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INTERNATIONAL JOURNAL OF MECHANICAL ENGINEERING
  International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
  6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME
                            AND TECHNOLOGY (IJMET)

ISSN 0976 – 6340 (Print)
ISSN 0976 – 6359 (Online)                                                 IJMET
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)            ©IAEME
www.jifactor.com




    PRODUCTION OF NYLON-6 FR LEVER USING AN INJECTION
      MOULDING TOOL AND IDENTIFICATION OF OPTIMUM
            PROCESS PARAMETER COMBINATION
                            S.Selvaraj1, Dr.P.Venkataramaiah2
                     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
                 2
                  Associate 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(Forward
  Reverse) 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

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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 Taguchi’s method and regression analysis to propose an approach for determining the
optimal process parameter settings in plastic injection molding under single quality
characteristic 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 mold
design 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
Taguchi’s 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 based
combined 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 tool
First, 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 Lever
The 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) =28.5g
2.1.3 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-75
Clamping 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     CAVITY PLATE              EN 24   150X100X50     1
    2     CORE PLATE                EN 24   150X100X50     1
    3.    CORE BACK PLATE            MS     150X100X15     1
    4.    EJECTOR PLATE              MS     150X55X15      1
    5.    EJECTOR BACK PLATE         MS     150X55X15      1
    6.    SPACER BLOCKS              MS     150X50X10      2
    7.    BOTTOM SUPPORT PLATE       MS     150X100X15     1
    8.    TOP PLATE                  MS     200X150X25     1
    9.    BOTTOM PLATE               MS     200X150X25     1
   10.    CORE INSERT               EN 36   φ 24X25        1
   11.    CORE SUB INSERT           EN 36   φ 12X31        1
   13.    CAVITY INSERT             EN 36   φ 11X41        1
   14.    SPRUE BUSH                EN 36   φ 23X52        1
   15.    EJECTOR PINS               STD    φ6             4
   16.    ALLEN SCREW                STD    M6X25          4
   17.    ALLEN SCREW                STD    M8X85          4
   18.    ALLEN SCREW                STD    M10X30         4




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2.2 FABRICATION OF INJECTION MOULDING TOOL FOR FR LEVER
Based 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 been
created 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 Tool
Core 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 and
ends 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 Coordinate
Measuring 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
                  (୴୭୪୳୫ୣ	୭୤	୲୦ୣ	୫୭୳୪ୢି୴୭୪୳୫ୣ	୭୤	୲୦ୣ	ୱ୮ୣୡ୧୫ୣ୬)
%of shrinkage=
                            ୴୭୪୳୫ୣ	୭୤	୲୦ୣ	୫୭୳୪ୢ



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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 lever
             S.N         Input parameters         Symbol Level 1 Level 2 Level 3
                    (Controllable parameters)
               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      40
                                         0
              10 Nozzle temperature ( C)              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.     A     B   C   D   E   F   G   H   J   K             Surface Roughness            Shrinkage
Run                                                    Ra (µ)      Ry (µ)    Rq (µ)          (%)
 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     5.232735172
 5       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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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

     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)
                min X i (k )
     X * (k ) =
                   X (k )                                                 ----(1)
     (b) HB (Higher-the-Better)
                      X i (k )
     X * (k ) =
                   max X i (k )                                           ----(2)
     (c) NB (Nominal-the-Best)
                min{X i (k ), X 0b (k )}
     X * (k ) =
                max{X i (k ), X 0b (k )}                                   ----(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=1,2,3…m ,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)

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Step 2: Checking for correlation between two quality characteristics
Let,
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:
         Cov(Q j , Q k )
ρ=                                              -----(4)
            σ    Q j × σ QK



           j =1, 2, 3......, n.
  here, k = 1, 2, 3, ........, n.,
          j ≠k
Here, ρjk 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 ; σ and σ are the standard deviation of quality characteristic j and k
quality characteristic k , respectively.
The correlation is checked by testing the following hypothesis.
H0: ρ jk = 0         (There is no correlation)
H1: ρ jk ≠ 0         (There is correlation)               -----(5)
Step 3: Calculation of the principal component score
(a)   Calculate the Eigen value λk and the corresponding eigenvector
βk (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:
           n
Yi (k ) = ∑Xi∗ (j)βkj, i = 0,1,2,.......,m; k =1, 2,........ n.
                                                           ,                  ---(6)
          J =1

