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8/17/2019 IPR - Leslie Thompson
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Inflow Performance
Relationship
IPR
by
Dr. Leslie Thompson
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Production System
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Fluid Production
• Path of produced fluids
– Reseroir
– Perforations! "rael pac#! etc.
– Downhole e$uipment! casin"! tubin".
• %i&in" with "as'lift "as
– (ellhead! production cho#es – Flow lines! manifolds
– Separator
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Fluid Production
• In each flow se"ment! the fluids interact
with the production components
– Pressure! temperature and flow elocityare altered.
– Fluid properties constantly chan"in".
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Pressure Losses
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Driin" Force
• The driin" force that moes fluids alon" the
reseroir and production system is the ener"y
stored in the form of compressed fluids in thereseroir.
– )s the fluids moe alon" the system components!
pressure drop occurs. The pressure in the
direction of flow continuously decreases from thereseroir pressure to the final downstream
pressure alue at the separator.
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IPR
• The flow of oil! "as and water from the
reseroir is characteri*ed by the Inflow
Performance relationship. – IPR is a measure of +Pressure losses, in the
formation.
• The functional relationship between flow rate
and bottomhole pressure is called IPR. – Indicator of well performance.
( ) ( ) p f p p f q wf ∆=−=
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Productiity Inde&
• %easure of the well-s capacity to
produce fluids from reseroir to
wellbore.• Definition Fluid production rate for / psi
pressure drop from reseroir to
wellbore.
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Productiity Inde&
( )
( ) ( )( )t pt pt q
PI wf −
=
PI Productiity Inde&! ST01d1psi
( )t p )era"e pressure in the well-s draina"e area! psi.
( )t pwf 0ottomhole flowin" pressure! psi
q(t ) Production rate! ST01d
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Parameters 2ontrollin" IPR or PI
• Roc# Properties – Permeability! Relatie permeability
• Fluid Properties – 0o! µo! 0w! µw! co! cw – 0"! µ"! *! c"
• Flow Re"ime in the Reseroir – Darcy Flow
– 3on'Darcy 4inertial! Forchheimer5 flow
• Phases Flowin" – Sin"le Phase 46il! 7as5
– Two Phases 4687! 68(! 78(5
– Three Phases 46878(5
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Parameters 2ontrollin" IPR or PI
• Fluid Saturation Distribution
• Reseroir Drie %echanisms
• Formation Dama"e of Stimulation
• Relationship between IPR1PI and other
ariables 4#! fluid properties! relatie
permeability! etc.5 can be ery comple&.
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Determination of PI• Testin" the (ell
– %easure q, pwf ,
• Deelop PI models 4e$uations5
– PI 9 f (k, k ro , k rg , k rw , Bo , B g , Bw , etc.5
– e.".! steady'state sin"le phase flow
p
( )
( ) ( )( )t pt pt q
PI wf −=
+−
µ
=−
=
s
r
r B
kh
p p
q PI
w
ewf
2
1ln2.141
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Steady'State Radial Flow
( e l l ! r w D a m a " e d : o n e , ( r s , k s )
R e s e r o i r , ( r e , k )
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Radial Flow
• 2onsider sin"le'phase radial flow in a cylindrical
reseroir of radius r e with a well in the center
produced at a constant rate q sc ST01D.
• If the outer boundary is held at a constant pressure
pe, after some time we will hae steady'state flow!
q(r )/ B = q sc for all r and t where q(r ) is the flow rate in
R01D throu"h a cylinder of radius r . %oreoer! ∂ p/∂t =0.
• Darcy-s Law becomes
( ) ( )
r
pr
B
kh
r
p
B
k rhr q sc
∂
∂
µ
=
∂
∂
µ
π×= −
2.141
210127.1 3
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Radial Flow
• In the outer *one! r e > r > r s
• Separatin" ariables and inte"ratin"
( ) r p
r B
khr q sc ∂
∂µ= 2.141
( )
( )
µ=−
µ= ∫ ∫
r
r
kh
Bqr p p
r
dr
kh
Bqdp
e sce
r
r
sc
p
r p
ee
ln2.141
2.141
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Radial Flow
• )t r = r s! the pressure is "ien by
• For the inner 4dama"ed *one5 Darcy-s
law
( )
µ−= s
e sc
e s r
r
kh
Bq
pr p ln
2.141
r
pr
B
hk q s sc ∂
∂µ
=2.141
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Radial Flow
• Separatin" ariables and inte"ratin"
• ;liminatin" p4r s5
( )
( )
( ) ( )
µ=−
µ=
∫ ∫ r
r
hk
Bqr pr p
r
dr
hk
Bqdp
s
s
sc s
r
r s
sc
r p
r p
s s
ln2.141
2.141
( )
+
µ=
µ+
µ=−
r
r
k
k
r
r
kh
Bq
r
r
hk
Bq
r
r
kh
Bqr p p
s
s s
e sc
s
s
sc
s
e sce
lnln2.141
ln2.141ln2.141
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Radial Flow
• ;&pandin" and simplifyin"
• ;aluatin" at the wellbore
( )
−+
µ=
+
−
+
µ=−
r
r
k
k
r
r
kh
Bq
r
r
k
k
r
r
r
r
r
r
kh
Bqr p p
s
s
e sc
s
s
s s
s
e sce
ln1ln2.141
lnlnlnln2.141
−+
µ=−
w
s
sw
e scwf e
r
r
k
k
r
r
kh
Bq p p ln1ln
2.141
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S#in
• (e define
• The term s is #nown as the 4
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3otes on S#in
• S#in is a dimensionless number
• If k = k s! the reseroir is not dama"ed!and s = 0.
