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  • 7/30/2019 Production of Nylon-6 Fr Lever Using an Injection Moulding Tool and Identification of Optimum Process Parameter

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    International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976

    6340(Print), ISSN 0976 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) IAEME

    270

    PRODUCTION OF NYLON-6 FR LEVER USING AN INJECTION

    MOULDING TOOL AND IDENTIFICATION OF OPTIMUM

    PROCESS PARAMETER COMBINATION

    S.Selvaraj1, Dr.P.Venkataramaiah

    2

    1

    Research Scholar, Department of Mechanical Engineering,Sri Venkateswara University College of Engineering and

    Senior Lecturer, Department of Tool & Die Making, Muruagapp Polytechnic

    College,Chennai

    2Associate Professor, Department of Mechanical Engineering,

    Sri Venkateswara University College of Engineering, Tirupati, Andhra Pradesh, India-

    517502.

    ABSTRACT

    This research work on Optimization of Injection Moulding has been done in three phases. In

    the first phase, an Injection Moulding Tool is designed and fabricated for FR(ForwardReverse) lever, which is to control the direction of rotation of spindles for conventional

    machines. In the second phase, the influential parameters, called input parameters which

    affect the quality of FR lever are identified. The response parameters, called output

    parameters such as Shrinkage and Surface Roughness which are considered as quality

    characteristics of this product have also been identified. FR levers are produced using the

    fabricated injection moulding tool according to Taguchi L27 OA and response data are

    recorded. In the third phase, recorded experimental data are analyzed and optimum process

    parameters combination has been found by a combined method which is developed from the

    integration of the Principal Component Analysis (PCA) and Utility based Taguchi method.

    The obtained optimum parameters combination is conformed experimentally.

    Keywords: Injection Moulding, Principal component analysis (PCA), Shrinkage, Surface

    roughness, Utility based Taguchi method

    1.0 INTRODUCTION

    Now a days, plastic products have more demand since they are of low cost, good corrosion

    resistant, light weight, flexible colours and have good life also. The costs of the plastic

    products are made less by production using various types of moulds. Many engineers and

    researchers have made research works on optimizing process parameters on Injecion

    INTERNATIONAL JOURNAL OF MECHANICAL ENGINEERINGAND TECHNOLOGY (IJMET)

    ISSN 0976 6340 (Print)

    ISSN 0976 6359 (Online)

    Volume 3, Issue 3, September - December (2012), pp. 270-284

    IAEME: www.iaeme.com/ijmet.asp

    Journal Impact Factor (2012): 3.8071 (Calculated by GISI)www.jifactor.com

    IJMET

    I A E M E

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    271

    moulding for various thermoplastic materials and attempt to reduce shrinkage and warpage.

    Some authors presented few case studies on improvement of Quality characteristic of surface

    roughness, shrinkage and warpage by applying Taguchi technique, Artificial Neural

    Network(ANN), Genetic Algorithm(GA), Fuzzy logics and combination methods. Deng et al.

    applied Taguchis method and regression analysis to propose an approach for determining the

    optimal process parameter settings in plastic injection molding under single qualitycharacteristic considerations [1]. Altan et al. minimized the shrinkage of rectangular- shaped

    specimens by Taguchi experimental design and Neural network to predict the shrinkage of

    the part [2]. Hasan Kurtaran et al. proposed an efficient minimization method of warpage on

    thin shell plastic parts by integrating finite element (FE) analysis, statistical design of

    experiment method, response surface methodology(RSM), and genetic algorithm [3]. Shen et

    al. minimized the shrinkage of a plastic part by using the artificial neural network and genetic

    algorithm [4]. Kurtaran et al. considered mold temperature, melt temperature, packing

    pressure, packing time and cooling time as the key process parameters during PIM and got

    the optimum values of process parameters in injection molding of a bus ceiling lamp base to

    achieve minimum warpage by using neural network model and genetic algorithm [5].

