CA2096034C - Horizontal well gravity drainage combustion process for oil recovery - Google Patents
Horizontal well gravity drainage combustion process for oil recoveryInfo
- Publication number
- CA2096034C CA2096034C CA002096034A CA2096034A CA2096034C CA 2096034 C CA2096034 C CA 2096034C CA 002096034 A CA002096034 A CA 002096034A CA 2096034 A CA2096034 A CA 2096034A CA 2096034 C CA2096034 C CA 2096034C
- Authority
- CA
- Canada
- Prior art keywords
- oil
- wells
- reservoir
- gas
- combustion
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH DRILLING; MINING
- E21B—EARTH DRILLING, e.g. DEEP DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B43/00—Methods or apparatus for obtaining oil, gas, water, soluble or meltable materials or a slurry of minerals from wells
- E21B43/30—Specific pattern of wells, e.g. optimizing the spacing of wells
- E21B43/305—Specific pattern of wells, e.g. optimizing the spacing of wells comprising at least one inclined or horizontal well
-
- E—FIXED CONSTRUCTIONS
- E21—EARTH DRILLING; MINING
- E21B—EARTH DRILLING, e.g. DEEP DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
- E21B43/00—Methods or apparatus for obtaining oil, gas, water, soluble or meltable materials or a slurry of minerals from wells
- E21B43/16—Enhanced recovery methods for obtaining hydrocarbons
- E21B43/24—Enhanced recovery methods for obtaining hydrocarbons using heat, e.g. steam injection
- E21B43/243—Combustion in situ
- E21B43/247—Combustion in situ in association with fracturing processes or crevice forming processes
Abstract
An in-situ combustion method is provided for the recovery of viscous oil from an oil-bearing reservoir. A linear array of vertical air injection wells is drilled into the reservoir; the wells are completed in the upper portion of the reservoir. One or more gas production wells are provided, remote from the row of injection wells, said gas production wells also being completed in the upper portion of the reservoir. A horizontal oil production well is completed in the bottom portion of the reservoir, aligned with and positioned in spaced relation beneath the vertical injection wells. The reservoir is prepared for ignition and combustion is initiated at each of the injection wells. A hot fluid-transmissive chamber is formed around each of the injection wells as combustion proceeds. Combustion gas communication is established with the gas production wells.
Heated oil and water, produced by the combustion front in each hot chamber, drains under the effect of gravity and is produced from the horizontal production well. The main features of the process are the implementation of gravity drainage to a basal horizontal well in a combustion process and the splitting of liquid and gas production.
Heated oil and water, produced by the combustion front in each hot chamber, drains under the effect of gravity and is produced from the horizontal production well. The main features of the process are the implementation of gravity drainage to a basal horizontal well in a combustion process and the splitting of liquid and gas production.
Description
-FIELD OF THE INVENTION 2 0 9 ~ 0 3 4
2 This invention relates to a process for recovering viscous hydrocarbons from
3 a subterranean reservoir using an in-situ combustion technique in combination with a
4 particular arrangement of vertical air injection wells, gas production wells, and separate horizontal oil production wells.
7 Combustion or fireflood methods are known for enhanced recovery of oil 8 from viscous oil reservoirs.
9 Generally, the reservoir is locally heated and then oxygen is supplied to the 10 oil bearing reservoir through one or more injection wells. The injection of oxygen sustains 11 combustion of in-situ oil and forms a vertical combustion front which produces hot gases.
12 The combustion front advances towards production wells spaced from the injection wells.
13 The known combustion processes may be generally characterized as 14 comprising: a burnt zone closest to the injection well; a combustion front; a vapour zone;
15 a condensation layer; an oil bank; and finally a cool region which oil must flow through 16 to be produced from a well. The combustion progresses in essentially a plug flow 17 manner. This plug flow progression experiences the following disadvantages: the lighter 18 hydrocarbons are in a layer ahead of the combustion, leaving only variable quality coke 19 behind as fuel; and it is difficult to supply and maintain adequate oxygen levels, for 20 continued combustion, at the ever extending front.
_ 2095031 Ideally, the combustion front remains vertical, extending throughout the 2 depth of the reservoir. If the combustion front contacts the entire reservoir, then 3 maximum production efficiency may be achieved.
4 Ultimately however, over time the hot gases rise and tend to move laterally
7 Combustion or fireflood methods are known for enhanced recovery of oil 8 from viscous oil reservoirs.
9 Generally, the reservoir is locally heated and then oxygen is supplied to the 10 oil bearing reservoir through one or more injection wells. The injection of oxygen sustains 11 combustion of in-situ oil and forms a vertical combustion front which produces hot gases.
12 The combustion front advances towards production wells spaced from the injection wells.
13 The known combustion processes may be generally characterized as 14 comprising: a burnt zone closest to the injection well; a combustion front; a vapour zone;
15 a condensation layer; an oil bank; and finally a cool region which oil must flow through 16 to be produced from a well. The combustion progresses in essentially a plug flow 17 manner. This plug flow progression experiences the following disadvantages: the lighter 18 hydrocarbons are in a layer ahead of the combustion, leaving only variable quality coke 19 behind as fuel; and it is difficult to supply and maintain adequate oxygen levels, for 20 continued combustion, at the ever extending front.
_ 2095031 Ideally, the combustion front remains vertical, extending throughout the 2 depth of the reservoir. If the combustion front contacts the entire reservoir, then 3 maximum production efficiency may be achieved.
4 Ultimately however, over time the hot gases rise and tend to move laterally
5 through the upper reaches of the reservoir toward the production wells. This
6 phenomenon is referred to as "overriding". The results of overriding are uneven areal
7 distribution of the combustion front and premature breaking through of gases at one or
8 more production wells. This latter situation is characterized by high gas flow rates
9 coupled with high temperature and oxygen effects at the production well. The need to
10 produce oil and water accompanied by a prolific combustion gas flow through a single
11 production well leads to high entrainment of sand, the formation of emulsions, and poor
12 oil recoveries. Further, the production well may be damaged by burning at the well.
13 Excessive sand rates can plug screens and impair the operation of downhole production 1 4 pumps.
It is therefore an objective of this invention to improve the production 16 efficiencies of combustion front enhanced oil recovery techniques and reduce the risks 17 to production equipment.
~_ 2~96031 SUMMARY OF THE INVENTION
2 The invention involves a combination of steps comprising:
3 - providing a row of injection wells, vertically disposed and completed 4 in the upper part of the reservoir, for injecting oxygen-containing gas into the reservoir to support a combustion front therein;
6 - providing at least one gas production well, spaced remotely from the 7 row and completed in the reservoir, for producing the combustion 8 gases;
9 - providing a horizontal oil production well, completed in spaced relation below the injection wells and being generally aligned with the 11 row, for producing hot liquid oil and water;
12 - preferably cyclically stimulating the reservoir with steam through the 13 injection wells and the oil production well to establish fluid
It is therefore an objective of this invention to improve the production 16 efficiencies of combustion front enhanced oil recovery techniques and reduce the risks 17 to production equipment.
~_ 2~96031 SUMMARY OF THE INVENTION
2 The invention involves a combination of steps comprising:
3 - providing a row of injection wells, vertically disposed and completed 4 in the upper part of the reservoir, for injecting oxygen-containing gas into the reservoir to support a combustion front therein;
6 - providing at least one gas production well, spaced remotely from the 7 row and completed in the reservoir, for producing the combustion 8 gases;
9 - providing a horizontal oil production well, completed in spaced relation below the injection wells and being generally aligned with the 11 row, for producing hot liquid oil and water;
12 - preferably cyclically stimulating the reservoir with steam through the 13 injection wells and the oil production well to establish fluid
14 communication between the injection wells and the oil production 1 5 well;
16 - injecting an oxygen-containing gas at less than fracturing pressure 17 through each injection well and establishing a combustion front 18 emanating from each such well to form a hot gas-containing, fluid 19 transmissive chamber extending around each injection well and down to the oil production well, so that heated oil and water will drain 21 downwardly through the chamber under the influence of gravity, said 22 combustion front further being operative to produce combustion gases which flow through the upper portion of the reservoir, as an 2 "overriding" stream, toward the gas production well(s) for production 3 therefrom; and 4 - producing hot oil and water in liquid form through the horizontal oil production well and combustion gases through the gas production 6 well(s).
