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Copyright 2001, Society of Petroleum Engineers Inc. This paper was prepared for presentation at the SPE Reservoir Simulation Symposium held in Houston, Texas, 11–14 February 2001. This paper was selected for presentation by an SPE Program Committee following review of information contained in an abstract submitted by the author(s). Contents of the paper, as presented, have not been reviewed by the Society of Petroleum Engineers and are subject to correction by the author(s). The material, as presented, does not necessarily reflect any position of the Society of Petroleum Engineers, its officers, or members. Papers presented at SPE meetings are subject to publication review by Editorial Committees of the Society of Petroleum Engineers. Electronic reproduction, distribution, or storage of any part of this paper for commercial purposes without the written consent of the Society of Petroleum Engineers is prohibited. Permission to reproduce in print is restricted to an abstract of not more than 300 words; illustrations may not be copied. The abstract must contain conspicuous acknowledgment of where and by whom the paper was presented. Write Librarian, SPE, P.O. Box 833836, Richardson, TX 75083-3836, U.S.A., fax 01-972-952-9435. Abstract The extension of a previously reported well model to compositional and thermal applications is discussed. This multisegment, multi-branching wellbore model has been fully coupled to a commercial reservoir simulator which can operate in black-oil, compositional or thermal modes. In this paper, the discussion will focus on thermal, heavy oil applications where simulation requires a better representation of the wellbore geometry and the physics of fluid flow and heat transfer. Introduction Gravity drainage processes with possible steam (SAGD) or gas vapour (VAPEX) assistance and other recovery technologies often require the use of long horizontal wells with flow in an inner tubing and outer annulus. For example, a discussion of the design of a commercial Canadian SAGD heavy oil project is given by Edmunds and Suggett1. Carpenter and Dazet2 review the use of horizontal wells in a steam drive project in the Midway Sunset field in Kern County, California. An overview of recent advances in steamflood technology that includes a good discussion of horizontal well applications, and the impact of numerical simulation on this technology is given by Hong3. Thermal studies which simulate horizontal and vertical wells have been discussed by many authors. We briefly review some of the work on thermal fields in western Canada and California, USA. Horizontal infill well performance in a mature Midway- Sunset cyclic-steam project was simulated and analyzed by Chona et al.4 and Al-Hadrami et al.5,6. Other engineering analyses using thermal horizontal cyclic well simulations in Midway Sunset include Hazlett et al.7, Rajtar and Hazlett8 and Deo and Schamel9. In this region, the oil can be 14° API and 6000 cp at 32°. C. Chiou et al.10 discuss utilising simulation to develop strategies for the South Belridge field in California. A typical oil API for this field is 13° and viscosity is 2000 cp at 32° C. Somewhat heavier oils are found in Canada. A simulation study was carried out of the Burnt Lake Oil Sands lease which is part of the Cold Lake oil sands deposit, by Kisman and Yeung11. Here the oil is 11-12° API and 7000 cp at 30° C. They simulated the SAGD process of a 1000 metre long horizontal well pair. There has also been some success in using a single horizontal well with a SAGD process, as discussed by Oballa and Buchanan12. They used two representative oils, one similar to a viscous oil found at the UTF project13 of 1,000,000 cp at 12° C (8° API), and a more mobile oil with a viscosity of 6000 cp at 12° C which is similar to a Cold Lake oil. The UTF project is situated in the Athabasca tar sands deposit. The above reviewed studies have, for the most part, used the conventional wellbore line source/sink model available in any thermal simulator. Simulation technology for horizontal wells has improved dramatically since the late 1980’s. At this time Stone et al.14 described a horizontal well model that featured a mechanistic multi-phase fluid flow model in the wellbore, and allowed flow simultaneously in an inner tubing and outer annulus. This was designed to handle simulations in the near wellbore region of a dual-well SAGD process and, because of the more detailed flow regime map, could not handle larger-scale simulations for stability reasons. Also during this time period, Nghiem et al.15 carried out the Seventh SPE Comparative Solution Project concerning the modelling of horizontal wells in reservoir simulation. A variety of methods was used by the participants to model the inflow into the horizontal well model. These included the use of an inflow performance relationship with a separate well model or direct coupling by modelling the well as part of the grid. Similarly, there were various wellbore hydraulics models from a constant-pressure line-sink to friction pressure drop relations or simple functional fits of published holdup correlations. All of these SPE 66373 Thermal Simulation with Multisegment Wells T. W. Stone, Schlumberger GeoQuest, J. Bennett, Schlumberger GeoQuest, D. H.-S. Law, Alberta Research Council, J. A. Holmes, Schlumberger GeoQuest SPE Members 2 T.W. STONE, J. BENNETT, D. H.