US3280911A - Well liner with permeable joint - Google Patents

Well liner with permeable joint Download PDF

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US3280911A
US3280911A US330129A US33012963A US3280911A US 3280911 A US3280911 A US 3280911A US 330129 A US330129 A US 330129A US 33012963 A US33012963 A US 33012963A US 3280911 A US3280911 A US 3280911A
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liner
sections
well
conduit
joint
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Lloyd K Strange
Jr James S Mcniel
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Mobil Oil AS
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    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21BEARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B43/00Methods or apparatus for obtaining oil, gas, water, soluble or meltable materials or a slurry of minerals from wells
    • E21B43/16Enhanced recovery methods for obtaining hydrocarbons
    • E21B43/24Enhanced recovery methods for obtaining hydrocarbons using heat, e.g. steam injection
    • E21B43/2405Enhanced recovery methods for obtaining hydrocarbons using heat, e.g. steam injection in association with fracturing or crevice forming processes
    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21BEARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B43/00Methods or apparatus for obtaining oil, gas, water, soluble or meltable materials or a slurry of minerals from wells
    • E21B43/02Subsoil filtering
    • E21B43/08Screens or liners

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  • This invention relates to a method and an apparatus for completing a well subject to the flow of hot, oxidizing fluids. More particularly, it relates to a liner and a method of completing oil Wells with this liner when the wells are associated with high temperature, secondary recovery projects.
  • thermal recovery techniques is the in-situ combustion process.
  • a combustion supporting gas such as air or oxygen is injected into the subterranean formation through one or more injection wells.
  • Hydrocarbons having lowered viscosity are produced from one or more surrounding production wells.
  • Most in-situ combustion processes are variations on two basic techniques. The first is straightforward combustion in which the zone of combustion or combustion front moves through the formation from the injection well to the production Well, the hydrocarbons flowing before it. The second is inverse combustion in which the combustion front moves from the production well to the injection well, the hydrocarbons flowing through the combustion front.
  • the temperature and amount of oxidizing fluids will not be as great in the production well. However, the corrosion is intensified by the erosion of the liner and other well equipment by produced fluids containing particulate matter such as sand grains.
  • a liner which is adapted for use in a well where oxidizing atmospheres at temperatures above 800 F. are encountered and which comprises a plurality of stacked, articulated conduit sections of a refractory material which conformably abut each to the other.
  • These articulated conduit sections should preferably be permeable, i.e., the walls of each section should be permeable to the flow of fluids therethrough.
  • the conformable abutment which will be referred to as a joint, between sections is permeable to the flow of fluid, this fluid either being injected or produced.
  • the joint is impermeable to the influx of solid particles such as sand.
  • the conduit sections will generally by cylindrical, although other shapes may be employed.
  • the invention also provides a well comprising the liner.
  • FIGURE 1 is a view in cross section of one embodiment of the invention.
  • FIGURE 2 is an isometric drawing of a conduit section having a protruding spherical end and a recessed spherical end.
  • FIGURE 3 is a cross-sectional view of two adjacent conduit sections in a lap-type abutting relationship, referred to as a lap-type joint.
  • FIGURE 4 is an elevation view of two conduit sections conformably abutting in a keyhole-type relationship, referred to as a keyhole joint.
  • FIGURE 5 is a cross-sectional view of a preferred embodiment of the invention.
  • Formation 13 is a permeable formation in which in-situ combustion will be carried out and the flow of hot, oxidizing fluids will be encountered.
  • Formations 14 and 15 are impermeable formations adjacent formation 13.
  • Casing 16 is cemented in place and provided with conventional cement foot 18. Casing 16 terminates short of formation 13.
  • Heat resistant plugs, or packers, 20 and 22 form a seal against the impermeable formations 14 and 15.
  • Packer 20 also forms a seal with conduit 24 penetrating therethrough and connecting with liner 28.
