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    2ndNational Conference on Latest Develeopments in Materials,

    Manufacturing and Quality Controlfrom 13-14th February, 2014.

    Abstract- In this paper, a multi factor decision makingapproach is presented for prioritizing failures causes for thedigester of pulping system of a paper mill as an alternative totraditional approach of failure mode and effect analysis

    (FMEA). The approach is based on the technique for orderpreference by similarity to ideal solution (TOPSIS). The

    priority ranking is formulated on the basis of six parameters(failure occurrence, non detection, maintainability, spare

    parts, economic safety and economic cost). The Shannon'sentropy concept is used for assigning objective weights tomaintenance parameters.

    Keywords - Maintenance, TOPSIS, FMECA, andMCDM, Risk priority number.

    I. INTRODUCTION

    Deciding on the best maintenance policy is not aneasy matter as the maintenance program must combine

    technical requirements with the management strategy. A

    good maintenance program must define maintenancestrategies for different facilities. The failure mode of every

    component must be studied in order to assess the best

    maintenance solution, in accordance with its failure

    pattern, impact and cost on the whole system. Thisinformation helps the maintenance personnel to decide the

    best suited maintenance action and to assign the different

    priorities to various plant components and machines. Themanagement of large number of tangible and intangible

    attributes that must be taken into account represents thecomplexity of the problem.

    Several techniques have been discussed in theliterature for planning maintenance activities of industrial

    plants. The most commonly used technique to evaluate the

    maintenance significance of the items/ failure modes andcategorise these in several groups of risk is based on usingfailure mode effect and criticality analysis FMCEA. This

    methodology has been proposed in different possiblevariants, in terms of relevant criteria considered and/or

    risk priority number formulation. Using this approach, theselection of a maintenance policy is performed through

    the analysis of obtained priority risk number.This technique was first proposed by NASA in 1963

    for their obvious reliability requirements. Since then, ithas been extensively used as a powerful technique for

    system safety and reliability analysis of products and

    processes in a wide range of industries [1], [2]. The main

    objective of FMEA is to discover and prioritise thepotential failure modes by computing respective RPN,which is a product of failure occurrence, severity and

    probability of non detection of a fault. Though RPN

    evaluation with FMEA is probably the most popular

    technique for reliability and failure mode analysis, severalproblems are associated with its practical implementation,

    which have been addressed by many authors[3],[4],[5],[6],[7]. The most important problems discussed

    were regarding the- FMCEA does not consider the interdependence among

    the various failure modes and effects;- It considers only three kinds of attributes whereas other

    important aspects like economic aspects, production

    quantities, and safety aspects etc. are not taken intoconsideration

    - It is assumed that the three indexes are equallyimportant and identifying situations with the same

    priority number characterized by different index levels.- the assumption that the scales of three severity (S),

    occurrence (O) and detection (D) indexes have the

    same metric and that the same design level corresponds

    to the same values on different index scales;- different sets of the three factors can produce exactly

    the same value of RPN, but the hidden implication maybe totally different

    - The method of multiplication adopted for calculatingthe risk priority number is questionable.

    Considering the importance and complexity of themaintenance design problem it is observed that further

    efforts are needed for the development of effectivemethods which will incorporate numerous evaluation

    criteria and help the maintenance staff in evaluating the

    impact of intangible factors in the maintenance decisionmaking and identify the best maintenance policy

    accordingly.

    In this paper, a new technique based on modifiedFMEA alongwith TOPSIS is proposed to determine the

    risk priority number and to overcome the limitations of theconventional RPN, as cited above. This technique permits

    to take into consideration the several possible aspectsconcerning the maintenance selection problem (failure

    chances, detectability, costs and safety aspect etc.) Themethod is based on a technique for order preference bysimilarity to ideal solution (TOPSIS). TOPSIS is a multi-

    attribute decision making methodology based on themeasurement of the Euclidean distance of an alternative

    from an ideal goal [8]. The procedure for TOPSIS

    methodology is presented in the subsequent section.

