Relative Permeability Studies of Gas-Water Flow Following Solvent Injection in Carbonate Rocks

1976 ◽  
Vol 16 (01) ◽  
pp. 23-30 ◽  
Author(s):  
F.N. Schneider ◽  
W.W. Owens

Abstract Flow studies were conducted of 19 preserved cores from four oil-wetcarbonate reservoirs to provide data for evaluating the water-rich, gas-injection improved recovery process. Results indicate that these cores werewater repellent following displacement of oil by a solvent similar to thereservoir solvent. Restored-state tests of some of the same cores followingcleaning by a polar solvent yielded water-wet flow behavior. These resultsindicate that tests of preserved cores are required if water-gas flow dataapplicable to oil-wet reservoirs are to be obtained. Water-gas relativepermeability data also were obtained from preserved cores following bothcomplete and preserved cores following both complete and incompletedisplacement of oil by solvent. The presence of a small "bypassed" oilsaturation presence of a small "bypassed" oil saturation significantlyincreased the trapped gas saturation and reduced water permeability atflood-out. Use of these data in a mathematical model of the reservoir processgave reduced water injectivities (compared process gave reduced waterinjectivities (compared with those attained during water preinjection) similarto those experienced in the field. Introduction Increased emphasis is being placed on the application of secondary andtertiary recovery processes for increasing oil recoveries from known fields.One of these processes involves the injection of gas that is rich either inlight hydrocarbons or in carbon dioxide. Under appropriate reservoir pressureand temperature conditions, rich-gas injections can develop a solvent zone thatwill miscibly displace the oil it contacts in the reservoir. A dry scavenginggas usually follows the injection of some predetermined volume of the rich gas.Water also may be injected alternately with the rich or dry gas to decrease thegas mobility and, thus, improve reservoir sweep efficiency. Mathematical modelstudies of these recovery processes are made frequently. In the planning stagesof the improved recovery program, the model studies assist in sizing therich-gas volume to be injected and the subsequent dry-gas and water volumes.Once the program has been put into operation, the model may be used to matchfield performance (such as injectivity, pressure, or productivity), diagnoseunexpected problems, and extrapolate the future performance. Relativepermeability data applicable to a reservoir recovery process are a prerequisiteto reliable performance predictions with a mathematical mode. This means thatthe predictions with a mathematical mode. This means that the displacementsequence and mechanisms that occur in the reservoir must be known andreproduced accurately in the laboratory flow test. One important additionalrequirement is the need for reservoir core samples that adequately representthe producing horizon. This paper is concerned with the development of relativepermeability data for application to a recovery process of permeability datafor application to a recovery process of the type just described. Theparticular reservoirs of interest are West Texas carbonates. In thesereservoirs, rich-gas injection is being used as a secondary recovery process.However, water preinjection was necessary to process. However, waterpreinjection was necessary to increase reservoir pressure to a level such thatmiscibility could be achieved between the reservoir oil and the subsequentlyinjected rich gas. Because of this water preinjection, the displacement processis essentially the same as would occur in a tertiary application (that is, after waterflooding). Thus, relative permeability data were obtained forseveral different displacement conditions, selected specifically to model thereservoir process shown schematically in Fig. 1. The stepwise simulation ofthis recovery process in laboratory flow tests is discussed later. Ofparticular interest in this study were the relative permeabilities applicableto the water-displacing-gas process, permeabilities applicable to thewater-displacing-gas process, permeabilities that are needed to model thegas-water injection permeabilities that are needed to model the gas-waterinjection process following solvent displacement of oil. process followingsolvent displacement of oil. SPEJ p. 23

2021 ◽  
Author(s):  
Mazda Irani ◽  
Nasser Sabet ◽  
Farzad Bashtani ◽  
Kousha Gohari