  • Liner 28 is comprised of multiple sections such as 32,
  • sections 33, 34, 35, and 36 which are relatively short, articulated sections of thick wall refractory tubes. These sections may be as short as six inches or less. They may be as long as four feet or longer. They may be stacked to any desired height to form a liner throughout the producing subterranean formation.
  • the sections can be constructed of any refractory material. For example, fused alumina, silicon carbide, fused quartz aggregate, and the refractory cements can be employed for this construction. Table 1 below shows specifications which are useful in connection with the manufacture of the articulated conduit sections.
  • the Walls of each section should preferably be permeable.
  • the permeability may be as low as about 10 millidarcies and as high as about 600 millidarcies or higher. Sections having even greater permeability are desirable if they have adequate compressive strengths and do not allow finely divided solids such as sand or silt to pass through.
  • the fused alumina sections had a permeability of about millidarcies and a porosity of approximately 28 percent.
  • an 8-inch section supported a compressive load of 41,000 pounds before breaking. This corresponds to a compressive strength of 5700 p.s.i.a.
  • a 12-inch long section was dropped onto a concrete floor from heights up to 4 feet with only chipping when the end struck the fioor squarely. Thirty feet of 18-inch sections of 4%" OD. x 3%" LD. fused alumina liner weighed only 150 pounds.
  • Each section terminates in a protruding end and a recessed end.
  • Each section is rough cast so the protruding and recessed ends, while conformably fitting together, provide a rough fit. This fit or joint provides adequate fluid permeability, yet restricts the flow of particulate matter such as sand grains.
  • the estimated pressure drop through a typical rough cast joint is less than 1 psi. for a joint providing an average opening on the order of 0.01 inch. Yet, because of the tortuous path through which the fluid must flow, sand grains of much smaller dimensions than the average opening are filtered out.
  • At least three types of ends will fit yet provide adequate fiexure to avoid emplacement problems and, once in place, control the influx of sand into the well.
  • FIGURE 2 illustrates the preferred embodiment wherein the section terminates in a spherical end.
  • Section 35 is rough cast having one protruding end 38 and one recessed end 39. Both the protruding end 38 and the recessed end 39 have approximately the same spherical radius of curvature. Thus, they conform when adjacent sections are stacked together as shown in FIGURE 1.
  • FIGURE 3 is a cross-sectional view of two sections conformably abutting in lap-type relationship. With this configuration, an inner protrusion 44 is adapted to fit conformably into a recessed cylindrical opening 45 of the adjacent section.
  • FIGURE 4 shows adjacent sections joined with a keyhole-type joint.
  • diametrically opposed protruding keyhole ends 50 are provided with an enlargement 51 at the extremity of neck 52 on one end of section 53.
  • a conformable end illustrated at the bottom of section 55 At the other end of section 53 there is provided a conformable end illustrated at the bottom of section 55.
  • an enlarged opening 56 adapted to fit enlargement 51 is provided at one end of notch 57 adapted to fit conformably with neck 52 of section 53.
  • a retaining ring 60 (shown in dotted lines) may be clipped around the joints between rings 61 and 62 to prevent lateral movement. Ring 60 need not be resistant to high temperature since its function is necessary only during the setting operation. While the keyhole-type joint is more elaborate and more expensive than the spherical or laptype abutment, it has some advantages in that it can sustain slight tension.
  • Conduit 24 should be constructed to heat and corrosion resistant material, such as titanium or stainless steel, when used in the production Well. Alternatively, it may be conventional tubing having a heat and corrosion resistant internal coating, such as a ceramic lining. It may be conventional tubing in the injection well.
  • heat and corrosion resistant material such as titanium or stainless steel
  • it may be conventional tubing having a heat and corrosion resistant internal coating, such as a ceramic lining. It may be conventional tubing in the injection well.
  • Conduit 24 may be connected to liner 28 by cap 26.
  • Cap 26 should be constructed of heat and corrosion resistant metallic alloys, such as those of stainless steel and titanium.