• If k > k s! the reseroir is dama"ed! and s
> 0.• If k < k s! the reseroir is stimulated! and
s < 0.
−=
w
s
s r
r
k
k s ln1
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Productiity Inde&
• For steady'state radial flow
• (ell-s productiity is increased if – s is reduced
– r w is increased
– µ is reduced – h is increased
+
µ
=
−
=
sr r B
kh
p p
q PI
w
ewf e ln2.141
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;&le
• ) reseroir with the followin" properties
is flowed at a bottomhole pressure of
=>?? psi. 2alculate the flow rate.Su""est two ways of increasin" the
wells production rate by a factor of @.
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PropertiesProperty Value Source
Permeability, md 5.2 Pressre !ransient "nalysis
!#i$%ness, &t 53 'ell ls
*is$sity, $+ 1.7 lid "nalysis
rmatin *lme a$tr, -/! 1.1 lid "nalysis
'ellbre radis, &t 0.32
'ell drainae area, a$re 40 'ell s+a$in
%in &a$tr 10 Pressre !ransient "nalysis
"erae reserir +ressre, +si 535 Pressre !ransient "nalysis
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Solution
• First! we conert the well-s draina"e area to an
e$uialent draina"e radius usin"
• The reseroir area is A=? acre 9 A=? acre×=B>A?ft@1acre 9 @CC=?? ft@. The e$uialent reseroir
draina"e area is r e 9 @ECE ft.
Ar e =π 2
+−
µ
=−
=
sr
r
B
kh
p p
q PI
w
ewf
2
1
ln2.141
( ) ( )
( ) ( ) ( )
!/+si 051.0
105.032.0
27ln7.11.12.141
532.5=
+−
= PI
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Solution
• Solin" for Rate
• To double the rate! we could double the pressure
drop. The current pressure drop is //B> psi! so
double this alue is @@C? psi! which means that we
must reduce the bottomhole pressure to >AB> – @@C?
9 B?E> psi.
( ) ( ) !/d .34500535 051.0 S p p PI q wf =−=−=
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Solution
• )nother method of doublin" the well-s rate would beto double the Productiity Inde& to a alue of ?.//@@ST01psi.
• (e would do this by decreasin" the s#in factor bystimulatin" the well.
• To determine the new s#in factor
• snew = 0.7.
( ) ( )
( )( )( )
+−
==
new s
PI
5.032.0
27ln7.11.12.141
532.51122.0
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Pseudosteady State Flow
• Rate of chan"e of pressure with time at
each point in a closed reseroir is
constant. – ;ach +point, in the reseroir contributes
e$ually to the flow.
• Productiity Inde&
+−
µ
=−
=
sr
r B
kh
p p
q PI
w
ewf
4
3ln2.141
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Diet* Shape Factors
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3otes
• (ith all else e$ual! asymmetric well'reseroirconfi"urations hae lower PI and flow ratecompared with a symmetric well'reseroirconfi"uration
• For psuedosteady state flow with constant wellflowin" pressure! aera"e reseroir pressure andflow rate decline continuously due to depletion.
• For sin"le phase flow! PI does not chan"e with
chan"es in chan"es in flow rate and aera"ereseroir pressure due to depletion.
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)bsolute 6pen Flow Potential
• )6F – For a "ien well'reseroir pair and aera"e
reseroir pressure! )6F is the ma&imum theoretical
flow rate that the well can proide.
• )6F is useful in analy*in" IPR in terms of
( ) p PI qq
p p PI q
AOF
wf
==−=
ma
ma
erssq
q
p
pwf
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Sin"le Phase IPR
q
wf P
( )wf p p PI q −=r P
maq
pwf p
q PI
∂∂
−=
p PI q =ma
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Future Linear IPR
q
wf P
( )wf r P P q −=
r P
maq
)s time t incresases! reseroir
pressure P r decreases and cumulatie
production N p increases.
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IPR for 7as (ells
• 7as PT properties are a function of pressure 4µ)! ! , B g , c g 5
• If p G @>?? psi and steady'state "as flow 4$ %scf1D5
• Pseudosteady'state flow
+
µ=− s
r
r
kh
" # q p p
w
ewf e ln
142422
+
µ=− s
C r
A
kh
" # q p p
Aw
wf 2
22 245.2ln2
11424
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PI for 7as (ells
• Pseudosteady'state flow
• PI for "as wells is a function of pressure.