-S. LAW, J.A. HOLMES SPE 66373 horizontal well models were designed to run robustly and stably in large-scale field simulations. However, some were limited in the ability to calculate a multi-phase pressure drop, others in not allowing the wellbore model geometry to correspond to the engineering design of the well rather than to the simulation grid. Some of the methods allowed multi-phase pressure drops using explicit updates or other approximations. Recently, Tan et al.16 have described a fully coupled discretized thermal wellbore model with the ability to simulate flow in casing/annulus wellbore cells. Estimates of the relative flow rates are made based on phase saturations and straight-line relative permeability curves. These estimates are passed to a subroutine that calculates flow rates from the correlated Beggs and Brill17 measurements. Wellbore cells are connected to reservoir cells. A multisegment well model which can simulate flow in advanced wells was discussed by Holmes et al.18,19. This model, implemented in a commercial black oil simulator, is able to determine the local flowing conditions (the flow rate of each fluid and the pressure) throughout the well. It allows for pressure losses along the wellbore and across any flow control devices. In addition to being fully implicitly coupled, with crossflow modelling and the standard group control facilities, horizontal, multi-lateral wells and ‘smart’ wells containing flow control devices can also be modelled. The trajectory is not constrained by the simulation grid. For example, the wellbore may run outside the grid or across layers. Properties and geometry can be updated at any time in the simulation. In this paper, we first describe the implementation and enhancements to the implicit multisegment well model discussed in Ref. 18 that allow this model to run in compositional and thermal modes. In these modes, the EOS or thermal K-value treatment of the fluid PVT is extended to the wellbore flow. Phase volumes are computed in each segment which are then used to calculate the multi-phase pressure drop. In thermal mode, an enhancement allows heat transfer coefficients to be defined which permit heat loss to the reservoir, to another segment or to the overburden. Another enhancement allows individual segments to inject or produce fluids which permits the direct modelling of gas lift, down- hole water pumps or circulating wells, availablein any mode. It is important to properly initialise compositional and especially thermal wellbore simulations. A method for predicting the initial state within the well is also shown below. We then present four case studies. Each case study has been set up from published engineering analyses of fields in western Canada and California. The well model used in these studies is considerably more detailed than in the original published simulation work. Not only are the wellbore hydraulics more accurately modelled with multi-phase flow models, but also the geometry of the wells is specified in more detail. Wellbore geometry includes the ability to run the well outside the simulation grid, allowing the modelling of heat loss from a steam injection well to the formation, between the surface and the simulation grid. Also, an undulating well trajectory can be specified and is demonstrated in one of the studies. Fluid flow down an inner tubing and back along an outer completed annulus is demonstrated in three of the studies where heat transfer occurs between the inner tubing and outer annulus as well as heat transfer from the annulus to formation. Two of these studies contain a segment at the heel of a horizontal annulus that removes fluids to an external sink, allowing part of the circulating fluids to return to the surface while the remainder are injected, produced or stored in the wellbore. Where possible, differences are shown between the multisegment model and a standard line source/sink model that demonstrate the effects of modelling the improved wellbore physics. Description of the Multisegment Well Model The multisegment well model reported by Holmes et al.18 was originally implemented in a black oil simulator. It uses four main variables: PFFG gwT ,,, . These are, respectively, a total fluid flow rate through the segment, weighted fractional flows of water and gas, and pressure in the segment. This model has now been implemented in a compositionally based commercial simulator. Multisegment well model variables were chosen to represent the segment pressure P , total molar flow rate in the segment TG , component moles per segment fluid volume cM and internal energy per segment bulk volume E . A simple drift-flux model18 has also been implemented for black oil and compositional simulation, but not thermal simulation. This allows the phases to flow with unequal flow rates. If a drift-flux flow model is chosen in some or all of the segments, the total molar flow rate variable in those segments is replaced with total volume flow rate. A schematic of an example multi-lateral multisegment well is shown in Figure 1. Each segment consists of a ‘node’ and a ‘flowpath’ to its parent segment’s node. The node lies at the far end of the segment, i.e. the end furthest from the wellhead. At branch points, two or more segments may connect to the same node. Flow from the reservoir grid cells may also enter the segment at its node. In thermal simulations, energy can be transferred to a segment by conduction, from the formation or from neighbouring segments. Each segment has a length, diameter, roughness, area and volume. The volume is used for wellbore storage calculations, while the other attributes are properties of the flowpath and are used in the pressure loss calculation. In thermal simulations the segments have a wall volume, heat capacity, area and conductivity. In black oil and compositional mode there are 2+cN variables and equations for each segment node where cN is the number of components in the simulation. In thermal mode an extra energy equation is needed. The first cN equations are material balance equations for each component, SPE 66373 THERMAL SIMULATION WITH MULTISEGMENT WELLS 3 0=+-- D D = åå ÎÎ cn nj cj ni ci cn cn QqQt m R …………(1) cnmD is the molar gain in the amount of component c in the segment n over the time step tD . ciQ represents the molar flow rate through each inlet junction i to segment n . cnQ is the flow rate through the outlet junction of segment n . In equation (1), cjq is the flow rate from any reservoir grid blocks j connecting with segment n which in turn is obtained from an inflow performance relationship as described in Ref. 18. For production from the formation, the component mobilities within the connecting grid block are used. For injecting flows, a mobility relation as described in Ref. 19 is evaluated using the segment’s main variables so that the fluid mixture flowing into the formation reflects the contents of the segment. This inflow performance relationship includes hydrostatic depth corrections between the centre of the grid block and the depth of the completion, and between the segment’s node depth and the depth of the completion. In the work described in this paper, the depth correction between the centre of the grid block and the depth of the completion differs slightly from that described in Ref. 18. Here, the head is calculated from an average of the mobile fluid densities in the grid block, weighted according to the fluid saturations in the grid block, instead of the grid block’s relative permeabilities which were used in the previous work. These depth corrections are implicit. They allow the depth of the segment node to be different from the depth of the grid block, which is useful for modelling undulating horizontal wells or wells whose trajectory does not align with the grid’s orthogonal directions. In thermal simulation, energy is conserved in the segments according to 0=++-- D D = åå ÎÎ EsEn nj Ej ni Ei n En QQqQt E R .