7 It will be noted that the process is characterized by the following features:
8 - there is split production of the liquid and gaseous products of the g process;
- because the hot oil and water liquids are recovered by draining 11 under the influence of gravity down to the oil production well and 12 they are produced to ground surface through that well; and 13 - because the combustion gases are recovered by forming an 14 overriding stream moving through the upper reaches of the reservoir to the gas production well(s) and they are produced to ground 16 surface through those wells.
17 However, it needs to be understood that the split is not totally complete - minor amounts 18 of liquids are produced with the gases and minor amounts of gases with the liquids.
19 The process is further characterized by the following advantages:
- the energy efficiency and low cost of a combustion process is 21 combined with the high recovery associated with gravity drainage to 22 a horizontal production well;
2~95~34 -- early gas breakthrough to the gas production wells can be avoided 2 by locating the wells remote from the injection wells, which is not a 3 problem to implement because the heated oil does not get produced 4 by the gas production wells - therefore the wells do not need to be relatively closely spaced relative to the injection wells so that the oil 6 can be driven to them;
7 - the gas production wells can be water cooled to better combat 8 problems arising from the arrival of the hot combustion gases;
9 - downhole pumps can be eliminated from the gas production wells, thereby avoiding gas locking and reducing corrosion problems;
11 - the process provides a hot fluid-transmissive chamber for the hot oil 12 to flow through on its way to the oil production well, thereby 13 facilitating oil movement;
14 - there is only a relatively short distance spacing the combustion front from the horizontal oil production well;
16 - the horizontal oil production well is protected from combustion 17 damage, since the oxygen flux and combustion front tend to stay 18 higher in the reservoir and liquid overlies the oil production well and 19 insulates it from the combustion front;
- production from the horizontal oil production well can be controlled 21 at low gas flow rates through it, to maintain a small head of liquid 22 over the well; and low air-injection pressurQ canbe used because only gravity forces 2 are required to displace oil to the oil production welll, whereas in 3 prior art combustion processes higher pressures are required to drive 4 oil between injection and production wells.
BRIEF DESCRIPTION OF THE DRAWINGS
6 Figure 1 is a perspective schematic view of a section of an oil-bearing 7 reservoir with injection wells, gas production wells, and oil production wells in place. The 8 overburden has been partially cutaway;
9 Figure 2 is a schematic diagram of a cross section of the reservoir perpendicular to the horizontal oil production well;
11 Figure 3 is a fanciful schematic view of the combustion front corresponding 12 to area A according to Figure 2;
13 Figure 4 is a perspective view of a modelled reservoir;
14 Figure 5 is a perspective view of a discrete 3-D model element according to the overall model of Figure 4;
16 Figure 6 is a chronological history of the modelled air injection rate 17 performance for a high density heavy oil-containing reservoir modelled according to 18 Figure 4;
19 Figure 7 is a chronological history of the modelled oil production performance at the gas production and oil production wells, corresponding to the case 21 presented in Figure 6;
--' 20~1h)3~
Figure 8 is a chronological history o t e modelled air injection rate for a low 2 density heavy oil-containing reservoir modelled according to Figure 4; and 3 Figure 9 is a chronological history of the modelled oil production 4 performance at the gas production and oil production wells, corresponding to the case 5 presented in Figure 8.
7 Referring to Figure 1, one may view a cutaway perspective view of an oil-8 bearing reservoir and the arrangement of wells used to carry out the method of the 9 invention.
A covering of overburden 1 lies above an oil-bearing reservoir 2. A row of 11 vertical injection wells 3 are drilled downward through the overburden 1 and are 12 completed in the upper portion of the reservoir 2.
13 Remote gas production wells 4 are drilled spaced apart and in a line parallel 14 from the row of injection wells 3. These primarily gas production wells 4 are also
16 - injecting an oxygen-containing gas at less than fracturing pressure 17 through each injection well and establishing a combustion front 18 emanating from each such well to form a hot gas-containing, fluid 19 transmissive chamber extending around each injection well and down to the oil production well, so that heated oil and water will drain 21 downwardly through the chamber under the influence of gravity, said 22 combustion front further being operative to produce combustion gases which flow through the upper portion of the reservoir, as an 2 "overriding" stream, toward the gas production well(s) for production 3 therefrom; and 4 - producing hot oil and water in liquid form through the horizontal oil production well and combustion gases through the gas production 6 well(s).
7 It will be noted that the process is characterized by the following features:
8 - there is split production of the liquid and gaseous products of the g process;
- because the hot oil and water liquids are recovered by draining 11 under the influence of gravity down to the oil production well and 12 they are produced to ground surface through that well; and 13 - because the combustion gases are recovered by forming an 14 overriding stream moving through the upper reaches of the reservoir to the gas production well(s) and they are produced to ground 16 surface through those wells.
17 However, it needs to be understood that the split is not totally complete - minor amounts 18 of liquids are produced with the gases and minor amounts of gases with the liquids.
19 The process is further characterized by the following advantages:
- the energy efficiency and low cost of a combustion process is 21 combined with the high recovery associated with gravity drainage to 22 a horizontal production well;
2~95~34 -- early gas breakthrough to the gas production wells can be avoided 2 by locating the wells remote from the injection wells, which is not a 3 problem to implement because the heated oil does not get produced 4 by the gas production wells - therefore the wells do not need to be relatively closely spaced relative to the injection wells so that the oil 6 can be driven to them;
7 - the gas production wells can be water cooled to better combat 8 problems arising from the arrival of the hot combustion gases;
9 - downhole pumps can be eliminated from the gas production wells, thereby avoiding gas locking and reducing corrosion problems;
11 - the process provides a hot fluid-transmissive chamber for the hot oil 12 to flow through on its way to the oil production well, thereby 13 facilitating oil movement;
14 - there is only a relatively short distance spacing the combustion front from the horizontal oil production well;
16 - the horizontal oil production well is protected from combustion 17 damage, since the oxygen flux and combustion front tend to stay 18 higher in the reservoir and liquid overlies the oil production well and 19 insulates it from the combustion front;
- production from the horizontal oil production well can be controlled 21 at low gas flow rates through it, to maintain a small head of liquid 22 over the well; and low air-injection pressurQ canbe used because only gravity forces 2 are required to displace oil to the oil production welll, whereas in 3 prior art combustion processes higher pressures are required to drive 4 oil between injection and production wells.
BRIEF DESCRIPTION OF THE DRAWINGS
6 Figure 1 is a perspective schematic view of a section of an oil-bearing 7 reservoir with injection wells, gas production wells, and oil production wells in place. The 8 overburden has been partially cutaway;
9 Figure 2 is a schematic diagram of a cross section of the reservoir perpendicular to the horizontal oil production well;
11 Figure 3 is a fanciful schematic view of the combustion front corresponding 12 to area A according to Figure 2;
13 Figure 4 is a perspective view of a modelled reservoir;
14 Figure 5 is a perspective view of a discrete 3-D model element according to the overall model of Figure 4;
16 Figure 6 is a chronological history of the modelled air injection rate 17 performance for a high density heavy oil-containing reservoir modelled according to 18 Figure 4;
19 Figure 7 is a chronological history of the modelled oil production performance at the gas production and oil production wells, corresponding to the case 21 presented in Figure 6;
--' 20~1h)3~
Figure 8 is a chronological history o t e modelled air injection rate for a low 2 density heavy oil-containing reservoir modelled according to Figure 4; and 3 Figure 9 is a chronological history of the modelled oil production 4 performance at the gas production and oil production wells, corresponding to the case 5 presented in Figure 8.
