Field of the Disclosure
[0001] The disclosure relates to the field of geophysical studies of oil and gas wells,
in particular to determining the inflow profile of fluids inflowing into the wellbore
from multi-zone reservoirs.
Background of the Disclosure
[0002] Usually when estimating flow rate of individual pay zones by temperature data, temperature
measurement along the entire wellbore is conducted, while temperature of a reservoir
near the wellbore is assumed close to the temperature of the undisturbed reservoir.
[0003] In particular, a method for determining relative flow rates of pay zones by quasi-stationary
flow temperatures measured along a wellbore is known. This method is, for example,
described in
Cheremensky G.A. Applied geothermy, Nedra Publishers, 1977, p. 181. The main assumption of the traditional approach is that an undisturbed temperature
of a reservoir near a wellbore must be known prior to the tests. This assumption is
not performed if temperature is measured at a first stage of production shortly after
perforation of the well. The influence of the perforation itself is not very significant,
but as a rule the temperature of the near-wellbore part of formation is considerably
lower than the temperature of the undisturbed reservoir due to the cooling resulting
from previous technological operations: drilling, circulation and cementing.
Summary of the Disclosure
[0004] The method for determining profile of fluid inflow from a multi-zone reservoir provides
the possibility to determine the inflow profile at an initial stage of production,
just after perforating a well, and in enhancing the accuracy of inflow profile determination
due to the possibility of determining inflow profile by transient temperature data.
[0005] The method comprises measuring temperature in a wellbore during a wellbore-return-to-thermal-equilibrium
time after drilling and then perforating the wellbore. Temperature of fluids inflowing
into the wellbore from pay zones is determined at an initial stage of production and
a specific flow rate for each pay zone is determined by rate of change of the measured
temperatures.
[0006] In case of direct measurement of temperature of the fluids inflowing into the wellbore
from each pay zone, specific flow rate of each pay zone is determined by the formula

where
Qi is a flow rate of an ith pay zone,
Ṫs is a rate of temperature recovery in the wellbore before perforation,
Ṫin ,i is a rate of change of temperature of the fluid inflowing into the wellbore from
the ith pay zone at an initial stage of production,
h
i is a thickness of the
ith pay zone,
a is a thermal diffusivity of a reservoir,

ρ
fcf is a volumetric heat capacity of the fluid,
ρ
rcr = φ · ρ
fcf + (1 - φ)·ρ
mCm is a volumetric heat capacity of the rock saturated with the fluid,
ρ
mcm is a volumetric heat capacity of a rock matrix;
φ is a porosity of the reservoir.
[0007] In case of impossibility to directly measure temperature of the fluids inflowing
into the wellbore from each pay zone, temperature of the fluids is determined with
the use of sensors installed on a tubing string, above each perforated interval. A
specific flow rate of a lower zone is determined by the formula

where
Q1 is a flow rate of a lower pay zone,
Ṫs is a rate of temperature recovery in the wellbore before perforation,
Ṫ1 is a rate of change of temperature of the fluid inflowing into the wellbore from
the pay zone at an initial stage of production as measured above the lower perforated
interval,
h1 is a thickness of this pay zone,
a is a thermal diffusivity of a reservoir,

ρ
fcf is a volumetric heat capacity of the fluid,
ρ
rcr = φ·ρ
fCf + (1-φ)·ρ
mCm is a volumetric heat capacity of the rock saturated with the fluid,
ρ
mcm is a volumetric heat capacity of a rock matrix;
φ is a porosity of the reservoir.
[0008] Then by temperatures measured by the sensors installed on the tubing string, specific
flow rates of overlying zones are determined, using values of flow rates determined
for the underlying zones.
[0009] The wellbore return-to-thermal-equilibrium time usually lasts for 5-10 days.
[0010] Temperature of the fluids inflowing into the wellbore from pay zones at the initial
state of production is preferably measured within 3-5 hours from start of production.
Brief description of the Figures
[0011] The disclosure is illustrated by drawings where Figure 1 shows a scheme with three
perforated intervals and three temperature sensors; Figures 2a and 2b show results
of calculation of inflow profiles for two versions of formation permeabilities; Figure
3 shows temperatures of fluids inflowing into the wellbore and temperatures of the
corresponding sensors for the case illustrated in Figure 2a, Figure 4 shows temperatures
of the fluids inflowing into the wellbore and temperatures of the corresponding sensors
for the case illustrated in Figure 2b; Figure 5 shows time derivatives of fluid temperature
and temperature of sensor 1 for the case illustrated in Figure 2a, Figure 6 shows
time derivatives of fluid temperature and temperature of sensor 1 for the case illustrated
in Figure 2b; Figure 7 shows ratios of temperature growth rates