…(2) nED is the gain in energy stored in the segment fluids and wall during the time step tD . A cross-sectional area is set which, when multiplied by the segment length, gives the volume of the segment wall in which energy is stored. The amount of stored energy in the segment bulk volume and the rate of heat conduction from a segment to its neighbour are determined by input heat capacities and thermal conductivities. EiQ represents the energy flow rate through each inlet junction i to segment n including convective and conductive heat flow. EnQ is the energy flow rate through the outlet junction of segment n or through a specified external sink. Ejq is the inflow rate from any reservoir grid blocks j . This inflow includes energy convected via an inflow performance relationship as well as energy conducted through a specified heat transfer coefficient. EsQ accounts for energy gain/loss by heat transfer, specified with a heat transfer coefficient, to an external source/sink with a known temperature. For example, because the multisegment well is not constrained to lie within the simulation grid, this term can account for conductive heat loss to the overburden from a steam injection well. EsQ also represents heat transfer from one segment to another via a heat transfer coefficient. In this case, the connecting segment may be neither an inlet segment nor the outlet segment. For example, in simulations involving an inner tubing and outer annulus, conductive heat transfer can be modelled from each inner tubing segment to its companion outer annulus segment. In order that the sum of all phase volumes equals the segment volume, a volume balance equation is solved. The final equation for each segment, except the topmost segment, calculates a pressure drop as a function of flow rate through its outlet junction and is described in Ref. 18. This pressure loss includes a hydrostatic, friction and acceleration pressure drop across the segment. The multisegment well model offers a choice of three methods for calculating the pressure drop: 1. A homogeneous flow model, in which all phases flow with the same velocity. 2. A simple ‘drift flux’ vertical and inclined flow modelwhich allows the phases to flow with different velocities. 3. Interpolating a pre-calculated pressure drop table. Here, pressure loss data as a function of outlet pressure, flow rate, water fraction and gas fraction are supplied in the form of a Vertical Flow Performance (VFP) table. This model enables the use of more sophisticated multiphase flow models such as published hold-up correlations, for example Beggs and Brill17. These correlations can be used to construct the table in a separate software program. VFP tables are also useful for modelling pressure drops across specific devices such as chokes, for which there are no correlations currently built into the well model. A pressure drop scaling factor is available that allows the user to tune the pressure drop calculation. This multiplier can be set for each segment to be a constant or to be a function of water-oil ratio and/or gas-oil ratio. The top segment is the segment that corresponds to the well’s bottom hole reference depth. Pressure in this segment is the same as the well’s bottom hole pressure (BHP). Material, energy and volume balance equations are solved in this segment as described above. In place of the pressure drop equation, the equation used in the top segment is the well’s control mode equation. All of the well and group control modes available with the standard well model in black-oil, compositional and thermal modes are available to the multisegment well model. In addition, the multisegment well model is fully compatible with the other available features 4 T.W. STONE, J. BENNETT, D. H.-S. LAW, J.A. HOLMES SPE 66373 such as group control options, pressure maintenance, economic limits (including completion limits), etc. Initialisation of the Multisegment Well Model To initialise the set of compositional molar densities, cM , and energy density E , we extend a simple idea originally used by Modine and Coats20. A wellbore reservoir volume balance was employed in their work to determine the wellbore phase saturations. Individual phase rates were calculated from the inflow performance relationship for each completion and the total volume flow rates for all nodes were accumulated throughout the wellbore. Then a tri-diagonal matrix equation was set up to solve for the corresponding phase saturations. An initial pressure is needed for each layer but they did not discuss the formulation of the wellbore pressure gradient. We use the same idea as follows. An initial pressure solution is estimated using an average wellbore density and a given BHP. Then the total volume flow rates for all segments are determined starting from the furthest nodes in all branches. For each component, the molar injection/production from each completion and, if applicable, from the surface injection stream is then used together with the total volume flow rate in all segments to set up a tri-diagonal matrix to solve for the moles of this component per total fluid volume. This initialisation, which conserves reservoir fluid volumes, neglects compressibility and mass transfer effects within the wellbore, and hence is an approximation to the exact mass conservation. An energy prediction for thermal mode follows the same idea. The volume flow rates together with