    Factors that affect the quality of a molded part can be classified into four categories:

    part design, mold design, machine performance and processing conditions. The part and molddesign are assumed as established and fixed. During production, quality characteristics may

    deviate due to variation in processing conditions caused by machine wear, environmental

    change or operator fatigue. Determining optimal process parameter settings critically

    influences productivity, quality, and cost of production in the plastic injection moulding

    (PIM) industry. Previously, production engineers used either trial-and-error method or

    Taguchis parameter design or ANN, Fuzzy method or combined method to determine

    optimal process parameter settings for PIM[6-12]. However, these methods are unsuitable in

    present PIM because the increasing complexity of product design and the requirement of

    multi-response quality characteristics. A Principal Component Analysis(PCA) has been used

    for optimation of process parameters in different industrial application.

    Literature review reveals that there is a lack of research on design and fabrication of

    injection moulding tool and finding the optimal process parameters setting using PCA basedcombined approach. Hence, this paper focused on design, fabrication of Injection mould and

    production of Nylon-6 FR lever as well as the application of combined method which is

    developed from the integration of the Principal Component Analysis (PCA) and Utility based

    Taguchi method to determine the optimum parameter combination.

    2.0 PHASE I: DESIGN AND FABRICATION OF AN INJECTION MOULDING

    TOOL FOR FR LEVER

    2.1 DESIGN OF AN INJECTION MOULDING TOOL FOR FR LEVER

    2.1.1 Modeling of FR lever and Injection moulding toolFirst, F-R lever model is modeled using ProE according to standard specifications. Two plate

    Injection moulding tool with taper parting surface is suitable for this kind of products and

    hence it is selected in the present work. It is decided to fabricate fully Automatic Injection

    moulding tool with ejectors assembly .Based upon the model of FR lever, the different parts

    of the injection moulding tool is identified and a model of injection moulding tool is created

    in ProE 5 wildfire. The different parts of injection moulding tool with materials and size is

    listed in Table 1

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    2.1.2 Volume and Weight of FR LeverThe volume and weight of FR lever are found from created model as follows

    Volume of the component from model =23.750 cc

    Density of the plastic material Used ( Nylon) =1.20g/cc (from standard data

    book)

    Weight of the component =volume * density = 23750*(1.20/10000) =28.5g2.1.3 Shot Capacity of Mould

    Shot capacity of mould is the maximum amount of materials injected into the mould for one

    shot.

    Shot capacity of mould= [total weight of the component]+[total weight of feed system]

    Weight of the feed system =10% of the component weight = (10/100)*28.5)=2.85g

    shot capacity= [total weight of the component no. of cavities] + weight of the feed system

    = (28.5*1) +2.85 = 31.35g

    2.1.4 Selection of Injection Moulding Machine

    Based on shot capacity calculated above, the suitable injection moulding machine has

    been selected. In the present study OPTIMA-75 of Electronica make is used for production of

    FR lever.

    Specification of OPTIMA-75Clamping force : 75 tons

    Injection pressure : 1486 bars

    Shot weight : 123 grams

    Pump drive : 7.5kw

    Mould thickness : 125 310 mm

    Distance between the bars : 350 x 300mm

    Max. Day light : 610 mm

    Screw diameter : dia 35mm.

    2.1.5 Selection of Plastic Material

    Nylon 6 has been selected for the F-R lever component because it have Very strong and rigid,

    Good abrasion resistant, heat resistant and dimensional accuracy, resistant to oils greases and

    cleaning fluids and high density.

    Fig.1 3D MODEL OF FR LEVER- CCOMPONENT DIAGRAM

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    Fig 2 2D MODEL OF THE COMPONENT Fig.3. OPTIMA 75 INJECTION MOULDING

    WITH DIMENSIONS IN mm MACHINE

    TABLE 1 BILL OF MATERIALS OF INJECTION MOULDING TOOL.