Here, Yi (k ) is the principal component score of the k th element in the ith series.
X * ( j) is the normalized value of the j th element in the i th sequence, and β kj is the j th
element of eigenvector β 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.
                    X 0 ∗ X i (k ) − X i ∗ (k)
                                                     no significant correlation between quality characteristics
∆0,i (k )=
                                                                                                                  -----(7)
                    Y 0 (k ) − Y i (k)
                                                     significant correlation between quality characteristics


Step 5: Adaptation of utility theory: Calculation of overall utility index
According 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:
U ( X1 , X 2 ,.........
                      ........,X n ) = f (U1 ( X1 ).U2 ( X 2 ).........
                                                                      .........Un ( X n ))
Here Ui ( X i ) is the utility of the ith attribute.


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The overall utility function is the sum of individual utilities if the attributes are
independent, and is given as follows:
                                        n
U ( X1, X 2 , ................., X n ) = ∑ Ui ( X i )                                   − − (8)
                                       i=1
The attributes may be assigned weights depending upon the relative importance or
priorities of the characteristics. The overall utility function after assigning weights to the
attributes can be expressed as:
                                        n
U ( X1, X 2 ,................., X n ) = ∑ Wi .Ui ( X i )
                                       i =1
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:
               Xi 
Pi = A × log ' 
               Xi                                            -----(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,
         9
 A=
          X∗
      log
           Xi                                                  ----(10)
The overall utility can be expressed as follows:
        n
U = ∑WiPi
       i −1                                                      ---(11)
Subject to the condition:
 n

∑Wi = 1
i =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 Pearson’s correlation coefficients. It has
been 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 (ψ ) . It has been found that the four principal components, ψ1 ,ψ 2 ,ψ 3, ψ 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.                                      % of
                          Ra           Ry         Rz
                  No                                      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 0.194881
                     4 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 0.825072
                    15 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




                                             280
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME

                   Table 5 Eigen values, Eigen vectors and Accountability proportion

                                      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
     Table 6: Major Principal Components and Quality loss estimates for principal
                                   components
                 Major Principal Components                  Quality loss estimates
Exp. No
              P1         P2        P3       P4      QL1         QL2        QL3         QL4
   Ideal
            -1.7368    -0.0193   0.1267    0.9834     -           -          -           -
 sequence
     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      -0.4778
     8      -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       -0.315
    21      -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


                                           281
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME

 Table 7 Utility values related Individual principal components and Overall utility
 index and S/N values

          Exp.                                                    Overall
                      U1         U2         U3          U4                      S/N
          No.                                                     utility
            1       0.3568     1.9108      4.1761        0        1.6109     4.1414
            2       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     9.3411
           25       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

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).



                                             282
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME

                                     1 t 1 
SN ( Higher − the − better) = −10 log ∑ 2                                 ---(12)
                                      t i =1 yi 
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 experiments
and 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 most
       powerful 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 ψ1 and
       fourth principal component ψ 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 optimum
       parameter setting for these kind of multi-objective optimization problems.
    • The proposed algorithm greatly simplifies the optimization of injection moulding
       parameters with multiple performance characteristics. Thus, the solutions from this
       method can be a useful reference for injection mould makers and related industry.