the energy injection/production from each completion and surface injection stream form a matrix equation which is solved for energy densities. Account is taken of the energy stored in the walls. Completion energy injection and production includes both convective and conductive heat transfer. Enhancements: External Source/Sink It is possible to import water or gas into a segment from a source that is external to the reservoir grid. The import rate may be defined either as a constant value or as a function of the segment’s pressure. The imported fluid is added to fluid flowing through the segment. There are a number of possible applications for this facility. Gas import may be used to model the effects of lift gas injection, to examine the kick-off process for example. Gas lift may even be used in a thermal SAGD heavy oil project as reported by Edmunds1. Water import may be used to take account of the water injected to power a down-hole hydraulic pump. There is also an option to remove fluid from a segment to an external sink, at a rate that is a function of the segment’s pressure. This facility is primarily intended for use with the thermal option to model recirculating wells. Enhancements: Heat Transfer Coefficients Heat transfer can take place along the well and across the well, from the segment to the reservoir grid, to another segment or to a specified fixed external temperature. The heat transfer rate, htQ , to/from the segment is ( ) hexicisseght RTTLQ /,,-×= ………………………….(3) where L is the thermal contact length, segT is the temperature in the segment exicisT ,, is the temperature of a target segment or completion grid block or external fixed temperature, hR is the specific thermal resistance Thermal resistance can be thought of as an inverse heat transfer coefficient per unit length, for example with metric units 1- ÷ ø ö ç è æ °×× CDm KJ . This thermal resistance to heat transfer from the segment to the formation can be determined as presented by Prats21. As shown in Figure 2, it may include resistance due to scale deposits on the pipe wall, insulation, annulus gas, casing wall, cement and altered formation. Along the well, heat transfer by conduction through the walls is included in the energy flow term EiQ in equation 2. Heat transfer is handled implicitly in the numerical scheme. Case Studies Four case studies were designed with two objectives. Firstly, the design of three of the four studies closely followed published engineering simulation studies of fields in western Canada and California, USA. As many of the reported parameters as possible were accounted for including wellbore design, placement, rock parameters such as absolute and relative permeabilities and injection rates. The fourth study uses parameters reported in a thermal SPE Comparative Solution Project22. Secondly, to highlight the capability of the multisegment well model reported in this paper, we then added parameters in wellbore design, heat loss and trajectory that may not have been used in the original work but were typical of the thermal operation on which the original simulation study was based. All additional parameters were found either in the original study or in other published accounts and are referenced. The purpose of adhering closely to the actual process and simulation conditions was to demonstrate the ability of the thermal multisegment well model to handle the wellbore physics and geometry. A second purpose was to demonstrate stability and robustness under these conditions. Table 1 contains reservoir properties for the four studies. Well design parameters are listed in Table 2. Table 3 contains well operation rates and limits and Table 4 contains some simulation parameters. SPE 66373 THERMAL SIMULATION WITH MULTISEGMENT WELLS 5 Case Study 1 Sheppard et al.23 review the operations of Husky Oil at the Pike’s Peak heavy oil field in Saskatchewan, Canada. This field is part of the Lloydminster deposit and features a 12° API oil, GOR of 15 m3/m3 and a gas-free viscosity of 25000 cp at 18° C. We have based our first case study on properties of this field. Two 400 m horizontal undulating wells have been simulated with a 7 m vertical separation. Net pay thickness is 20 m. A schematic of a section of the upper injector and lower producer is shown in Figure 3. Figure 4a shows the undulating trajectory. This study models the start of a SAGD operation, where these two horizontal wells are initially circulating hot steam for 60 days in order to heat the region of reservoirnear the wells for the purpose of establishing hot communication. Both wells are open during this time so that some of the circulating steam may enter the reservoir and reservoir fluids may be produced. Subsequently, after 60 days, circulation is stopped, the upper horizontal well becomes an injector, the lower a producer. Both wells were modelled with inner tubing and outer annulus segments for fluid and energy flow. During the startup period, 65% quality steam at 250° C was injected into the inner tubing of both wells and circulated back along the annulus. An external sink was defined at the heel of the annulus of both wells where fluids were removed to a specified external pressure. Heat transfer was modelled between the inner tubing and outer annulus as well as from the annulus to formation. An annulus to formation heat transfer coefficient was obtained from Prats21 who calculates this coefficient for heat loss from a steam injection well to undisturbed formation. For purposes of this study, heat transfer coefficients from inner tubing to outer annulus were estimated to be an order of magnitude larger than those to the formation, because of the lower thermal resistance. We obtained Lloydminster oil-water and oil-gas relative permeability curves and endpoints from Wang and Chen24 who also did a simulation study of a field in this region. The P-T solution gas K-value function was taken to be that of methane25. The heavy component was non-volatile. The problem is symmetric along the axis of the wells. To simulate half of a multisegment well, we have used half the cross-sectional flow areas for the tubing/casing and the full hydraulic diameters for each. The retention of the original diameters was in order to correctly calculate the