– (hen aera"e reseroir pressure chan"es! "as propertieschan"e.
– PI is not constant durin" the well-s life
( )
+
µ
+=
−
==
sC r A" #
p pkh
p p
q PI PI
Aw
wf
wf 2245.2ln2
11424
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Typical 7as IPR
Gas IPR
?
/???
@???
B???
=???
>???
A???
? /???? @???? B???? =???? >???? A???? C????
Rate, MSCF/d
W e l l P r e s s u r e , p s
i
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Pseudosteady State 7as Flow
• For Pseudosteady state flow
• 0ac# Pressure ;$uation 4Rawlins – Schellhardt5
++
µ=− $q s
C r
A
kh
" # q p p
Aw
wf 2
22 245.2ln2
11424
222 %q&q p p wf +=−
+
µ= sC r
A
kh
" # & Aw
2
245.2ln2
11424
kh
"$ # %
µ=
1424
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Limitin" 2ases
• (hen non'Darcy flow is ne"li"ible 4%
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7enerali*ed 7as Flow
• Limitin" forms of the "as flow e$uation can be
"enerali*ed as
– 3e"li"ible non'Darcy flow! n 9 /
– Purely non'Darcy flow! n 9 ?.>
– 0oth components play a role! ?.> G n G /
• ;$uation can be rearran"ed as
( )
n
wf p pC q
22
−=
( ) ( ) ( )C n
qn
p p wf l1
l1
l 22 −=−
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0ac# Pressure )nalysis
• )t constant reseroir pressure! flow at
four different flow rates.
– %easure stabili*ed bottomhole pressure ateach rate.
• Plot
• Strai"ht line with slope /1n.• (ith n! can construct the IPR.
( ) ( )q p p wf l()erssl() 22 −
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%ultiphase Flow
• 3eed rates of oil! "as! water
– PI o , PI g , PI w
+
µ
=−= s
C r
A B
hk
p p
q PI
Aw
oo
o
wf
oo
2
245.2ln
2
12.141
+
µ
=−
=
sC r A B
hk
p p
q PI
Aw
ww
w
wf
ww
2245.2ln212.141
+
µ
=−
=
sC r
A B
hk
p p
q PI
Aw
g g
g
wf
g
g
2
245.2ln2
12.141
roo kk k =
rww kk k =
rg g kk k =
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%ultiphase IPR
• IPR under multiphase flow conditions cannot beeasily calculated.
• The most accurate method is by solin" thee$uations "oernin" the flow in the porousmedia throu"h a reseroir simulator.
• The IPR is so important to Production;n"ineers that simplified or empirical methodsto estimate it are necessary.
• The most common correlations are o"el andFet#oich
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o"el IPR
• o"el used a numerical reseroir simulator to
"enerate the IPR.
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*el 6P-
0
0.2
0.4
0.6
0.8
1
0 0.2 0.4 0.6 0.8 1mar f w
2
ma
.02.01
−
−=
p p
p p
qq wf wf
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o"el IPR
• o"el IPR can be obtained from well tests.
• )lthou"h the method was deeloped for
solution "as drie reseroirs! the e$uation is"enerally accepted for other drie
mechanisms as well.
• It is found to "ie e&cellent results for any well
with a reseroir pressure below the oil bubblepoint! i.e.! saturated reseroirs.
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Hndersaturated Reseroirs
P r
P %
P
q
( )wf r P P q −=
?
q% q'&(
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Hndersaturated Reseroirs
P r
P %
P
q
q% q'&(
q) = q * q%
P r ) = P %
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Hndersaturated Reseroirs
P r
P %
P
q
( )wf r P P q −=
q% q'&(
−
−=
−−
%
wf
P
P
P
P
%
wf
%
%
2
ma
.02.01
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;&le
ien data,
p = 2,400 +sia
qo = 100 !/d
wf = 100 +sia
enerate in&l8 +er&rman$e $re sin
bt# *el9s and et%i$#9s (n = 1)e:atins.
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;&le
Solution •*el9s ;:atin
etermine qo,ma
2
ma, 2400
100.0
2400
1002.01
100
−
−=
oq
250ma, =oq !/d
*els e:atin be$mes
2
2400.0
24002.01
250
−
−= wf wf o p pq
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;&le
•et%i$#9s ;:atin
etermine qo,ma
2
ma, 2400
1001
100
−=
oq
.22ma, =oq !/d
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;&le
*el et%i$#
pwf , +sia qo, !/d pwf , +sia
qo, !/d
0 250.0 0 22.
00 225.0 00 214.3
1200 175.0 1200 171.5
100 100.0 100 100.0
2400 0.0 2400 0.0
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Multi-layer inflow Performance
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rss?l8 bet8een 2 @ayers