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IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 91
AVAILABILITY ANALYSIS OF PARALLEL TRANSIT FUEL SYSTEM
IN PETROL ENGINE UNDER HEAD OF LINE REPAIR
Reena Garg1
1
Assistant Professor Mathematics, YMCA University of Science & Technology, Faridabad 121006
Abstract
In this paper, the author has considered a fuel system in petrol engine with one alternative fuel source (like LPG, CNG etc.)
keeping in standby arrangement and followed online through a perfect switching device. The whole system can fail due to either
its normal working or human error. All the failures follow exponential time distribution where as all repairs follow general time
distribution.
Keywords: Fuel system, standby, exponential time distribution, general time distribution.
--------------------------------------------------------------------***------------------------------------------------------------------
1. INTRODUCTION
In this paper, the considered fuel system consists of three
subsystems, namely A, B and C, connected in series.
Subsystem A is fuel source having two units in standby
redundancy. Subsystem B consists of two units (Transfer
pump and carburetor) connected in series while subsystem C
having N-cylinders [identical] in series and is of j-out-of-
N:G nature, fig-1 shows the system configuration. Head-of-
line policy is being adopted for repair purpose. The concept
of human-error is also incorporated to make the model more
compatible. Laplace transform of various state probabilities,
availability and long run availability, some particular cases
and profit function for the system are obtained. Fig-2 shows
the state-transition diagram and states descriptions have
mentioned in table-1.
By using supplementary variables technique and Laplace
transform, various reliability parameters have been obtained.
One numerical example together with graphical illustration
has also been given at the end to highlight important results
of the study.
Table-1: States Description
STATE SUBSYSTEM SYSTEM’S
STATE
SUPPLEMENTARY
VARIABLE USEDA B C
S1 0 0 0 0 Nil
S2 0 F 0 F u
S3 0 0 (N-j)0 0 Nil
S4 0 0 F F v
S5 1F 0 (N-j)0 0 Nil
S6 1F F (N-j)0 F y
S7 0 F (N-j)0 F u
S8 1F 0 0 0 Nil
S9 1F F 0 F y
S10 FH FH FH FH m
S11 F 0 0 F n
S12 F 0 (N-j)0 F r
O: All Operable; F : all Failed; FH : failure due to human-error; rF :r units have failed; rO : r units are operable.
2. ASSUMPTIONS
The following assumptions have been associated with this
model:
1. Initially, all the units are new and the system is in
good condition of full efficiency.
2. Repair has given only when the system is in failed
condition and a single service channel is available.
3. After repair, system works like a new one and never
damages anything.
4. 1-A unit is a petrol tank while 2-A unit is an
alternative fuel source (like CNG, LPG etc.) and the
perfect switching device has been used to online the
standby unit.
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 92
3. NOTATIONS
The following notations have been used throughout the
model:
)(tPK
: The probability that at time t, the system
is operable and is in Kth
state, where
K=1, 3, 5, 8.
),( tsPK
: The probability that at time t, the system
is in rth failed state and elapsed repair
time lies in the interval (s, s + Δ).
K=2, 4, 6, 7, 9, 10, 11, 12 and s=u, v, y,
u, y, m, n, r respectively.
21 /bb : Constant failure rate of 1B/2B unit and
note that b1+b2=b (say).
a/c : Constant failure rate of any unit of
subsystem A/C.
H : Human-error rate.
)(sK : The probability that the subsystem K
will be repaired in the time interval
(s,s+Δ) conditioned that it was not
repaired up to time s, where K=A, B, C
and s=u, v, y, n, r.
)(mh : The probability that the system will be
repaired from state S10 in time interval
(m, m+Δ) conditioned that it was not
repaired up to time m.
)(xSi
:
 dxxx ii )(-.exp)(
0
 

kM :
Mean time to repair kth
unit ),0(

 kS
for all k.
P : Time independent probability.
)(sDk
:   ssSK /)(1 , for all k =A,B and C.
Fig-1: System configuration
Fig-2: State-transition diagram
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 93
4. FORMULATION OF THE MATHEMATICAL
MODEL
Using continuity argument, we obtain the following set of
difference-differential equations governing the behavior of
the system under consideration:






 )()( 1 tPhcjNba
dt
d


0
2 )(),( duutuP B
 dtPdmmtmP ch 


0
4
0
10 )(),()(),(
…(1)
0),()( 2 











tuPu
tu
B
…(2)
 








0
713 )(,)()()( duutuPtcPjNtPabcj
dt
d
B
…(3)
0),()( 4 











tP
t
c 

…(4)
)()( 35 taPtPba
dt
d







…(5)
0),()( 6 











tyPy
ty
A
…(6)
0),()( 7 











tuPy
tu
B
…(7)









0
1118 )(),()()( dnntnPtaPtPba
dt
d
A
…(8)
0),()( 9 











tyPy
ty
A
…(9)
0),()( 10 











tmPm
tm
h
…(10)
0),()( 11 











tnPn
tn
A
…(11)
0),()( 12 











trPr
tr
c
…(12)
Boundary conditions are:
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 94



0
912 )(),()(),0( dyytyPtbPtP A
…(13)
)(),0( 34 tcjPtP 
…(14)
)(),0( 56 tbPtP 
…(15)
)(),0( 37 tbPtP 
…(16)
)(),0( 89 tbPtP 
…(17)
)(),0( 110 thPtP 
…(18)
drrtrPtaPtP c )(),()(),0( 12
0
811 


…(19)
)(),0( 512 taPtP 
…(20)
Initial conditions are:
,1)0(1 P otherwise zero.
…(21)
5. SOLUTION OF THE MODEL
Taking Laplace transforms of equations (1) through (20) by
making use of (21) and then on solving them, we have
following Laplace transforms of different state probabilities:
)(
1
)(1
sA
sP  …(22)
)()()(
)(
)(
)(
1
)(1
)(
)(2 sDsSsS
sB
sC
bas
a
sB
sSa
sA
b
sP BAcA 













…(23)
)(
)(
)(3
sA
sC
sP 
…(24)
 sD
sA
sC
cjsP c
)(
)(
)(4 
…(25)
)(
)(
)(5
sA
sC
bas
a
sP


…(26)
)(
)(
)(
)(6 sD
sA
sC
bas
ab
sP A


…(27)
…(28)
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 95
 sD
sA
sC
bsP B
)(
)(
)(7 
 






 sSsS
sA
sC
bas
a
sBsA
a
sP Ac )(
)(
)(
)(
1
)(
)(8 …(29)
 sDsPbsP A)()( 89  …(30)
 sD
sA
h
sP h
)(
)(10 
…(31)
 sDsS
sA
sC
bas
a
sPasP Ac 






 )(
)(
)(
)()( 811
…(32)
)(
)(
)(
)(
2
12 sD
sA
sC
bas
a
sP c


…(33)
where,   sSabssB A 1)(
 )(1
)(
)(
sSbcjas
cjN
sC
B


…(34)
…(35)
and   )()()()(1)()( sSbsCsScjsShcjNbassA Bch 







 )()(
)(
)(
)(
1
)()( sSsS
sB
sC
bas
a
sB
sSsSab AcBA
…(36)
6. ERGODIC BEHAVIOUR OF THE SYSTEM
By making use of Abel‟s Lemma viz.,
)()(lim)(lim
0
sayFtFsFs
ts


, provided the limit on
right exists, we have the following time independent state
probabilities from equations (22) through (33):
)0(
1
1
A
P


…(37)
BM
ba
aH
ab
A
P 














 1
)0(
1
2
…(38)
)0(
3
A
H
P


…(39)
cM
A
cjH
P
)0(
4


…(40)
)0(
1
5
Aba
aH
P




…(41)
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 96
  AM
Aba
abH
P
)0(
6


…(42)
BM
A
bH
P
)0(
7


…(43)










ba
aH
Ab
a
P 1
)0(
8
…(44)
AM
ba
aH
A
a
P 








 1
)0(
9
…(45)
hM
A
h
P
)0(
10


…(46)
  AMH
Ab
a
P 

 1
)0(
2
11
…(47)
  cM
Aba
Ha
P
)0(
2
12


…(48)
where,
 
cja
cjN
H


 ; and    
0
0








s
sA
ds
d
A …(49)
6. SOME PARTICULAR CASES
6.1 When Repairs Follow Exponential Time Distribution:
Setting  AAA ssS   /)( etc. in equations (22) through (33), we obtained:
)(
1
)(1
sE
sP 
…(50)
BA
A
c
c
A
A
ssssF
sG
bas
a
sFs
a
sE
b
sP

