multi-phase Reynold’s number in the pressure drop calculation, while the flow areas and volumes were halved to account for the symmetry. The thermal resistance was doubled. Injection rates as noted in Ref. 23 were halved. The size of the first grid cell in the direction orthogonal to the well axis and well PI were also halved to account for the symmetry. Figures 4a and 4b show temperature contours along the axis of the well at the end of the 60 day circulation period and at 365 days. During the initial 60 days, there was insufficient injectivity for any notable steam penetration into the formation – all of the heat present in the reservoir was conducted from the wells. Undulation of the wells causes some areas of the formation to heat more readily than others. There is a hotter zone that can be seen in Figure 4 at 365 days around the middle of the upper injection well. This zone is in the region of a depression in the trajectory of this injector. It results from a local crossflow that is causing the steam to inject from adjoining segments and produce at a single segment in the middle, depressed region. A local circulation cell is established. Part of the steam injected in this region is immediately produced due to the local crossflow cell, part travels downward to be produced in the lower producer while the rest flows upwards to enhance the steam chest. There is also a smaller circulation cell near the toe. Both of these cells are stable in time. The circulation rate slowly decreases as the steam chamber builds in these regions of the well and the cells can eventually die out. Figure 5 shows temperature contours in the plane orthogonal to the well at the same times as in Figure 4. Figure 6 is a plot at 365 days of the hydrostatic, frictional and accelerational pressure drops in the upper injection well. Hydrostatic and frictional heads are presented along the outer annulus while the accelerational head is shown through the entire length. The acceleration pressure drop, which models a change in fluid inertia, is important only in the last inner tubing segment before the annular segments begin. Acceleration pressure drop is caused by a change in velocity of the fluids at the toe of the well where the cross section to flow changes. The friction pressure drop is highest in magnitude at the point where some multi-phase production is occurring in the middle of the annulus as discussed in the above paragraph. Hydrostatic contributions to the pressure drop are also shown. These are a result of the undulating trajectory. The largest contribution to the hydrostatic head occurs at the heel of the annulus, where stagnant water has pooled (liquid holdup fraction = 0.98). Case Study 2 We have followed Kisman et al.11 who carried out a two- dimensional simulation study of the Burnt Lake oil sands lease situated in the Cold Lake Alberta oil sands deposit. Oil is 12° API, dead oil viscosity is 80,000 cp at 12° C and the GOR is 7.5 m3/m3. Net pay thickness is 30 m. Their 2-D grid has been extended to 3-D in our study. We have retained the same x-y grid sizes and dimensions as in the original simulation and have added the extra dimension because this study concerns the simulation of a single-well SAGD operation which is more three dimensional in nature. The single well in our simulation study features an inner tubing and outer annulus. 90% quality steam was injected into the inner tubing at a temperature of 295° C. All fluids were removed from the heel of the annulus to a specified external pressure. Since the well is open, upon leaving the toe of the tubing the injected steam can either return down the outer annulus and out of the well to the external sink, or inject into the formation. Fluids from the formation can be produced at 6 T.W. STONE, J. BENNETT, D. H.-S. LAW, J.A. HOLMES SPE 66373 any completion along the well. The well was simulated over a ten year time period. Symmetry was again employed as in the first study and heat transfer coefficients were evaluated similarly. The above paragraphs on these topics under Case Study 1 are applicable here as well. A schematic of this study is presented in Figure 7. We did not include an undulating trajectory. The well is 800 m in length. As can be noted in Table 2, the ID and OD of the outer annulus are less than in the first study. The smaller diameters were chosen since an elevated pressure drop in the outer annulus is necessary to promote injection into the reservoir. Relative permeability curves and endpoints were also obtained from Reference 11. The intermediate volatility oil discussed in that reference was used in this study including K- value parameters and other oil properties. Measured volatility of the light component was less than that of methane and seems to resemble ethane or propane25. Oil saturations for each vertical layer and the use of permeability barriers were also taken from Ref. 11. Although different relative permeability curves were used for each layer in that reference, only those for layer 2 were presented and these were used throughout the grid in this study. Figures 8a and 8b show temperature contours at two times along the axis of the well demonstrating growth of the hot zone near the toe. Steam and hot water are injected into the formation here and fluids are produced further back towards the heel of the annulus. Figure 9 shows injection and production rates along the outer annulus at selected times. Production is favored at the heel because of the higher pressure drop down the annulus. This causes a more favorable drawdown at the heel. Injection can be seen moving back from the toe to the heel in the same figure. Case Study 3 This case study concerns a modification of one of the problems used for the Fourth SPE Comparative Solution Project: Comparison of Steam Injection Simulators22. We have employed the same two-dimensional radial cross- sectional grid together with an oil consisting of two volatile components and one nonvolatile component as described in that paper. Singlewell cyclic steam injection is modelled. A schematic of the well used in this simulation is shown in Figure 10. The injection well in our study extends from the surface in order to model the reduction of steam quality due to heat loss in the overburden. Pressure