    S.NO MOULD ELEMENT MATERIAL SIZE IN mm QTY

    1 CAVITYPLATE EN 24 150X100X50 1

    2 COREPLATE EN 24 150X100X50 1

    3. COREBACKPLATE MS 150X100X15 1

    4. EJECTORPLATE MS 150X55X15 1

    5. EJECTORBACKPLATE MS 150X55X15 1

    6. SPACERBLOCKS MS 150X50X10 2

    7. BOTTOMSUPPORTPLATE MS 150X100X15 1

    8. TOPPLATE MS 200X150X25 1

    9. BOTTOMPLATE MS 200X150X25 110. COREINSERT EN 36 24X25 1

    11. CORESUBINSERT EN 36 12X31 1

    13. CAVITYINSERT EN 36 11X41 1

    14. SPRUEBUSH EN 36 23X52 1

    15. EJECTORPINS STD 6 4

    16. ALLENSCREW STD M6X25 4

    17. ALLENSCREW STD M8X85 4

    18. ALLENSCREW STD M10X30 4

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    2.2 FABRICATION OF INJECTION MOULDING TOOL FOR FR LEVERBased upon the design (shown in Table 1) of injection moulding tool, the following parts or

    elements are fabricated as follows:

    2.2.1 Making of Cavity plate and Core plate

    The cavity and core plate provides the complete profile of the FR lever and taper parting

    surface is used because of complicated profile of the FR lever. CNC program has beencreated from the profile drawing of FR lever and then the profile is made using VMC milling

    machine. The runner is produced in the plate using EDM spark erosion machine, the ends are

    chamfered to avoid sharp corners and the profile is polished by diamond polish.

    2.2.2 Making other Elements of Injection Moulding ToolCore Back Plate, Ejector Plate, Ejector Back Plate, Spacer Block, Bottom Plate, and Bottom

    Support Plate are prepared with help of shaping machine, grinding machine and the holes are

    made and the counter bore for some plates are produced by position with DRO.

    2.2.3 Making of Core Sub Insert, Cavity Insert, Core Insert And Sprue Bush

    Core sub insert, cavity insert, core insert and sprue bush are produced by lathe and surface

    grinding machine. Raw material is taken and the dimensions are checked, turning and facing

    operation is done by using lathe machine to the required dimension. Grinding is done by

    using surface grinding machine andends are chamfered.VMC milling machine is used producing special profile on core insert

    and the profile is polished by diamond polish. Vertical machining center (VMC) is a

    computer numerical control machine used to fabricate any type of complicated jobs. This

    machine is used to produce core plate, cavity plate and top plate.After each component is

    fabricated and assembled to get an injection moulding tool by checking the all alignment for

    required mating parting as shown in Fig 6.

    Fig 4 Core back plate and other elements of the mould

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    Fig 5 Vertical milling and VMC machine for Injection mould fabrication

    Fig 6 Cavity plate, core plate, top plate and Assembly of Injection moulding tool

    3.0 PHASE-II: PRODUCTION OF FR LEVER AND MEASUREMENT OF

    RESPONSES

    The fabricated injection mould tool is fitted in selected moulding machine and

    experiments are conducted according to Taguchi L27 Orthogonal Array(OA) with 3 levels

    and 10 input process parameters as shown in Table 2.

    Dimension of each specimen component have been measured using 3D CoordinateMeasuring Machine with a machine resolution of 0.05 micron at Accurate Calibration

    Service Laboratory which was certified by by National Accreditation Board for Testing and

    Calibration Laboratories(NABL). Based on the dimensions of the specimen, the Volume of

    each specimen has been calculated by creating a Model ProE 5.0 wildfire software.

    Percentage of Shrinkage of the each specimen has been calculated using the formula

    %of shrinkage=()

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    The calculated value of percentage of shrinkage is recorded for each experiment as shown in

    Table 3.

    Surface roughness of each specimen is measured with portable stylus-type Talysurf

    (Mitutoyo make) as shown in Fig 7 and recorded in Table.3.

    Table 2 Process parameters and their levels in injection moulding machine of ER leverS.N Input parameters

    (Controllable parameters)

    Symbol Level 1 Level 2 Level 3

    1 Injection speed( mm/s , %) A 15 20 25

    2 Injection pressure, (Bar) B 20 25 30

    3 Holding pressure (Bar) C 15 20 25

    4 Holding speed ( mm/s , %) D 15 20 25

    5 Clamping pressure (Bar) E 30 40 50

    6 Clamping speed ( mm/s , %) F 25 35 45

    7 Injection time (Sec) G 1 1.5 2

    8 Holding time (Sec) H 1.5 2 2.5

    9 Cooling time (Sec) J 30 35 4010 Nozzle temperature (0C) K 235 245 255

    The other conditions are maintained as Refill speed is 80 mm/s, Refill pressure is 100 bar,

    Shot weight is 50 gram and Pre heat temp is 850 C .