1
)(
)(
)(
1
1
)(
)(2
…(51)
)(
)(
)(3
sE
sG
sP 
…(52)
cssE
sG
cjsP


1
)(
)(
)(4
…(53)
)(
)(
)(5
sE
sG
bas
a
sP


…(54)
AssE
sG
bas
ab
sP


1
)(
)(
)(6
…(55)
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 97
BssE
sG
bsP


1
)(
)(
)(7 …(56)








A
A
c
c
sssF
sG
bas
a
sFsE
a
sP




)(
)(
)(
1
)(
)(8
…(57)
As
sPbsP


1
)()( 89
…(58)
hssE
h
sP


1
)(
)(10
…(59)
Ac
c
sssE
sG
bas
a
sPasP











1
)(
)(
)()( 811
…(60)
cssE
sG
bas
a
sP


1
)(
)(
)(
2
12
…(61)
where,
As
as
bssF

)( ;
Bs
bs
cjas
cjN
sG




)(
)( …(62)
and
B
B
c
c
h s
b
sG
s
cj
s
hs
cjNbassE




 




 )()()(
     









Ac
Ac
BA
BA
sssF
sG
bas
a
sFss
ab




)(
)(
)(
1
…(63)
6.2 Availability and Cost Function for the System :
Now, Laplace transform of availability of petrol engine is given by:
  












bas
a
bcjas
cjN
hcjNbas
sPup
)(
1
)(
1 …(64)
on inverting this, one can obtain the availability at any time „t‟ as under
     tbatbcjathcjNba
up SeQetP 
 Re)( )(
where
hcjN
a
hcjN
cjN
Q





)()2(
)(
1 ;
hcjN
a
hcjN
cjN
R





)(
Sand
)2(
)(
…(65)
…(66)
…(67)
Note that   10 upP
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 98
Also, Profit function for the system, working up to the time t, is given by
    3
0
21 CtCdttPCtK
t
up  
…(68)
where,
  tP
t
up
0
     
ba
e
S
bcja
e
R
hcjNba
e
Q
tbatbcjathcjNba







 
11
)(
1 )( …(69)
where, C1 ,C2 and C3 are the revenue, repair and
establishment cost per unit time respectively also Q ,R and
S are given in the equations (66)and (67).
6.3 Steady- State Availability
The steady state availability of the system is given by
  
