(19)
(11) EP 0 176 410 B1

(12) EUROPEAN PATENT SPECIFICATION

(45) Mention of the grant of the patent:
07.12.1988 Bulletin 1988/49

(21) Application number: 85401719.1

(22) Date of filing: 05.09.1985
(51) International Patent Classification (IPC)4E21B 49/00, E21B 49/08, E21B 47/10

(54)

Method for uniquely estimating permeability and skin factor for at least two layers of a reservoir

Verfahren zur Einzelbestimmung der Durchlässigkeit und des Wandfaktors von wenigstens zwei Schichten eines Untertagespeichers

Procédé pour l'estimation individuelle de la perméabilité et de l'effet pariétal de deux couches au moins d'un réservoir


(84) Designated Contracting States:
AT DE FR GB IT NL

(30) Priority: 07.09.1984 US 648113

(43) Date of publication of application:
02.04.1986 Bulletin 1986/14

(73) Proprietors:
  • Schlumberger Limited
    New York, N.Y. 10017 (US)
    Designated Contracting States:
    DE GB NL AT 
  • SOCIETE DE PROSPECTION ELECTRIQUE SCHLUMBERGER
    F-75340 Paris Cédex 07 (FR)
    Designated Contracting States:
    FR IT 

(72) Inventors:
  • Kucuk, Fikri
    Houston Texas 77042 (US)
  • Ayestaran, Luis C.
    Houston Texas 77024 (US)

(74) Representative: Hagel, Francis et al
Etudes et Productions Schlumberger A L'ATTENTION DU SERVICE BREVETS 26, rue de la Cavée B.P. 202
92142 Clamart Cédex
92142 Clamart Cédex (FR)


(56) References cited: : 
FR-A- 2 434 923
US-A- 3 636 762
US-A- 3 321 965
US-A- 4 328 705
   
  • PETROLEUM ENGINEER INTERNATIONAL, vol. 51, no. 7, June 1979, pages 129-130, Dallas, Texas, US; E.H. TIMMERMAN: "Various methods used to average permeability"
  • OIL & GAS JOURNAL, vol. 81, no. 17, April 1983, pages 96-100, Tulsa, Oklahoma, US; N.N. MOLINA: "Relative permeability-2. How to use relative permeability correlations"
  • PETROLEUM ENGINEER INTERNATIONAL, vol. 51, no. 12, October 1979, pages 81-92, Dallas, Texas, US; L. DOUGLAS PATTON et al.: "Well completion and workover. Part 5 - Pseudodamage"
  • PETROLEUM ENGINEER INTERNATIONAL, vol. 52, no. 11, September 1980, pages 80-90, Dallas, Texas, US; L. DOUGLAS PATTON et al.: "Well compltions and workovers - Part 10. The systems approach to well testing (feedback)"
  • Lefkovits, H.C. et al.: "A Study of the Behavior of Bounded Reservoirs Composed of Stratified Layers," Soc. Pet. Eng. J. (March 1961) 43-58; Trans., AIME, 222 (copy enclosed)
  • Dogru, A.H. and Steinfeld, J.H., "Design of Well Tests to Determine the Properties of Stratified Reservoirs," Proceedings of 5th SPE Symposium on Reservoir Simulation, Denver, CO, February 1-2, 1979.
  • Dogru, A.H., Dixon, T.N, and Edgar, T.F: "Confidence Limits on the Parameters and Prediction of Slightly Compressible, Single-Phase Reservoirs," Soc. Pet. Eng. J. (Feb 1977) 42-56.
  • Rosa, A.J. and Horne, U.N.: "Automated Type-Curve Matching in Well Test Analysis Using Laplace space Determination of Parameter Gradients," SPE paper SPE 12131 presented at the SPE-AIME 58th Annual Fall Technical Conference and Exhibition, San Francisco, CA (Oct. 5-8, 1983).
   
Note: Within nine months from the publication of the mention of the grant of the European patent, any person may give notice to the European Patent Office of opposition to the European patent granted. Notice of opposition shall be filed in a written reasoned statement. It shall not be deemed to have been filed until the opposition fee has been paid. (Art. 99(1) European Patent Convention).


Description

Background of the invention


Field of the invention



[0001] The invention relates to well testing in general and in particular to a method for downhole measurements and recording of data from a multiple layered formation of an oil and gas well and for estimating individual permeabilities and skin factors of the layers using the recorded data.

Description of the prior art



[0002] The estimation of parameters of stratified layers without crossflow of an oil and gas well is not a new problem. Over the years, many authors have investigated the behavior of layered reservoirs without cross flow. Much work has been done on estimating parameters of layered reservoirs because they naturally result during the process of sedimentation. Layered reservoirs are composed of two or more layers with different formation and fluid characteristics.

[0003] One of the major problems for layered reservoirs is the definition of the layers. It has been found that it is essential to integrate all logs and pressure transient and flowmeter data in order to determine flow capacities, skin factors, and the pressure of individual layers. This invention relates primarily to two-layer reservoirs with a flow barrier between the layers (without crossflow). The production is commingled at the wellbore only.

[0004] During a buildup test, fluid may flow from the high pressure zone to the low pressure zone through the wellbore as a result of a differential depletion. The crossflow problem becomes more severe if the drainage radius of each zone is different. Wellbore crossflow could occur while the pressure is building up. A straight line may be observed on the Horner plot. This behavior has been observed many times in North Sea reservoirs Lefkovits, H.C. et al.: "A Study of the Behavior of Bounded Reservoirs Composed of Stratified Layers" Soc. Pet. Eng. J. (March 1961) 43-58; Trans., AIME, 222.

[0005] The crossflow problem has been overlooked by the prior art because in many instances the pressure data itself does not reveal any information about the wellbore crossflow. Furthermore, the end of the wellbore crossflow between the layers cannot be determined either quantitatively or qualitatively. If fluid segregation in the tubing and wellbore geometry is added to the complication mentioned above, the buildup tests from even two-layer reservoirs without crossflow cannot easily be analyzed.