    Fig 7 Measurement using CMM, Taylsurf and Injection moulding Tool with FR lever

    Table 3 Average Surface Roughness Characteristics and % of shrinkage value

    Exp.

    Run

    A B C D E F G H J K Surface Roughness Shrinkage(%)Ra () Ry () Rq ()

    1 1 1 1 1 1 1 1 1 1 1 2.515 16.8225 3.26875 2.290960976

    2 1 1 1 1 2 2 2 2 2 2 2.6425 16.62875 3.565 5.878247823

    3 1 1 1 1 3 3 3 3 3 3 2.85875 16.79125 3.645 2.131741189

    4 1 2 2 2 1 1 1 2 2 2 2.64 16.71125 3.47125 5.2327351725 1 2 2 2 2 2 2 3 3 3 3.585 22.84375 4.70625 5.265334059

    6 1 2 2 2 3 3 3 1 1 1 3.87375 22.91 5.0775 4.029811766

    7 1 3 3 3 1 1 1 3 3 3 3.11125 22.31875 4.39875 5.746519484

    8 1 3 3 3 2 2 2 1 1 1 3.35625 18.83 4.18625 6.77336339

    9 1 3 3 3 3 3 3 2 2 2 3.17375 20.78625 4.13625 3.15421767

    10 2 1 2 3 1 2 3 1 2 3 2.8775 16.89125 3.68875 7.372633732

    11 2 1 2 3 2 3 1 2 3 1 3.94 25.10125 5.225 5.867920125

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    4.0 PHASES-III: IDENTIFICATION OF OPTIMUM PARAMETERS USING A

    COMBINED APPROACH

    The recorded responses data are analysed and optimum analysis of experimental data using

    combined approach of Principle Components Analysis and utility based taguchi method.

    The experimental data(Table 3) are analyzed using Combined Approach to identify the

    optimum process parameters setting as follows

    Step 1: Normalization of the responses (quality characteristics)When the range of the series is too large or the optimal value of a quality characteristic is too

    enormous, it will cause the influence of some factors to be ignored. The original experimental

    data must be normalized to eliminate such effect. There are three different types of data

    normalization according to the requirement LB (Lower-the-Better),HB (Higher-the-Better)

    and NB (Nominal-the-Best). The normalization is taken by the following equations.

    (a) LB (Lower-the-Better)

    )(kX

    )(kiXmin=)(k*X

    ----(1)(b) HB (Higher-the-Better)

    )(kiXmax

    )(kiX)(k*X =

    ----(2)

    (c) NB (Nominal-the-Best)

    )}(k0bX),(kimax{X

    )}(k0bX),(kimin{X)(k*X =

    ----(3)

    Here,

    i = 1, 2, ........, m;

    k = 1, 2, ........., n

    X * (k ) is the normalized data of the k th element in the i th sequence.

    X 0 (k ) is the desired value of the k th quality characteristic. After data normalization ,the

    Value of X*(K) will be between 0-1.The series X*i i=1,2,3m ,can be viewed as a

    comparative sequence used in the present case. For present study LB is applicable because

    there is a need to minimize the responses (surface roughness, shrinkage)