7 Referring to Figure 1, one may view a cutaway perspective view of an oil-8 bearing reservoir and the arrangement of wells used to carry out the method of the 9 invention.
A covering of overburden 1 lies above an oil-bearing reservoir 2. A row of 11 vertical injection wells 3 are drilled downward through the overburden 1 and are 12 completed in the upper portion of the reservoir 2.
13 Remote gas production wells 4 are drilled spaced apart and in a line parallel 14 from the row of injection wells 3. These primarily gas production wells 4 are also
15 completed in the upper portion of the reservoir. The gas production wells 4 are spaced
16 one on either side of each row of injection wells for optimal utilization of the injection 1 7 wells.
In the embodiment shown, horizontal gL production wells 4 are used.
2 Optionally, a series of vertical gas production wells could be used in place of the 3 horizontal wells 4. These vertical gas production wells would also be completed in the 4 upper portion of the reservoir initially, but could be recompleted lower in the reservoir at late stages of the process.
6 A horizontal oil production well 7 is provided near the base of the reservoir 7 2. Each oil production well 7 is aligned with and positioned in spaced relation beneath 8 the perforations of a row of injection wells 3. Each oil production well 7 will typically have 9 a slotted liner (not shown) to permit ingress of produced fluid. The oil production well 7 collects and recovers the oil and water liquid product from the reservoir 2.
11 In the case where the oil reservoir is saturated with low mobility heavy oil, 12 it is desirable to form an initial hot, fluid transmissive chamber 9 linking each injection well 13 3 and the oil production well 7, whereby fluid communication can be established between 14 the wells. This can be accomplished by subjecting the reservoir to cyclic steam stimulation through the injection wells 3 and oil production well 7. During cyclic steam 16 injection, oil is recovered from both the oil production well 7 and the gas production wells
In the embodiment shown, horizontal gL production wells 4 are used.
2 Optionally, a series of vertical gas production wells could be used in place of the 3 horizontal wells 4. These vertical gas production wells would also be completed in the 4 upper portion of the reservoir initially, but could be recompleted lower in the reservoir at late stages of the process.
6 A horizontal oil production well 7 is provided near the base of the reservoir 7 2. Each oil production well 7 is aligned with and positioned in spaced relation beneath 8 the perforations of a row of injection wells 3. Each oil production well 7 will typically have 9 a slotted liner (not shown) to permit ingress of produced fluid. The oil production well 7 collects and recovers the oil and water liquid product from the reservoir 2.
11 In the case where the oil reservoir is saturated with low mobility heavy oil, 12 it is desirable to form an initial hot, fluid transmissive chamber 9 linking each injection well 13 3 and the oil production well 7, whereby fluid communication can be established between 14 the wells. This can be accomplished by subjecting the reservoir to cyclic steam stimulation through the injection wells 3 and oil production well 7. During cyclic steam 16 injection, oil is recovered from both the oil production well 7 and the gas production wells
17 4. When the reservoir 2 is sufficiently preheated, combustion is initiated. Preheating with
18 steam may require a three month duration. Optionally a downhole burner may be used
19 to initially heat the area around each injection well 3 to start combustion.
Referring to Figure 2, gas containing oxygen 8 is injected through each of 21 the injection wells 3 at less than fracturing pressure, to initiate combustion. Air is usually 22 used, however it may be substituted directly with oxygen or with recycled gases enriched with oxygen. Water may also be injected continuously or as slugs to improve the 2 combustion process.
3 A fluid-transmissive chamber 9 is formed around each injection well 3. The 4 chamber 9 is hot, fluid transmissive, and gradually extends downwardly until it establishes 5 fluid communication between the injection wells 3 and the oil production well 7.
6 Continuous gas injection and cold water circulation in the injection wells can 7 be used to minimize combustion damage to the wells.
8 A thin overriding gas layer 10 is formed, extending to the gas production 9 wells 4. The pressures at the injection wells 3 and at the gas production wells 4 are 10 almost the same once combustion is well established. If communication between the 11 injection wells 3 and the gas production wells 4 is initially insufficient, gas can be injected 12 through the injection wells 3 to create a communication path prior to initiation of 1 3 combustion.
14 In the early phases of the initiation of combustion, the rate of oil being 15 produced from the gas production well 4 declines quickly, while the oil rate of the 16 horizontal production well 7 increases. A stable combustion front 17 is soon developed, 17 forming a fluid-transmissive chamber 9 localized about each of the injection wells 3 and 18 extending down to the oil production well 7. Eventually, as the overriding gas layer 10 19 is established, the gas production wells 4 produce substantially only combustion gases
Referring to Figure 2, gas containing oxygen 8 is injected through each of 21 the injection wells 3 at less than fracturing pressure, to initiate combustion. Air is usually 22 used, however it may be substituted directly with oxygen or with recycled gases enriched with oxygen. Water may also be injected continuously or as slugs to improve the 2 combustion process.
3 A fluid-transmissive chamber 9 is formed around each injection well 3. The 4 chamber 9 is hot, fluid transmissive, and gradually extends downwardly until it establishes 5 fluid communication between the injection wells 3 and the oil production well 7.
6 Continuous gas injection and cold water circulation in the injection wells can 7 be used to minimize combustion damage to the wells.
8 A thin overriding gas layer 10 is formed, extending to the gas production 9 wells 4. The pressures at the injection wells 3 and at the gas production wells 4 are 10 almost the same once combustion is well established. If communication between the 11 injection wells 3 and the gas production wells 4 is initially insufficient, gas can be injected 12 through the injection wells 3 to create a communication path prior to initiation of 1 3 combustion.
14 In the early phases of the initiation of combustion, the rate of oil being 15 produced from the gas production well 4 declines quickly, while the oil rate of the 16 horizontal production well 7 increases. A stable combustion front 17 is soon developed, 17 forming a fluid-transmissive chamber 9 localized about each of the injection wells 3 and 18 extending down to the oil production well 7. Eventually, as the overriding gas layer 10 19 is established, the gas production wells 4 produce substantially only combustion gases
20 13.
- - 209603~
The gas production wells 4 may be spaced far enough away from the 2 injection wells 3 so that the produced gas 13 is sufficiently cooled to avoid combustion 3 damage related to residual contained oxygen. Should the gas production wells 4 4 experience heating, they can be cooled with water circulation. The water circulation will not adversely affect oil production and quality, as liquid production is now occurring at the 6 separate oil production well 7.
7 The flow mechanisms guiding the behaviour at the combustion front 17 are 8 somewhat different from those understood to occur in the prior art plug flow combustion 9 processes.
Referring to Figure 3, the mechanisms believed to occur at the combustion 11 front are separately identified. Mass transfer processes occur in a burnt zone 14 in the 12 area of the upper portion of the reservoir 2, which act to draw fresh air and oxygen 15 13 down to the combustion front 17, maintaining efficient combustion.
14 Light hydrocarbons 16, released by the heat transmitted from the high 15 temperature combustion front 17, rise through to a transition layer 11, providing high 16 grade fuels to the combustion process. The combustion process extends throughout the 17 transition layer and combustion front areas, consuming coke, light hydrocarbons and 18 oxygen, leaving water vapor, nitrogen, and carbon dioxide. Hydrocarbons are either 19 burned or drain downward from this area.
Combustion water vapor condenses in a condensation layer 18 in the cooler
- - 209603~
The gas production wells 4 may be spaced far enough away from the 2 injection wells 3 so that the produced gas 13 is sufficiently cooled to avoid combustion 3 damage related to residual contained oxygen. Should the gas production wells 4 4 experience heating, they can be cooled with water circulation. The water circulation will not adversely affect oil production and quality, as liquid production is now occurring at the 6 separate oil production well 7.
7 The flow mechanisms guiding the behaviour at the combustion front 17 are 8 somewhat different from those understood to occur in the prior art plug flow combustion 9 processes.