[0006] This invention relates to the behavior of a well in an infinite two-layered reservoir. If the well has a well-defined drainage boundary (symmetrics about the well axis for both layers), and if a well test is run long enough, the prior art has shown that it is possible to estimate the individual layer permeabilities and an average skin. However, cost or operational restrictions can make it impractical to carry out a test of sufficient duration to attain a pseudo steady-state period. Moreover, even if the test is run long enough, an analyzable pseudo steady-state period may not result because of non-symmetric or irregular drainage boundaries for each layer. It is also difficult to maintain a constant production rate long enough to reach a pseudo steady-state period.

[0007] A major problem for layered systems not addressed by the prior art is how to estimate layer permeabilities, skins, and pressures from conventioal well testing. In practice, the conventional tests (drawdown and/or buildup) only reveal the behavior of a two-layer formation which cannot be distinguished from the behavior of a single-layer formation even though a two-layer reservoir has a distinct behavior without wellbore storage effect. There are, of course, a few special cases for which the conventional tests will work.

[0008] The effect of wellbore storage on the behavior of the layered reservoirs is more complex than that of single-layer reservoirs. First, the wellbore storage may vary according to the differences in flow contribution of each layer. Second, it has been observed that it takes longer to reach the semilog straight line than that of the equivalent single-layer systems.

[0009] It is important for the operator of an oil and gas well having a multiple layer reservoir to be able to determine the skin factor, s, and the permeability, k, of each layer of the formation. Such information aids the operator in his determination of which zone may need reperforation or acidizing. Such information may also aid the operator to determine whether loss of well production is caused by damage to one layer or more layers (high skin factor) as distinguished from other reasons such as gas saturation buildup. Reperforation or acidizing may cure damage to the well while it will be useless for a gas saturation buildup problem.

Identification of objects of the invention



[0010] It is a general object of the invention to provide a well test method to estimate multi-layered reservoir parameters.

[0011] It is a more specific object of the invention to provide a well test method to estimate uniquely the permeability k and the skin factor s for each layer in a multiple layer reservoir.

Summary of the invention



[0012] According to the invention, a well test method for uniquly estimating permeability and skin factor for each of at least two layers of a reservoir includes the positioning of a logging tool of a logging system at the top of the upper layer of a wellbore which traverses the two layers. The logging system has means for measuring downhole fluid flow rate and pressure as a function of time. The surface flow rate of the well is changed from an initial flow rate at an initial time, t1, during a first time interval. The downhole fluid flow rate, qi(t), and downhole pressure, pl(t), are measured and recorded during the first interval, t, to 2, at the top of the upper layer.

[0013] The logging tool is then positioned to the top of the lower layer where the downhole flow rate, q12, from the top of the lower layer is measured and recorded if possible at a stabilized flow. The surface flow rate is then changed at time t3, to another flow rate. The downhole fluid flow rate, q22(t), and downhole pressure, p2(t), are measured and recorded during the second interval, t3 to t4, at the top of the lower layer.

[0014] The functions k and 5 are determined, where





where

k1=permeability of upper layer

k2=permeability of lower layer

h,=known thickness of upper layer

h2=known thickness of lower layer

by matching the measured change in downhole pressure, p1(t), with the convolution of the measured fluid flow rate ql(t) and an influence function Δpsf(t) which is a function of combined-layerred permeability, k, and skin effect s.



[0015] The permeability k2, of the lower layer and the skin factor, s2, of the lower layer are determined by matching the measured fluid flow rate, q22(t), with the convolution of the measured changed in downhole pressure, Δp2(t)=p1(t3)-p2(t), and an influence function, f(t), which is a function of the lower layer permeability, k2, and skin factor, s2. The parameters k1 and s1 for the first layer are determined from estimates of k2, s2 and k and s.

[0016] Testing regimes are defined for non-flowing wells and for flowing wells. Estimation methods are presented for matching measured values of pressure and flow rate with calculated values, where the calculated value changes as a result of changes in the parameters to be estimated, k and s.

Brief description of the drawings



[0017] The objects, advantages and features of the invention will become more apparent by reference to the drawings which are appended hereto and wherein like numerals indicate like parts and wherein an illustrative embodiment of the invention is shown of which:

Figure 1 illustrates schematically a two layer reservoir in which a logging tool of a wireline logging system is disposed at the top of the upper producing zone;

Figure 2 illustrates the same system and formation as that of Figure 1 but in which the logging tool of the wireline logging system is disposed at the top of the lower producing zone;

Figure 3A illustrates the sequential flow rate profile for a new well according to the invention;

Figure 3B illustrates the downhole pressure profile which results from the flow rate profile of Figure 3A.

Figure 4A illustrates the sequential flow rate profile for a producing well according to the invention;

Figure 4B illustrates the downhole pressure profile which results the flow rate profile of Figure 4A;

Figure 5 is a graph of measured downhole pressure as a function of time of a synthetic drawdown test according to the invention; and

Figure 6 is a graph of measured downhole flow rates as a function of time of a synthetic drawdown test corresponding to the measued pressure of Figure 5.


Description of the invention



[0018] Figures 1 and 2 illustrates a two layered reservoir, the parameters of permeability, k, and skin factor s, of each layer of which are to be determined according to the method of this invention. Although a two-layered reservoir is illustrated and considered, the invention may be used equally advantageously for reservoirs of three or more layers. A description of a mathematical model of the reservoir is presented which is used in the method according to the invention.

Mathematical model



[0019] The reservoir model of Figures 1 and 2 consists of two layers that communicate only through the wellbore. Each layer is considered to be infinite in extent with the same initial pressure.

[0020] From a practical point of view, it is easy to justify an infinite-acting reservoir if only the data is analyzed that is not affected by the outer boundaries. However, often a differential depletion will develop in layered reservoirs as they are produced. It is possible that each layer may not have the same average pressure before the test. It is also possible that each layer may have different initial pressures when the field is discovered. The method used in this invention is for layers having equal initial pressures, but the method according to the invention may be extended for the unequal initial pressure case.

[0021] It is assumed that each layer is homogeneous, isotropic, and horizontal, and that it contains a slightly compressible fluid with a constant compressibility and viscosity.