    12 2 1 2 3 3 1 2 3 1 2 2.9525 19.255 3.9475 7.058997561

    13 2 2 3 1 1 2 3 2 3 1 3.22 17.41875 4.02 4.438114356

    14 2 2 3 1 2 3 1 3 1 2 3.0275 18.035 3.89625 9.0251992

    15 2 2 3 1 3 1 2 1 2 3 3.2625 18.9925 4.2 8.166390242

    16 2 3 1 2 1 2 3 3 1 2 2.6575 16.67375 3.53125 4.02846559

    17 2 3 1 2 2 3 1 1 2 3 3.14875 20.37875 4.08375 7.519388001

    18 2 3 1 2 3 1 2 2 3 1 3.24625 15.7025 3.84 10.93867623

    19 3 1 3 2 1 3 2 1 3 2 2.18375 13.3575 2.93375 7.680699715

    20 3 1 3 2 2 1 3 2 1 3 2.85375 17.3525 3.85375 7.405005069

    21 3 1 3 2 3 2 1 3 2 1 2.84 18.19375 3.6775 6.721344377

    22 3 2 1 3 1 3 2 2 1 3 2.17125 13.8325 3.0275 5.754424446

    23 3 2 1 3 2 1 3 3 2 1 2.8125 15.6575 3.625 2.464883534

    24 3 2 1 3 3 2 1 1 3 2 2.49 16.29375 3.2275 6.36134543

    25 3 3 2 1 1 3 2 3 2 1 2.4275 14.6275 3.19875 5.012226112

    26 3 3 2 1 2 1 3 1 3 2 2.26625 13.6825 3.08375 6.149924974

    27 3 3 2 1 3 2 1 2 1 3 2.49625 16.82875 3.3125 5.441488134

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    Step 2: Checking for correlation between two quality characteristicsLet,

    Qi = {X 0 (i), X1 (i), X 2 (i), ............, X m (i)}

    where, i = 1, 2, ......., n

    It is the normalized series of the ith quality characteristic. The correlation coefficient between

    two quality characteristics is calculated by the following equation:

    -----(4)

    j =1, 2, 3......, n.here, k=1, 2, 3, ........, n.,

    j k

    Here, jk is the correlation coefficient between quality characteristic j and quality

    characteristic k ; Cov (Q j , Qk ) is the covariance of quality characteristic j and quality

    characteristic k ; and are the standard deviation of quality characteristic j and k

    quality characteristic k , respectively.

    The correlation is checked by testing the following hypothesis.0=:0H jk (There is no correlation)

    0:H1 jk (There is correlation) -----(5)

    Step 3: Calculation of the principal component score(a) Calculate the Eigen value k and the corresponding eigenvector

    k (k = 1, 2, ......, n) from the correlation matrix formed by all quality characteristics.

    (b) Calculate the principal component scores of the normalized reference sequence

    and comparative sequences using the equation shown below:

    ---(6)

    Here, Yi (k ) is the principal component score of the kth element in the ith series.X * ( j) is the normalized value of the j

    thelement in the i

    thsequence, and kj is the j

    th

    element of eigenvector k

    Step 4: Estimation of quality loss 0,i (k )0,i (k ) is the absolute value of difference between X 0 (k ) and X i (k ) difference

    between desired value and ith experimental value for kth response. If responses are

    correlated then instead of using X 0 (k ) and X i (k ) , Y0 (k ) and Yi (k ) should be used.

    0,i (k )=

    Step 5: Adaptation of utility theory: Calculation of overall utility indexAccording to the utility theory, if X i is the measure of effectiveness of an attribute (or quality

    characteristics) i and there are n attributes evaluating the outcome space, then the joint utility

    function can be expressed as:

    Here Ui ( X i ) is the utility of the ith

    attribute.

    n.,2,........1,=km;2,.......,0,1,=i,(j)X=)(kY1J

    ii =

    n

    kj

    X i0 i

    0 i

    X (k) X (k)

    Y (k) Y (k)

    j

    j k

    Q

    Cov(Q , Q )

    KQ

    =

    ))X(.........U).........X().UX((Uf=)X........,,.........X,X(U nn2211n21

    no significant correlation between quality characteristics

    -----(7)

    significant correlation between quality characteristics

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    The overall utility function is the sum of individual utilities if the attributes are

    independent, and is given as follows:

    (8))X(U=)X.......,..........,X,X(U ii1i

    n21 =

    n

    The attributes may be assigned weights depending upon the relative importance or

    priorities of the characteristics. The overall utility function after assigning weights to theattributes can be expressed as:

    )X(.UiW=)X........,,.........X,X(U iin

    1i

    n21 =

    Here, Wi is the weight assigned to the attribute i . The sum of the weights for all the

    attributes must be equal to 1.

    A preference scale for each quality characteristic is constructed for determining its utility

    value. Two arbitrary numerical values (preference number) 0 and 9 are assigned to the just

    acceptable and the best value of quality characteristic respectively. The preference number

    Pi can be expressed on a logarithmic scale as follows:

    =

    'log i

    i

    X

    X

    APi -----(9)

    Here, X i is the value of any quality characteristic or attribute i,Xi ' is just acceptable value of

    quality characteristic or attribute i and A is a constant. The value A can be found by the

    condition that if Xi = X * (where X * is the optimal or best value), then Pi = 9 .