and

for Figure 5, Figure 8 shows the same ratios for Figure 6; Figure 9 shows correlation
between the time derivative
Tin and specific flow rate
q.
Detailed description
[0012] The method may be used with a tubing-conveyed perforation. It is based on the fact
that a near-wellbore space, as a result of drilling, usually has a lower temperature
than temperature of surrounding rocks.
[0013] After drilling of a wellbore, circulation and cementing, temperature of a reservoir
in a near-borehole zone is significantly (by 10-20 K and more) lower than an original
temperature of the surrounding reservoir at a depth under consideration. After these
stages, a relatively long period of wellbore-returning-to-thermal-equilibrium follows
during which other working operations in the well are carried out, including installation
of a testing string with perforator guns. In the process of wellbore-returning-to-thermal-equilibrium
after drilling resulting cooling of near-wellbore formations, temperature measurements
in the wellbore are conducted.
[0014] After perforation, an initial stage of production follows - cleanup of the near-borehole
zone of the reservoir. At the initial stage of production, when a significant change
takes place in the temperature of fluids inflowing into the wellbore (usually during
3-5 hours), temperature of the fluids inflowing into the wellbore form each pay zone
is measured.
[0015] In case of a homogeneous reservoir, radial profile of temperature in the reservoir
prior to start of the cleanup is determined with the use of some general relationship
that follows from the equation of conductive heat transfer (1).

where "a" is a heat diffusivity of the reservoir.
[0016] From the physical viewpoint, it will be justifiable to suppose that with a long wellbore-returning-to-thermal-equilibrium
time, some near-wellbore zone (
r<rc) exists within which the rate of increase of temperature in the formation is constant,
i.e. it does not depend on distance from the wellbore:

[0017] Equations (1) and (2) have the following boundary conditions at the wellbore axis:

where
Ta is temperature at the axis (r=0).
[0018] The solution of the problem (1), (2), (3) is

where

[0019] Formulas (4), (5) give an approximate radial temperature profile near the wellbore
prior to start of production. A numerical simulation demonstrates that after 50 hours
of borehole-return-to-thermal-equilibrium time, these formulas are adequate for
r < 0.5 ÷ 0.7 m (with accuracy of 1÷5 %) for an arbitrary possible initial (before
closure) temperature profile.
[0020] Formulas (4), (5) do not take into consideration the influence of heat emission in
course of perforation and radial non-uniformity of thermal properties of the wellbore
and the reservoir, that is why after comparison with results of numerical simulation,
introduction of some correction coefficient might be necessary.
[0021] After start of production, the radial profile of temperature in the reservoir and
transient temperatures of the produced fluid is determined, mainly, by convective
heat transfer that is determined by the formula

where

[0022] is a velocity of radial filtration of the fluid
, q [m
3/m/s] is a specific flow rate, ρ
fcf is a volumetric heat capacity of the fluid, ρ
rCr = φ·ρ
fcf + (1-φ)·ρ
mCm is a volumetric heat capacity of the rock saturated with the fluid, ρ
mcm is a volumetric heat capacity of the rock matrix, φ is a porosity of the reservoir.
[0023] Equation (6) does not account for conductive heat transfer, the Joule-Thomson effect
and the adiabatic effect. The influence of the conductive heat transfer will be accounted
for below, while the Joule-Thomson effect (Δ
T = ε
0Δ
P) and the adiabatic effect are small due to a small pressure differential Δ
P and a relatively big typical cooling of the near-wellbore zone (5-10 K) before start
of production.
[0024] Equation (6) has the following solution

where
T0(
r) is an initial temperature profile in the reservoir (4),

[0025] Temperature of the fluid inflowing into the wellbore is (4), (8):

or

where

[0026] In accordance with (9), rate of fluid temperature increase at the inlet is

[0027] This formula for rate of temperature increase of the produced fluid is not fully
correct because Equation (6) does not take into consideration the conductive heat
transfer. Even in case of very small production rate (
q→0), temperature of the inflow must increase due to the conductive heat transfer and
the approximate formula accounting for this effect can be written in the following
way

[0028] Thus, with direct measurement of temperature of the fluid inflowing into the well,
specific flow rate of each pay zone
Qi can be determined by the formula