  • Cap 26 is provided with an annular recess 30 adapted to fit conformably the top end of the section 36, and with threads 27 adapted to screw onto conduit 24.
  • Cap 26 should be somewhat removed from the turbulent, high temperature zone adjacent formation 13, as shown in FIGURE 1. Obviously, other connecting means can be employed.
  • FIGURE 5 is a cross-sectional view of this preferred embodiment wherein the heat resistant liner has been emplaced in the preperforated metal liner.
  • the articulated conduit sections as exemplified by section '70 hav-e been inserted into preperforated metal liner 71.
  • This preperforated metal liner 71 is a conventional mild steel liner having preperforations such as shown at 73.
  • Metal liner 71 is expendable and is used only in setting the heat resistant or refractory liner 28.
  • Metal liner 71 will have closure 74 at its bottom end to support sections 70 of liner 28. Closure '74 rests on heat resistant packer 22 which may be, for example, a plug of high temperature oement. Metal liner 71 is connected to conduit 24 in communication with surface equipment. Where the diameter of the conduit 24, which may be, for example, tubing, is different from the diameter of liner 71, as will generally be the case, an appropriate cross-over connection 76 will be used to connect the two. Obviously, threaded or welded connections can be used conjunctively or alternatively.
  • the top articulated section 70 may be sealed to liner 71 by high temperature cement 77 or other suitable material. With such a seal, heat resistant packer 20 may be set below threads 78. Alternatively, heat resistant packer 20 may be set above threads 78 as shown'in FIGURE 1. In either construction, packer 20 will force fluids to flow in the interior of conduit 24 and through liner 28.
  • the insertion of heat resistant liner 28 within metal liner 71 obviously presents no problems in lengths of less than one joint of metal liner. Where it must be longer and thus not readily handled by the rig available, the liner is assembled for emplacement as follows. The first joint of preperforated liner 71 having inserted within it a section of liner 28 is partially lowered into wellbore 10 and held in place. A second joint of preperforated metal liner 71 having inserted inside it another section of liner 28 is positioned directly above the first. By way of example only, a piece of strap steel welded across the bottom end of the second joint will hold the second section of internal liner 28 satisfactorily during such positioning.
  • liner 28 is not too heavy, it can be held manually while the strap steel is cut from across the open end of the second length of metal liner 71.
  • the second length of liner 28 is then lowered onto the first length, and the second length of metal liner 71 is lowered onto and welded to the first length of liner 71. In this manner, any desired length liner can be assembled and lowered into the wellbore.
  • a well liner adapted for use in oxidizing atmospheres at temperatures above 800 F. which comprises stacked, articulated conduit sections of a refractory material, said sections having protruding and recessed ends and conformably abutting one to another toform joint means providing flexibility in permitting lateral movement of said sections individually and maintaining said sections in fluid permeable, sand impermeable relationship.
  • a well liner adapted for use in oxidizing atmospheres at temperatures above 800 F. which comprises stacked, permeable, articulated, cylindrical conduit sections of a refractory material, said sections having protruding and recessed ends and conformably abutting one to another to form joint means providing flexibility in permitting lateral movement of said sections individual-1y and maintaining said sections in fluid permeable, sand impermeable relationship.
  • a well liner adapted for use in oxidizing atmospheres at temperatures above 800 P. which comprises permeable, articulated, cylindrical conduit sections of a refractory material stacked within a preperforated, expendable metal conduit closed at its bottom end, said sections having protruding and recessed ends and conformably abutting one to another to form joint means providing flexibility in permitting lateral movement of said sections individually and maintaining said sections in fluid permeable, sand impermeable relationship.
  • a well adapted for use in recovering hydrocarbons from a subsurface formation by thermal methods wherein flow of hot, oxidizing fluids will be encountered which comprises a wellbore penetrating the formation; a liner comprised of stacked, articulated, cylindrical conduit sections of refractory material, said sections having protruding and recessed ends and conformably abutting one to another to form joint means providing flexibility in permitting lateral movement of said sections individually and maintaining said sections in fluid permeable, sand impermeable relationship disposed within the borehole; conduit means connected to said liner and communicating with the surface; and sealing plugs located within the borehole near the top and bottom of the formation supporting said liner and isolating the interior of said conduit, said liner, and said formation from the remainder of the wellbore and well in such manner that any fluid flow between surface and subsurface formation will be via said isolated interior, and through said liner.

