Availability Modelling

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    RELIABILITY ENGINEERING UNIT

    ASST4403

    Lecture 27-28 AVAILABILITY MODELLING

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    earn ng outcomes

    xp a n e ramewor o ava a y re a e o

    reliability, maintainability and maintenance Interpret and analyse different times for availability

    and downtime

    Understand mathematical basis for availability

    measures

    rt cu ate t e system ava a ty assessmentmethods

    Predict availability of simple systems

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    reliability, maintainability and

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    Dependability, framework of reliability,availabilit maintainabilit etc

    AS IEC 60300.12004

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    ome e n ons

    availability performance and its influencing factors:

    reliability performance, maintainability performance andmaintenance support performance

    given conditions of use, to be retained in, or restored to astate in which it can perform a required function, whenmaintenance is performed under given conditions and

    using stated procedures and resources Maintenance support performance is the ability of a

    maintenance organization, under given conditions, toprovide upon demand, the resources required tomaintain an item, under a given maintenance policy

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    MTBF

    t

    etR

    )(

    yearst 30

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    v w y

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    Review of Reliability System A

    Modem POD A

    Rin Pair A1

    0.659

    0.9500.950

    0.950 0.942

    0.741 0.8610.861

    0.861

    0.6590.942

    0.741 0.950Ring Pair A2

    0.9500.741 0.861 0.659

    0.659

    0.950 0.9420.861

    SCM(16

    Wires)

    Junction(incl

    Conrs)System B

    ep0.9500.861 0.942

    Modem POD B

    POD B

    0.659

    0.950

    0.950 0.942

    0.861

    0.861

    0.942

    Ring Pair B1

    0.741

    .. .

    0.950Ring Pair B2

    0.9500.741 0.861

    .

    0.6590.950 0.9420.861

    .

    0.9500.861 0.942

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    Review of Reliability

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    Review of Reliability

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    Review of Reliability

    Step 6

    ys em

    0.689SCM(16

    Wires)

    Junction(incl

    Conrs)

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    Reliability and Confidence

    Reliability is the probability, at a specified confidence level, that a deviceor s stem will erform its intend function for a iven interval of timeunder specified operating conditions.

    What is the relationship between confidence and reliability?

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    Eg Haul Pack Operational Capability

    Task Haul Pack required to travel into operational area return and dump its load

    Success Criteria - Haul Pack successfully travels to the AO return and dump its load

    Mission Phases:

    Haul Pac

    Available

    tart

    Haul Pack

    Transits toHaul Pac

    Dumps Load

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    Eg Haul Pack Operational Capability

    Pr(HPA) = Probability that HP is Available = 0.7

    Pr(HPS) = Probability that HP Starts = 0.95 Pr(HPT) = Probability that HP Transits = 0.9

    Pr(HPD) = Probability that HP Dumps Load = 0.8

    HPTransits to &

    HP HP HP

    from AO

    (HPT)

    (HPA) (HPS)

    (HPD)

    Pr(Mission Success) = Pr(HPA) x Pr(HPS) x Pr(HPT) x Pr(HPD)

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    Eg - HP Operational Capability

    Pr(HPA) = Probability that HP is Available = 0.7

    Pr(HPS) = Probability that HP Starts = 0.95 Pr(HPT) = Probability that HP Transits to AO = 0.9

    Pr(HPD) = Probability that HP Dumps Load = 0.8

    Pr(HPA)Pr(HPT) Pr(HPT)Pr(HPG) Pr(Mission Success)0.700 0.950 0.900 0.800 0.479

    .

    0.000

    Pr(Mission Success) = Pr(HPA) x Pr(HPS) x Pr(HPT) x Pr(HPD)= .

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    Eg - HP Operational Capability

    What if the probabilities of each event are increased?

    What is the impact on the mission success ?

    Pr(HPA) = Probability that HP is Available from 0.7 to 0.8 Pr(HPS) = Probability that HP Starts from 0.95 to 0.975 Pr HPT = Probabilit that HP Transits from 0.9 to 0.95

    Pr(HPD) = Probability that HP Dumps from 0.8 to 0.9

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    Eg - HP Operational Capability

    Pr(HPA) = Probability that HP is Available = 0.8

    Pr(HPS) = Probability that HP Starts = 0.975 Pr(HPT) = Probability that HP Transits = 0.95

    Pr(HPD) = Probability that HP Dumps = 0.9

    Pr(HPA)Pr(HPT) Pr(HPT)Pr(HPG) Pr(Mission Success)0.700 0.950 0.900 0.800 0.479

    . . . . .

    0.000

    Pr(Mission Success) = Pr(HPA) x Pr(HPS) x Pr(HPT) x Pr(HPD)= .

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    Eg - HP Operational Capability

    Case 1 - 47.9% of missions succeed

    Case 2 - 66.7% of missions succeed

    Pr(HPA)Pr(HPT) Pr(HPT)Pr(HPG) Pr(Mission Success)0.700 0.950 0.900 0.800 0.479

    . . . . .

    Increase in Capability 39.29%

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    Eg - HP Operational Capability

    Question?