  hcjNbacjab
baNca
AVSS



)(
(70)
Where,   cjacjNH  / (71)
6.4 Numerical Computation
For a numerical computation, let us consider the values:
N=5, j=2, a=0.01, b=0.02, c=0.03, h=0.001, C1=Rs.5.00,
C2=Re1.00 and C3 =Rs2.00.
Also t= 0, 1, 2,-----------10 and h=0.001,0.0015, 0.002--------
--- 0.01.
Table-2
Fig-3
Table-3
0
0.2
0.4
0.6
0.8
1
0 1 2 3 4 5 6 7 8 9 10
Pup(t)-->
t-->
Availability Vs Time
Time Availability
0 1
1 0.976302
2 0.94806
3 0.916399
4 0.882266
5 0.846451
6 0.809611
7 0.772289
8 0.734929
9 0.697892
10 0.661467
11 0.625883
12 0.591317
13 0.557903
14 0.525739
15 0.494891
Time Profit Function
0 -2
1 -0.03425
2 1.853275
3 3.650692
4 5.349202
5 6.942611
6 8.426888
7 9.799798
8 11.06059
9 12.2097
10 13.24855
11 14.17934
12 15.00487
13 15.7284
14 16.35354
15 16.88414
16 17.32424
17 17.67793
18 17.94936
19 18.14267
20 18.26195
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 99
Fig-4
Table-4
Fig-5
7. CONCLUSIONS
The plots of equations (65), (68) and (70) have shown in
figs-(3), (4) and (5), respectively.
Fig-3 shows that availability of the system decreases slowly
with time initially but there after it decreases approximately
in a constant manner.
Fig-4 shows that profit with the system under consideration.
For t=0 and 1, there is no profit but after this profit increases
in constant way.
Fig-5 shows long run availability of the system. Its value is
0.283353. Now as we increase the value of h, the long run
availability decreases correspondingly.
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Refrigeration and Air-Conditioning”, Dhanpat Rai &
Co. (P) Ltd., 2006.
[2] Billinton, R.; Allan, R.: “Reliability Evaluation of
Power Systems”, Springer Publication, 1996.
[3] Billinton, R.; Allan, R.: “Reliability Evaluation of
Engineering Systems: Concepts and Techniques",
Springer Publication, 1992.
[4] Capasso, V.; Bakstein, D.: “An Introduction to
Continuous-time Stochastic Processes: Theory,
Models and Applications", Birkhauser Publication,
2004.
[5] Culp, W. Archie: “Principles of Energy
Conversion”, McGraw Hill Book Company, New
York, 2000.
[6] Dhillon, B.S.: “Design Reliability”, CRC Press,
1999.
[7] Dhillon, B.S.: “Reliability, Quality and Safety
Engineers”, Taylor Francis, 2004.
[8] Gopal, M.: "Modern Control System Theory", New
Age International (P) Ltd., Publishers, India, 2004.
[9] Heyman, D.P.; Sobel, M.J.: “Stochastic Models in
Operations Research: Stochastic Processes and
Operating Characteristics”, Dover Publication, 2003.
[10] Kuo, W.; Zuo, M.J.: “Optimal Reliability Modeling:
Principles and Applications”, John Wiley & Sons.,
2002.
[11] Linkov, L.N.: "Asymptotic Statistical Methods for
Stochastic Processes", American Mathematical
Society, 2001.
[12] Nikolaidis , E.; Ghiocel , D.M. ; Singhal , S. :
"Engineering Design Reliability Handbook", CRC
Press, 2004.
Research Papers
[1] Agrafotis, G.S.; Tsoukalas, M. Z.: "Reliability
Analysis and Optimization Applications of a Two
Unit Standby Redundant System with Spare Units",
Microelectronic Reliab. , Vol. 34 (5), pp 1469 –
1476, 1994.
-5
0
5
10
15
0 1 2 3 4 5 6 7 8 9 10
K(t)-->
t-->
Profit Function Vs Time
0
0.2
0.4
0.6
0.8
1
Avss-->
H-->
Steady- state availability
Vs H
h A VSS
0.001 0.283353
0.0015 0.282187
0.002 0.28103
0.0025 0.279883
0.003 0.278746
0.0035 0.277617
0.004 0.276498
0.0045 0.275387
0.005 0.274286
0.0055 0.273193
0.006 0.272109
0.0065 0.271033
0.007 0.269966
0.0075 0.268908
0.008 0.267857
0.0085 0.266815
0.009 0.265781
0.0095 0.264755
0.01 0.263736
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 100
[2] Agnihotri, R.R.; Satsangi, S. K.: "Two Non-identical
Unit System with Priority Based Repair and
Inspection", Microelectronic Reliab. , Vol. 36 (2) ,
pp 279 – 282, 1996.
[3] Cassady, C.R.; Lyoob, I.M.; Schneider, K.; Pohi, E.
A.: "A Generic Model of Equipment Availability
under Imperfect Maintenance”, IEEE TR on
Reliability, Vol.54, issue - 4, pp 564 – 571, 2005.
[4] Chung, W.K.: “Reliability Analysis of a Repairable
Parallel System with Standby Involving
Human Error and Common Cause Failure”,
Microelectronic Reliab. , Vol.27, pp 269-274, 1987.
[5] Chung, W.K.: “Reliability Analysis of a Series
System with Repair", Microelectronic Reliab. ,
Vol.31, pp 363-365, 1991.
[6] Chung, W. K.: "A k-out -of n: G Redundant System
with the Presence of Chance with Multiple Critical
Errors”, Microelectronic Reliab. , Vol. 33, pp
334-338, 1993.
[7] Chung, W. K.: " Reliability Analysis of a k-out -of
n: G Redundant System in the Presence of Chance
with Multiple Critical Errors", Microelectronic
Reliab. , Vol. 32, pp 331 – 334, 1993.
[8] Cluzeau, T.; Keller, J.; Schneeweiss, W.: “An
Efficient Algorithm for Computing the Reliability of
Consecutive-k-out-of-n:F Systems”, IEEE TR. on
Reliability, Vol.57 (1), PP 84-87, 2008.
[9] Dhillon, B. S.; Vishvanath, H. C.: "Reliability
Analysis of Non - identical Units Parallel System
with Common Cause Failure", Microelectronic
Reliab., Vol. 31, pp 429 – 441, 1991.
[10] Dhillon, B. S. and Yang N. J.: "Stochastic Analysis
of Standby System with Common Cause Failure and
Human Error”, Microelectronic Reliab. , Vol. 32, pp
1699 – 1712, 1992.