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  • Engineering & Computer Science (AREA)
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Description

Oct. 25, 1966 L, K, STRANGE ETAL 3,280,911
WELL LINER WITH PERMEABLE JOINT Filed Dec. 12, 1963 2 Sheets-Sheet l LLOYD K. STRANGE JAMES S. MCNIEL,JR.
INVENTORS W a m PATENT AGENT 25, 1966 L. K. STRANGE ETAL 3,
WELL LINER WITH PERMEABLE JOINT Filed Dec. 12, 1963 2 Sheets-Sheet 2 LLOYD K. STRANGE JAMES S. MCNIEL,JR.
INVENTORS BY f PATENT AGENT United States Patent Ofitice 3,286,911 Patented Oct. 25, 1966 3,280,911 WELL LINER WITH PERMEABLE JOINT Lloyd K. Strange, Grand Prairie, and James S. McNiel, .Ir., Dallas, Tex., assiguors to Mobil Oil Corporation, a corporation of New York Filed Dec. 12, 1963, Ser. No. 330,129 11 Claims. (Cl. 166-228) This invention relates to a method and an apparatus for completing a well subject to the flow of hot, oxidizing fluids. More particularly, it relates to a liner and a method of completing oil Wells with this liner when the wells are associated with high temperature, secondary recovery projects.
Oil exists in subterranean formations in accumulations called reservoirs. Wells are drilled into the formation to tap these reservoirs and produce the oil by using the reservoir energy. Many times a large part of the oil cannot be produced from the formation utilizing solely the reservoir energy.
To increase the amount of oil produced from the formation, various methods have been used. One group of these methods utilizes thermal recovery techniques.
One of these thermal recovery techniques is the in-situ combustion process. In this process, a combustion supporting gas such as air or oxygen is injected into the subterranean formation through one or more injection wells. Then, as the name implies, there is burning in situs, or in the formation, of either an injected fuel or the hydrocarbons native to the formation using the injected combustion supporting gas. Hydrocarbons having lowered viscosity are produced from one or more surrounding production wells. Most in-situ combustion processes are variations on two basic techniques. The first is straightforward combustion in which the zone of combustion or combustion front moves through the formation from the injection well to the production Well, the hydrocarbons flowing before it. The second is inverse combustion in which the combustion front moves from the production well to the injection well, the hydrocarbons flowing through the combustion front.
With both in-situ combustion techniques there is encountered the problem of high temperature corrosion of any well liner and other well equipment used, because of the hot, oxidizing fluids. The temperature can be especially severe in an injection well, running as high as 1600 to 2000 F. Even at best, the temperatures will range from 800 to 1200 F. Where the injection well is completed in a relatively thick section, oil may drain by gravity into the injection well. In such cases, this high temperature may be sustained for an extended period of time. Under the extended high temperature conditions and in the presence of the hot oxidizing fluids, the conventional metal liner disintegrates, permitting sloughing of sand into the well, which reduces air injectivity.
The temperature and amount of oxidizing fluids will not be as great in the production well. However, the corrosion is intensified by the erosion of the liner and other well equipment by produced fluids containing particulate matter such as sand grains.
Attempts to alleviate these ditficulties have resulted in the use of plastic liners, glass liners, stainless steel tubing, and even titanium tubing. The use of none of these materials has been eminently successful. These materials are brittle and rather inflexible. Further, the wells are often crooked. One of the problems encountered in attempting to set in place a liner made of one of these materials is sticking of the liner in the crooked well. Where the liner will not sustain much tensile stress, the problem can be severe.