Referring to Figure 3, the mechanisms believed to occur at the combustion 11 front are separately identified. Mass transfer processes occur in a burnt zone 14 in the 12 area of the upper portion of the reservoir 2, which act to draw fresh air and oxygen 15 13 down to the combustion front 17, maintaining efficient combustion.
14 Light hydrocarbons 16, released by the heat transmitted from the high 15 temperature combustion front 17, rise through to a transition layer 11, providing high 16 grade fuels to the combustion process. The combustion process extends throughout the 17 transition layer and combustion front areas, consuming coke, light hydrocarbons and 18 oxygen, leaving water vapor, nitrogen, and carbon dioxide. Hydrocarbons are either 19 burned or drain downward from this area.
Combustion water vapor condenses in a condensation layer 18 in the cooler
21 layers ahead of the transition layer 11. This transfers heat to the oil-bearing reservoir 2,
22 mobilizing the oil and condensing water 19, which drains towards the production well 7.
Conduction of heat from the condensation layer 18 then acts as the primary 2 heat transfer mechanism to heat and mobilize more oil and water flow 19 in a conduction 3 zone 20, draining to the horizontal production well 7.
4 The process has been numerically simulated to verify the physical principles 5 of the design and evaluate its potential over the prior art.
6 In order to forecast production, a three dimensional (3-D) model was 7 prepared to simulate the process.
8 Referring to Figure 4, a 16 meter deep reservoir was modelled with a 480 9 meter long horizontal production weil placed near the bottom. Two horizontal gas 10 production wells were placed in the upper portion of the reservoir. Each gas production 11 well was 72 meters spaced apart from and parallel to the production well. Ten vertical 12 injection wells were placed into the upper portion of the reservoir, aligned along the 13 horizontal production well and spaced 48 meters apart. This then defines a 480 meter 14 long by 144 meter wide by 16 meter deep overall model.
Referring now to Figure 5, considering the symmetry of the 3-D computer 16 model, one has only to consider one lateral side of one injector. Thus the actual reservoir 17 modelling element was 24 meters long by 72 meters wide by 16 meters deep.
18 In order to better study the process mechanisms through the combustion 19 front (Fig. 3), an additional 2-D model was used, extending through the 16 meter depth 20 and to the gas production wells, 72 meters away.
2~96034 A commercial simulator (CMG STARS, Computer Modelling Group, Calgary, 2 Alberta) was used to simplify creation of the model. CMG STARS is a simulation 3 package for Steam and Additive Reservoir Simulation (STARS). The simulation routines 4 provided can handle many aspects of reservoir modelling, some of which include: vertical 5 and horizontal wellbores, multi-component oils, steam, gases, combustion and channelling 6 analyses.
7 Hydrocarbons behaviour was simulated using a two component system: a 8 non-volatile heavy component and a volatile light component. The heavy component was 9 assumed to burn in its liquid phase when exposed to oxygen. The light component was 10 assumed to be volatile and burns in its gas phase only. No cracking reactions were 1 1 modeled.
12 The actual reaction kinetics were not specifically modelled, as they were 13 believed to be unreliable in a coarse grid system as modeled. The process is more 14 conducive to high temperature combustion because there is gas and liquid phase 15 combustion as well as coke combustion. Heat generation was based upon spontaneous 16 and complete conversion of the hydrocarbons to combustion byproducts when exposed 17 to oxygen.
The gravity draining behaviour of steam heated oils in reservoirs is known 2 through studies of Steam-Assisted Gravity Drainage (SAGD) developed by R. M. Butler 3 et al., "Theoretical Studies on the Gravity Drainage of Heavy Oil during In-Situ Steaming 4 Heatingn, Can. J. Chem. Eng., Vol. 59, P.455-460, August 1981, and pilot-tested in the 5 Athabasca Oilsands near Ft. McMurray, Alberta. The hot chamber was assumed to 6 act similarly to a steam chamber acting in the SAGD process.
7 The properties of a high density heavy oil and a low density heavy oil 8 reservoir and its hydrocarbon components used for the model are listed in Table 1 as 9 follows.
RESERVOIR PROPt~ l ltS 2 0 9 6 D 3 4 2 units Reservoir Overburden &
3 Rock Underburden 4 Pay Ihickness (m) 16 Porosity 30%
6 Oil Saturation 83%
7 Water Saturation 17%
8 Gas Saturation o%
9 Solution GOR (m3/m3) 12.40 H. Permeability (Md) 3000 11 V. Permeability 2000 12 Res. Temperature (C) 26.8 13 Res. Pressure (kPa) 5450 4 Rock Compressibility (/Kpa) 0.000035 1 5 Conductivity (J/m.d.C) 149500 149500 16 Heat Capacity (J/m3.C) 2347000 2347000 18 (a) High Density Units Heavy Light Live Oil 1 9 Heavy Oil Component Component Density (kg/m~) 994 866 977 21 Viscosity (cp) 4875 17 2250 22 MolecularWeight 340 20 296
Conduction of heat from the condensation layer 18 then acts as the primary 2 heat transfer mechanism to heat and mobilize more oil and water flow 19 in a conduction 3 zone 20, draining to the horizontal production well 7.
4 The process has been numerically simulated to verify the physical principles 5 of the design and evaluate its potential over the prior art.
6 In order to forecast production, a three dimensional (3-D) model was 7 prepared to simulate the process.
8 Referring to Figure 4, a 16 meter deep reservoir was modelled with a 480 9 meter long horizontal production weil placed near the bottom. Two horizontal gas 10 production wells were placed in the upper portion of the reservoir. Each gas production 11 well was 72 meters spaced apart from and parallel to the production well. Ten vertical 12 injection wells were placed into the upper portion of the reservoir, aligned along the 13 horizontal production well and spaced 48 meters apart. This then defines a 480 meter 14 long by 144 meter wide by 16 meter deep overall model.
Referring now to Figure 5, considering the symmetry of the 3-D computer 16 model, one has only to consider one lateral side of one injector. Thus the actual reservoir 17 modelling element was 24 meters long by 72 meters wide by 16 meters deep.
18 In order to better study the process mechanisms through the combustion 19 front (Fig. 3), an additional 2-D model was used, extending through the 16 meter depth 20 and to the gas production wells, 72 meters away.
2~96034 A commercial simulator (CMG STARS, Computer Modelling Group, Calgary, 2 Alberta) was used to simplify creation of the model. CMG STARS is a simulation 3 package for Steam and Additive Reservoir Simulation (STARS). The simulation routines 4 provided can handle many aspects of reservoir modelling, some of which include: vertical 5 and horizontal wellbores, multi-component oils, steam, gases, combustion and channelling 6 analyses.
7 Hydrocarbons behaviour was simulated using a two component system: a 8 non-volatile heavy component and a volatile light component. The heavy component was 9 assumed to burn in its liquid phase when exposed to oxygen. The light component was 10 assumed to be volatile and burns in its gas phase only. No cracking reactions were 1 1 modeled.
12 The actual reaction kinetics were not specifically modelled, as they were 13 believed to be unreliable in a coarse grid system as modeled. The process is more 14 conducive to high temperature combustion because there is gas and liquid phase 15 combustion as well as coke combustion. Heat generation was based upon spontaneous 16 and complete conversion of the hydrocarbons to combustion byproducts when exposed 17 to oxygen.
The gravity draining behaviour of steam heated oils in reservoirs is known 2 through studies of Steam-Assisted Gravity Drainage (SAGD) developed by R. M. Butler 3 et al., "Theoretical Studies on the Gravity Drainage of Heavy Oil during In-Situ Steaming 4 Heatingn, Can. J. Chem. Eng., Vol. 59, P.455-460, August 1981, and pilot-tested in the 5 Athabasca Oilsands near Ft. McMurray, Alberta. The hot chamber was assumed to 6 act similarly to a steam chamber acting in the SAGD process.