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Availability analysis of parallel transit fuel system in petrol engine under head of line repair

  • 1. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 91 AVAILABILITY ANALYSIS OF PARALLEL TRANSIT FUEL SYSTEM IN PETROL ENGINE UNDER HEAD OF LINE REPAIR Reena Garg1 1 Assistant Professor Mathematics, YMCA University of Science & Technology, Faridabad 121006 Abstract In this paper, the author has considered a fuel system in petrol engine with one alternative fuel source (like LPG, CNG etc.) keeping in standby arrangement and followed online through a perfect switching device. The whole system can fail due to either its normal working or human error. All the failures follow exponential time distribution where as all repairs follow general time distribution. Keywords: Fuel system, standby, exponential time distribution, general time distribution. --------------------------------------------------------------------***------------------------------------------------------------------ 1. INTRODUCTION In this paper, the considered fuel system consists of three subsystems, namely A, B and C, connected in series. Subsystem A is fuel source having two units in standby redundancy. Subsystem B consists of two units (Transfer pump and carburetor) connected in series while subsystem C having N-cylinders [identical] in series and is of j-out-of- N:G nature, fig-1 shows the system configuration. Head-of- line policy is being adopted for repair purpose. The concept of human-error is also incorporated to make the model more compatible. Laplace transform of various state probabilities, availability and long run availability, some particular cases and profit function for the system are obtained. Fig-2 shows the state-transition diagram and states descriptions have mentioned in table-1. By using supplementary variables technique and Laplace transform, various reliability parameters have been obtained. One numerical example together with graphical illustration has also been given at the end to highlight important results of the study. Table-1: States Description STATE SUBSYSTEM SYSTEM’S STATE SUPPLEMENTARY VARIABLE USEDA B C S1 0 0 0 0 Nil S2 0 F 0 F u S3 0 0 (N-j)0 0 Nil S4 0 0 F F v S5 1F 0 (N-j)0 0 Nil S6 1F F (N-j)0 F y S7 0 F (N-j)0 F u S8 1F 0 0 0 Nil S9 1F F 0 F y S10 FH FH FH FH m S11 F 0 0 F n S12 F 0 (N-j)0 F r O: All Operable; F : all Failed; FH : failure due to human-error; rF :r units have failed; rO : r units are operable. 2. ASSUMPTIONS The following assumptions have been associated with this model: 1. Initially, all the units are new and the system is in good condition of full efficiency. 2. Repair has given only when the system is in failed condition and a single service channel is available. 3. After repair, system works like a new one and never damages anything. 4. 1-A unit is a petrol tank while 2-A unit is an alternative fuel source (like CNG, LPG etc.) and the perfect switching device has been used to online the standby unit.