in the first segment of the multisegment well model is therefore a tubing head pressure. Segments that model flow in the tubing are defined from the surface downwards to the midpoint of the lowest grid block and annular segments are then used to model flow up to a packer situated at the top of the pay zone. Heat transfer coefficients were employed as discussed by Prats21. Above the packer, heat loss occurred from tubing through a gas filled annulus, annulus wall and cement to formation. Below the packer, heat loss occurred from the annulus to disturbed formation and then to undisturbed formation. Heat transfer coefficients from tubing to annulus in the lower completed part of the well were estimated as discussed above under Case Study 1. Cycles of the same duration, injection/production rates and other parameters from Reference 22 were used. The producer is represented by a standard (non multisegment) well model with a BHP reference depth at the top of the formation. Figure 11 is a plot of the steam quality along the injector at selected times. Steam quality is lost down the injector because of energy loss due to conduction heat transfer in the overburden. It remains roughly constant throughout the three cycles because the wellbore temperature and pressure stay the same. Figure 12 shows differences between production with and without the multisegment well model for the injector. The simulation without the multisegment well model was corrected for the loss of steam quality in the injector predicted by the multisegment well model study, as shown in Figure 11. Using this correction in the standard well model case makes it agree it closely with the multisegment well model case. Case Study 4 Our final case study simulates the cyclic recovery of a California Midway-Sunset oil from a short radius horizontal well. Various published studies of Midway-Sunset fields were merged to define this simulation. Figures 13a and 13b contain schematics for this study. A short radius horizontal well as described by Carpenter and Dazet2 was modelled. They discussed drilling and completion design of horizontal wells in a Midway-Sunset steam drive. Of the three wells mentioned in that paper, we use parameters for the second. This is a well placed just above an oil-water contact with tubing extending from the surface through a gas-filled annulus (with a packer at the casing point) to a kick-off-point (KOP), a turning radius and then to a horizontal completed liner. The slotted length is 113 m, turning radius is 13 m, KOP is at a depth of 528 m and diameter of the liner is .09 m. There is no flow through the annulus. The gridding for our simulation follows that of Chona et al.4 who analysed the performance of a horizontal infill well in a mature cyclic-steam project in Midway-Sunset. We have used their grid dimensions and sizes. Oil viscosities, PVT and relative permermeability curves including temperature- dependent endpoints were taken from Al-Hadrami et al.5 who simulated the same field. Although several vertical wells were interspersed with infill horizontal wells in References 4 and 5, we have simply placed a single short radius horizontal well along a plane of symmetry. In addition to the design parameters of this well as discussed in the above paragraph, we have added an 8° dip in the horizontal section. In Reference 5, the top of the simulated reservoir was a mature steam-chest which we have included in our study. Initial temperatures, oil, water and gas saturations as presented in SPE 66373 THERMAL SIMULATION WITH MULTISEGMENT WELLS 7 that reference were used together with a non-equilibrium initialisation to fix the initial conditions. We have taken a representative cycle to be 15 days injection, 3 days soak and 90 days production. The simulation was run out to 3 years (10 cycles). The multisegment well in this study cuts across grid lines. It initially starts 12 m above the oil-water contact but continues into the transition zone at the toe. While angling slightly downwards with an 8° dip, it cuts across grid layers while maintaining a linear direction (as discussed above, the simulator corrects for segment nodes that are at a different depth than grid nodes). One of the purposes of this study is to illustrate a thermal multisegment well trajectory that does not follow the grid, another is to simulate a less than optimal well placement. Figure 14 shows the change in steam quality along the well at the end of several injection cycles. In this figure, the contributions to heat loss from the overburden and reservoir are shown. During the early stages of the first cycle, the injection steam quality is reduced from 70% at the surface to zero at a point approximately half way down the completed liner. By the end of the first injection cycle, quality at the toe has risen to 24%, as can be seen in the figure. This is a result of energy (heat) loss from the wellbore in the overburden and reservoir. As the first cycle progresses, pressure in the injection well lowers somewhat as steam injectivity increases in the reservoir. As the pressure in the well lowers, the steam temperature lowers and heat loss decreases. In cycle 2 through to the last cycle, injection pressure stays approximately the same, which in turn allows the temperature and heat loss to remain constant. In this part of the run, there is only a 3% loss of steam quality from the surface to the toe of the well. Figure 15 shows the injection rates along the well at selected cycles. At the beginning of the simulation, injection occurs more uniformly from the middle towards the toe. During the second and third cycles, injectivity has notably improved at the toe. Injection during the final 10th cycle is approximately the same as during the third. In the first cycle, although the drawdown at the toe is less than in the middle, the PI to water is higher there because the toe is located in the water-to-oil transition zone. Once steam has gained a foothold in a part of the formation around the toe, injection tends to concentrate at that point for two reasons. Firstly, heating the oil here causes the viscosity to drop thereby increasing the total fluid mobility. Secondly, higher water saturations increase the water mobility and hence also increase