Summary Although the steam assisted gravity drainage (SAGD) process is still the preferred thermal-recovery process method for Athabascan deposits in Alberta, Canada, the interest in solvent-based techniques is growing due to reduce greenhouse-gas (GHG) emissions and water treatment concerns. In SAGD process, the thermodynamic trapping or subcool trapping is quite efficient due to strongly dependency of bitumen viscosity to temperature. As Irani (2018) discussed subcool trapping for solvent applications such NsolvTM recovery process is inefficient due to week dependency of solvent viscosity to temperature. Other factor that effects the efficiency of the thermodynamic trapping is that the pure solvent injection recovery processes are operated at low pressure and it is not large temperature window for operators to apply large subcools. Such challenges make the pure solvent injection recovery processes a perfect case for deployment of Flow-Control-Devices (FCDs). FCDs have demonstrated significant potential for improving recovery in SAGD production wells. FCD experience in SAGD has been primarily positive and most producers performed better with FCDs. Application of FCDs are even more important in pure-solvent injection recovery processes due to large amount of solvent in the liquid pool and also low latent heat of solvent in comparison of water. With FCDs, the draw-down pressure is typically higher, resulting in flashing near the well bore, which is largely correlated to latent heat of the main fluid in the liquid pool. The flashing creates either steam or vapour breakthrough that causes the reduction in the relative permeability of the liquid phase. Such mobility reduction creates new equilibrium that stabilizes at lower rates. Such new equilibrium analysis is conducted by forcing a new temperature gradient to the model. Such condition creates an environment that leads into extensive solvent-breakthrough called solvent-coning in this study. The main output of such analysis is the produced solvent gas-fraction produced at the sand-face. The gas-fraction is an important input for the flow control devices (FCDs) especially at subcools close to the zero, as it controls its behavior. EoS model is also created and simplified to be possible to used in defining different equilibrium conditions. This type of analysis can help the operators evaluate the effectiveness of different type of FCDs, whether they are primarily momentum- or friction-style devices for application of the pure solvent injection recovery processes. This study is the first of its kind that couple the EoS and Darcy flow in the liquid pool. The model includes all the factors into a liquid-relative-permeability, and limitation of the liquid flow into producer is modeled by Darcy flow and reduction of such relative-permeability.


2021 ◽  
Author(s):  
Farasdaq Sajjad ◽  
Steven Chandra ◽  
Alvin Wirawan ◽  
Silvya Dewi Rahmawati ◽  
Michelle Santoso ◽  
...  

Abstract In the implementation of gas lift, understanding flow behavior in highly-deviated well is critical in avoiding production loss due to liquid fallback and blockage, even in highly-productive reservoir. In this work, we utilize Computational Fluid Dynamics (CFD) to optimize gas lift design under various flow behavior in highly-deviated well. The analysis is directly implemented into Arjuna offshore field case. Arjuna offshore field has gas-lifted wells, producing from a high-permeability reservoir. However, several wells suffer from huge production loss due to the effect of well's deviation. In deviated well, there exists frequent liquid fallback causes blockage, therefore, reducing the production. Motivated by this issue, we use CFD framework to perform gas lift optimization. We firstly adopt the geometry of gas-lifted wells as the computational domains for our simulation. An image-based meshing technique is deployed to capture the well's trajectory and internal geometry. We secondly utilize compressible Navier-Stokes equation and Finite Volume Method to evaluate the flow behavior. We capture the location of liquid fallback and liquid accumulation at elbows to estimate production loss. We consider the variation of viscosity, density, gas lift valve placement, injected gas rate, and reservoir pressure. We finally perform gradient-based optimization utilizing production loss as the objective function to obtain optimum design. The final result is then used to optimize the current design. The simulation results show that productivity index, pipe diameter, and deviation heavily influence the amount of production loss. At big pipe diameter and high deviation, the gravitational force governs the fluid flow. Therefore, slugs are developed and accumulated at elbows. This accumulation blocks gas flow and reduces production. Changing the gas injection rate affects the lifted density. High injection rate triggers segregation between the liquid and gas, while low injection rate does not reduce the liquid density. Shifting the gas lift valve placement influence the mixing between the liquid and gas. It also determines the cost of gas injection. Hence, we need to optimize both parameters at once. Six of thirty wells in Arjuna field experience severe liquid fallback, therefore, the production significantly decreases. The simulation shows up to 40% coverage of the pipe internal diameter, which blocks the gas flow. We perform the optimization by shifting the gas lift valve placement and adjusting the gas injection rate. By implementing the study result into the field case, we manage to improve the production by 20%. We provide an effective way to connect high-resolution simulation to the field design and revise the current concept in designing gas lift well completion. The simulation allows engineers to provide more insight on flow assurance in highly deviated wells.