  • 2. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 92 3. NOTATIONS The following notations have been used throughout the model: )(tPK : The probability that at time t, the system is operable and is in Kth state, where K=1, 3, 5, 8. ),( tsPK : The probability that at time t, the system is in rth failed state and elapsed repair time lies in the interval (s, s + Δ). K=2, 4, 6, 7, 9, 10, 11, 12 and s=u, v, y, u, y, m, n, r respectively. 21 /bb : Constant failure rate of 1B/2B unit and note that b1+b2=b (say). a/c : Constant failure rate of any unit of subsystem A/C. H : Human-error rate. )(sK : The probability that the subsystem K will be repaired in the time interval (s,s+Δ) conditioned that it was not repaired up to time s, where K=A, B, C and s=u, v, y, n, r. )(mh : The probability that the system will be repaired from state S10 in time interval (m, m+Δ) conditioned that it was not repaired up to time m. )(xSi :  dxxx ii )(-.exp)( 0    kM : Mean time to repair kth unit ),0(   kS for all k. P : Time independent probability. )(sDk :   ssSK /)(1 , for all k =A,B and C. Fig-1: System configuration Fig-2: State-transition diagram
  • 3. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 93 4. FORMULATION OF THE MATHEMATICAL MODEL Using continuity argument, we obtain the following set of difference-differential equations governing the behavior of the system under consideration:        )()( 1 tPhcjNba dt d   0 2 )(),( duutuP B  dtPdmmtmP ch    0 4 0 10 )(),()(),( …(1) 0),()( 2             tuPu tu B …(2)           0 713 )(,)()()( duutuPtcPjNtPabcj dt d B …(3) 0),()( 4             tP t c   …(4) )()( 35 taPtPba dt d        …(5) 0),()( 6             tyPy ty A …(6) 0),()( 7             tuPy tu B …(7)          0 1118 )(),()()( dnntnPtaPtPba dt d A …(8) 0),()( 9             tyPy ty A …(9) 0),()( 10             tmPm tm h …(10) 0),()( 11             tnPn tn A …(11) 0),()( 12             trPr tr c …(12) Boundary conditions are:
  • 4. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 94    0 912 )(),()(),0( dyytyPtbPtP A …(13) )(),0( 34 tcjPtP  …(14) )(),0( 56 tbPtP  …(15) )(),0( 37 tbPtP  …(16) )(),0( 89 tbPtP  …(17) )(),0( 110 thPtP  …(18) drrtrPtaPtP c )(),()(),0( 12 0 811    …(19) )(),0( 512 taPtP  …(20) Initial conditions are: ,1)0(1 P otherwise zero. …(21) 5. SOLUTION OF THE MODEL Taking Laplace transforms of equations (1) through (20) by making use of (21) and then on solving them, we have following Laplace transforms of different state probabilities: )( 1 )(1 sA sP  …(22) )()()( )( )( )( 1 )(1 )( )(2 sDsSsS sB sC bas a sB sSa sA b sP BAcA               …(23) )( )( )(3 sA sC sP  …(24)  sD sA sC cjsP c )( )( )(4  …(25) )( )( )(5 sA sC bas a sP   …(26) )( )( )( )(6 sD sA sC bas ab sP A   …(27) …(28)
  • 5. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 95  sD sA sC bsP B )( )( )(7           sSsS sA sC bas a sBsA a sP Ac )( )( )( )( 1 )( )(8 …(29)  sDsPbsP A)()( 89  …(30)  sD sA h sP h )( )(10  …(31)  sDsS sA sC bas a sPasP Ac         )( )( )( )()( 811 …(32) )( )( )( )( 2 12 sD sA sC bas a sP c   …(33) where,   sSabssB A 1)(  )(1 )( )( sSbcjas cjN sC B   …(34) …(35) and   )()()()(1)()( sSbsCsScjsShcjNbassA Bch          )()( )( )( )( 1 )()( sSsS sB sC bas a sB sSsSab AcBA …(36) 6. ERGODIC BEHAVIOUR OF THE SYSTEM By making use of Abel‟s Lemma viz., )()(lim)(lim 0 sayFtFsFs ts   , provided the limit on right exists, we have the following time independent state probabilities from equations (22) through (33): )0( 1 1 A P   …(37) BM ba aH ab A P                 1 )0( 1 2 …(38) )0( 3 A H P   …(39) cM A cjH P )0( 4   …(40) )0( 1 5 Aba aH P     …(41)