    Maintenance criticality analysis using TOPSIS

    Anish Sachdeva1, Pradeep Kumar

    2, Dinesh Kumar

    2

    1Department of Industrial and Production Engineering, National Institute of Technology, Jalandhar, India

    ([email protected])2Department of Mechanical and Industrial Engineering, Indian Institute of Technology, Roorkee, India

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    TABLE 1

    SCORE FOR CHANCE OF FAILURE

    Occurrence MTBF Score

    Almost never >3 years 1

    Rare 2-3 years 2

    Very few 1-2 years 3

    few 3/4-1 year 4

    Medium 6 - 9 months 5

    Moderately high 4 - 6 months 6

    High 2 - 4 months 7

    Very high 1 - 2 months 8

    Extremely high < 30 days 9

    TABLE 2SCORE FOR NON DETECTION OF FAILURES

    Likelihood ofNon-detection (%)

    Criteria for non detection offailures

    Score

    < 10 Extremely low 1

    10-20 Very low 2

    21-30 Low 3

    31-40 fair 4

    41-50 medium 5

    51-60 moderately high 6

    61-70 High 7

    71-80 Very high 8

    > 80 Extremely high 9

    TABLE 3

    SCORE FOR MAINTAINABILITY

    Criteria Maintainability Score

    Mt > 0.8 Almost certain 1

    0.7 < Mt0.8 Very high 20.6 < Mt0.7 High 3

    0.5 < Mt0.6 Moderate ly high 4

    0.4 < Mt0.5 Medium 5

    0.3 < Mt0.4 Low 6

    0.2 < Mt0.3 Very low 7

    0.1 < Mt0.2 Slight 8

    Mt< 0.1 Extremely low 9

    TABLE 4SCORING CRITERIA FOR SPARE PARTS

    CriticalityAvailability

    Easy Difficult Scarce

    Desirable 1 4 7

    Essential 2 5 8

    Vital 3 6 9

    TABLE 5

    SCORES FOR ECONOMIC SAFETY LOSS

    Status of the equipment/ sub system Score

    With no moving parts 2

    With one moving part/ critical category 3

    With two moving parts/ critical category 5

    With three moving parts/ critical category 7With more than three moving parts/ critical category 9

    TABLE 6

    SCORES FOR ECONOMIC COST

    Criteria for Economic Cost Score

    Extremely low 1

    Very low 2

    Low 3

    Fair 4

    Medium 5

    Moderat ely high 6

    High 7

    Very high 8

    Extremely high 9

    TABLE 7

    SCORES FOR FAILURE CAUSES OF DIGESTERMajor Components and

    Potential cause of failureO D M SP ES EC

    Wire mesh

    Abrasion of mesh [D1]

    Corrosion [D2]

    Foreign material [D3]

    Vacuum pumps

    Lack of lubrication in moving parts.

    [D4]

    Bearing failure [D5]

    Inclusion of solid particles[D6]

    Seal failure [D7]

    Let down relief valve

    Mechanical failure [D8]

    Blockage. [D9]

    3

    5

    8

    4

    5

    5

    8

    5

    4

    5

    5

    8

    5

    5

    7

    5

    8

    7

    3

    6

    4

    6

    8

    5

    6

    5

    4

    4

    4

    2

    4

    4

    3

    3

    8

    7

    3

    3

    3

    6

    6

    6

    3

    3

    3

    3

    4

    4

    5

    7

    7

    5

    7

    6

    Figure labels should be legible, approximately 8 to 10

    point type.

    Fig. 1 Mapping nonlinear data to a higher dimensional feature

    space

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    2ndNational Conference on Latest Develeopments in Materials,

    Manufacturing and Quality Controlfrom 13-14th February, 2014.

    V.CONCLUSIONS

    This paper presents a new modified FMECA approach todeal with the problems encountered while defining the

    best mix of maintenance policies. An objective weightedfunction based multi criteria failure mode analysis

    technique using TOPSIS is proposed to find more accurate

    and reliable priority risk numbers for performing the

    criticality analysis. This enables to obtain a ranking offailure modes/components by incorporating several types

    of information related to performance, safety and society.

    In particular, the analysis of prioritization of failure causesprovides a framework to decide upon the type of

    maintenance strategies for different failure modes. Ifreliable quantitative judgments are available for some

    criteria, then it can also be easily included in the analysis.So the use of the proposed approach forms a basis for the

    continuous process of reliability design and maintenance

    strategy decisions.

