In-Situ Combustion Model

1980 ◽  
Vol 20 (06) ◽  
pp. 533-554 ◽  
Author(s):  
Keith H. Coats

Abstract This paper describes a numerical model forsimulating wet or dry, forward or reverse combustionin one, two, or three dimensions. The formulation isconsiderably more general than any reported to date.The model allows any number and identities ofcomponents. Any component may be distributed inany or all of the four phases (water, oil, gas, andsolid or coke.The formulation allows any number of chemicalreactions. Any reaction may have any number ofreactants, products, and stoichiometry, identifiedthrough input data. The energy balance accounts forheat loss and conduction, conversion, and radiationwithin the reservoir.The model uses no assumptions regarding degreeof oxygen consumption. The oxygen concentration iscalculated throughout the reservoir in accordancewith the calculated fluid flow pattern and reactionkinetics. The model, therefore, simulates the effectsof oxygen bypassing caused by kinetic-limitedcombustion or conformance factors.We believe the implicit model formulation resultsin maximum efficiency (lowest computing cost), andrequired computing times are reported in the paper.The paper includes comparisons of model resultswith reported laboratory adiabatic-tube test results.In addition, the paper includes example field-scalecases, with a sensitivity study showing effects on oilrecovery of uncertainties in rock/fluid properties. Introduction Recent papers by Ali, Crookston et al., andYoungren provide a comprehensive review of earlierwork in numerical modeling of the in-situcombustion process.The trend in this modeling has been toward morerigorous treatment of the fluid flow and interphasemass transfer; inclusion of more components, morecomprehensive reaction kinetics, and stoichiometry;and more implicit treatment of the finite differencemodel equations.The purpose of this work was to extend thegenerality of previous models while preserving orreducing the associated computing-time requirement.The most comprehensive or sophisticated combustionmodels described to date appear to be thoseof Crookston et al. and Youngren. Therefore, wecompare our model formulation and results here withthose models.A common objective of different investigators'efforts in modeling in-situ combustion is developmentof more efficient formulations and methods ofsolution. This is especially important in thecombustion case because of the large number ofcomponents and equations involved. For a given numberof components and reactions, computing time pergrid block per time step will increase rapidly as theformulation is rendered more implicit. However, increasing implicitness tends to allow larger timesteps, which in turn reduces overall computingexpense. To pursue the above objective, then, authorsshould present as completely as possible the details oftheir formulations and the associatedcomputing-time requirements.The thermal model described here simulateswet or dry, forward or reverse combustion in one, two, or three dimensions. The formulation allowsany number and identities of components and anynumber of chemical reactions, with reactants, products, and stoichiometry specified through input products, and stoichiometry specified through input data. SPEJ P. 533