  • 6. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 96   AM Aba abH P )0( 6   …(42) BM A bH P )0( 7   …(43)           ba aH Ab a P 1 )0( 8 …(44) AM ba aH A a P           1 )0( 9 …(45) hM A h P )0( 10   …(46)   AMH Ab a P    1 )0( 2 11 …(47)   cM Aba Ha P )0( 2 12   …(48) where,   cja cjN H    ; and     0 0         s sA ds d A …(49) 6. SOME PARTICULAR CASES 6.1 When Repairs Follow Exponential Time Distribution: Setting  AAA ssS   /)( etc. in equations (22) through (33), we obtained: )( 1 )(1 sE sP  …(50) BA A c c A A ssssF sG bas a sFs a sE b sP                          1 )( )( )( 1 1 )( )(2 …(51) )( )( )(3 sE sG sP  …(52) cssE sG cjsP   1 )( )( )(4 …(53) )( )( )(5 sE sG bas a sP   …(54) AssE sG bas ab sP   1 )( )( )(6 …(55)
  • 7. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 97 BssE sG bsP   1 )( )( )(7 …(56)         A A c c sssF sG bas a sFsE a sP     )( )( )( 1 )( )(8 …(57) As sPbsP   1 )()( 89 …(58) hssE h sP   1 )( )(10 …(59) Ac c sssE sG bas a sPasP            1 )( )( )()( 811 …(60) cssE sG bas a sP   1 )( )( )( 2 12 …(61) where, As as bssF  )( ; Bs bs cjas cjN sG     )( )( …(62) and B B c c h s b sG s cj s hs cjNbassE            )()()(                Ac Ac BA BA sssF sG bas a sFss ab     )( )( )( 1 …(63) 6.2 Availability and Cost Function for the System : Now, Laplace transform of availability of petrol engine is given by:                bas a bcjas cjN hcjNbas sPup )( 1 )( 1 …(64) on inverting this, one can obtain the availability at any time „t‟ as under      tbatbcjathcjNba up SeQetP   Re)( )( where hcjN a hcjN cjN Q      )()2( )( 1 ; hcjN a hcjN cjN R      )( Sand )2( )( …(65) …(66) …(67) Note that   10 upP
  • 8. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 98 Also, Profit function for the system, working up to the time t, is given by     3 0 21 CtCdttPCtK t up   …(68) where,   tP t up 0       ba e S bcja e R hcjNba e Q tbatbcjathcjNba          11 )( 1 )( …(69) where, C1 ,C2 and C3 are the revenue, repair and establishment cost per unit time respectively also Q ,R and S are given in the equations (66)and (67). 6.3 Steady- State Availability The steady state availability of the system is given by      hcjNbacjab baNca AVSS    )( (70) Where,   cjacjNH  / (71) 6.4 Numerical Computation For a numerical computation, let us consider the values: N=5, j=2, a=0.01, b=0.02, c=0.03, h=0.001, C1=Rs.5.00, C2=Re1.00 and C3 =Rs2.00. Also t= 0, 1, 2,-----------10 and h=0.001,0.0015, 0.002-------- --- 0.01. Table-2 Fig-3 Table-3 0 0.2 0.4 0.6 0.8 1 0 1 2 3 4 5 6 7 8 9 10 Pup(t)--> t--> Availability Vs Time Time Availability 0 1 1 0.976302 2 0.94806 3 0.916399 4 0.882266 5 0.846451 6 0.809611 7 0.772289 8 0.734929 9 0.697892 10 0.661467 11 0.625883 12 0.591317 13 0.557903 14 0.525739 15 0.494891 Time Profit Function 0 -2 1 -0.03425 2 1.853275 3 3.650692 4 5.349202 5 6.942611 6 8.426888 7 9.799798 8 11.06059 9 12.2097 10 13.24855 11 14.17934 12 15.00487 13 15.7284 14 16.35354 15 16.88414 16 17.32424 17 17.67793 18 17.94936 19 18.14267 20 18.26195
  • 9. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 99 Fig-4 Table-4 Fig-5 7. CONCLUSIONS The plots of equations (65), (68) and (70) have shown in figs-(3), (4) and (5), respectively. Fig-3 shows that availability of the system decreases slowly with time initially but there after it decreases approximately in a constant manner. Fig-4 shows that profit with the system under consideration. For t=0 and 1, there is no profit but after this profit increases in constant way. Fig-5 shows long run availability of the system. Its value is 0.283353. Now as we increase the value of h, the long run availability decreases correspondingly. REFERENCES [1] Arora, S.C.; Domkundwar, S.: “A Course in Refrigeration and Air-Conditioning”, Dhanpat Rai & Co. (P) Ltd., 2006. [2] Billinton, R.; Allan, R.: “Reliability Evaluation of Power Systems”, Springer