    REFERENCES

    [1] P. O'Connor, Practical Reliability Engineering, Singapore: JohnWiley & Sons, 2003.

    [2] S. H. Teng, and S. Y. Ho, Failure mode and effects analysis: anintegrated approach for product design and process control,

    International Journal of Quality & Reliability Management, vol.

    13, no. 5, pp. 8-26, 1996.

    [3] B. G. Dale and C. Cooper, Total Quality and Human Resources:An Executive Guide, Oxford :Blackwell Publishers, 1992.

    [4] D. Straker, A Tool book for Quality Importance and ProblemSolving, London: Prentice-Hall International Limited, 1995.

    [5] J. B. Bowles and C. E. Pelaez, Fuzzy logic prioritization offailures in a system failure mode, effects and criticality analysis,

    Reliability Engineering and System Safety, vol. 50, pp. 203213,

    1995.

    [6] M. Braglia, MAFMA: multi-attribute failure mode analysis,International Journal of Quality & Reliability Management, vol.

    17, pp. 1017-1033, 2000.[7] N. R. Shankar and B. S. Prabhu, Modified approach for

    prioritizat ion of failures in a system failure mode and effects

    analysis, Internat ional Journal of Quality & ReliabilityManagement, vol. 18, no. 3, pp. 324-335, 2001.

    [8] M. Braglia, M. Frosolini, and R. Montanari, Fuzzy TOPSISapproach for failure mode, effects and criticality analysis,Quality and Reliability Engineering International, vol. 19, pp.

    425443, 2003.

    [9] C. L. Hwang, and K. Yoon, Multi Attribute Decision MakingMethods and Applications, New York: Springer-Verlag, 1981.

    [10] C. Parkan, and M. Wu, Decision-making and performancemeasurement models with applications to robot selection,

    Computers & Industrial Engineering, vol. 36, pp. 503-23,1999.[11] D. Jee, and K. Kang, A method for optimal material selection

    aided with decision making theory, Materials and Design, vol.

    21, pp. 199-206, 2000.[12] H. Deng, C. Yeh and R. J. Willis, Inter-company comparison

    using modified TOPSIS with objective weights, Computers &

    Operations Research, vol. 27, pp. 963-973, 2000.

    APPPENDIX A

    THE DISTANCES OF FAILURE CAUSES FROM IDEAL SOLUTION

    Failure Causes

    O D M SP ES EC

    +

    i1d -

    i1d +

    i2d -

    i2d +

    i3d -

    i3d +

    i4d -

    i4d +

    i5d -

    i5d +

    i6d -

    i6d

    D1 0.1064 0.0000 0.0545 0.0000 0.1064 0.0000 0.0571 0.0571 0.0476 0.0000 0.0833 0.0000

    D2 0.0638 0.0426 0.0545 0.0000 0.0426 0.0638 0.0571 0.0571 0.0476 0.0000 0.0625 0.0208

    D3 0.0000 0.1064 0.0000 0.0545 0.0851 0.0213 0.1143 0.0000 0.0476 0.0000 0.0625 0.0208

    D4 0.0851 0.0213 0.0545 0.0000 0.0426 0.0638 0.0571 0.0571 0.0000 0.0476 0.0417 0.0417

    D5 0.0638 0.0426 0.0545 0.0000 0.0000 0.1064 0.0571 0.0571 0.0000 0.0476 0.0000 0.0833

    D6 0.0638 0.0426 0.0182 0.0364 0.0638 0.0426 0.0857 0.0286 0.0000 0.0476 0.0000 0.0833D7 0.0000 0.1064 0.0545 0.0000 0.0426 0.0638 0.0857 0.0286 0.0476 0.0000 0.0417 0.0417

    D8 0.0638 0.0426 0.0000 0.0545 0.0638 0.0426 0.0000 0.1143 0.0476 0.0000 0.0000 0.0833

    D9 0.0851 0.0213 0.0182 0.0364 0.0851 0.0213 0.0286 0.0857 0.0476 0.0000 0.0208 0.0625

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