[0022] The Laplace transform of the pressure drop for a well producing at a constant rate in a two-layered infinite reservoir is given by

where:

η=hydrauIic diffusivity

z=Laplace image space variable

n1=number of layers=2



[0023] The other symbols are defined in Appendix A at the end of this description where the nomenclature of symbols is defined.

[0024] The Laplace transform of the production rate for each layer can be written as:



[0025] Eqs. 1 and 2 give the unsteady-state pressure distribution and individual production rate, respectively, for a well producing at a constant rate in an infinite two-layered reservoir.

[0026] For drawdown or buildup tests, Eq. 1 cannot be used directly in the analysis of wellbore pressure because of the wellbore storage (afterflow) effect (unless the semilog straight line exists). However, most studies on layered reservoirs have essentially investigated the behavior of Eq. 1 for different layer parameters. The principal conclusions of these studies can be outlined as follows:

1. From buildup or drawdown tests, an average flow capacity and skin factor can be estimated for the entire formation.

2. The individual flow capacities can be obtained if the stabilized flow rate from one of the layers is known and if the skin factors are zero or equal to one another.



[0027] Estimating layer parameters by means of an optimum test design has been investigated by the prior art using a numerical model similar to that of equation 1 except that skin factors were not included. Such prior art shows that there are serious problems with observability and the question of wellposedness of the parameter estimation for layered reservoirs. Dogru, A. H. and Steinfeld, J. H., "Design of Well Tests to Determine the Properties of Stratified Reservoirs", Proceedings of the 5th SPE Symposium on Reservoir Simulation, Denver, CO, February 1-2, 1979.

[0028] The basic problem of prior art methods for estimating layer parameters is that the pressure data are not sufficient to estimate the properties of layered reservoirs. The invention described here is for a two-step drawdown test with the simultaneously measured wellbore pressure and flow rate data which provides a better estimate for layer parameters than prior art drawdown or buildup tests. Eqs. 1 and 2 will be used to describe the behavior of two-layered reservoirs.

Wellbore pressure behavior



[0029] Certain aspects of the pressure solution for two-layer systems were discussed in the previous section; basically the constant rate solution was presented. In reality, the highly compressible fluid in the production string will affect this solution. This effect is usually called wellbore storage or afterflow, depending on the test type. It has been a common practice to assume that the fluid compressibility in the production string remains constant during the test. Strictly speaking, this assumption may only be valid for water or water-injection wells. The combined effects of opening or closing the wellhead valve and two-phase flow un the tubing will cause the wellbore storage to vary as a function of time. In many cases, it is difficult to recognize changing wellbore storage because it is a gradual and continuous change. Nevertheless, the constant wellbore storage case is considered here as well.

[0030] The convolution integral (Duhamel's theorem) is used to derive solutions from Eq. 1 for time-dependent wellbore (inner boundary) conditions. For example, the constant wellbore storage case is a special time-dependent boundary condition. For a reservoir with an initially constant and uniform pressure distribution, the wellbore pressure drop is given by



where

Δpwf=Pf-pwf for drawdown tests

Δpsr=p1-Psf for drawdown tests

Δpwf=pws-pwf for buildup tests

ΔPsf=Psf-pwf for buildup tests

Δps=pressure drop caused by skin

psf=sandface pressure of a well producing at constant rate

qD<tD)=qsf(t)/qt

q.f=sandface flow rate

qt=reference flow rate

'=indicates derivative with respect to time



[0031] The Laplace transform of Δpwf is given by



[0032] If the wellbore storage is constant, qo can be expressed as



[0033] Substitution of the Laplace transform of Eq. 5 and Eq. 1 in Eq. 4 yields the wellbore pressure solution for the constant wellbore storage case.

[0034] Wellbore storage effects for layered reservoirs may be expressed as:

where a is dependent on reservoir and wellbore fluid properties.

[0035] This condition can be interpreted as a special variable wellbore storage case. It is also possible that for some wells, Eq. 6 describes wellbore storage phenomena far better than Eq. 5. If the sandface rate is measured with available flowmeters, it is not necessary to guess the wellbore storage behavior of a well.

[0036] A drawdown test with a periodically varying rate with a different period is considered in order to increase the sensibility of pressure behavior to each layer parameter. This case is expressed as:

where T=period.

Identifiability of layer parameters in well test analysis



[0037] The problem of identifiability has received considerable attention in history matching by the prior art. The purpose here is to give an identifiability criterion to nonlinear estimation of layer parameters, Dogru, A. H., Dixon, T. N., and Edgar, T. F: "Confidence Limits on the Parameters and Prediction of Slightly Compressible, Single-Phase Reservoirs", Soc. Pet. Eng. J. (Feb. 1977) 42-56. The identifiability principles given here are very general, and are also applied to other similar reservoir parameter estimations.

[0038] The main objective of this section is to estimate layer parameters using the model presented by Eq. 1 and measured wellbore pressure data. For convenience, it is assumed that the measured pressure is free of errors.

[0039] Suppose that wellbore pressure, p°, is measured m times as a function of time from a two-layered reservoir. It is desired to determine individual layer permeabilities and skin factors from the measured data by minimizing:

where

pj=measured pressure

η=calculated pressure as a function of time, and β

β=(k1,k2,s1,s2)τ =parameter vector

k1,k2=permeabilities of first and second layers, respectively

s1,s2=skin factors of first and second layers, respectively

m=number of measurements



[0040] Eq. 8 can also be written as:

where

r=m dimensional residual vector

Assume that β* is the true solution to Eq. 8. The necessary condition for a unique minimum is:

1. g (β*)=0 and

2. H(β*) must be positive definite


where g the gradient vector with respect to β and H is the Hessian matrix of Eq. 8. A positive definite Hessian, also known as the second order condition, ensures that the minimum is unique. Furthermore, without measurement errors, or when the residual is very small, the Hessian can be expressed as:

where A is the sensitivity coefficient matrix with mxn elements







[0041] The positive definiteness of the Hessian matrix requires that all of the eigenvalues corresponding to the system

be positive and greater than zero. If an eigenvalue of the Hessian matrix is zero, the functional defined by Eq. 8 does not change along the corresponding eigenvector, and the solution vector β* is not unique. Therefore, the number of observable parameters from m measurements can be determined theoretically by examining the rank of the Hessian matrix H, which is equal to the number of nonzero eigenvalues.