Publication, 1996. [3] Billinton, R.; Allan, R.: “Reliability Evaluation of Engineering Systems: Concepts and Techniques", Springer Publication, 1992. [4] Capasso, V.; Bakstein, D.: “An Introduction to Continuous-time Stochastic Processes: Theory, Models and Applications", Birkhauser Publication, 2004. [5] Culp, W. Archie: “Principles of Energy Conversion”, McGraw Hill Book Company, New York, 2000. [6] Dhillon, B.S.: “Design Reliability”, CRC Press, 1999. [7] Dhillon, B.S.: “Reliability, Quality and Safety Engineers”, Taylor Francis, 2004. [8] Gopal, M.: "Modern Control System Theory", New Age International (P) Ltd., Publishers, India, 2004. [9] Heyman, D.P.; Sobel, M.J.: “Stochastic Models in Operations Research: Stochastic Processes and Operating Characteristics”, Dover Publication, 2003. [10] Kuo, W.; Zuo, M.J.: “Optimal Reliability Modeling: Principles and Applications”, John Wiley & Sons., 2002. [11] Linkov, L.N.: "Asymptotic Statistical Methods for Stochastic Processes", American Mathematical Society, 2001. [12] Nikolaidis , E.; Ghiocel , D.M. ; Singhal , S. : "Engineering Design Reliability Handbook", CRC Press, 2004. Research Papers [1] Agrafotis, G.S.; Tsoukalas, M. Z.: "Reliability Analysis and Optimization Applications of a Two Unit Standby Redundant System with Spare Units", Microelectronic Reliab. , Vol. 34 (5), pp 1469 – 1476, 1994. -5 0 5 10 15 0 1 2 3 4 5 6 7 8 9 10 K(t)--> t--> Profit Function Vs Time 0 0.2 0.4 0.6 0.8 1 Avss--> H--> Steady- state availability Vs H h A VSS 0.001 0.283353 0.0015 0.282187 0.002 0.28103 0.0025 0.279883 0.003 0.278746 0.0035 0.277617 0.004 0.276498 0.0045 0.275387 0.005 0.274286 0.0055 0.273193 0.006 0.272109 0.0065 0.271033 0.007 0.269966 0.0075 0.268908 0.008 0.267857 0.0085 0.266815 0.009 0.265781 0.0095 0.264755 0.01 0.263736
  • 10. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 03 Issue: 09 | Sep-2014, Available @ http://www.ijret.org 100 [2] Agnihotri, R.R.; Satsangi, S. K.: "Two Non-identical Unit System with Priority Based Repair and Inspection", Microelectronic Reliab. , Vol. 36 (2) , pp 279 – 282, 1996. [3] Cassady, C.R.; Lyoob, I.M.; Schneider, K.; Pohi, E. A.: "A Generic Model of Equipment Availability under Imperfect Maintenance”, IEEE TR on Reliability, Vol.54, issue - 4, pp 564 – 571, 2005. [4] Chung, W.K.: “Reliability Analysis of a Repairable Parallel System with Standby Involving Human Error and Common Cause Failure”, Microelectronic Reliab. , Vol.27, pp 269-274, 1987. [5] Chung, W.K.: “Reliability Analysis of a Series System with Repair", Microelectronic Reliab. , Vol.31, pp 363-365, 1991. [6] Chung, W. K.: "A k-out -of n: G Redundant System with the Presence of Chance with Multiple Critical Errors”, Microelectronic Reliab. , Vol. 33, pp 334-338, 1993. [7] Chung, W. K.: " Reliability Analysis of a k-out -of n: G Redundant System in the Presence of Chance with Multiple Critical Errors", Microelectronic Reliab. , Vol. 32, pp 331 – 334, 1993. [8] Cluzeau, T.; Keller, J.; Schneeweiss, W.: “An Efficient Algorithm for Computing the Reliability of Consecutive-k-out-of-n:F Systems”, IEEE TR. on Reliability, Vol.57 (1), PP 84-87, 2008. [9] Dhillon, B. S.; Vishvanath, H. C.: "Reliability Analysis of Non - identical Units Parallel System with Common Cause Failure", Microelectronic Reliab., Vol. 31, pp 429 – 441, 1991. [10] Dhillon, B. S. and Yang N. J.: "Stochastic Analysis of Standby System with Common Cause Failure and Human Error”, Microelectronic Reliab. , Vol. 32, pp 1699 – 1712, 1992.