First International Conference on Emerging Trends in Engineering and Technology Machinery Condition Monitoring System Selection – A Multi-Objective Decision Approach using GA A.K. Verma*, A. Srividya*, P.G. Ramesh@ * Indian Institute of Technology, Bombay @ Defence Institute of Advanced Technology, Pune [email protected] maintenance effects[6-8]. Soft computing techniques and Genetic algorithms are increasingly being used in maintenance decision problems as they provide an efficient platform for both modeling and solution phases of the problem[9-13]. Most models in literature use deterioration levels of machinery systems to schedule inspection or condition monitoring. But, in many cases, particularly for large engineering plants, it is not possible to precisely identify the level of deterioration since there are several components in the plant and each of them has several modes of deterioration. Further, there are interdependencies between the components. Therefore, for a maintenance decision maker on site, it is preferable to identify the state of the sub-system by means of the level of repairs that are necessary to restore the prevailing state to a “as-good-as-new” state. There is also a need to optimize the characteristics of the condition monitoring system at a macro level. This will enable decisions regarding the area and extent of effective applicability of CBM for a large plant consisting of several subsystems arranged in a complex way. Abstract In this paper, a framework for Condition Based Maintenance (CBM) of large engineering systems has been suggested to address the need to optimize the characteristics of both the condition monitoring system and the plant that is being maintained at a macro level. CBM for large engineering systems has been modeled using Markov process. The issues which are critical to CBM, namely, predictability, detectability as well as implications of availability and cost have been considered in the framework to provide effective decision support. The application of the framework has been demonstrated using a numerical example. The trade offs between the Pareto optimal solutions of various objectives have been studied and the effects of variation of the maintenance objective function values with detectability and predictability have been brought out. . 1. Introduction Maintenance has an essential role in ensuring that engineering systems perform at expected levels of reliability, availability and safety in a cost effective manner and in keeping with the corporate demands. In the case of Maintenance of Large Engineering Plants (LEP) like, aircraft, shipboard machinery, power plants and nuclear installations, owing to their peculiarities, Time Based Maintenance (TBM) is preferred as an effective strategy [1]. But TBM is based on the assumption that failures are age related which is contrary to a study where it is shown that about 80% to 85% of equipment failures are caused due to the effects of random events that happen in the system [2]. Therefore it is necessary to augment TBM of large engineering plants with Condition Based Maintenance (CBM) so as to optimally realize the objectives of maintenance. Features of condition monitoring, diagnostic and prognostic systems have been discussed in literature[3-5]. There has been a widespread use of Markov and semi-Markov processes for studying 978-0-7695-3267-7/08 $25.00 © 2008 IEEE DOI 10.1109/ICETET.2008.127 This paper presents a framework for providing decision support to select condition monitoring systems based on their detectability and predictability and provide for them at appropriate locations of the system. In section 2 the CBM model is described as a discrete space, continuous time Markov process. In sections 3 and 4, objective and constraint functions are developed. This is followed by formulation of expressions for detectability and predictability of the condition monitoring system in section 5. A numerical example is presented in section 6. Results and Conclusions are discussed in sections 7 and 8 respectively. 