[0029] For such cases where no possibility exists to directly measure temperature of the
fluids inflowing into the wellbore from the pay zones, it is suggested to use results
of temperature measurements above each perforated interval, for example, with the
use of sensors installed on a tubing string utilized for perforating. In accordance
with the numerical simulation, in 20÷30 minutes after start of production, the difference
between temperature of the fluid inflowing into the wellbore
Tin,1 and temperature
T1 measured in the wellbore above a first perforated interval is practically constant:
Tin,1 - T1 = Δ
T1 ≈ const, and

In accordance with Formula (12), this means that a flow rate of the lower pay zone
Q
1 can be determined (
Q1 =
h1 ·
q1) (
h1 is a thickness of this pay zone) by temperature measured above the first perforated
interval:

or, taking into consideration Formula (11), we find

[0030] All parameters in this formula can be approximately estimated ("a" and χ) or measured.
The value of
Ṫs is measured with the use of temperature sensors after installing the tubing string
before the perforation. The value of
Ṫ1 is measured above the first perforation interval at the initial stage of production.
[0031] In case of three or more perforated zones, numerical simulation can be used for determining
the inflow profile. For any set of values of flow rate {
Qi} (i=1,2..n, where n is number of perforated zones), transient temperatures of produced
fluids can be calculated in the following way (9):

[0032] The parameter β (11) is one and the same for all zones; the parameters α
i are different because they depend on the temperature of the reservoir
Ta,i recorded in the wellbore before start of production.
[0033] For this set of flow rate values, the numeric model of the producing wellbore should
calculate transient temperatures of the flow at each depth of placement of the sensor
with consideration of heat losses into the surrounding reservoir, the calorimetric
law for the fluids being mixed in the wellbore, and the thermal influence of the wellbore
which is understood here as the influence of the fluid initially filling the wellbore.
The flow rate is determined with the use of the procedure of model fitting that minimizes
differences between the recorded and calculated temperatures of the sensors.
[0034] An approximate solution of the problem can be obtained with the use of the above-described
analytical model, which utilizes rates of increase of sensor temperatures.
[0035] The calorimetric law for the second perforated zone is described by the equation

where
T1* are
T2* are temperatures of the fluid below and above the perforated zone. In accordance
with the numeric simulation, the difference between
T1 and
T1*,
T2 and
T2* remains practically constant and instead of Equation (18) we can use the following
equation for time derivatives of the measured temperatures:

[0036] Taking into consideration the above-presented relationships (11) and (16), this formula
can be written as an equation for the dimensionless flow rate
y2 of the second perforated zone
y2 =
Q2/
Q1 :

where

[0037] If
Ṫ2 >
Ṫ1 (
f21 > 1), a unique solution exists. In the opposite version (
f21 < 1), this equation has two solutions. The physical sense of this peculiarity is
quite obvious for
f21 =1, that corresponding to equal increase rates of temperatures
T2 and
T1. Indeed, this may take place in two cases: (1)
Q2=0 (
y2=0) and above the upper zone the behavior of the temperature is the same as below
it; (2)
Q2=
Q1 (
y2=1) - both zones are equal and they have the same rate of temperature increase.
[0038] The possible solution of the problem of non-uniqueness of solution consists in the
combination of two approaches. After evaluating
Q1 with the use of Equation (12) and determining
y2 by Equation (20), the true value
y2 of can be chosen using the known total flow rate
Q (for two perforated zones):

[0039] Relative flow rates for perforated zones 3 and 4 can be calculated using the dimensionless
values y
2, y
3 and so on, which were determined previously for the perforated zones located down
the wellbore.