    Therefore,

    iX

    XA

    =

    log

    9

    ----(10)

    The overall utility can be expressed as follows:

    =

    n

    i

    iiPWU1 ---(11)

    Subject to the condition:

    =

    =

    n

    i

    Wi1

    1

    Among various quality characteristics types, viz. Lower-the-Better, Higher-the-Better, and

    Nominal-the-Best suggested by Taguchi, the utility function would be Higher-the- Better

    type. Therefore, if the quality function is maximized, the quality characteristics considered

    for its evaluation will automatically be optimized (maximized or minimized as the case may

    be).In the proposed approach based on quality loss (of principal components) utility values

    are calculated. Utility values of individual principal components are accumulated to

    calculate overall utility index. Overall utility index servers as the single objective function

    for optimization.Step 6: Optimization of overall utility index using Taguchi method

    Finally overall utility index is optimized (maximized) using Taguchi method. For

    calculating S/N ratio, HB criterion is selected.

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    5.0 RESULTS AND DISCUSSION

    Experimental data with L27 OA are noted and listed in Table 3. For all surface roughness

    parameters and % of shrinkage, LB criterion has been selected. Normalized experimental

    data are shown in Table 4. The correlation coefficients between individual responses have

    been computed using Equation 4. Table 5 represents Pearsons correlation coefficients. It hasbeen observed that all the responses are correlated (coefficient of correlation having non-zero

    value). Table 5 presents Eigen values, eigenvectors, accountability proportion (AP) and

    cumulative accountability proportion (CAP) computed for the four major quality

    indicators ( ) . It has been found that the four principal components, 1 , 2 , 3, 4 can

    take care of 71.48%, 0.3%, 2.93% and 25.29% variability in data respectively.

    Table 4 Normalized values of Surface roughness and % of shrinkage

    Exp.

    NoRa Ry Rz

    % of

    shrinkage

    1 0.638325 0.670186 0.625598 0.209437

    2 0.670685 0.662467 0.682297 0.537382

    3 0.725571 0.668941 0.697608 0.1948814 0.670051 0.665754 0.664354 0.47837

    5 0.909898 0.910064 0.900718 0.48135

    6 0.983185 0.912704 0.97177 0.3684

    7 0.789657 0.889149 0.841866 0.52534

    8 0.85184 0.750162 0.801196 0.619212

    9 0.80552 0.828096 0.791627 0.288355

    10 0.73033 0.672925 0.705981 0.673997

    11 1 1 1 0.536438

    12 0.749365 0.767093 0.755502 0.645325

    13 0.817259 0.69394 0.769378 0.405727

    14 0.768401 0.71849 0.745694 0.82507215 0.828046 0.756636 0.803828 0.746561

    16 0.674492 0.66426 0.675837 0.368277

    17 0.799175 0.811862 0.781579 0.687413

    18 0.823921 0.625566 0.734928 1

    19 0.554251 0.532145 0.561483 0.70216

    20 0.724302 0.6913 0.73756 0.676956

    21 0.720812 0.724815 0.703828 0.614457

    22 0.551079 0.551068 0.579426 0.526062

    23 0.713832 0.623774 0.69378 0.225337

    24 0.63198 0.649121 0.617703 0.581546

    25 0.616117 0.58274 0.612201 0.458211

    26 0.57519 0.545092 0.590191 0.562218

    27 0.633566 0.670435 0.633971 0.497454

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    Table 5 Eigen values, Eigen vectors and Accountability proportion

    Table 6: Major Principal Components and Quality loss estimates for principal

    components

    Eigen values

    2.8594 0.0119 0.1172 1.0115

    V =Eigen vectors

    -0.5757 -0.5371 -0.6127 0.0685-0.5677 -0.2800 -0.0903 -0.0903

    -0.5884 0.7957 -0.1433 0.0118

    -0.0049 0.0021 0.1138 0.9935

    Accountability Proportion (AP)