7 The properties of a high density heavy oil and a low density heavy oil 8 reservoir and its hydrocarbon components used for the model are listed in Table 1 as 9 follows.
RESERVOIR PROPt~ l ltS 2 0 9 6 D 3 4 2 units Reservoir Overburden &
3 Rock Underburden 4 Pay Ihickness (m) 16 Porosity 30%
6 Oil Saturation 83%
7 Water Saturation 17%
8 Gas Saturation o%
9 Solution GOR (m3/m3) 12.40 H. Permeability (Md) 3000 11 V. Permeability 2000 12 Res. Temperature (C) 26.8 13 Res. Pressure (kPa) 5450 4 Rock Compressibility (/Kpa) 0.000035 1 5 Conductivity (J/m.d.C) 149500 149500 16 Heat Capacity (J/m3.C) 2347000 2347000 18 (a) High Density Units Heavy Light Live Oil 1 9 Heavy Oil Component Component Density (kg/m~) 994 866 977 21 Viscosity (cp) 4875 17 2250 22 MolecularWeight 340 20 296
23 Mole Fraction 86% 14% 100%
24 Heat Capacity (J/gmole.C) 1278 19 1106 Combust. Enthalpy ~ 25C (J/gmole) 1.68E+07 1.07E+06 1.47E+07 26 (b) Low Density Units Heavy Light Live Oil 27 Heavy Oil Component Component 28 Density (kg/m~ ) 944 866 934 29 Viscosity (cp) 488 17 308 Mc' ul r Weight 340 20 296 31 Mole Fraction 86% 14% 100%
32 Heat Capacity (J/gmole.C) 1278 19 1106 33 Combust. Enthalpy ~25C (J/gmole) 1.68E+07 1.07E+06 1.47E+07 34 The wells were controlled using the following constraints:
- Air injection pressure (Max) = 6000 Kpa 36 Production pressure (Min) = 500 Kpa 37 - Liquid production rate (Max) = 240 m3/d 38 Steam production rate (Max) = 9.6 m3/d 39 - Liquid producer gas rate (Max) = 9600 m3/d - Gas-producer gas rate (Max) = 288000 m3/d Operation of the model with the above parameters provided a prediction of 2 the pe, r~" " lance of the process over time. A five year timeline was modelled. Two types 3 of reservoirs were modelled; a reservoir conlaining high density heavy oil, and one 4 containing low density heavy oil.
5In both reservoir cases, the reservoir was treated by steam pre-heating at 66000 Kpa for three n,onti,s. Oil rates of about 80 m3/d were achieved at the oil 7 production well during pre-heat.
8Air injection was started in the fourth month. Characteri:jlically, oil 9 production at the gas production wells declined quickly, while the hori~onlal oil production 10 well oil rates increased.
11After some years into the production, when oxygen breakthrough was 12 detected (Oxygen conce, IlldliOnS > 1 %) at a gas production well, the gas production well 13 was shut in. Air injection was reduced to minimum levels, and liquid production continued 14 at diminishing rates. The-resicluAI heat in the reservoir formation continued to heat and 15 mobilize new oil, albeit at lower and lower rates. The model production forecasts were 16 continued until oil production at the ho,i~ontal oil production well dropped to the economic 17 Iimit of 20 m3/day per well.
18Referring specifically to the high density heavy oil reservoir case whose data 19 are set forth in Figure 6, the model presents the air injection rates as starting in the fourth 20month and rising steeply to stable rates of about 300,000 m3/day. About three years 21 later, oxygen breakthrough was delected and the air injection rate was reduced to a very 22 low level.
Referring to Figure 7, the oil production rates at the hGriL~, It~l oil production 2 well were seen to rise steadily, achieving a steady production rate of about 100 m3/day 3 which was maintained for over 3 years. Oil production at the gas production well fell 4 rapidly with the increase in air injecffon, falling to economic limits in less than one year, 5 and to non-detectable levels within two years.
6 When the air injection rate was reduced, the oil production rates at the 7 horizontal production well were seen, correspondingly, to steadily diminish over the 8 following 1.5 years to the economic limit.
9 Referring now to Figures 8 and 9, similar modelling was performed for a low 10 density heavy oil reservoir. Oxygen breakthrough was detected much sooner (after two 11 years) than in the high density heavy oil case, but the oil production through the steady 12 state period was significantly higher at 180 m3/day. Once the air injection was reduced, 13 economic oil production was possible for a remaining 2.5 years.
14 In an altemaffve procedure, it may be desirable as a preliminary step to 15 inject gas through the injecffon wells, prior to i~ iali,1g combusffon, to establish gas 16 communicaffon with the gas production wells.
17 The scope of the invention is set forth in the claims now following.
32 Heat Capacity (J/gmole.C) 1278 19 1106 33 Combust. Enthalpy ~25C (J/gmole) 1.68E+07 1.07E+06 1.47E+07 34 The wells were controlled using the following constraints:
- Air injection pressure (Max) = 6000 Kpa 36 Production pressure (Min) = 500 Kpa 37 - Liquid production rate (Max) = 240 m3/d 38 Steam production rate (Max) = 9.6 m3/d 39 - Liquid producer gas rate (Max) = 9600 m3/d - Gas-producer gas rate (Max) = 288000 m3/d Operation of the model with the above parameters provided a prediction of 2 the pe, r~" " lance of the process over time. A five year timeline was modelled. Two types 3 of reservoirs were modelled; a reservoir conlaining high density heavy oil, and one 4 containing low density heavy oil.
5In both reservoir cases, the reservoir was treated by steam pre-heating at 66000 Kpa for three n,onti,s. Oil rates of about 80 m3/d were achieved at the oil 7 production well during pre-heat.
8Air injection was started in the fourth month. Characteri:jlically, oil 9 production at the gas production wells declined quickly, while the hori~onlal oil production 10 well oil rates increased.
11After some years into the production, when oxygen breakthrough was 12 detected (Oxygen conce, IlldliOnS > 1 %) at a gas production well, the gas production well 13 was shut in. Air injection was reduced to minimum levels, and liquid production continued 14 at diminishing rates. The-resicluAI heat in the reservoir formation continued to heat and 15 mobilize new oil, albeit at lower and lower rates. The model production forecasts were 16 continued until oil production at the ho,i~ontal oil production well dropped to the economic 17 Iimit of 20 m3/day per well.
18Referring specifically to the high density heavy oil reservoir case whose data 19 are set forth in Figure 6, the model presents the air injection rates as starting in the fourth 20month and rising steeply to stable rates of about 300,000 m3/day. About three years 21 later, oxygen breakthrough was delected and the air injection rate was reduced to a very 22 low level.
Referring to Figure 7, the oil production rates at the hGriL~, It~l oil production 2 well were seen to rise steadily, achieving a steady production rate of about 100 m3/day 3 which was maintained for over 3 years. Oil production at the gas production well fell 4 rapidly with the increase in air injecffon, falling to economic limits in less than one year, 5 and to non-detectable levels within two years.
6 When the air injection rate was reduced, the oil production rates at the 7 horizontal production well were seen, correspondingly, to steadily diminish over the 8 following 1.5 years to the economic limit.
9 Referring now to Figures 8 and 9, similar modelling was performed for a low 10 density heavy oil reservoir. Oxygen breakthrough was detected much sooner (after two 11 years) than in the high density heavy oil case, but the oil production through the steady 12 state period was significantly higher at 180 m3/day. Once the air injection was reduced, 13 economic oil production was possible for a remaining 2.5 years.
14 In an altemaffve procedure, it may be desirable as a preliminary step to 15 inject gas through the injecffon wells, prior to i~ iali,1g combusffon, to establish gas 16 communicaffon with the gas production wells.