1980 ◽  
Vol 20 (01) ◽  
pp. 39-51 ◽  
Author(s):  
Gary K. Youngren

Youngren, Gary K., SPE-AIME, ARCO Oil and Gas Co. Abstract This paper describes a three-dimensional, three-phase in-situ combustion reservoir simulator that rigorously models fluid flow, heat transfer, and vaporization/ condensation. It has five components: water, oxygen, nonvolatile oil, and two arbitrary volatile components. The volatile components partition between the oil and gas phases. The physical mechanisms modeled, the comprehensive mathematical solution method employed, and four applications of the simulator are presented. The applications demonstrate that the simulator can be used to interpret laboratory results and predict the effects of reservoir characteristics and operating strategy on field performance. Introduction Crookston et al. and Farouq Ali thoroughly reviewed previous developments in the mathematical simulation of in-situ combustion processes. Briefly, the earliest studies modeled certain aspects of the process using simple assumptions for the remaining process using simple assumptions for the remaining features in order to make the problem tractable. For example, Chu modeled one-dimensional thermal conduction, convection, and the thermal effects of vaporization and condensation, but multi phase fluid flow effects were simplified by assuming constant fluid saturations. Smith and Farouq Ali simulated conduction, convection, heat losses, and heat generation in two-dimensions, but assumed single-phase flow and constant fuel consumption. Recently, Farouq Ali and Crookston et al. described comprehensive three-phase, two-dimensional simulators that model the most essential features of in-situ combustion; however, results were presented only for hypothetical one- and two-dimensional examples with relatively few grid blocks.The objective of this work was to develop an in-situ combustion simulator that would rigorously model fluid flow, heat transfer, and vaporization/ condensation and still be efficient enough to allow simulation of realistic reservoir problems. Accordingly, the simulator employs a stable, efficient, highly implicit solution method. It is formulated to handle three dimensions, three phases, five components, gravity and capillary forces, heat transfer by convection and conduction within the reservoir and conductive heat loss to adjacent strata. Quantitative data on high-temperature combustion kinetics of crude oils in porous media is inadequate to allow rigorous treatment of reaction kinetics; thus, the combustion reaction is treated simply, yet realistically, by assuming that the combustion rate is limited only by the oxygen flux. This paper first describes the simulator, outlining the physical mechanisms modeled and the numerical solution method employed. It concludes by presenting analysis of real laboratory and field data in one, two, and three dimensions. Simulator Description Physical Properties Physical Properties The most significant features of the simulator are listed in Table l and detailed in Appendix A.The simulator has five components: water, nonvolatile (dead) oil, oxygen, and two arbitrary volatile components that partition between the oil and gas phases. The last four components are considered insoluble in water. The last two components are arbitrary and may be any one of the combinations: nitrogen (N2) and solution gas, N2 and carbon dioxide (CO2), N2 and a distillable hydrocarbon, CO2 and solution gas, or CO2 and a distillable hydrocarbon. SPEJ p. 39


1981 ◽  
Vol 103 (4) ◽  
pp. 296-300
Author(s):  
S. M. Farouq Ali ◽  
J. Ferrer

Thermal recovery models for oil recovery consist of steam injection and in-situ combustion simulators. At the present time, steam injection simulators have been developed to a point where it is possible to reliably simulate portions of a fieldwide flood. Cyclic steam stimulation simulation still entails a number of questionable assumptions. Formation parting cannot be simulated in either case. In-situ combustion simulators lack the capability for front tracking. Even though the models are rather sophisticated, process mechanism description and input data are inadequate.


2008 ◽  
Vol 76 (2) ◽  
pp. 219-246 ◽  
Author(s):  
Morten R. Kristensen ◽  
Margot G. Gerritsen ◽  
Per G. Thomsen ◽  
Michael L. Michelsen ◽  
Erling H. Stenby

2015 ◽  
Vol 162 (4) ◽  
pp. 960-977 ◽  
Author(s):  
Sean Lovett ◽  
Franck Monmont ◽  
Nikolaos Nikiforakis

Geofluids ◽  
2017 ◽  
Vol 2017 ◽  
pp. 1-18
Author(s):  
Weslley da Silva Pereira ◽  
Grigori Chapiro

Gas-solid combustion appears in many applications such as in situ combustion, which is a potential technique for oil recovery. Previous work has analyzed traveling wave solutions and obtained analytical formulas describing combustion wave temperature, velocity, and gas velocity for one-dimensional gas-solid combustion model using geometrical singular perturbation theory. In the present work these formulas are generalized. Using numerical simulation we show that they can be adapted and then applied to describe more general two-dimensional models for in situ combustion in a nonhomogeneous porous medium.


Fractals ◽  
1998 ◽  
Vol 06 (04) ◽  
pp. 401-408 ◽  
Author(s):  
Jesper M. Smidt ◽  
Donald M. Monro

Image analysis was carried out on images of laboratory-made synthetic sandstone, which is used in air injection/in situ combustion experiments, and statistically similar sandstone was computer modeled in two (and three) dimensions. The pore space of both the synthetic and the modeled sandstones was found to be fractal. The equations governing the flow through porous rocks were developed, approximating the in situ combustion process with an immiscible displacement of resident oil by injected gas maintained at a constant pressure. A successive over-relaxation (SOR) scheme was applied to solve these equations. Finally, the similarity of simulations of flow through the laboratory-made synthetic and the computer-modeled sand-stones was demonstrated.


Fuel ◽  
1995 ◽  
Vol 74 (11) ◽  
pp. 1632-1635 ◽  
Author(s):  
Ramazan Ocalan ◽  
Mustafa Versan Kok

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