[0042] In the above analysis, it is assumed that the observations are free of any measurement errors. In presence of such errors and limitations related with the pressure gauge resolution, a non-zero cutoff value must be used in estimating the rank of the.Hessian. Also, in order to compare parameters with different units, a normalization of the sensitivity coefficient matrix can be carried out by multiplying every column of the sensitivity coefficient matrix by the corresponding nonzero parameter value. That is,

Furthermore, the largest sensitivity of the functional two parameters is along the eigenvector corresponding to the largest eigenvalue. Each element of the eigenvector vj corresponds to a parameter in the n dimensional parameter space. The magnitude indicates the relative strength of that parameter along the eigenvector vj.

Nonlinear estimation of layer parameters from conventional transient tests



[0043] In this section an attempt is made to estimate layer parameters by minimizing Eq. 8. The eigenvalue analysis of the sensitivity coefficient is done for four cases.

1. Constant flow rate with no wellbore storage C=0,0 I/kPa (C=0,0 bbl/psi),

2. Constant flow rate with wellbore storage C=23 1/kPa (C=0.01 bbl/psi)

3. Periodically varying flow rate with a period of 0.1 hours,

4. Periodically varying flow rate with a period of 1 hour.



[0044] The pressure data for each case are generated by using Eq. 1 and Eq. 3 with the corresponding qD solution. Reservoir and fluid data are given in Table 1 for all these cases.



[0045] The nonlinear least squares Marquardt method with simple constraints is used for the minimization of Eq. 8 with respect to k1, k2, s, and s2.

[0046] Table 2 shows the eigenvalues of the Hessian matrix for each test.



[0047] The results of Table 2 clearly indicate that in all cases only two of the eigenvalues are greater than 6,9 kPa (1 psi). Thus, only two parameters can be uniquely estimated from wellbore pressure data. The largest sensitive parameters are those of the high-permeability layer.

[0048] The above analysis has also been done for different combinations of k1, k2, s" and s2; and the conclusions essentially do not change. The periodical variable rate with 0.1 hours period improves the nonuniqueness problem somewhat. However, the uniqueness problem remains the same for the estimation of ki, k2, si, and s2 for two-layered reservoirs without crossflow.

[0049] The above analysis was also extended to a case with an unknown wellbore storage coefficient can be estimated from wellbore pressure data if it remains constant during the test.



[0050] It is clear from the above discussion that using prior art methods, transient pressure data does not give enough information to determine uniquely flow capacity and skin factor for each individual layer.

New testing methods for layered reservoirs



[0051] As indicated above, a drawdown test is best suited for two-layered reservoirs without crossflow. Ideally, a reservoir to be tested should be in complete pressure equilibrium (uniform pressure distribution) before a drawdown test. In practice, the complete pressure equilibrium condition cannot be satisfied throughout the reservoir if wells have been producing for some time from the same formation. Nevertheless, the pressure equilibrium condition can easily be obtained in new and exploratory reservoirs.

[0052] For developed reservoirs, it is also possible to obtain pressure equilibrium if the well is shut in for a long time. However, in developed layered reservoirs, it is difficult to obtain pressure equilibrium within the drainage area of a well. On the other hand, it is very common to observe pressure differential between the layers.

[0053] In addition to these fluid flow characteristics in layered reservoirs, cost and/or operational restrictions can make it impractical to close a well for a long time.

[0054] With respect to these different initial conditions, two drawdown test procedures for two-layer reservoirs without crossflow are described according to the invention. Either the initial condition or the stabilized period is important in a given test because during the analysis, the delta pressure (p-pbase) is used for the estimation of parameters. During the test, it is not crucial to keep the rate constant, since it is measured.

New or shut-in wells



[0055] The method according to the invention will work well for the wells in a new field of exploratory wells. Figures 1 and 2 illustrate a two zone reservoir with a wellbore 10 extending through both layers and to the earth's surface 11. A well logging tool 14 having means for measuring downhole pressure and fluid flow rate communicates via logging cable 16 to a computerized instrumentation and recording unit 18.

[0056] As indicated in Figure 1, the parameters ki, s, of layer 1 and k2, s2 of layer 2 are desired to be uniquely estimated. One layer, such as layer 2, may have a damaged zone which would result in a high value of s2, skin factor of layer 2, which if known by measurement by the well operator, could aid in decisions relating to curing low flow or pressure from the well.

[0057] For shut-in wells, before starting the test, pressure should be recorded for a reasonable time in order to obtain the rate of pressure decline or to observe a uniform pressure condition in the reservoir. Figure 3A shows the test procedure. First the well tool 14 of Figure 1 should be just above both producing layers. At time ti, the well should be started to produce at a constant rate at the surface, if possible. Although production rate does not affect the analysis, a rapid rate increase can cause problems. A few of these are:

1. Wellbore fluid momentum effect,

2. Non-Darcy flow around the wellbore, and

3. Two-phase flow at the bottom of the well.



[0058] The third problem, which is the most important one, can be avoided by monitoring the flowing wellbore pressure and adjusting the rate accordingly. These three complicating factors should be avoided for all the transient tests, if possible.

[0059] During the first drawdown, when an infinite acting (without storage effect) period is reached approximately, the test is continued a few more hours depending on the size of the drainage area.

[0060] Next, the well tool 14 is lowered to the top of the lower zone as illustrated in Figure 2 while monitoring measured flow rate and pressure. If there is a recordable rate from this layer, at time t2, the production rate should be changed to another rate. The rate can be increased or decreased according to the threshold value of the flowmeter and the bubble point pressure of the reservoir fluid. As can be seen in Figure 3A, the flow rate is increased. If the rate is not recordable the test is terminated. A buildup test for further interpretation as a single-layered reservoir could be performed.

[0061] If the rate is recordable, the test should be continued from t3 to t4 for another few hours until another storage-free infinite acting period is reached. The test can be terminated at time t4. The interpretation of measured rate and pressure data is discussed below after the test for a producing or short shut-in well is described.