17 The scope of the invention is set forth in the claims now following.
Claims (5)
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. An in-situ process for recovering oil from an oil-bearing reservoir, comprising:
providing a row of vertical injection wells completed for injection at an interval in the upper part of the reservoir, for injecting oxygen-containing gas into the reservoir to support a combustion front therein;
providing at least one gas production well spaced laterally from the row and completed in the reservoir, for producing the combustion gases;
providing a horizontal oil production well, positioned in spaced relation below the injection interval and being generally aligned with the row, for producing oil and water in liquid form;
injecting an oxygen-containing gas at less than fracturing pressure through each injection well and establishing a combustion front emanating from each such well to form a hot gas-containing fluid-transmissive chamber extending around each injection well and down to the oil production well, so that heated oil and water will drain downwardly through the chamber under the influence of gravity, said combustion front further being operative to produce combustion gases which flow through the reservoir toward the gas production wells; and producing hot oil and water in liquid form through the horizontal oil production well and combustion gases through the gas production well.
providing a row of vertical injection wells completed for injection at an interval in the upper part of the reservoir, for injecting oxygen-containing gas into the reservoir to support a combustion front therein;
providing at least one gas production well spaced laterally from the row and completed in the reservoir, for producing the combustion gases;
providing a horizontal oil production well, positioned in spaced relation below the injection interval and being generally aligned with the row, for producing oil and water in liquid form;
injecting an oxygen-containing gas at less than fracturing pressure through each injection well and establishing a combustion front emanating from each such well to form a hot gas-containing fluid-transmissive chamber extending around each injection well and down to the oil production well, so that heated oil and water will drain downwardly through the chamber under the influence of gravity, said combustion front further being operative to produce combustion gases which flow through the reservoir toward the gas production wells; and producing hot oil and water in liquid form through the horizontal oil production well and combustion gases through the gas production well.
2. The process as set forth in claim 1 wherein:
a plurality of gas production wells are provided, said wells being completed for production at intervals located in the upper part of the reservoir.
a plurality of gas production wells are provided, said wells being completed for production at intervals located in the upper part of the reservoir.
3. The process as set forth in claims 1 or 2 wherein the gas production rate through the horizontal well is controlled at low rates to maintain a head of liquid over the oil production well.
4. The process as set forth in claim 1 comprising:
cyclically steam stimulating the injection wells and oil production well, before initiating injection of oxygen-containing gas, to develop fluid communication between the injection wells and the oil production well.
cyclically steam stimulating the injection wells and oil production well, before initiating injection of oxygen-containing gas, to develop fluid communication between the injection wells and the oil production well.
5. The process as set forth in claim 1 or 2 wherein gas is injected into the injection wells prior to combustion operations until gas communication is established with the gas production wells.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA002096034A CA2096034C (en) | 1993-05-07 | 1993-05-07 | Horizontal well gravity drainage combustion process for oil recovery |
| US08/189,966 US5456315A (en) | 1993-05-07 | 1994-02-01 | Horizontal well gravity drainage combustion process for oil recovery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA002096034A CA2096034C (en) | 1993-05-07 | 1993-05-07 | Horizontal well gravity drainage combustion process for oil recovery |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2096034A1 CA2096034A1 (en) | 1994-11-08 |
| CA2096034C true CA2096034C (en) | 1996-07-02 |
Family
ID=4151626
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002096034A Expired - Lifetime CA2096034C (en) | 1993-05-07 | 1993-05-07 | Horizontal well gravity drainage combustion process for oil recovery |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US5456315A (en) |
| CA (1) | CA2096034C (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104453821A (en) * | 2014-11-10 | 2015-03-25 | 中国石油天然气股份有限公司 | In-situ combustion layered ignition method |
Families Citing this family (85)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5626191A (en) * | 1995-06-23 | 1997-05-06 | Petroleum Recovery Institute | Oilfield in-situ combustion process |
| US6729394B1 (en) * | 1997-05-01 | 2004-05-04 | Bp Corporation North America Inc. | Method of producing a communicating horizontal well network |
| US6257334B1 (en) | 1999-07-22 | 2001-07-10 | Alberta Oil Sands Technology And Research Authority | Steam-assisted gravity drainage heavy oil recovery process |
| US20020038069A1 (en) * | 2000-04-24 | 2002-03-28 | Wellington Scott Lee | In situ thermal processing of a coal formation to produce a mixture of olefins, oxygenated hydrocarbons, and aromatic hydrocarbons |
| US7096953B2 (en) * | 2000-04-24 | 2006-08-29 | Shell Oil Company | In situ thermal processing of a coal formation using a movable heating element |
| CA2325777C (en) | 2000-11-10 | 2003-05-27 | Imperial Oil Resources Limited | Combined steam and vapor extraction process (savex) for in situ bitumen and heavy oil production |
| CA2342955C (en) | 2001-04-04 | 2005-06-14 | Roland P. Leaute | Liquid addition to steam for enhancing recovery of cyclic steam stimulation or laser-css |
| US6994169B2 (en) * | 2001-04-24 | 2006-02-07 | Shell Oil Company | In situ thermal processing of an oil shale formation with a selected property |
| US7055600B2 (en) * | 2001-04-24 | 2006-06-06 | Shell Oil Company | In situ thermal recovery from a relatively permeable formation with controlled production rate |
| CA2349234C (en) | 2001-05-31 | 2004-12-14 | Imperial Oil Resources Limited | Cyclic solvent process for in-situ bitumen and heavy oil production |
| AU2002363073A1 (en) | 2001-10-24 | 2003-05-06 | Shell Internationale Research Maatschappij B.V. | Method and system for in situ heating a hydrocarbon containing formation by a u-shaped opening |
| CA2503394C (en) | 2002-10-24 | 2011-06-14 | Shell Canada Limited | Temperature limited heaters for heating subsurface formations or wellbores |
| AU2004235350B8 (en) | 2003-04-24 | 2013-03-07 | Shell Internationale Research Maatschappij B.V. | Thermal processes for subsurface formations |
| US7073577B2 (en) * | 2003-08-29 | 2006-07-11 | Applied Geotech, Inc. | Array of wells with connected permeable zones for hydrocarbon recovery |
| CA2462359C (en) | 2004-03-24 | 2011-05-17 | Imperial Oil Resources Limited | Process for in situ recovery of bitumen and heavy oil |
| JP4794550B2 (en) | 2004-04-23 | 2011-10-19 | シエル・インターナシヨナル・リサーチ・マートスハツペイ・ベー・ヴエー | Temperature limited heater used to heat underground formations |
| US7493952B2 (en) * | 2004-06-07 | 2009-02-24 | Archon Technologies Ltd. | Oilfield enhanced in situ combustion process |