the total fluid mobility. The simulator uses an implicit fluid mobility for injection wells. Figure 16 presents water and oil production rates along the well as a function of time. There is negligible water and oil production during the first production cycle. In the early cycles, oil production is more uniform along the length of the well with some oil production at the heel because of the higher oil PI. As the cycles progress, higher water production rates at the toe and a higher rate of heating around the toe due to steam injection cause oil production to improve notably here. Although there is only a very small water injection at the heel, oil production also improves somewhat in this region because of the gradual improvement in oil PI due to conduction heating of the formation. Water production is initially highest at the toe because the toe is located in the transition zone and this does not change in time. Figure 17 displays differences in oil production between the standard well model and multisegment well model simulations. During all production cycles, the standard well model produced much more water from the toe of the well and less oil from other areas, in particular the heel of the liner. The multisegment well model was able to producemore uniformly along the length of the well, as seen in Figure 16 and discussed above. Conduction heating improves the oil PI all along the liner. At the end of the 10 cycles, the oil PI at the heel is an order of magnitude higher than the simulation without the multisegment well due to heating of the formation. As a consequence, after 10 cycles the predicted oil production by the multisegment well was more than 2.5 that with the standard well model. Oil production from the toe region is approximately the same in both simulations. Stability and Robustness Figure 18 shows the time step sizes for all four studies. The most difficult case to simulate was the first study after the initial 60 day startup phase. No simulation problems were experienced during this initial period. After the changeover in the wells from circulation to injector and producer, the time step sizes were slow to improve, not reaching a 1 day size for 20 days. Once the steam chest had begun to develop and expand, the simulation proceeded more robustly, as can be seen in Figure 18. On the other hand, Case Study 2 proceeded robustly right from the beginning. A considerable degree of crossflow exists in this single well simulation study. Injection is occurring from nearer the toe of the outer annulus. Production is simultaneously occurring nearer the heel. The crossover point moves from the toe towards the heel in time. However, none of these appeared to degrade robustness. Case Study 3, the vertical cyclic simulation, demonstrated average stability and robustness for a cyclic run of this type. The small volumes of the innermost radial grid blocks and the high production rates combined with the heat loss were the primary reason for any reductions in time step size. Study 4, the cyclic run whose well trajectory crossed vertical layers, was very robust. Conclusions 1. We have described the implementation of a previously reported multisegment well model into a compositional simulator. Several enhancements were discussed which are important for the simulation of thermal processes. 2. Four case studies were constructed to highlight features of the thermal multisegment wells. Each was 8 T.W. STONE, J. BENNETT, D. H.-S. LAW, J.A. HOLMES SPE 66373 designed to realistically simulate thermal operations using horizontal or vertical wells. In each of these studies, we have hopefully demonstrated an improved understanding of the reservoir engineering by using an improved description of the well geometry, design and fluid/energy flow with the multisegment well model. Acknowledgements We would like to thank Schlumberger GeoQuest for permission to publish this paper. References 1. Edmunds, N.R. and Suggett, J.C.: “Design of a Commercial SAGD Heavy Oil Project”, SPE 30277 presented at the international Heavy Oil Symposium, Calgary, Alberta, Canada, 19-21 June 1995. 2. Carpenter, D.E., and Dazet, S.C.: “Horizontal Wells in a Steamdrive in the Midway Sunset Field”, SPE/DOE 24127 presented at the SPE/DOE Eighth Symposium on Enhanced Oil Recovery, Tulsa, Oklahoma, April 23-24, 1992. 3. Hong, K.C.: “Recent Advances in Steamflood Technology”, SPE 54078 presented at the 1999 International Thermal Operations and Heavy Oil Symposium held in Bakersfield, California, 17-19 March 1999. 4. Chona, R.A., Love, C.L. and Rajtar, J.M.: “Evaluation of a Horizontal Infill Well in a Mature Cyclic-Steam Project”, SPE 37087 presented at the 1996 SPE International Conference on Horizontal Well Technology, Calgary, Canada, 18-20 November, 1996. 5. Al-Hadrami, H., Rajtar, J.M., Chona, R.A., and Hazlett, W.G.: “Simulation Study of Development Strategies for a Gravity-Assisted, Cyclic-Steam Project”, SPE 38289 presented at the 1997 SPE Western Regional Meeting held in Long Beach, California, 25-27 June, 1997. 6. Al-Hadrami, H., Rajtar, J.M., Hazlett, W.G.: “Optimization of Horizontal Well Performance in a Mature Cyclic-Steam Project”, SPE 39081 presented at the Fifth Latin American and Caribbean SPE Conference, Rio de Janeiro, Brazil, 30 Aug – 3 Sept, 1997. 7. Hazlett, W.G., Love, C.L., Chona, R.A., and Rajtar, J.M.: “Simulation of Development Strategies for a Mature Midway-Sunset Cyclic-Steam Project”, SPE 37552 presented at the 1997 SPE International Thermal Operations and Heavy Oil Symposium, Bakersfield, California, 10-12 February, 1997. 8. Rajtar, J.M. and Hazlett, W.G.: “Cyclic-Steam Injection Initiation Project in Heavy Oil Reservoir – A Simulation Study”, SPE 53692 presented at the 1999 SPE Latin American and Caribbean Petroleum Engineering Conference held in Caracas, Venezuela, 21-23 April, 1999. 9. Deo, Milind D., Forster, Craig and Schamel, Steven: “Strategies for Steam Flood Optimization in a High-Water Saturation Reservoir in the Midway-Sunset Field”, SPE 54075 presented at the 1999 SPE International Thermal Operations and Heavy Oil Symposium held in Bakersfield, California, 17-19 March, 1999. 