Producing or short shut-in wells



[0062] If the well is already producing at a stabilized rate, a short flow profile (production logging) test should be conducted to check if the bottom layer is producing. If there is enough production from the bottom layer to be detected, then as in Figure 1, the production logging tool 14 is returned to the top of the whole producing reservoir and the test is started by decreasing the flow rate, q1 (t1 as in Figure 4A to another rate, q1(t2). The well is allowed to continue flowing until time t2, when the well reaches the storage-free infinite acting period. At the end of this period, the tool string should be lowered just to the top of the bottom layer as in Figure 2. At the time t3, the flow rate is increased back to approximately q1 (t1 During the test, the rates should be kept above the threshold value of the flowmeter, and well bore pressure should be kept above the bubble point pressure of the reservoir fluid.

[0063] If the test precedes a short shut-in, the procedure will be the same, but the interpretation will be slightly different.

[0064] The test procedure described above is applicable for a layer system in which the lower zone permeability in less than the upper zone. If the upper zone is less permeable, then the testing sequence should be changed accordingly.

Analysis of sequential drawdown test



[0065] In this section, the method according to the invention is described to estimate individual layer parameters from measured wellbore pressure and sandface rate data. The automatic type-curve (history) matching techniques are used to estimate k1, k2, sy, and s2. In other words, Eq. 8 is minimized with respect to parameters k1, k2, S1 and s2. An automatic type-curve matching method is described in Appendix B to this description of the invention. Unlike the semilog method, the automatic type curve matching usually fits early time data as well as the storage-free infinite acting period if it exists to a given model.

Analysis of the first drawdown test:



[0066] Figure 5 presents the wellbore pressure data for synthetic sequential drawdown tests, and Figure 6 presents sandface flow rate data for the same test using the reservoir and fluid data given in Table 1. As can be seen from Figure 6, the test is started from the initial conditions and the well continues to produce 238 m3/day (1,500 bbl/day) for 12 hours. For the second drawdown, the rate is increased from 238 m3/day (1,500 bbl/day) to 476 m3/day (3,000 bbl/day). Figure 6 shows the total and individual flow rates from each zone. In an actual test, during the first drawdown, only total flow rate, ql(t), will be measured. During the second drawdown, only the rate from the bottom zone will be measured. It is also important to record the flow rate from the lower layer for a few minutes just before the second drawdown test.

[0067] The automatic type-curve matching approach is suitable for this purpose. If it is applicable, the semilog portion of the pressure data should also be analyzed. In general, type-curve matching with the wellbore pressure and sandface rate is rather straightforward. A brief mathematical description of the automatic type-curve matching procedure is given in Appendix B. In any case, the automatic type-curve method that is used fits the first drawdown data to a single layered, homogeneous model. The estimated values of and 5 are where





[0068] At the end of the first drawdown test, the rate from the bottom layer, q12, should also be measured before starting the second drawdown test.

[0069] Strictly speaking, from the first test, k1, k2, s1, and s2 can be calculated by using deconvolution methods. However, the deconvolution process is very sensitive to measurement errors, particularly errors in flow rate measurements. On the other hand, the convolution process, Eq. 3 is a smoothing operation, and it is less sensitive to measurement errors. Thus, the second drawdown test described below almost assures an accurate estimation of the layer parameters. Furthermore, the second transient creates enough sensitivity to the parameters of the less permeable layer.

Analysis of the second drawdown test



[0070] During this test, the wellbore pressure for the whole system and flow rate for the bottom layer are measured. Figures 5 and 6 present wellbore pressure and rate data respectively for the second as well as the first drawdown. These data are analyzed using the automatic type-curve matching method described above.

[0071] To estimate k2 and s2 from measured wellbore pressure and sandface rate data, the following equation is minimized:

where

β=[k2,s2]

q221(t1)=measured sandface rate data from the bottom layer

ηi(β,t1)=computed sandface rate for the bottom layer

Two different methods can be used for the minimization of Eq. 15.


First method



[0072] The computed sandface rate of the bottom layer-for a variable total rate can be expressed as:

In Eq. 2, Δpwf is the measured well bore pressure during the second drawdown. The Laplace transform of f(t) function in Eq. 16 can be expressed as (from Eq. 2):

The function f(z) in Eq. 17 is only a function of the lower layer parameters, k2 and s2. From the convolution of f(t) and Δpwf(t), η(β,t) can be obtained by automatic type-curve matching. Thus, using η(β,t) and measured q22(t), Eq. 15 is used to estimate k2 and s2. The estimated values are:



These estimated values of k2 and s2 are somewhat lower than the actual values (k2=10 and s2=10) which raises the question of whether or not Eq. 16 is indeed a correct solution. The direct solution of Eq. 16 gives correct values of the sandface flow rate for the constant wellbore storage case.

[0073] The f(z) function is the Laplace transform of the dimensionless rate, qo, for a well producing a constant pressure in an infinite radial reservoir. The flow rate qD changes very slowly with time. In other words, f(t) is not very sensitive to change in k2 and s2. This ill-posedness becomes worse if the sandface rate is not accurately measured at very early times. Thus, an alternate approach for the estimation of k2 and s2 is used to produce a more accurate estimate.

Second method



[0074] Eq. 16 can also be expressed as:

where

q'D=qsf/qt=total normalized rate, and Δpsf is defined by Eq. 1.



[0075] In order to compute n(β,t), the total rate, qo, must be measured. The total rate cannot be measured unless two flowmeters are used simultaneously. This is not practical using currently available logging tools. Thus, qo must be determined independently. This is not difficult since during the first drawdown, the behavior of the wellbore storage is known. The sandface flow rate can either be approximated by Eq. 5 or 6 or any other form. It is also important to measure total flow rate just at the end of the second drawdown test. If the wellbore storage is constant, the problem becomes easier. The Laplace transform of η(β,t) can be written from Eq. 18 as,

C=wellbore storage constant



[0076] Since k and 5 are known from the first test, k2 and s2 can be estimated by minimizing Eq. 15 with respect to measured rate, q22(t), and calculated rate, η(β,t), from Eq. 19.