| WO2005121504A1 (en) * | 2004-06-07 | 2005-12-22 | Archon Technologies Ltd. | Oilfield enhanced in situ combustion process |
| CA2492306A1 (en) * | 2005-01-13 | 2006-07-13 | Encana | In situ combustion following primary recovery processes utilizing horizontal well pairs in oil sands and heavy oil reservoirs |
| US7942197B2 (en) | 2005-04-22 | 2011-05-17 | Shell Oil Company | Methods and systems for producing fluid from an in situ conversion process |
| US7559367B2 (en) | 2005-10-24 | 2009-07-14 | Shell Oil Company | Temperature limited heater with a conduit substantially electrically isolated from the formation |
| US7581587B2 (en) * | 2006-01-03 | 2009-09-01 | Precision Combustion, Inc. | Method for in-situ combustion of in-place oils |
| US8167036B2 (en) * | 2006-01-03 | 2012-05-01 | Precision Combustion, Inc. | Method for in-situ combustion of in-place oils |
| US7809538B2 (en) | 2006-01-13 | 2010-10-05 | Halliburton Energy Services, Inc. | Real time monitoring and control of thermal recovery operations for heavy oil reservoirs |
| US20090044940A1 (en) * | 2006-02-15 | 2009-02-19 | Pfefferle William C | Method for CAGD recovery of heavy oil |
| US20070187093A1 (en) * | 2006-02-15 | 2007-08-16 | Pfefferle William C | Method for recovery of stranded oil |
| EP2010755A4 (en) | 2006-04-21 | 2016-02-24 | Shell Int Research | Time sequenced heating of multiple layers in a hydrocarbon containing formation |
| US7832482B2 (en) | 2006-10-10 | 2010-11-16 | Halliburton Energy Services, Inc. | Producing resources using steam injection |
| US7770643B2 (en) | 2006-10-10 | 2010-08-10 | Halliburton Energy Services, Inc. | Hydrocarbon recovery using fluids |
| WO2008051834A2 (en) | 2006-10-20 | 2008-05-02 | Shell Oil Company | Heating hydrocarbon containing formations in a spiral startup staged sequence |
| AU2008242808B2 (en) | 2007-04-20 | 2011-09-22 | Shell Internationale Research Maatschappij B.V. | Varying properties of in situ heat treatment of a tar sands formation based on assessed viscosities |
| WO2009052042A1 (en) | 2007-10-19 | 2009-04-23 | Shell Oil Company | Cryogenic treatment of gas |
| US7740062B2 (en) | 2008-01-30 | 2010-06-22 | Alberta Research Council Inc. | System and method for the recovery of hydrocarbons by in-situ combustion |
| US7841404B2 (en) * | 2008-02-13 | 2010-11-30 | Archon Technologies Ltd. | Modified process for hydrocarbon recovery using in situ combustion |
| EA019751B1 (en) | 2008-04-18 | 2014-06-30 | Шелл Интернэшнл Рисерч Маатсхаппий Б.В. | Method and system for treating a subsurface hydrocarbon containing formation |
| US8127842B2 (en) * | 2008-08-12 | 2012-03-06 | Linde Aktiengesellschaft | Bitumen production method |
| US8261832B2 (en) | 2008-10-13 | 2012-09-11 | Shell Oil Company | Heating subsurface formations with fluids |
| US7793720B2 (en) * | 2008-12-04 | 2010-09-14 | Conocophillips Company | Producer well lugging for in situ combustion processes |
| US8132620B2 (en) * | 2008-12-19 | 2012-03-13 | Schlumberger Technology Corporation | Triangle air injection and ignition extraction method and system |
| US8176980B2 (en) | 2009-02-06 | 2012-05-15 | Fccl Partnership | Method of gas-cap air injection for thermal oil recovery |
| CA2692885C (en) * | 2009-02-19 | 2016-04-12 | Conocophillips Company | In situ combustion processes and configurations using injection and production wells |
| US8448707B2 (en) | 2009-04-10 | 2013-05-28 | Shell Oil Company | Non-conducting heater casings |
| CA2709241C (en) * | 2009-07-17 | 2015-11-10 | Conocophillips Company | In situ combustion with multiple staged producers |
| CA2678347C (en) * | 2009-09-11 | 2010-09-21 | Excelsior Energy Limited | System and method for enhanced oil recovery from combustion overhead gravity drainage processes |
| CA2698454C (en) * | 2010-03-30 | 2011-11-29 | Archon Technologies Ltd. | Improved in-situ combustion recovery process using single horizontal well to produce oil and combustion gases to surface |
| US8833453B2 (en) | 2010-04-09 | 2014-09-16 | Shell Oil Company | Electrodes for electrical current flow heating of subsurface formations with tapered copper thickness |
| US8739874B2 (en) | 2010-04-09 | 2014-06-03 | Shell Oil Company | Methods for heating with slots in hydrocarbon formations |
| US8631866B2 (en) | 2010-04-09 | 2014-01-21 | Shell Oil Company | Leak detection in circulated fluid systems for heating subsurface formations |
| US9033042B2 (en) | 2010-04-09 | 2015-05-19 | Shell Oil Company | Forming bitumen barriers in subsurface hydrocarbon formations |
| MX2011004735A (en) * | 2010-05-11 | 2011-11-10 | Resource Innovations Inc | Thermal mobilization of heavy hydrocarbon deposits. |
| GB2481594B (en) * | 2010-06-28 | 2015-10-28 | Statoil Petroleum As | A method of recovering a hydrocarbon mixture from a subterranean formation |
| GB201100549D0 (en) | 2011-01-13 | 2011-03-02 | Statoil Canada Ltd | Process for the recovery of heavy oil and bitumen in situ combustion |
| US9016370B2 (en) | 2011-04-08 | 2015-04-28 | Shell Oil Company | Partial solution mining of hydrocarbon containing layers prior to in situ heat treatment |
| US9551207B2 (en) | 2011-05-19 | 2017-01-24 | Jason Swist | Pressure assisted oil recovery |
| US9328592B2 (en) | 2011-07-13 | 2016-05-03 | Nexen Energy Ulc | Steam anti-coning/cresting technology ( SACT) remediation process |
| WO2013006950A1 (en) | 2011-07-13 | 2013-01-17 | Nexen Inc. | Hydrocarbon recovery with in-situ combustion and separate injection of steam and oxygen |
| CN103958824B (en) | 2011-10-07 | 2016-10-26 | 国际壳牌研究有限公司 | Regulate for heating the thermal expansion of the circulation of fluid system of subsurface formations |
| CN104011331B (en) * | 2011-10-21 | 2017-09-01 | 尼克森能源无限责任公司 | With the SAGD method of oxygenation |
| CA2791323A1 (en) * | 2011-10-21 | 2013-04-21 | Nexen Inc. | Steam assisted gravity drainage processes with the addition of oxygen addition |
| CN102392626A (en) * | 2011-10-25 | 2012-03-28 | 联合石油天然气投资有限公司 | Method for exploiting thick-layer heavy oil reservoir by in situ combustion assisted gravity drainage |
| US9605524B2 (en) | 2012-01-23 | 2017-03-28 | Genie Ip B.V. | Heater pattern for in situ thermal processing of a subsurface hydrocarbon containing formation |
| CA2862463A1 (en) | 2012-01-23 | 2013-08-01 | Genie Ip B.V. | Heater pattern for in situ thermal processing of a subsurface hydrocarbon containing formation |
| CA2771703A1 (en) * | 2012-03-16 | 2013-09-16 | Sunshine Oilsands Ltd. | Fully controlled combustion assisted gravity drainage process |
| CA2815737C (en) | 2012-05-15 | 2020-05-05 | Nexen Inc. | Steam assisted gravity drainage with added oxygen geometry for impaired bitumen reservoirs |
| WO2014035788A1 (en) | 2012-08-28 | 2014-03-06 | Conocophillips Company | In situ combustion for steam recovery infill |
| US9738837B2 (en) | 2013-05-13 | 2017-08-22 | Cenovus Energy, Inc. | Process and system for treating oil sands produced gases and liquids |
| CA2852542C (en) | 2013-05-24 | 2017-08-01 | Cenovus Energy Inc. | Hydrocarbon recovery facilitated by in situ combustion |
| US10030491B2 (en) * | 2013-11-15 | 2018-07-24 | Nexen Energy Ulc | Method for increasing gas recovery in fractures proximate fracture treated wellbores |
| CA2871569C (en) | 2013-11-22 | 2017-08-15 | Cenovus Energy Inc. | Waste heat recovery from depleted reservoir |
| CN103953321B (en) * | 2014-04-02 | 2016-08-31 | 中国石油天然气股份有限公司 | Inclined shaft combustion in situ continuous pipe electric ignition tubing string and ignition method |