    What is the effect of Improved Reliability and Maintainability on Cost and

    Data:

    Require Haul Packs for four (4) Mine Sites 12 HPs are re uired to be available er Mine Site

    Each HP costs $2 million

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    Eg - HP Operational Capability

    MTBF = 10 hours

    MTTR = 5 hours Inherent Availability = MTBF/(MTBF+MTTR)

    Inherent Availability of Each HP = 67%

    = = .

    Total Cost of Task Forces No of HPs x # per Mine Site x Unit Cost

    == $144M

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    Eg - HP Operational Capability

    MTBF = 20 hours (double original Baseline)

    MTTR = 5 hours (same as original Baseline) Inherent Availability of Each HP = 80%

    HPs required for each Mine Site = 12/ 0.8 = 15 Total Cost of Task Forces

    No of HPs x # per Mine Site x Unit Cost=15 x 4 x $2M= $120M

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    Eg - HP Operational Capability

    MTBF = 20 hours (double original Baseline)

    MTTR = 2.5 hours (half the original Baseline)

    Inherent Availability of Each HP = 88.8%

    HPs required for each Mine Site = 12/ 0.888 = 14

    No of HPs # per Mine Site x Unit Cost=14 x 4 x $2M= $112M

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    g - pera ona apa y

    Capability Cost Comparison

    Baseline

    System

    Case 1 Case 2

    MTBF hrs

    MTTR (hrs) 5 5 2.5Availability 67% 80% 88.8%

    Data

    Ca abilito o s

    $144M $120M $112MCOST($M)

    A $32M saving and this only includes procurement costs

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    Types of availability to be discussed

    Inherent availability, Ai

    Achieved availability, Aa

    , o

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    Different times for availabilit and downtime

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    What is time

    All approaches to availability are time related

    , OT=operating time per given total calendar time

    ST=standby time (not operating but assumed operable) TCMT=Total corrective maintenance time TPMT=TCMT=Total preventive maintenance time =

    Adapted from the Defence Reliability Management Course, 2/2005

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    Breakdown of downtime

    Supply delay: total delay time in

    components for the repair external factors,not art of the

    Maintenance delay: time spent waitingfor maintenance resources or facilities

    system

    Repair time: sum of the following

    Access time

    n erent repa rtime

    Diagnosis Repair or replacement

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    Factors influencing downtime

    Main factors are equipment design and maintenance

    Active repair is determined by the design

    philosophy

    Ke desi n areas: access ad ustment built-in testequipment, display & indicators, handling & ergonomics,

    Interchangeability, least replaceable assembly (LRA),mounting, redundancy, test points

    Maintenance strate ies

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    Some mathematical basics for availability

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    A note before we head on

    Some of the slides that follow in this topiccontain quite a few mathematic expressionsand formulas. These are intended from the

    author to be reference material for the easeof the participants

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    systems is working at time t

    The (average) interval or mission availability in the time

    atwor ngssystem tPt

    interval (t1, t2) is

    2

    )(1

    ),( 21t

    tav dttAttA

    which can be interpreted as the mean proportion of time in

    12

    .t1=0, t2=, we have

    0

    )()( dttAA av

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    v y The long run availability of system is

    0

    )(1

    lim dttAA av

    which can be interpreted as the average proportion of along period of time where the system is able to function

    The limiting or steady-state availability is , when the limitexists,lim tAt

    riodMission

    downtimeunplannedtotalmeandowntimeplannedtotalmean1

    opA

    av

    The operational availability is the mean proportion of amission period the system is able to perform its intended

    function

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    Long run average availability

    A failed item is replaced to an as good as new

    Up-times T1, T2, , Tn are independent and identicallydistributed (iid) with mean time to failure MTTF

    Down-times D , D , , D are inde endent andidentically distributed (iid) with mean downtime MDT

    ,

    MTTFTEAav

    )(

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    Inherent availability

    MTTF

    tAAinh )(lim

    Inherent availability is based solely on the failure distribution and-

    Equipment design parameter, based on which trade-offs betweenreliability and maintainability can be made

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    component

    Assuming constant failure rate (exponential timeo a ure an cons an repa r ra e exponen atime to repair), where =1/(MTTR)

    Steady-state availability MTTRMTTFA

    Instantaneous availability teA )(

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    ome most common y app e ava a tymeasures

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    If we are only concerned with correctivemaintenance

    Adapted from the Defence Reliability Management Course, 2/2005

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    Inherent availabilit

    Ai is availability when we are only concerned with

    ,maintenance, no administrative & logistic delay time

    TCMOTA

    MTTRMTBFA

    ii

    timeofin termsor

    where OT=operating time, TCM=total correctivemaintenance

    Ai is primarily a function of design

    Adapted from the Defence Reliability Management Course, 2/2005

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    Exam le of inherent s stem availabilit

    Assume the system had been running for two yearsan you a een mon or ng e a ures.

    If you had 20 failures the MTBF would be?

    What would the Inherent Availability be if the meantime to repair was 4 hours?