[0077] For the test data presented by Figures 5 and 6, the estimated k2 and s2 are:

and

These values are very close to the actual values. The eigenvalues for k2 and s2 are λ1=22,3 MPa (3244 psia) and λ2≈26 MPa (3771 psia), respectively. As can be seen from these two eigenvalues, the sensitivity of each parameter to the model and the measurement is very high.

[0078] Because no a priori information is assumed about the wellbore storage behavior during the analysis of the second drawdown, the first method can be used to estimate the lower limit of k2 and s2 in order to check the values calculated from the second method.

[0079] Thus there has been provided according to the invention a method for testing a well to estimate individual permeabilities and skin factors of layered reservoirs. A novel two-step sequential drawdown method for layered reservoirs has been provided. The invention provides unique estimates of layer parameters from simultaneously measured wellbore and sandface flow rate data which are sequentially acquired from both layers. The invention provides unique estimates of the parameters distinguished from prior art drawdown or buildup tests using only wellbore pressure data.

[0080] The invention uses in its estimation steps the nonlinear least-squares (Marquardt) method to estimate layer parameters from simultaneously measured wellbore pressure and sandface flow rate data. A general criterion is used for the quantitative analysis of the uniqueness of estimated parameters. The criterion can be applied to automatic type-curve matching techniques.

[0081] The new testing and estimation techniques according to the invention can be extended to multilayered reservoirs. In principle, one drawdown test per layer should be done for multilayered reservoirs. During each drawdown test, the wellbore pressure and the sandface rate should be measured simultaneously.

[0082] The new testing technique can be generalized straightforwardly to layered reservoirs with crossflow.

[0083] The testing method according to the invention also can be used to estimate skin factors for each perforated interval of a well in a single layer reservoir.

[0084] If the initial pressures of each layer are different, the analysis technique has to be slightly modified. For new wells, the initial pressure of each layer can be obtained easily from wireline formation testers.

[0085] Nonlinear parameter estimation methods used in the testing method according to the invention provides a means to determine the degree of uncertainty of the estimated parameters as a function of the number of measurements as well as the number of parameters to be estimated for a given model. Prior art graphical type-curve methods cannot provide quantitative measures to the "matching" with respect to the quality of the measured data and the uniqueness of the number of parameters estimated.

Appendix A


Nomenclature



[0086] 

A=sensitivity matrix

AT=transpose of matrix A

a=element of matrix A

C=wellbore storage coefficient, cm3/atm

ct=system total compressibility, atm-'

Ei(-x)=exponential integral

g=gradient vector

h=layer thickness, cm

h=average thickness of a layered reservoir, cm

H=Hessian matrix

Ko=modified Bessel function of the second kind and order zero

K1=modified Bessel function of the second kind and order one

k=permeability, darcy

k=average permeability, darcy

m=number of data points

nl=number of layers in a stratified system

p=pressure, atm

pwf=flowing bottomhole pressure, atm

q=production rate, cm3/s

qsf=sandface production rate cm3/s

qt=total bottomhole flow rate, cm3/s

r=radial distance, cm

r=residual vector

rw=wellbore radius, cm

s=skin factor, dimensionless

s=average skin factor of multilayer systems

S=sum of the squares of the residuals in the least-squares method

t=time, second

v=eigenvector

z=Laplace image space variable


Greek symbols



[0087] 

α=rw/√ηj,s½

β=kh/µ=transmissability, darcy - cm/cp

β=parameter vector

β*=estimate of parameter vector β

A=difference

η=k/φµc=hydraulic diffusivity, cm2/s

η=computed dependent variable

λ=eigenvalue

φ=reservoir porosity, fraction

µ=reservoir fluid viscosity, cp

T=dummy integration variable

ξ=dummy integration variable


Subscripts and superscripts



[0088] 

D=dimensionless

j=layer number in a multilayer system

sf=sandface

w=wellbore

wf=flowing wellbore

-=Laplace transform of

'=derivative with respect to time


Appendix B



[0089] Type-curve matching sandface flow rate

[0090] Eq. 3 can be discretized as:



[0091] The integral in Eq. A-1 can be approximated from step t1 to t1+1 as



[0092] The right-hand side of Eq. A-2 can be integrated directly. Substitution of the integration results in Eq. 3 yields

where

and the first term in Eq. A-4 is given by

In Eqs. A-3 to A-5,qd is normalized measured sandface rate defined as



[0093] For type-curve matching the Δpsf is model dependent. For a homogeneous single-layer system, Δpsf is given by



[0094] The cylindrical source solution can also be used instead of the line source solution that is given by Eq. A-7. However, the difference between the two solutions is very small. Furthermore, for the minimization of Eq. 8, many function evaluations may be needed. Thus, Eq. A-7 will be used. If the Laplace transform solution is used, the minimization becomes very costly because for a given time, at least 8 function evaluations have to be made in order to obtain △psf(t).

[0095] In Eq. A-3, the time step is fixed by the sampling rate of the measured data. It is preferred for the integration that the data sampling rate be less than 0.1 hours; i.e., t1-t1-1<0.1 hours.

[0096] In order to estimate k and s from measured wellbore pressure and sandface flow rate data, Eq. 8 is minimized. Eq. 8 can be written as

where

β=[k.s]T

η(β,t1)=Δpwf(t1) in Eq. (A-3)

p1(T1)=the measured wellbore pressure


As mentioned earlier, S(β) is minimized by using the Marquardt method with simple constraints.

[0097] In the case of two-layered reservoirs, Eq. 1 should be used for Δpsf(t) instead of Eq. A-7.