2. Model description Consider a Large Engineering Plant (LEP) in which n modules are subjected to Condition Based Maintenance (CBM). Each of the n modules of the plant is subjected to a particular condition monitoring 787 Authorized licensed use limited to: INDIAN INSTITUTE OF TECHNOLOGY BOMBAY. Downloaded on June 5, 2009 at 03:09 from IEEE Xplore. Restrictions apply. arrangement. The condition monitoring arrangements comprise of one or more techniques, including manual inspection and assessment of condition of the module. Each of the n modules is essential for the plant to be in the operational state. In respect of each of the n modules, initially, periodic monitoring of its condition is done at a particular monitoring rate. When an exceeding of the threshold values of one or more of those parameters indicating the healthy condition of the module (Relevant Condition Indicators, RCI [16]) is detected by the condition monitoring system, the module is subjected to a more detailed condition monitoring strategy. In this strategy, prediction of time to carry out preventive maintenance so as to prevent a catastrophic failure is done using the monitored parameters (Relevant Condition Predictor, RCP[16]). Again, when crossing of threshold value of the RCP of the module is detected by the condition monitoring system, the module is subjected to an appropriate level of preventive maintenance (PM). If the RCP or RCI is detected but the instant of failure is not detected by the monitoring system sufficiently in advance, the PM of the module is delayed for necessary logistic preparation. On the other hand, if the exceeding of an RCI or an RCP is not detected, the module fails catastrophically, necessitating Corrective Maintenance (CM). Both PM and CM restore the module to “as good as new” condition. The model provides for the ability to enable regression to a previous operationally better state in case the measured deterioration value reduces due to state changes or cessation of some external disturbing factors [14]. The model is shown schematically in Figure 1. The above CBM problem is modeled as a discrete space, continuous time Markov process as shown in Figure 2. In constructing the model and formulating the objective functions, the discussions in reference [15] have been taken forward to include logistic delay and a detailed analysis of detectability and predictability features of condition monitoring system on the maintenance objectives of LEP. Pi,p Di,d Fi λAi,aBi,π LEP – n modules under CBM Y Is condition within threshold value ? N Increased rate/or continuous/monitoring/ condition prediction Stopped – Level 1 prev. maintenance Y Is condition within threshold value ? N Required maintenance level Log delay Stopped – Level 2 prev. maintenance Catastrophic Failure – Corrective Maintenance Log delay Figure 1. Schematic diagram showing CBM of LEP Maintenance (CBM) of the plant, and the proportion of probabilities of CM to PM. A A 11,1,1 A A 11,a, a A A 1 1,A ,A F F1 1 B B1 ,1 1 ,1 B B1, 1 ,π π D D 1 ,1 1 ,1 3. Notation The condition of the module in each state of the Markov model is determined by the extent or level of repairs or maintenance required to restore it to as good as new condition. It is required to minimize the Unavailability, overall cost of Condition Based P P 1 ,1 1 ,1 B B 1 ,W 1 ,W D D 1 ,d 1,d D D 1 ,D P P 1 ,p P P 1 ,P 1 ,p 1 ,D 1 ,P Figure 2. Markov model of CBM of a LEP Further, if δi,π ∈ [0,1] is the detectability feature of the relevant condition monitoring arrangement π of module i, and αi ,π and βi ,π are the failure rates of the module i while undergoing condition monitoring of Table 1. Description of states of the Markov model i Ai,a 1,2,….,A Module i under condition monitoring strategy ‘π’, П = 1,2,….,W Module i under preventive maintenance of level p , p = 1,2,….,P Module i held up for preventive maintenance due to logistic delay of category d, d = 1,2,….,D Module i in the catastrophic failure state Transition rate from state Ai,a to Bi,π and so on for all other state transitions. Bi,π Number of the module, i = 1,2,……,n Operational