Author(s):  
Ehsan Roohi ◽  
Masoud Darbandi ◽  
Vahid Mirjalili

The current research uses an unstructured direct simulation Monte Carlo (DSMC) method to numerically investigate supersonic and subsonic flow behavior in micro convergent–divergent nozzle over a wide range of rarefied regimes. The current unstructured DSMC solver has been suitably modified via using uniform distribution of particles, employing proper subcell geometry, and benefiting from an advanced molecular tracking algorithm. Using this solver, we study the effects of back pressure, gas/surface interactions (diffuse/specular reflections), and Knudsen number, on the flow field in micronozzles. We show that high viscous force manifesting in boundary layers prevents supersonic flow formation in the divergent section of nozzles as soon as the Knudsen number increases above a moderate magnitude. In order to accurately simulate subsonic flow at the nozzle outlet, it is necessary to add a buffer zone to the end of nozzle. If we apply the back pressure at the outlet, boundary layer separation is observed and a region of backward flow appears inside the boundary layer while the core region of inviscid flow experiences multiple shock-expansion waves. We also show that the wall boundary layer prevents forming shocks in the divergent part. Alternatively, Mach cores appear at the nozzle center followed by bow shocks and an expansion region.


1999 ◽  
Vol 121 (2) ◽  
pp. 96-101 ◽  
Author(s):  
H. Baca ◽  
J. Smith ◽  
A. T. Bourgoyne ◽  
D. E. Nikitopoulos

Results from experiments conducted in downward liquid-gas flows in inclined, eccentric annular pipes, with water and air as the working fluids, are presented. The gas was injected in the middle of the test section length. The operating window, in terms of liquid and gas superficial velocities, within which countercurrent gas flow occurs at two low-dip angles, has been determined experimentally. The countercurrent flow observed was in the slug regime, while the co-current one was stratified. Countercurrent flow fraction and void fraction measurements were carried out at various liquid superficial velocities and gas injection rates and correlated to visual observations through a full-scale transparent test section. Our results indicate that countercurrent flow can be easily generated at small downward dip angles, within the practical range of liquid superficial velocity for drilling operations. Such flow is also favored by low gas injection rates.


2003 ◽  
Vol 125 (5) ◽  
pp. 843-850 ◽  
Author(s):  
G. Roy ◽  
D. Vo-Ngoc ◽  
D. N. Nguyen ◽  
P. Florent

The application of pneumatic metrology to control dimensional accuracy on machined parts is based on the measurement of gas flow resistance through a restricted section formed by a jet orifice placed at a small distance away from a machined surface. The backpressure, which is sensed and indicated by a pressure gauge, is calibrated to measure dimensional variations. It has been found that in some typical industrial applications, the nozzles are subject to fouling, e.g., dirt and oil deposits accumulate on their frontal areas, thus requiring more frequent calibration of the apparatus for reliable service. In this paper, a numerical and experimental analysis of the flow behavior in the region between an injection nozzle and a flat surface is presented. The analysis is based on the steady-state axisymmetric flow of an incompressible fluid. The governing equations, coupled with the appropriate boundary conditions, are solved using the SIMPLER algorithm. Results have shown that for the standard nozzle geometry used in industrial applications, an annular low-pressure separated flow area was found to exist near the frontal surface of the nozzle. The existence of this area is believed to be the cause of the nozzle fouling problem. A study of various alternate nozzle geometries has shown that this low-pressure recirculation area can be eliminated quite readily. Well-designed chamfered, rounded, and reduced frontal area nozzles have all reduced or eliminated the separated recirculation flow area. It has been noted, however, that rounded nozzles may adversely cause a reduction in apparatus sensitivity.


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