                                                     283
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 –
6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME

REFERENCES
 [1] Deng WJ, Chen CT, Sun CH, Chen WC, Chen CP. An effective approach for process parameter
optimization in injection molding of plastic housing components. Polym-Plast Technol Eng
2008;47:910–9.
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methods. Mater Des 2010;31:599–604.
[3] Kurtaran H, Erzurumlu T. Efficient warpage optimization of thin shell plastic parts using response
surface methodology and genetic algorithm. Int J Adv Manuf Technol 2006;27: 468–72.
[4] Shen CY, Wang LX, Li Q. Optimization of injection molding process parameters using
combination of artificial neural network and genetic algorithm method. J Mater Process Technol
2007;183:412–8.
[5] Kurtaran H, Ozcelik B, Erzurumlu T. Warpage optimization of a bus ceiling lamp base using
neural network model and genetic algorithm. J Mater Process Technol 2005;169:314–9.
 [6]Chen, R.S., Lee, H.H., Yu, C.Y., 1997. Application of Taguchi’s method on the optimal process
design of an injection molded PC/PBT automobile bumper. Compos. Struct. 39, 209–214.
 [7] Ozcelik B, Sonat I. Warpage and structural analysis of thin shell plastic in the plastic injection
molding. Mater Des 2009;30:367–75.
[8] Huang MC, Tai CC. The effective factors in the warpage problem of an injection molded part with
a thin shell feature. J Mater Process Technol 2001;110:1–9.
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Production of nylon 6 fr lever using an injection moulding tool and identification of optimum process parameter combination