state ‘a’ of module, ‘i' , a = 788 Authorized licensed use limited to: INDIAN INSTITUTE OF TECHNOLOGY BOMBAY. Downloaded on June 5, 2009 at 03:09 from IEEE Xplore. Restrictions apply. strategy π, then the transition rates to the states of higher levels of condition monitoring and various categories of logistic delays are respectively, λAi,aBi,π = δi,π αi ,π (1) λAi,aDi,d = Li,l δi,π βi ,π (2) Where, Li,l is the probability of the module i undergoing level ‘l’ of PM. Also, the corresponding transition rates to the states of catastrophic failure are λAi,aFi,π = (1-δi,π) αi ,π (3) (4) λAi,aFi,π = (1-δi,π) βi ,π The transition from the states of logistic delays will depend on the predictability. Higher the predictability, faster will be the rate of transition from the state of logistic delay to that of PM. If ρ ∈ [0,1] is the predictability feature of the condition monitoring system of an impending failure, then, (5) λDi,dPi,p = Li,l ρ δi,π βi ,π 4. Formulation constraint functions 4.1 of objective preventively when the condition demands or when the component of module fails. This can be given by P F 1 1 (10) T = min ∑ ,∑ ; i = 1, 2...., n Rp (f ) P F ( )( ) p =1 λ = 1 f i F (r ) i P ( Pi , p )(∑ λPi , p ) r =1 where λP( r ) is the rth transition rate out of state Pi,p and i,p λF( f ) is the fth transition out of state Fi (f = 1,2,…,F). i C Plant = P W C π δ π + Cρ ∑ π i, i, p =1 ,i ρi + Ci P ( Fi ) + =1 D ∑C i , p P ( Pi , p ) + ∑ Ci , d P ( Di ,d ) d =1 } (11) Where Ci ,π , Cρ ,i , Ci , Ci , p and Ci ,d are the cost related to the detectability of the condition monitoring system, predictability of the condition monitoring system, cost of catastrophic failure, cost of PM and the cost due to logistic delay respectively. and Objective functions 4.1.3 The ratio, (Prob(CM)/Prob(PM))Plant The ratio of the sum of the probabilities of CM and the sum of probabilities of PM in respect of all the modules of the plant is proposed an indicator towards the efficacy of the condition monitoring system. 4.1.1. Unavailability. The steady state unavailability of the plant is given in respect of the probabilities of catastrophic failures of the constituent modules and the down time of the plant due to logistic delay. Since all modules are necessary for the operation of the plant, the steady state unavailability of the module is given by: D (6) U Module = P( Fi ) + ∑ P ( Di , d ) d =1 And, for the entire plant, n D U Plant = 1 − ∏ 1 − P( Fi ) + ∑ P( Di ,d ) d =1 i =1 1 n ∑{ T i =1 n CM = PM ∑ P( F ) (12) i n i =1 P ∑∑ P( P i, p ) i =1 p =1 4.2 Constraint Function (7) The CBM model for the plant has to integrate with the Time Based Maintenance or Scheduled Preventive Maintenance (SPM) Model. One of the approaches proposed for the same is by trying to ensure that the Mean Time Between Failures (MTBF) derived from the CBM model is greater or equal to the SPM interval, tSPM . The least MTBF of all the modules must be greater than or equal to the SPM interval and this is proposed as a constraint to the optimization problem. 4.1.2 Cost. The cost of CBM is dependent on the initial and operational cost of the condition monitoring system as represented in this model by their detectability and predictability. Higher detectability and predictability imply higher cost. Cost is incurred when the plant is down for CM owing to not only the lost operational time, but also the secondary damages suffered and the safety compromised. Cost is also incurred due to the logistic delay, again due to the lost operational time as well as the extra effort and resources required for emergency arrangements for repairs and maintenance. A short logistic delay is possible if adequate warning of failure is given by the condition monitoring system, which in turn depends on its predictability. Further, the cost of CBM is proposed as a time rate which will be the rate of cost over an operational window of duration T. As per the CBM policy, replacement or repair or maintenance is done A 1 min ∑ ; i = 1, 2,..., n ≥ t SPM Ra a =1 (r) P ( Ai ,a )(∑ λ Ai ,a ) r =1 (13) 4.3 Constrained Multi-Objective Optimisation Problem The CBM problem modeled above is solved as a Constrained Multi-Objective Optimisation Problem. 