Claims

1. A well test method for uniquely estimating the respective permeabilities k1, k2 and skin factor s1, s2 of at least two layers (layer-1, layer-2) of respective thicknesses h1, h2 of a reservoir, wherein a logging tool (14) which is equipped with means for measuring downhole fluid flow rates and pressures as a function of time is lowered into the wellbore, said test method comprising the following steps:-

positioning said logging tool (14) at the top of the upper layer (layer-1);

changing the surface flow rate from an initial flow rate at an initial time, ti;

measuring and recording the downhole fluid flow rate q1(t) and downhole pressure p1(t) during a first time interval t1 to t2;

positioning said logging tool (14) at the top of the lower layer (layer-2);

measuring and recording the downhole fluid flow rate q12(t3) at time t3;

changing the surface flow rate at time t3 to another flow rate;

measuring and recording the downhole fluid flow rate q22(t) and downhole pressure p2(t) during a second time interval t3 to t4;

estimating values k and s respectively representative of the permeability and the skin factor of the reservoir according to a single layered, homogeneous reservoir model, where

and

by matching the measured change in downhole pressure

with the convolution of the measured fluid flow rate q1(t), and an influence function Δpsf(t) which is a function of permeability k and skin factor s;

determining the permeability k2 and the skin factor s2 of the lower layer (layer-2) by matching the measured fluid flow rate q22(t) with the convolution of the measured change in downhole pressure

and an influence function f(t) which is a function of the lower layer (layer-2) permeability k2 and skin factor s2; and

determining permeability k1 and skin s1 from estimates of permeabilities k, k2 and skin factors s, s2.


 
2. The method of Claim 1 wherein the influence function Δpsf(t) is,

where

µ=reservoir fluid viscosity, cp

φ=reservoir porosity, fraction

rw=wellbore radius

Ei=Exponential integral.


 
3. The method of Claim 2 whereby the measured change in downhole pressure Δp1 (t) is matched to the calculated downhole pressure, Δpwf(t), where

by minimizing the function

where

β=[Lk, s].


 
4. The method of Claim 1 wherein for the lower layer, the measured fluid flow rate, q22(t), is matched with a calculated fluid flow rate η(β,t) according to the relation,

where qo=total normalized rate and the Laplace transform of the relation is,

where

β2=k2h2

C=wellbore storage constant

z=the Laplace image space variable

rw=wellbore radius

Ko=modified Bessel function of the second kind and order zero

K1=modified Bessel function of the second kind and order one

µ=reservoir fluid viscosity.


 
5. The method of Claim 4 whereby the measured fluid flow rate q22(t) is matched to the calculated fluid flow rate η(β,t) by minimizing the function

where

β=[k2, s2].


 
6. The method of Claim 1 wherein the well test is for a non-flowing well, and the surface flow rate is increased from a q, (t1 ) of zero flow rate at an initial time t1 to a stabilized flow rate of q, (t2) at a time t2 and is increased from the surface flow rate q2(t3) at a time t3 to a stabilized flow rate of q2(t4) at a later time, t4.
 
7. The method of Claim 1 wherein the well test is for a flowing well and the surface flow rate is decreased from a q1(t1) non-zero flow rate at an initial time t1 to a stabilized flow rate of q1(t2) at a time t2 and is increased from the surface flow rate from q, (t3) at a time t3 to a stabilized flow rate of q2(t4) at a later time.
 


Ansprüche

1. Bohrlochuntersuchungsverfahren zum eindeutigen Abschätzen der entsprechenden Durchlässigkeiten k1, k2 und des Wandfaktors s1, s2 von wenigstens zwei Schichten (layer-1, layer-2) entsprechender Mächtigkeit h1, h2 eines Untertagespeichers, wobei ein Logwerkzeug (14), das mit Mitteln zum Messen von bohrlochseitigen Fluiddurchflußleistungen und Drücken als Funktion der Zeit, in das Bohrloch abgesenkt wird, wobei das Untersuchungsverfahren folgende Schritte umfaßt:-

Positionieren des besagten Logwerkzeugs (14) an der Oberseite der oberen Schicht (layer-1);

Ändern der Oberflächendurchflußleistung von einer anfänglichen Durchflußleistung zu einer Anfangszeit t1;

Messen und Aufzeichnen der bohrlochseitigen Fluiddurchflußleistung q1(t) und des bohrlochseitigen Drucks p1(t) während eines ersten Zeitintervals t, bis t2;

Positionieren des besagten Logwerkzeugs (14) an der Oberseite der unteren Schicht (layer-2);

Messen und Aufzeichnen der bohrlochseitigen Fluiddurchflußleistung q12(t3) zur Zeit t3;

Ändern der Oberflächendurchflußleistung zur Zeit t34 auf eine andere Durchflußleistung;

Messen und Aufzeichnen der bohrlochseitigen Fluiddurchflußleistung q22(t) und des bohrlochseitigen Drucks p2(t) während eines zweiten Zeitintervals t3 bis t4;

Abschätzen von Werten k bzw. s, die für die Durchlässigkeit und den Wandfaktor des Untertagespeichers repräsentativ sind, und zwar entsprechend einem Modell für einen einschichtigen, homogenen Untertagespeicher, wobei

und

ist, indem die gemessene Änderung im bohrlochseitigen Druck

mit der Faltung der gemessenen Fluiddurchflußleistung q1(t) und einer Einflußfunktion Δpsf(t), die eine Funktion der Durchlässigkeit k und des Wandfaktors 5 ist, angepaßt wird;

Bestimmen der Durchlässigkeit k2 und des Wandfaktors s2 der unteren Schicht (layer-2) durch Anpassen der gemessenen Fluiddurchflußleistung q22(t) mit der Flatung der gemessenen Änderung im bohrlochseitigen Druck

und einer Einflußfunktion f(t), die eine Funktion der Durchlässigkeit k2 und des Wandfaktors s2 der unteren Schicht (layer-2) ist; und

Bestimmen der Durchlässigkeit k, und des Wandfaktors s, aus Abschätzungen der Durchlässigkeiten k, k2 und der Wandfaktoren s, s2.


 
2. Verfahren nach Anspruch 1, wobei die Einflußfunktion Δpsf(t)

ist, wobei

µ=Fluidviskosität des Untertagespeichers in cP,

φ=Untertagespeicherporosität, Bruchteil,

rw=Bohrlochradius und

Ei=Exponentialintegral ist.


 
3. Verfahren nach Anspruch 2, wobei die gemessen Änderung im bohrlochseitigen Druck Δp1(t) an den berechneten bohrlochseitigen Druck Δpwf(t) angepaßt wird, wobei

ist, durch Minimieren der Funktion

wobei

β=[k, s] ist.


