the optimal level.

The MRPI was predicted based on the Equation (3) and new experiment has been designed and conducted with the optimal levels of the machining parameters to verify the improvement of the multiple performance characteristics. Table 8 shows the confirmation test table using optimal machining parameters. This table evaluates the predicted and actual MRPI value and MRPI is increased from 0.784 to 0.8637. It is shown clearly that MRPI is greatly improved. . The metal removal rate is (MRR) is improved from 192 to 3002 mm3/min and surface roughness (SR) is improved from 9.02 to 4.0185μm. It is clearly shown that the multiple performance characteristics in the Al-SiC machining process are greatly improved through this study.

TABLE 8 Confirmation Test Initial Machining parameters

Optimal machining parameters Prediction Experiment Setting

Level A1B1C1D1E1 A1B3C1D3E1 A1B3C1D3E1 Metal

Removal Rate (MRR)

192 3002

Surface Roughness (SR)

9.02 4.0185

Flank

Wear (FW) 0.141 0.3576

Specific Energy (SE)

38.157 40.575

MRPI 0.784 0.8637 0.8530

Improvement in MRPI = 0.069

V. CONCLUSION

A hybrid optimization technique fuzzy along with Taguchi’s design is proposed to find out the optimal setting of process parameters to simultaneously improve four responses. In this experimental study, it is found that the hardness of MMC is increasing with the increasing weight% of SiC in the composite and mesh size. A fuzzy reasoning of the multiple performance characteristics has been performed by the fuzzy logic unit. As a result, the performance characteristics such as MRR, SR, FW and SE can be improved through this approach. An experiment was conducted to confirm this approach. Based on the experimental results and confirmation test the conclusion can be drawn as follows 1.The recommended levels of drilling parameters for minimizing flank wear, surface roughness and specific energy for increase in metal removal rate (at exit condition )simultaneously are the content of SiC at level 1 (10 %), Spindle speed at level 3 (1500m/min), feed rate at level 1 (0.12 mm/rev), Drill diameter at level 3 (10 mm ) and Machining time at level 1 (2 min) Among the tested parameters, the machining time, cutting speed and % vol of SiC shows the strongest correlation to the flank wear, surface roughness, specific energy and Metal removal rate at exit condition

2. An increase in the value of predicted (MRPI) from 0.784 to 0.8637 confirms the improvement in the performance of drilling of metal matrix composites when using the optimal values of process parameters.

3. The experimental results for optimal settings show that there is a considerable improvement in the performance characteristics of machining process. This technique is more convenient and economical to predict the effect of different influential combinations of the parameters within the levels studied.

REFERENCES

[1] Zadeh, L 1965, ‘Fuzzy sets’, Information and

Control, vol. 8, no. 3,

pp. 338-353.

[2] Klir, GJ & Yuan, B 1998, Fuzzy system and fuzzy logic – theory and practice, Englewood Cliffs, Prentice alHl, NJ.

[3] El-Sonbaty, I, Khashaba, UA & Machaly, T 2004, ‘Factors affecting the machinability of GFR/epoxy composites’, Composite Structures, vol. 63, pp. 329-338.

[4] Lin, JL, & Lin, CL, 2005, ‘The use of grey- fuzzy logic for the optimization of the manufacturing process’. Journal of Materials Processing Technology, vol. 160, pp.9–14.

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[5] Basheer, AC, Dabade, UA, Joshi, SS &

Bhanuprasad, VV 2008, ‘Modeling of surface roughness in precision machining of metal matrix composites using ANN’, Journal of Material Processing Technology, vol. 197, pp. 439-444.

[6] Palanikumar, K, Shanmugam, K & Paulo Davim, J 2010, ‘Analysis and optimization of cutting parameters for surface roughness in machining Al/SiC particulate composites by PCD tool’, International Journal of Materials and Product Technology, vol. 37, no.1-2, pp.117-128.

[7] Palanikumar, K, Davim, JP, 2007,

‘Mathematical model to predict tool wear on the machining of glass fibre reinforced plastic composites’, Materials and Design, vol.28,

pp.2008– 2014.

[8] Latha, B & Senthilkumar, VS 2009, ‘Fuzzy rule based modeling of drilling parameters fordelamination in drilling GFRP composites’, Journal of Reinforced Plastics and Composites, vol. 28, no. 8, pp. 951-964.

[9] Latha, B & Senthilkumar, VS 2010, ‘Modeling and analysis of surface roughness parameters indrilling GFRP composites using fuzzy logic’, Materials and Manufacturing Processes, vol. 25, no. 8, pp. 817-827.

[10] Montgomery, DC 1997, Design and Analysis of Experiments, 4th Edition, John Wiley, New York.

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