    Ap1 Ap2 Ap3 Ap4

    0.7148 0.003 0.0293 0.2529

    Cumulative Accountability Proportion (CAP)

    cap1 cap2 cap3 cap4

    0.7148 0.7178 0.7471 1

    Exp. No

    Major Principal Components Quality loss estimates

    P1 P2 P3 P4 QL1 QL2 QL3 QL4

    Idealsequence

    -1.7368 -0.0193 0.1267 0.9834 - - - -

    1 -1.1171 -0.0323 0.0584 0.1986 0.6197 -0.013 -0.0683 -0.7848

    2 -1.1663 -0.0017 0.0618 0.528 0.5704 0.0176 -0.0649 -0.4554

    3 -1.2089 -0.0215 -0.008 0.1911 0.5278 -0.0022 -0.1347 -0.7923

    4 -1.157 -0.0167 0.0606 0.4688 0.5798 0.0026 -0.0661 -0.5146

    5 -1.5729 -0.0258 0.068 0.4689 0.1639 -0.0065 -0.0587 -0.5145

    6 -1.6578 -0.0096 0.0021 0.3623 0.079 0.0097 -0.1247 -0.6211

    7 -1.4574 -0.0021 0.139 0.5056 0.2794 0.0172 0.0123 -0.47788 -1.3908 -0.0288 0.0106 0.6152 0.346 -0.0095 -0.1162 -0.3682

    9 -1.4011 -0.034 0.0626 0.2762 0.3357 -0.0147 -0.0641 -0.7073

    10 -1.2212 -0.0175 0.0455 0.6672 0.5156 0.0018 -0.0812 -0.3163

    11 -1.7345 -0.0203 0.074 0.5229 0.0023 -0.001 -0.0528 -0.4605

    12 -1.3146 -0.0148 0.0959 0.6321 0.4221 0.0045 -0.0308 -0.3514

    13 -1.3192 -0.0202 -0.0312 0.4054 0.4176 -0.0009 -0.1579 -0.578

    14 -1.2931 -0.0188 0.0687 0.8162 0.4437 0.0005 -0.058 -0.1672

    15 -1.3829 -0.0154 0.0442 0.7395 0.3538 0.0039 -0.0825 -0.2439

    16 -1.1649 -0.0097 0.0426 0.36 0.5719 0.0096 -0.0842 -0.6234

    17 -1.3843 -0.0332 0.1008 0.6736 0.3525 -0.0139 -0.0259 -0.3099

    18 -1.2669 -0.0308 -0.0153 1.0021 0.4699 -0.0115 -0.142 0.0186

    19 -0.9551 0.0016 0.069 0.6941 0.7817 0.0209 -0.0577 -0.2893

    20 -1.2468 0.0057 0.0591 0.6684 0.49 0.025 -0.0676 -0.31521 -1.2436 -0.0288 0.0847 0.6026 0.4931 -0.0095 -0.042 -0.3808

    22 -0.9737 0.0119 0.0629 0.5174 0.7631 0.0312 -0.0638 -0.466

    23 -1.1744 -0.0055 -0.0315 0.2246 0.5624 0.0138 -0.1582 -0.7588

    24 -1.0987 -0.0285 0.0896 0.5697 0.6381 -0.0092 -0.0371 -0.4137

    25 -1.048 -0.006 0.035 0.452 0.6888 0.0133 -0.0917 -0.5314

    26 -0.9907 0.0092 0.0461 0.5557 0.7461 0.0285 -0.0806 -0.4278

    27 -1.1209 -0.0225 0.0931 0.4845 0.6159 -0.0032 -0.0336 -0.4989

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    Table 7 Utility values related Individual principal components and Overall utility

    index and S/N values

    Major principal components is obtained using Equation 6. These have been furnished in

    Table 6. Quality loss estimates (difference between ideal and actual gain) for aforesaid

    major principal components have been calculated (Equation7) and also presented in Table 6.

    Based on quality loss, utility values corresponding to the four principal components have

    been computed using Equations 9, 10.

