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8/12/2019 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