where

[0040] The possibility of determining the inflow profile with the use of the suggested method
for a case where direct measurement of temperatures of fluids inflowing into the wellbore
from pay zones is impossible was checked up on synthetic examples prepared with the
use of numerical simulation software package for the producing wellbore, which performs
modeling of the unsteady-state pressure field in the "wellbore-formation" system,
flow of non-isothermal fluids in a porous medium, mixing of the flows in the wellbore,
and heat transfer in the "wellbore-formation" system, etc.
[0041] Modeling of the process operations carried out under the following time schedule
was performed:
- Circulation of the well during 110 hours. The temperature of fluids at the formation
occurrence depth is assumed to be 40°C.
- Borehole-return-to-thermal-equilibrium time is 90 hrs.
- Production for 6 hrs with flow rate Q = 60 m3/day.
[0042] Geothermal gradient equals 0.02 K/m. The temperature of the undisturbed reservoir
at the depth of sensor 1 (274 m) is 65.5°C that at the depth of sensor 3 (230 m) is
64.6°C. Thermal diffusivity of the reservoir
is a = 10
-6 m
2/s and χ=0.86.
[0043] Figure 1 shows the scheme of a well with three perforated intervals (#1: 280-290
m, #2: 260-270 m, #3: 240-250 m) and three temperature sensors: T
1 at the depth of 274 m, T
2 at the depth of 254 m and T
3 at the depth of 230 m.
[0044] Two options were considered with different combinations of formation permeabilities
and the following flow rate parameters:
Option 1 (Figure 2a): Q1=10 m3/day, Q2=23.4 m3/day, Q3=26.6 m3/day; and
Option 2 (Figure 2b): Q1=46 m3/day, Q2=13 m3/day, Q3=1 m3/day.
[0045] During circulation and the return-to-thermal-equilibrium time, the reservoir/wellbore
temperature is the same in both cases under consideration. At the end of the return-to-thermal-equilibrium
time, the rate of temperature growth was
Ṫs(200h) = 0.034 K/hr.
[0046] Figures 3 and 4 show temperatures of the produced fluids (thin curves) and temperatures
of the corresponding sensors (bold curves). The difference between
Tin,1 and
T1 remains practically constant after ~1 hr of production. Time derivatives of fluid
temperature and temperature of sensor #1 are presented in Figures 5 and 6. One can
see that approximately 3 hours after start of production, the difference between
dTin,1/
dt and
Ṫ1 amounts to about 6-8%, that confirming our assumption made in the analysis presented
above.
[0047] The correlation between time derivative
Tin and specific flow rate
q (data for all of the perforated intervals are utilized) is presented in Figure 9.
For flow rate
q tending to zero, the linear regression equation gives:
Ṫin(q → 0) = 0.0374 K/hr. This value is close to the rate of temperature recovery
Ṫs(200h) = 0.034 K/hr due to the conductive heat transfer. This result confirms Formula
(14) suggested above for correlation between flow rate and rate of temperature growth
of the produced fluid.
[0048] Let us estimate the values of the flow rate from the lowermost perforated zone. With
duration of production equaling 4 hours, Figures 5 and 8 give: Option #1 -
Ṫ1 = 0.067 K/hr, Option #2 -
Ṫ1 = 0.17 K/hr. Substituting these values in Formula (1), we find:
Option #1: Q1=11 m3/day (the true value is Q1=10 m3/day);
Option #2: Q1= 46.5 m3/day (the true value is Q1=46 m3/day).
[0049] Flow rate values for other perforated zones are determined by Formulas (20), (23).
Option # 1:
[0050] For the estimated value
Q1=11 m
3/day presented above, we
find ya =1.1. For production duration of 4 hours, Figure 7 gives
f21 ≈ 1.45, while Equation (2) gives one positive solution
y2 = 2.346 and flow rate
Q2 =
Q1 · y2 = 25.8 m
3/day.
[0051] For the third perforated zone Figure 7 gives
f32 ≈ 1.08 and from Equation (22) we find one positive solution
y3 = 0.75 and
Q3 = (
Q1 +
Q2)
· y3 = 27.6 m
3/day.
[0052] The total flow rate calculated by temperature data amounts to
Qe =
Q1 +
Q2 +
Q3 = 64.4 m
3/day (the true value is 60 m
3/day).
[0053] Using this value for determining relative flow rates, we find:
Y2 = 0.4;
Y3 = 0.43
[0054] The corresponding flow rate values for different zones are:
Q1 = Q·Y1 =10.2 m3/day (the true value is 10 m3/day)
Q2 = Q·Y2 = 24 m3/day (the true value is 23.4 m3/day)
Q1 = Q·Y1 = 25.8 m3/day (the true value is 26.6 m3/day)
[0055] Relative errors (related to the total flow rate) are 0.3%, 1%, and 1.3%.
Option #2:
[0056] For the above-estimated flow rate value
Q1=46.5 m
3/day, we find
ya = 0.25. Figure 8 gives for production duration of 4 hours
f21 ≈ 0.85. In this case, Equation (20) has no solution and as the approximate solution
we have to take the value of
y2 that corresponds to the minimum value of
f21 (
f21min ≈ 0.863), which provides for the real solution:
y2 = 0.413.
[0057] The corresponding flow rate is
Q2 =19.85 m
3/day.
[0058] For the third perforated zone, Equation 8 gives
f32 ≈ 0.96, while from Equation (22) we find two roots:
y3 = 0.5, Q3 = (Q1 + Q2)·y3 = 34 m3/day and total flow rate Qe = 102 m3/day, and
y3 = 0.062, Q3 = (Q1 + Q2) · y3 = 4.18 m3/day and total flow rate Qe = 72 m3/day.
[0059] As the approximate solution of the problem, we will take the value of
y3 = 0.062, which gives the total flow rate value
Qe = 72 m
3/day that is closer to the true value.
[0060] In the second case the estimate of
Q1 is more reliable than the estimate of
Q2 and
Q3, hence, we fix the value of
Q1 and use the previously determined values of
Q2 and
Q3 for distributing the remaining flow rate
Q-Q1 between these zones:

and

[0061] At last, the determined flow rate values are as follows:
Q1 = 46.5 m3/day (the true value is 46 m3/day)
Q2 = 11.2 m3/day (the true value is 13 m3/day)
Q3 = 2.3 m3/day (the true value is 1 m3/day)
[0062] Relative errors (related to the total flow rate) are 0.8%, 3% and 2.2%.
[0063] For solving the inverse problem, this inflow profile (a low inflow rate of the uppermost
zone) is the most complex. Nonetheless, results of solving the inverse problem are
well consistent with the data utilized in direct simulation.
[0064] In general case, the most reliable inversion of temperature measured among perforated
intervals immediately after perforating can be made with the use of a specialized
numerical model and fitting the transient temperature data with consideration of absolute
values of temperature as well as time derivatives of temperature.
1. A method for determining profile of fluid inflow from multi-zone reservoirs into a
wellbore comprising:
- measuring temperature in the wellbore during a wellbore-retum-to-thermal-equilibrium
time after drilling,
- perforating the wellbore,
- determining temperature of the fluids inflowing into the wellbore from each pay
zone at an initial stage of production, and
determining a specific flow rate for each pay zone by rate of change of the measured
temperatures.
2. The method of Claim 1 wherein the temperature of the fluids inflowing into the wellbore
from the pay zones is determined by direct measurement of temperature of the fluids
inflowing into the wellbore from each pay zone, and a specific flow rate of each pay
zone is determined by the formula

where
Qi is a flow rate of the
ith pay zone,
Ṫs is a rate of temperature recovery in the wellbore before perforation,
Ṫin, i is a rate of temperature variation of the fluid inflowing into the wellbore from
the
ith pay zone at the initial stage of production,
hi is a thickness of the ith pay zone,
a is a thermal diffusivity of the reservoir,

ρ
fcf is a volumetric heat capacity of the fluid,
ρ
rcr = φ · ρ
fcf + (1 - φ)·ρ
mCm is a volumetric heat capacity of the rock saturated with the fluid,
ρmcm is a volumetric heat capacity of a rock matrix ,
φ is a porosity of the reservoir.
3. The method of claim 1 wherein the wellbore-retum-to-thermal-equilibrium time is 5-10
days.
4. The method 1 of claim 1 wherein the temperature of the fluids inflowing into the wellbore
from each pay zone at the initial stage of production is measured within 3-5 hours
after start of production.
5. The method of claim 1 wherein the temperature of the fluids is determined by sensors
installed on a tubing string being used for perforating, above each perforated interval,
a specific flow rate of a lower pay zone is determined by the formula

where Q
1 is a flow rate of the lower zone,
Ṫs is a rate of temperature recovery in the wellbore before perforation,
Ṫ1 is a rate of temperature change of the fluid inflowing into the wellbore from the
pay zone at the initial stage of production as measured above the lower perforated
interval,
h1 is a thickness of the lower pay zone,
a is a thermal diffusivity of the reservoir,

ρ
fcf is a volumetric heat capacity of the fluid,
ρ
rcr = φ · ρ
fcf + (1
-φ)·ρ
mCm is a volumetric heat capacity of the rock saturated by the fluid,
ρ
mcm is a volumetric heat capacity of the rock matrix,
φ is a porosity of the reservoir,
and specific flow rates of overlying pay zones are determined by temperatures measured
by the sensors installed on the tubing string, using the flow rates determined for
the underlying pay zones.
6. The method of claim 5 wherein the wellbore-retum-to-thermal-equilibrium time is 5-10
days.
7. The method of claim 5 wherein the temperature of the fluids inflowing into the wellbore
from each pay zone at the initial stage of production is measured within 3-5 hours
after start of production.