    In all the cases minimum observed value of the quality loss (from Table 6) has been

    considered as its optimal value or most expected value; whereas maximum observed value

    for the quality loss has been treated as the just acceptable value. Individual utility measures

    corresponding to four major principal components have been furnished in Table 7. The

    overall utility index has been computed using Equation 11 and tabulated in Table 7 with their

    corresponding (Signal-to-Noise) S/N ratio. In this computation it has been assumed that all

    quality indices are equally important (same priority weight age, 25%). Figure 8 reflects S/N

    ratio plot for overall utility index; S/N ratio being computed using equation (12).

    Exp.

    No.U1 U2 U3 U4

    Overall

    utilityS/N

    1 0.3568 1.9108 4.1761 0 1.6109 4.14142 0.4839 1.2448 4.4327 1.3088 1.8676 5.4254

    3 0.6031 5.7564 0.7997 -0.023 1.784 5.0281

    4 0.459 5.3827 4.3393 1.015 2.799 8.9401

    5 2.3994 3.4099 4.927 1.0155 2.938 9.3609

    6 3.521 2.5484 1.1854 0.5627 1.9544 5.8202

    7 1.5801 1.2982 12.7112 1.1933 4.1957 12.4561

    8 1.2519 2.5983 1.5359 1.8198 1.8015 5.1126

    9 1.2984 1.6366 4.4892 0.2502 1.9186 5.6597

    10 0.6393 6.2312 3.3151 2.1857 3.0928 9.8071

    11 8.9583 7.54 5.4619 1.2819 5.8105 15.2843

    12 0.9464 4.1981 8.1303 1.9326 3.8018 11.5999

    13 0.963 7.6904 0.008 0.7356 2.3492 7.4186

    14 0.87 9.021 4.9887 3.7183 4.6495 13.3481

    15 1.2175 4.5444 3.2381 2.8106 2.9526 9.4042

    16 0.4801 2.5729 3.1392 0.5537 1.6865 4.5395

    17 1.2233 1.7583 9.0018 2.2347 3.5545 11.0156

    18 0.7817 2.1721 0.5362 8.9959 3.1215 9.8872

    19 -0.0001 0.8768 5.0174 2.3997 2.0735 6.3339

    20 0.7174 0.4815 4.2288 2.1951 1.9057 5.6011

    21 0.7076 2.5956 6.5992 1.7392 2.9104 9.2791

    22 0.0369 0.0022 4.5161 1.2535 1.4522 3.2404

    23 0.5059 1.7838 -0.0008 0.0809 0.5924 -4.5473

    24 0.3118 2.6676 7.2061 1.5396 2.9313 9.341125 0.1944 1.8558 2.7113 0.9376 1.4248 3.0749

    26 0.0715 0.1945 3.354 1.4594 1.2699 2.0751

    27 0.3661 4.9475 7.7004 1.0894 3.5259 10.9453

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    =

    =

    t

    i iytbettertheHigherSN

    12

    11log10)( ---(12)

    Here t is the number of measurements, and yi the measured ith

    characteristic value i.e. ith

    quality indicator. Optimal parameter setting has been evaluated from Figure. The optimal

    setting should confirm highest utility index (HB criterion).

    Fig 8 S/N ratios for predicated optimal setting

    The predicted optimal setting is A2 B1 C2 D2 E3 F2 G1 H2 J3 K3

    6.0 CONCLUSIONS

    Combined approach of PCA and Utility based Taguchi method is successfully applied in the

    present study and the following conclusions are drawn from the results of the experimentsand analysis of the experimental data in connection with correlated multi- response

    optimization in injection moulding of FR lever.

    Based on the analysis and results, it is concluded that PCA is mostpowerful tool to eliminate response correlation by converting the correlated

    responses into uncorrelated quality indices, called principal components which have

    been treated as response variables for optimization.

    Based on the PCA method, it has been found that first principal component 1 andfourth principal component 4 can take care of 71.48% and 25.29% variability in

    data respectively, which shows that Surface roughness Ra and % of shrinkage are the

    most influence quality characteristics.

    Utility based Taguchi method has been found fruitful for evaluating the optimumparameter setting for these kind of multi-objective optimization problems.

    The proposed algorithm greatly simplifies the optimization of injection mouldingparameters with multiple performance characteristics. Thus, the solutions from this

    method can be a useful reference for injection mould makers and related industry.

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