    MTBF

    TTRMTBFinh inh ____

    Reproduced with courtesy from Mark Mackenzie

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    If we are concerned with both corrective andreventive maintenance

    Adapted from the Defence Reliability Management Course, 2/2005

    A hi d il bili

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    Achieved availability

    Aa is availability when we are concerned with both,

    logistic delay time

    TPMTCMOTA

    MMTMTBMA aa

    timeofin termsor

    where MTBM=mean time between maintenance MMT=mean maintenance time OT=operating time,

    TPM=total preventive maintenance

    A is now both a function of desi n and reventivemaintenance (may also be partly a function of design)

    Adapted from the Defence Reliability Management Course, 2/2005

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    Example of achieved availability

    A generator runs non-stop for 3 months and fails 3 times.

    =once which takes 5 hrs.

    e ac eve ava a y s

    24313 OT.

    52524313

    TPMTCMOTa

    Adapted from the Defence Reliability Management Course, 2/2005

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    Is more frequent preventive maintenancer f r v il ili ?

    C.E. Ebeling (1997), Introduction to reliability and maintainability engineering, McGraw-Hill, Boston

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    administration and logistics

    Adapted from the Defence Reliability Management Course, 2/2005

    Ope ational a ailabilit

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    Operational availability

    Ao is availability when we are concerned with corrective& preventive maintenance, also administrative & logisticdelay time

    timeofin termsorMALDTMMTMTBM

    Ao

    OT

    where MTBM=mean time between maintenance

    TALDTTPMTCMOT

    o

    MMT=mean maintenance time MALDT,TALDT = mean/total adm. and logistic delay time

    , TCM, TPM=total corrective/preventive maintenance

    organisational effectivenessAdapted from the Defence Reliability Management Course, 2/2005

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    What do the factors mean for operationalavailabilit

    What can we do about each of these?

    Adapted from the Defence Reliability Management Course, 2/2005

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    What about the administrative logistics down time, a e ea me or pump par s was one

    week? mean down time (MDT) = 172hrs

    What if there was preventative maintenance orscheduled maintenance? MTBM = 504hrs

    MTBM

    MDTMTBMo o ____

    Reproduced with courtesy from Mark Mackenzie

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    Most common approaches

    RBD

    FTA

    Flow networks

    Petri Nets

    on e ar o s mu a on

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    Series systems

    Assuming constant failure

    rate (exponential time to

    R1 R2

    failure) and constant repairrate (exponential time to

    =

    Steady-state availability 21122121

    21

    A

    Generally for n components n

    iA

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    Parallel systems

    Assuming constant failure

    rate (exponential time to

    R1

    failure) and constant repairrate (exponential time to

    =

    R2

    Steady-state availability *) 22 22

    2

    A

    Generally for n components n

    iA 1

    * 1 2 . , . .

    team is assumed

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    Standby systems Unit 1

    Assuming constant failure

    rate (exponential time to

    Sensor

    failure) and constant repairrate (exponential time to

    =

    Unit 2

    Steady-state availability *) 22

    A

    * 1 2 .

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    - - - Unit 1 Assuming constant failure

    rate (exponential time to Unit 2

    rate (exponential time torepair), where =1/(MTTR) Unit 3

    Steady-state availability *),

    e.g. n=3, k=23223

    223

    63 A

    k1 For general n and k ini

    in i

    A

    0)(

    1

    *) Assuming 1= 2 = 3 = .

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    Example: ship missile system

    .

    Q: find steady-state availability of the system excluding themissiles and disregard switching failure

    Exam le: shi missile s stem

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    Exam le: shi missile s stem

    A: Availability of the radar system is

    999996.0

    001.05.05.0

    22

    2

    22

    2

    radarA

    The availabilit of the launch and uidance s stem

    ....

    9974.00013.05.0

    5.0

    LGA

    The system availability is

    ... LGradarsys

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    Monte Carlo simulation

    Benefits

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    Benefits

    The designer can be confident that the system hasspec e re a ty or t e r t o componentcharacteristics, provided all the analytical results are

    It is suitable for computerized design;

    Any probability distribution is simulated;

    No complex mathematical treatments are needed.

    An advantage with Monte Carlo simulation is that theevents in the RBD do not have to be combinedanalytically since the simulation itself takes into account

    whether each block is failed or functional

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    Key elements

    Identification of the probability distribution for each

    Identification of random variable generation for designparame ers ase on e g ven pro a y s r u on y

    computer;

    Identification of the probability distribution, its mean andvariance of system performance by simulation.

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    Limitations

    Mathematical models for simulation are required;

    All the system components need to be included inorder to obtain reasonable analytical results;

    A large number of replicas of the system aresimulated.

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    Example:

    repair logicfor a typicalsystem

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    Simulation results of depot stock levels

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    A type of state-space analysis technique

    probability of state transitions from failed state too eratin state and vice versa

    A component in a system is assumed to be in either

    Probability of failure and of returning to an available state

    are o n eres s

    Particularly useful to maintained systems for which RBDcan be not directly applicable

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    Example (1-out-of-2 active redundantsys em 11 5

    When the two componentsare identical

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    The solution

    The

    availability, A S0 (t) is

    The unavailabilitfor some specificand is shown

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    SUMMARY

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    Inherent

    Achieved