10. Chiou, C.S., Badger, S.D., Carlsen, M.M., Pereira, K.S.: “A Focus Development for Heavy Oil Reservoir: The Last Frontier at the South Belridge Field”, SPE 54625 presented at the 1999 SPE Western Regional Meeting held in Anchorage, Alaska, 26-28 May, 1999. 11. Kisman, K.E. and Yeung, K.C.: “Numerical Study of the SAGD Process in the Burnt Lake Oil Sands Lease”, SPE 30276 presented at the International Heavy Oil Symposium held in Calgary, Alberta, Canada, 19-21 June, 1995. 12. Oballa, Viera and Buchanan, W. Lloyd: “Single Horizontal Well in Thermal Recovery Processes”, SPE 37115 presented at the 1996 SPE International Conference on Horizontal Well Technology held in Calgary, Canada, 18-20 November, 1996. 13. Edmunds, N.R., Kovalsky, J.A., Gittins, S.D., and Pennacchioli, E.D.: “Review of the Phase A Steam Assisted Gravity Drainage Test at the AOSTRA UTF”, SPE 21529 presented at the First International Thermal Operations Symposium, Bakersfield, February 7-8, 1991.. 14. Stone, T.W., Edmunds, N.R. and Kristoff, B.J.: “A Comprehensive Wellbore/Reservoir Simulator”, SPE 18419 presented at the 10th SPE Symposium on Reservoir Simulation, Houston, Feb. 1989. 15. Nghiem, Long, Collins, David A. and Sharma, Ravi: “Seventh SPE Comparative Solution Project: Modelling of Horizontal Wells in Reservoir Simulation”, SPE 21221 presented at the 11th SPE Symposium on Reservoir Simulation held in Anaheim, California, February 17-20, 1991. 16. Tan, T.B., Butterworth, E. and Yang, P.: “Application of a Thermal Simulator With Fully Coupled Discretized Wellbore Simulation to SAGD”, Paper 2000-15 presented at the Canadian Institute of Mining, Metallurgy & Petroleum Society’s Canadian International Petroleum Conference 2000, June 4-8, 2000. 17. Beggs, H.D., Brill, J.P., Palmer, C.M., Payne, G.A.: “Evaluation of Inclined-Pipe, Two-Phase Liquid Holdup and Pressure-Loss Correlation Using Experimental Data”, SPE 6874, Journal of Petroleum Technology, p. 1198, 1979. 18. Holmes, J.A., Barkve, T., Lund, O.: “Application of a Multisegment Well Model to Simulate Flow in Advanced Wells”, SPE 50646 presented at the 1998 SPE European Petroleum Conference, The Hague, The Netherlands, 20- 22 October, 1998. 19. Holmes, J.A.: “Enhancements to the Strongly Coupled, Fully Implicit Well Model: Wellbore Crossflow Modeling and Collective Well Control”, SPE 12259 presented at the SPE Reservoir Simulation Symposium held in San Francisco, CA, November 15-18, 1983. 20. Modine, A.D., Coats, K.H.: “A Superposition Method for Representing Wellbore Crossflow in Reservoir SPE 66373 THERMAL SIMULATION WITH MULTISEGMENT WELLS 9 Simulation”, SPE 20746 presented at the 65th Annual Technical Conference and Exhibition of the Society of Petroleum Engineers, New Orleans, LA, Sept 23-26, 1990. 21. Prats, Michael: “Thermal Recovery”, SPE Monograph Series, Society of Petroleum Engineers,1986, Dallas. 22. Aziz, K., Ramesh, A.B., Woo, P.T.: “Fourth SPE Comparative Solution Project: Comparison of Steam Injection Simulators”, Journal of Petroleum Technology, 1576-1584, December, 1987. 23. 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Table 1 – Reservoir Properties for Case Studies Case Depth (m) Max Dip (m) Poros (%) Perm (d) Oil Sat (%) Init Press (bar) 1 500 0 34 5 89 33.5 2 396 0 22-33 1.5- 2.5 40- 80 31 3 457 0 33 0.5- 2.0 55 5.5 4 300 44 30 .3 80 1.4 Table 2 – Well Design Case ID Tubing (m) OD Tubing (m) ID Casing (m) OD Casing (m) Compl Length (m) 1 .076 .089 .219 .241 400 2 .090 .102 .125 .138 800 3 .076 .089 .219 .241 24 4 .089 .114 NA NA 94 Table 3 – Well Operation Case Water Inj Rate (m3/D) CWE Max Inj BHP (bar) Liquid Prod Rate (m3/D) Min Prod BHP (bar) Circ Rate (m3/D) 1 1200 50 1200 30 120 2 200 70 NA NA NA 3 160 70 160 1.2 NA 4 103 48 320 1.0 NA Table 4 – Simulation Parameters Case Gridding Time Simulated (yr) Max Time Step Size (D) 1 20´12´15 1 20 2 30´20´15 10 20 3 13´1´4 3 90 4 11´24´21 3 20 Figure 1: Schematic diagram illustrating the segment structure for an example multilateral well. 10 T.W. STONE, J. BENNETT, D. H.-S. LAW, J.A. HOLMES SPE 66373 Figure 2: Resistance to heat transfer between a bulk flow in a segment and unaltered formation (after Prats23). Figure 3: Schematic of the simulation in Case Study 1 – a dual- well SAGD study. Flow directions are shown for operation after the 60 day startup period. Figure 4a: Case Study 1: Temperature contours along the well axis at 60 days (end of circulation period) Figure 4b: Case Study 1: Temperature contours along the well axis at 365 days. Figure 5: Case Study 1: Temperature contours orthogonal to the well axis at 60 days (end of circulation period) and 365 days. SPE 66373 THERMAL SIMULATION WITH MULTISEGMENT WELLS 11 Figure 6: Case Study 1: Pressure drop along the annulus at 365 days. Figure 7: Schematic of the simulation in Case Study 2 – a single- well SAGD study. Figure 8a: Case Study 2: Temperature contours along the well axis at 350 days illustrating growth of the hot zone near the toe. Figure 8b: Case Study 2: Temperature contours along the well axis at 1460 days illustrating growth of the hot zone near the toe. Figure 9: Case Study 2: Production and Injection along the annulus at selected times. Figure 10: Schematic of the simulation in Case Study 3 – single vertical well cyclic steam injection. 12 T.W. STONE, J. BENNETT, D. H.-S. LAW, J.A. HOLMES SPE 66373 Figure 11: Case Study 3 – Steam quality along the injector at selected times. Figure 12: Case Study 3 – Production rates with and without the multisegment well model. Figure 13a: Schematic of the wellbore in Case Study 4 – single short radius horizontal well cyclic injection and production (after Carpenter and Dazet2). Figure 13b: Schematic of the simulation grid in Case Study 4 – single short radius horizontal well cyclic injection and production. (For clarity, some vertical grid refinement near the well has not been shown.) Figure 14: Case Study 4 – Steam quality in the well as a function of time. Figure 15: Case Study 4 – Injection rates along the well at selected cycles. SPE 66373 THERMAL SIMULATION WITH MULTISEGMENT WELLS 13 Figure 16: Case Study 4 – Water and Oil production rates along the well as a function of time. Figure 17: Case 4 oil production rate with and without a multi- segment well. Figure 18: Stability and Robustness - Timestepping for the four case studies.
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