 
4. Verfahren nach Anspruch 1, wobei für die untere Schicht die gemessene Fluiddurchflußleistung q22(t) mit einer berechneten Fluiddurchflußleistung η(ß,t) gemäß folgender Relation

angepaßt wird, wobei q'D die gesamte normierte Leistung und die Laplace-Transformation der Relation



ist, wobei

β2=k2h2/µ,

C=Bohrlochspeicherkonstante,

z=Laplacesche Bildraumvariable,

rw=Bohrlochradius,

Ko=modifizierte Besselfunktion zweiter Art und nullter Ordnung,

K1=modifizierte Besselfunktion zweiter Art und erster Ordnung und

µ=Fluidviskosität des Untertagespeichers ist.


 
5. Verfahren nach Anspruch 4, wobei die gemessen Fluiddurchflußleistung q22(t) an die berechnete Fluiddurchflußleistung η)(ß,t) durch Minimieren der Funktion

angepaßt wird, wobei β=[k2,s2] ist.
 
6. Verfahren nach Anspruch 1, wobei die Bohrlochuntersuchung für ein strömungsfreies Bohrloch ist und die Oberflächendurchflußleistung von einem Wert q1(t1) einer Null-Durchflußleistung zu einer Anfangszeit t1 auf eine stabilisierte Durchflußleistung q1(t2) zu einer Zeit t2 erhöht sowie von der Oberflächendurchflußleistung q2(t3) zu einer Zeit t3 auf eine stabilisierte Durchflußleistung q2(t4) zu einer späteren Zeit t4 erhöht wird.
 
7. Verfahren nach Anspruch 1, wobei die Bohrlochuntersuchung für ein förderndes Bohrloch ist und die Oberflächendurchflußleistung von einer Durchflußleistung q1(t1) ungleich null zu einer Anfangszeit t, auf eine stabilisierte Durchflußleistung q1(t2) abgesenkt und von der Oberflächendurchflußleistung q1(t3) zu einer Zeit t3 auf eine stabilisierte Durchflußleistung q2(t4) zu einer späteren Zeit erhöht wird.
 


Revendications

1. Une méthode d'essai de puits, ayant pour objet d'estimer de manière unique les perméabilités k1, k2, et les coefficients pariétaux s1, s2 se rapportant à au moins deux couches (couche-1, couche-2) d'une épaisseur respective h1, h2, d'un réservoir, dans lequel un outil de diagraphie (14), équipé d'un dispositif de mesure du débit et de la pression de fond du fluide en fonction du temps, est descendu dans le puits, ladite méthode d'essai comprenant les étapes de:-

positionnement dudit outil de diagraphie (14) au sommet de la couche supérieure (couche 1);

changement du débit de surface à partir d'un débit initial à un instant initial tl;

mesure et enregistrement du débit de fond du fluide ql(t) et de la pression de fond pi(t), pendant un premier intervalle de temps t, à t2;

positionnement dudit outil de diagraphie (14) au sommet de la couche inférieure (couche-2);

mesure et enregistrement du débit de fond q12(t3) du fluide à l'instant t3;

changement du débit de surface à l'instant t3 pour au autre débit;

mesure et enregistrement du débit de fond q22(t) du fluide et de la pression de fond pz(t) du fluide pendant un second intervalle de temps t3 à t4;

estimation de valeurs k et s respectivement représentatives de la perméabilité et du coefficient pariétal du réservoir selon un modèle de réservoir homogène à une seule couche, dans lequel:

et

faisant correspondre le changement mesuré dans la pression de fond

avec la convolution du débit q1(t) mesuré et d'une fonction d'influence Δpsf(t) qui est fonction de la perméabilité k et du coefficient pariétal s;

détermination de la perméabilité k2 et du coefficient pariétal s2 de la couche inférieure (couche-2) en faisant correspondre le débit q22(t) du fluide mesuré

à la convolution du changement mesuré de la pression de fond

et d'une fonction d'influence f(t), qui est fonction de la perméabilité k2 et du coefficient pariétal s2 de la couche inférieure (couche-2); et

détermination de la perméabilité k1 et du coefficient s1 à partir d'estimations des perméabilités k, k2 et des coefficients pariétaux s, s2.


 
2. La méthode de la revendication 1, dans laquelle la fonction d'influence Δpsf(t) est

dans laquelle

µ=viscosité du fluide du reservoir, (cp)

φ=porosité du réservoir, (fraction)

rw=rayon du puits

Ei=intégrale exponentielle.


 
3. La méthode de la revendication 2, dans laquelle on fait correspondre le changement mesuré de la pression de fond ΔP1(t) à la pression de fond calculée Dpwf(t), où:

en minimisant la fonction

dans laquelle β=[k, s].
 
4. La méthode de la revendication 1, dans laquelle, pour la couche inférieure on fait correspondre le débit du fluide mesuré, q22(t) à un débit calculé η(β, t) du fluide, selon la relation

dans laquelle q'D=débit total normalisé, et la transformée de Laplace de la relation est:



β2=k2h2

C=constante d'accumulation du puits

z=variable de l'espace image de Laplace

rw=rayon du puits

Ko=fonction de Bessel de deuxième espèce et d'ordre zéro modifiée

K1=fonction de Bessel de deuxième espèce et d'ordre 1 modifiée

µ=viscosité du fluide du réservoir.


 
5. La méthode de la revendication 4, dans laquelle on fait correspondre le débit du fluide mesuré q22(t) au débit du fluide calculé η(β,t) en minimisant la fonction

où β=[k2,s2].
 
6. La méthode de la revendication 1, dans laquelle le puits testé est un puits sans écoulement et le débit de surface est augmenté depuis un débit q1(t1) égal à zéro, à un instant initial t1, jusqu'à un débit stabilisé q1(t2) à un instant t2, et augmente d'un débit de surface q2(t3) à un instant t3 jusqu'à un débit stabilisé q2(t4) à un instant ultérieur t4.
 
7. La méthode de la revendication 1, dans laquelle le puits testé est un puits en écoulement et le débit de surface est réduit depuis un débit non nul q1(t1), à un instant initial t1, jusqu'à un débit stabilisé q1(t2) à un instantt2, et augmente d'un débit de surface q1(t3) à un instant t3 jusqu'à un débit stabilisé q2(t4) à un instant ultérieur t4.
 




Drawing