789 Authorized licensed use limited to: INDIAN INSTITUTE OF TECHNOLOGY BOMBAY. Downloaded on June 5, 2009 at 03:09 from IEEE Xplore. Restrictions apply. (b) Diagnostic Ability Let the set of parametric and non-parametric symptoms gathered by the condition predicting system (17) be Pi ,π = Pi ,π ,1 , Pi ,π ,2 ,...., Pi ,π , j ,...Pi ,π , J The optimization problem is solved using Genetic Algorithms (GA). GA is proposed since it is suitable for handling non linear multiple objectives with several variables and requiring to be optimized simultaneously with each objective maintaining its identity. On execution of the GA, a population of solutions is obtained each of which is optimum with trade offs [10]. Each optimal solution corresponds to a set of decision parameters, namely, in the present case, detectability and predictability factors in respect of each module. The decision maker can choose the optimum solution that is acceptable for the given multi-criteria situation. Domain information pertaining to the failure rates, repair rates, inspection intervals, relative probabilities various levels of PM are incorporated in the problem to narrow down the decision space and aid in the search for the optima. { Si ,π = { All possible combinations of symptoms that are found to occur together to yield meaningful diagnosis} f : Si ,π → Di , Define (19) Si ,π ⊆ Pi ,π σ ie,π + σ ia,π = 1 (22) where, (23) σ d i ,π +σ p i ,π =1 A plant consists of two modules, both of which are required for the functioning of the plant. The CBM decision model proposed above is applied to the plant, appropriately adopting the Markov diagram in Figure 2. The values of the constants used in the problem are αi ,π = 0.033; βi ,π = 0.05; λAi,aBi,π = 1 & 0.166; λBi,πAi,a = 1 & 4; λFi,Ai,a = 0.06; λPi,pAi,a = 1. For simplicity, the failure rates are assumed to be identical for both the modules. The constrained multi-objective optimization problem was solved using Non-Dominated Sorting Genetic Algorithm (NSGA-II) [18]. The parameters for the GA are based on experimental/conservative values. The steady state Probabilities and other terms in the objective and constraint functions are obtained by solving the matrix equation, 24 [19]. these are essential for the predicting system to provide maximum lead time for preparation for maintenance and thereby reducing logistic delays and enabling better planning of maintenance. Following quantitative measures are proposed for determining Predictability: (a) Prognostic ability: ρip,π = P(ξi −Ti,π ) <<ε × P(Ti,π −tid,π ) ≥ LDT;Ti,π < tSPM (16) where, ε is a small positive number t Predictability: ρi ,π = σ id,π ρid,π + σ ip,π ρip,π 6. Numerical Example time. Predictability is proposed to be further divided into prognostic ability ρip,π and diagnose-ability. Both of 7. Results } d i ,π (21) Further, it is proposed that both the detectability and predictability be given as the weighted sum of their constituent parts. e a (22) Detectability : δ i ,π = σ i ,π eπ + σ i ,π aπ where µi = E[ξi ] , ξi is the failure time random variable of module i and Ti ,π is the preventive replacement { (20) Ai ,π ,a ∈Si ,π a =1,2,....α (15) µi Ai ,π ,a ∈ Si,π a = 1, 2,....α Thus, diagnostic ability is given by ρid,π = ∑ P (Ai ,π , a ) P ( f ( Ai ,π , a ) givenAi ,π , a ) The overall outputs of the condition monitoring arrangements can be divided into detectability (representing RCI) and predictability (RCP) factors. Detectability is further divided into effectiveness and accuracy. Effectiveness eπ is the proportion of the expected number of failures avoidable by technique π relative to the total expected number of failures under Failure Replacement Policy (FRP). Accuracy aπ of the same strategy is defined as the proportion of total expected number of failures under Failure Replacement Policy to the expected number of total removals. For the long run they are defined as [17] : µ P(ξi ≤ Ti,π ) (14) eπ = 1 − i E[min(ξi , Ti,π )] E[min(ξ i , Ti ,π )] Ai ,π ,a → Di ,k Also, 5. Detectability and predictability aπ = } The set of diagnosis leading to preventive maintenance (18) be Di = { Di ,1 , Di ,2 ,..., Di , k ,...Di , K } The result of multi-objective optimisation using the GA is a set of optimal solutions which form Pareto optimal fronts in the objective spaces. Each solution corresponds to a set of values for the objectives, which in turn correspond to a set of decision variables. All is the time of detection of the impending fault or failure of module i using the technique π and LDT is the logistic delay time. 790 Authorized licensed use limited to: INDIAN INSTITUTE OF TECHNOLOGY BOMBAY. Downloaded on June 5, 2009 at 03:09 from IEEE Xplore. Restrictions apply. -λ −λ ( 1,1) A1,1B1,1 A1,1B1,1 PA PB λA1,1B1,1 ( 1,1) PA ( 1,2) 0 ( 1,2) =0 PB PP ( 1,1) 0 ( 1,1) PD 0 PF ( 1) 1 λB A 0 λP A 0 λFA −λB1,1A1,1 −λB1,1A1,2 0 0 0 0 0 1,1 1,1 1 1,1 λB A −λA1,2B1,2 −λA1,2F1 λB1,2A1,2 0 λA B 0 0 0 −λP1,1A1,1 λD1,1P1,1 0 0 0 λB D 0 −λD1,1P1,1 0 1 1 1 1 1 1,1 1,2 1,2 1,2 0 0 0 −λB1,2A1,2 −λB1,2D1,1 0 0 0 1,2 1,1 decision maker. Likewise, Figure 4 shows the variation of cost with unavailability. Figure 5 gives the relation between the ratio of probabilities CM/PM and unavailability. It can be seen from Figure 6 that the variation of average predictability is more rapid than that of average of detectability with respect to unavailability. In other words, availability is relatively more sensitive to predictability. Extending this observation, detectability is more important in the early stages of monitoring which will improve reliability and safety of the plant and predictability is more important −1 0 1,1 1,1 1 0 0 0 0 0 0 1 (24) solutions are optimal, one differing from the other due to the trade off between the objectives. The trade offs between the relative cost rate of CBM and the ratio of probabilities of CM/PM is shown in Figure 3. It can be 350 300 350 250 Prob(CM)/Prob(PM) 300 P rob (C M )/P rob (P M ) 250 200 200 150 100 150 50 100 0 0.1 50 0.15 0.2 0.25 0.3 0.35 Unavailbaility 0 55 65 75 85 95 105 115 Figure 5. Unavailability of the plant vs. the ratio of the probabilities of CM and PM Relative Cost Rate Figure 3. The trade offs between the relative cost rate of CBM and the ratio of probabilities of CM/PM 1.05 Average P red ictability and Detectability 0.95 115 105 Relative Cost Rate 95 85 0.85 0.75 0.65 0.55 0.45 0.35 75 0.25 65 0.1 0.15 0.2 0.25 0.3 Unavailability Ave Predictability 55 0.1 0.15 0.2 0.25 Ave Detectability Figure 6. Averages of detectability and predictability of both modules compared against Unavailability 0.3 0.35 Unavailability Figure 4. Trade off between Unavailability of the plant and relative cost rate of CBM in the later stages, which will improve steady state availability. Finally, the decision maker can select the most acceptable solution from among the Pareto optimal solutions using the decision statements for seen that the cost of CBM increases along with greater demand for PM in preference to CM. This result is on expected lines. However, the results give more precise decision support in respect of the two objectives to the 791 Authorized licensed use limited to: INDIAN INSTITUTE OF TECHNOLOGY BOMBAY. Downloaded on June 5, 2009 at 03:09 from IEEE Xplore. Restrictions apply. 0.35 predictability and detectability (equations 14-23), which in turn can be ascertained based on statistical data or expert opinion or both. [7] J.S. Ivy and H.B. Nembhard, “A Modeling Approach to Maintenance Decisions Using Statistical Quality Control and Optimization”, Quality and Reliability Engineering International, 2005, vol 21, pp 355-366. 8. Conclusions [8] D. Chen and K.S. Trivedi, “Optimisation for Condition Based Maintenance with Semi Markov Decision Process”, Reliability Engineering and System Safety, 2005 pp 177-187. CBM is aimed at preventing catastrophic failures of equipment and providing sufficient lead time for planning, preparing and undertaking preventive maintenance. 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