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8/12/2019 Paper Format MMQC14
1/4
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
8/12/2019 Paper Format MMQC14
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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
8/12/2019 Paper Format MMQC14
3/4
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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