| CN104265249B (en) * | 2014-09-03 | 2017-10-20 | 北京普新石油技术开发有限公司 | A kind of combustion in situ huff and puff oil recovery method |
| CN104481485B (en) * | 2014-11-10 | 2017-02-01 | 中国石油天然气股份有限公司 | Layered ignition device for in-situ combustion |
| CN104405357A (en) * | 2014-10-31 | 2015-03-11 | 中国石油天然气股份有限公司 | Oil-layer fire-flooding mining method |
| CA2972203C (en) | 2017-06-29 | 2018-07-17 | Exxonmobil Upstream Research Company | Chasing solvent for enhanced recovery processes |
| US10815761B2 (en) * | 2017-07-05 | 2020-10-27 | Cenovus Energy Inc. | Process for producing hydrocarbons from a subterranean hydrocarbon-bearing reservoir |
| RU2657036C1 (en) * | 2017-07-21 | 2018-06-08 | Федеральное государственное бюджетное учреждение науки Институт проблем управления им. В.А. Трапезникова Российской академии наук | Method of in-situ combustion |
| RU2715572C2 (en) * | 2017-07-21 | 2020-03-02 | Федеральное государственное бюджетное учреждение науки Институт проблем управления им. В.А. Трапезникова Российской академии наук | Device for in-situ burning |
| CA2974712C (en) | 2017-07-27 | 2018-09-25 | Imperial Oil Resources Limited | Enhanced methods for recovering viscous hydrocarbons from a subterranean formation as a follow-up to thermal recovery processes |
| CA2978157C (en) | 2017-08-31 | 2018-10-16 | Exxonmobil Upstream Research Company | Thermal recovery methods for recovering viscous hydrocarbons from a subterranean formation |
| CA2983541C (en) | 2017-10-24 | 2019-01-22 | Exxonmobil Upstream Research Company | Systems and methods for dynamic liquid level monitoring and control |
| CN111155986B (en) * | 2019-12-27 | 2021-06-11 | 中国石油大学(北京) | Method, device, equipment and system for determining well spacing of multi-layer commingled production gas well |
| US11697983B2 (en) | 2020-08-10 | 2023-07-11 | Saudi Arabian Oil Company | Producing hydrocarbons with carbon dioxide and water injection through stacked lateral dual injection |
| CN112196505A (en) * | 2020-09-04 | 2021-01-08 | 中国石油工程建设有限公司 | Oil reservoir in-situ conversion hydrogen production system and hydrogen production process thereof |
| US11708736B1 (en) | 2022-01-31 | 2023-07-25 | Saudi Arabian Oil Company | Cutting wellhead gate valve by water jetting |
| CN116044368B (en) * | 2023-04-03 | 2023-06-30 | 中国电建集团西北勘测设计研究院有限公司 | Curve directional drilling geological exploration drilling layout method |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2365591A (en) * | 1942-08-15 | 1944-12-19 | Ranney Leo | Method for producing oil from viscous deposits |
| US2901043A (en) * | 1955-07-29 | 1959-08-25 | Pan American Petroleum Corp | Heavy oil recovery |
| US2958519A (en) * | 1958-06-23 | 1960-11-01 | Phillips Petroleum Co | In situ combustion process |
| US3044545A (en) * | 1958-10-02 | 1962-07-17 | Phillips Petroleum Co | In situ combustion process |
| US3441083A (en) * | 1967-11-09 | 1969-04-29 | Tenneco Oil Co | Method of recovering hydrocarbon fluids from a subterranean formation |
| US3727686A (en) * | 1971-03-15 | 1973-04-17 | Shell Oil Co | Oil recovery by overlying combustion and hot water drives |
| US3794113A (en) * | 1972-11-13 | 1974-02-26 | Mobil Oil Corp | Combination in situ combustion displacement and steam stimulation of producing wells |
| SU925094A1 (en) * | 1980-02-21 | 1988-08-15 | Всесоюзный Научно-Исследовательский Институт Использования Газа В Народном Хозяйстве И Подземного Хранения Нефти,Нефтепродуктов И Сжиженных Газов | Method of underground gasification of coal |
| US4384613A (en) * | 1980-10-24 | 1983-05-24 | Terra Tek, Inc. | Method of in-situ retorting of carbonaceous material for recovery of organic liquids and gases |
| US4356866A (en) * | 1980-12-31 | 1982-11-02 | Mobil Oil Corporation | Process of underground coal gasification |
| US4390067A (en) * | 1981-04-06 | 1983-06-28 | Exxon Production Research Co. | Method of treating reservoirs containing very viscous crude oil or bitumen |
| US4422505A (en) * | 1982-01-07 | 1983-12-27 | Atlantic Richfield Company | Method for gasifying subterranean coal deposits |
| US4454916A (en) * | 1982-11-29 | 1984-06-19 | Mobil Oil Corporation | In-situ combustion method for recovery of oil and combustible gas |
| US4566537A (en) * | 1984-09-20 | 1986-01-28 | Atlantic Richfield Co. | Heavy oil recovery |
| US4718485A (en) * | 1986-10-02 | 1988-01-12 | Texaco Inc. | Patterns having horizontal and vertical wells |
| CA2046107C (en) * | 1991-07-03 | 1994-12-06 | Geryl Owen Brannan | Laterally and vertically staggered horizontal well hydrocarbon recovery method |
| US5211230A (en) * | 1992-02-21 | 1993-05-18 | Mobil Oil Corporation | Method for enhanced oil recovery through a horizontal production well in a subsurface formation by in-situ combustion |
-
1993
- 1993-05-07 CA CA002096034A patent/CA2096034C/en not_active Expired - Lifetime
-
1994
- 1994-02-01 US US08/189,966 patent/US5456315A/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104453821A (en) * | 2014-11-10 | 2015-03-25 | 中国石油天然气股份有限公司 | In-situ combustion layered ignition method |
| CN104453821B (en) * | 2014-11-10 | 2017-02-01 | 中国石油天然气股份有限公司 | In-situ combustion layered ignition method |
Also Published As
| Publication number | Publication date |
|---|---|
| US5456315A (en) | 1995-10-10 |
| CA2096034A1 (en) | 1994-11-08 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2096034C (en) | Horizontal well gravity drainage combustion process for oil recovery | |
| US10655441B2 (en) | Stimulation of light tight shale oil formations | |
| US6328104B1 (en) | Upgrading and recovery of heavy crude oils and natural bitumens by in situ hydrovisbreaking | |
| US5339897A (en) | Recovery and upgrading of hydrocarbon utilizing in situ combustion and horizontal wells | |
| CA2643285C (en) | Method for producing viscous hydrocarbon using steam and carbon dioxide | |
| CA2569676C (en) | Oilfield enhanced in situ combustion process | |
| US4303126A (en) | Arrangement of wells for producing subsurface viscous petroleum | |
| CA1295547C (en) | Overburn process for recovery of heavy bitumens | |
| US20060042794A1 (en) | Method for high temperature steam | |
| CA2713703C (en) | A fishbone well configuration for in situ combustion | |
| CA2698454C (en) | Improved in-situ combustion recovery process using single horizontal well to produce oil and combustion gases to surface | |
| US4691773A (en) | Insitu wet combustion process for recovery of heavy oils | |
| US20140096961A1 (en) | Thermal mobilization of heavy hydrocarbon deposits | |
| US4436153A (en) | In-situ combustion method for controlled thermal linking of wells | |
| CA1228533A (en) | Heavy oil recovery | |
| US3024841A (en) | Method of oil recovery by in situ combustion | |
| US9284827B2 (en) | Hydrocarbon recovery facilitated by in situ combustion | |
| CA2856914C (en) | In situ combustion with a mobile fluid zone | |
| CA2028531A1 (en) | Enhanced oil recovery for oil reservoir underlain by water | |
| CA2363909C (en) | Upgrading and recovery of heavy crude oils and natural bitumens by in situ hydrovisbreaking | |
| US3138202A (en) | Thermal oil recovery process | |
| CA2678348C (en) | Reduction of fluid loss from operating chambers in steam assisted gravity drainage to increase in situ hydrocarbon recovery | |
| CA1221026A (en) | Method for recovering oil by in-situ combustion using oxygen | |
| US20220074296A1 (en) | Well configuration for coinjection | |
| Satman et al. | Survey of in-situ combustion field experience and correlation of results |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed |
Effective date: 20130507 |
|
| MKEC | Expiry (correction) |
Effective date: 20131009 |