  • 1. INTERNATIONAL JOURNAL OF MECHANICAL ENGINEERING International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME AND TECHNOLOGY (IJMET) ISSN 0976 – 6340 (Print) ISSN 0976 – 6359 (Online) IJMET 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) ©IAEME www.jifactor.com PRODUCTION OF NYLON-6 FR LEVER USING AN INJECTION MOULDING TOOL AND IDENTIFICATION OF OPTIMUM PROCESS PARAMETER COMBINATION S.Selvaraj1, Dr.P.Venkataramaiah2 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 2 Associate 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(Forward Reverse) 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 270
  • 2. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME 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 Taguchi’s method and regression analysis to propose an approach for determining the optimal process parameter settings in plastic injection molding under single quality characteristic 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 mold design 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 Taguchi’s 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 based combined 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 tool First, 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 1 271
  • 3. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME 2.1.2 Volume and Weight of FR Lever The 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) =28.5g 2.1.3 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-75 Clamping 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 272
  • 4. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME 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 CAVITY PLATE EN 24 150X100X50 1 2 CORE PLATE EN 24 150X100X50 1 3. CORE BACK PLATE MS 150X100X15 1 4. EJECTOR PLATE MS 150X55X15 1 5. EJECTOR BACK PLATE MS 150X55X15 1 6. SPACER BLOCKS MS 150X50X10 2 7. BOTTOM SUPPORT PLATE MS 150X100X15 1 8. TOP PLATE MS 200X150X25 1 9. BOTTOM PLATE MS 200X150X25 1 10. CORE INSERT EN 36 φ 24X25 1 11. CORE SUB INSERT EN 36 φ 12X31 1 13. CAVITY INSERT EN 36 φ 11X41 1 14. SPRUE BUSH EN 36 φ 23X52 1 15. EJECTOR PINS STD φ6 4 16. ALLEN SCREW STD M6X25 4 17. ALLEN SCREW STD M8X85 4 18. ALLEN SCREW STD M10X30 4 273
  • 5. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME 2.2 FABRICATION OF INJECTION MOULDING TOOL FOR FR LEVER Based 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 been created 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 Tool Core 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 and ends 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 274
  • 6. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME 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 Coordinate Measuring 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 (୴୭୪୳୫ୣ ୭୤ ୲୦ୣ ୫୭୳୪ୢି୴୭୪୳୫ୣ ୭୤ ୲୦ୣ ୱ୮ୣୡ୧୫ୣ୬) %of shrinkage= ୴୭୪୳୫ୣ ୭୤ ୲୦ୣ ୫୭୳୪ୢ 275
  • 7. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME 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 lever S.N Input parameters Symbol Level 1 Level 2 Level 3 (Controllable parameters) 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 40 0 10 Nozzle temperature ( C) 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. A B C D E F G H J K Surface Roughness Shrinkage Run Ra (µ) Ry (µ) Rq (µ) (%) 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 5.232735172 5 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 276
  • 8. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME 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 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) min X i (k ) X * (k ) = X (k ) ----(1) (b) HB (Higher-the-Better) X i (k ) X * (k ) = max X i (k ) ----(2) (c) NB (Nominal-the-Best) min{X i (k ), X 0b (k )} X * (k ) = max{X i (k ), X 0b (k )} ----(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=1,2,3…m ,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) 277
  • 9. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME Step 2: Checking for correlation between two quality characteristics Let, 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: Cov(Q j , Q k ) ρ= -----(4) σ Q j × σ QK j =1, 2, 3......, n. here, k = 1, 2, 3, ........, n., j ≠k Here, ρjk 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 ; σ and σ are the standard deviation of quality characteristic j and k quality characteristic k , respectively. The correlation is checked by testing the following hypothesis. H0: ρ jk = 0 (There is no correlation) H1: ρ jk ≠ 0 (There is correlation) -----(5) Step 3: Calculation of the principal component score (a) Calculate the Eigen value λk and the corresponding eigenvector βk (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: n Yi (k ) = ∑Xi∗ (j)βkj, i = 0,1,2,.......,m; k =1, 2,........ n. , ---(6) J =1 Here, Yi (k ) is the principal component score of the k th element in the ith series. X * ( j) is the normalized value of the j th element in the i th sequence, and β kj is the j th element of eigenvector β 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.  X 0 ∗ X i (k ) − X i ∗ (k)  no significant correlation between quality characteristics ∆0,i (k )=  -----(7)  Y 0 (k ) − Y i (k)  significant correlation between quality characteristics Step 5: Adaptation of utility theory: Calculation of overall utility index According 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: U ( X1 , X 2 ,......... ........,X n ) = f (U1 ( X1 ).U2 ( X 2 )......... .........Un ( X n )) Here Ui ( X i ) is the utility of the ith attribute. 278
  • 10. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME The overall utility function is the sum of individual utilities if the attributes are independent, and is given as follows: n U ( X1, X 2 , ................., X n ) = ∑ Ui ( X i ) − − (8) i=1 The attributes may be assigned weights depending upon the relative importance or priorities of the characteristics. The overall utility function after assigning weights to the attributes can be expressed as: n U ( X1, X 2 ,................., X n ) = ∑ Wi .Ui ( X i ) i =1 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:  Xi  Pi = A × log '   Xi  -----(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, 9 A= X∗ log Xi ----(10) The overall utility can be expressed as follows: n U = ∑WiPi i −1 ---(11) Subject to the condition: n ∑Wi = 1 i =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. 279
  • 11. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME 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 Pearson’s correlation coefficients. It has been 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 (ψ ) . It has been found that the four principal components, ψ1 ,ψ 2 ,ψ 3, ψ 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. % of Ra Ry Rz No 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 0.194881 4 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 0.825072 15 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 280
  • 12. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME Table 5 Eigen values, Eigen vectors and Accountability proportion 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 Table 6: Major Principal Components and Quality loss estimates for principal components Major Principal Components Quality loss estimates Exp. No P1 P2 P3 P4 QL1 QL2 QL3 QL4 Ideal -1.7368 -0.0193 0.1267 0.9834 - - - - sequence 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 -0.4778 8 -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 -0.315 21 -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 281
  • 13. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME Table 7 Utility values related Individual principal components and Overall utility index and S/N values Exp. Overall U1 U2 U3 U4 S/N No. utility 1 0.3568 1.9108 4.1761 0 1.6109 4.1414 2 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 9.3411 25 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 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). 282
  • 14. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online) Volume 3, Issue 3, Sep- Dec (2012) © IAEME 1 t 1  SN ( Higher − the − better) = −10 log ∑ 2  ---(12)  t i =1 yi  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 experiments and 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 most powerful 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 ψ1 and fourth principal component ψ 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 optimum parameter setting for these kind of multi-objective optimization problems. • The proposed algorithm greatly simplifies the optimization of injection moulding parameters with multiple performance characteristics. Thus, the solutions from this method can be a useful reference for injection mould makers and related industry. 283
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