It is an object of this invention to provide a well liner capable of withstanding high temperatures. It is a further object of this invention to provide for a well a heat resistant liner which is capable of being set in place regardless of the degree of straightness of the well. For a more complete understanding of the invention and further objects, reference may be had to the description and figures which follow.
In accordance with the invention, there is provided a liner which is adapted for use in a well where oxidizing atmospheres at temperatures above 800 F. are encountered and which comprises a plurality of stacked, articulated conduit sections of a refractory material which conformably abut each to the other. These articulated conduit sections should preferably be permeable, i.e., the walls of each section should be permeable to the flow of fluids therethrough. In any case, the conformable abutment, which will be referred to as a joint, between sections is permeable to the flow of fluid, this fluid either being injected or produced. However, the joint is impermeable to the influx of solid particles such as sand. The conduit sections will generally by cylindrical, although other shapes may be employed. The invention also provides a well comprising the liner.
FIGURE 1 is a view in cross section of one embodiment of the invention.
FIGURE 2 is an isometric drawing of a conduit section having a protruding spherical end and a recessed spherical end.
FIGURE 3 is a cross-sectional view of two adjacent conduit sections in a lap-type abutting relationship, referred to as a lap-type joint.
FIGURE 4 is an elevation view of two conduit sections conformably abutting in a keyhole-type relationship, referred to as a keyhole joint.
FIGURE 5 is a cross-sectional view of a preferred embodiment of the invention.
Referring to FIGURE 1, well 10 penetrates subsurface formations 13, 14, and 15. Formation 13 is a permeable formation in which in-situ combustion will be carried out and the flow of hot, oxidizing fluids will be encountered. Formations 14 and 15 are impermeable formations adjacent formation 13. Casing 16 is cemented in place and provided with conventional cement foot 18. Casing 16 terminates short of formation 13. Heat resistant plugs, or packers, 20 and 22 form a seal against the impermeable formations 14 and 15. Packer 20 also forms a seal with conduit 24 penetrating therethrough and connecting with liner 28.
Liner 28 is comprised of multiple sections such as 32,
33, 34, 35, and 36 which are relatively short, articulated sections of thick wall refractory tubes. These sections may be as short as six inches or less. They may be as long as four feet or longer. They may be stacked to any desired height to form a liner throughout the producing subterranean formation. The sections can be constructed of any refractory material. For example, fused alumina, silicon carbide, fused quartz aggregate, and the refractory cements can be employed for this construction. Table 1 below shows specifications which are useful in connection with the manufacture of the articulated conduit sections.
Table 1 Operating temperature 2500" F. Outside diameter (0.1).) 4" to 4 /2". Wall thickness /2" approx. Length l to 2'. Stacking height Preferred type joint spherical.
As stated, the Walls of each section should preferably be permeable. The permeability may be as low as about 10 millidarcies and as high as about 600 millidarcies or higher. Sections having even greater permeability are desirable if they have adequate compressive strengths and do not allow finely divided solids such as sand or silt to pass through.
In a specific example, the fused alumina sections had a permeability of about millidarcies and a porosity of approximately 28 percent. In longitudinal compressive tests, an 8-inch section supported a compressive load of 41,000 pounds before breaking. This corresponds to a compressive strength of 5700 p.s.i.a. A 12-inch long section was dropped onto a concrete floor from heights up to 4 feet with only chipping when the end struck the fioor squarely. Thirty feet of 18-inch sections of 4%" OD. x 3%" LD. fused alumina liner weighed only 150 pounds.
Each section terminates in a protruding end and a recessed end. Each section is rough cast so the protruding and recessed ends, while conformably fitting together, provide a rough fit. This fit or joint provides adequate fluid permeability, yet restricts the flow of particulate matter such as sand grains.
For example, with air being injected at a fiow rate of 6.28 M c.f. per day per joint of 4 /4 O.D. X 3%" LD. conduit at a pressure of 200 p.s.i.g., the estimated pressure drop through a typical rough cast joint is less than 1 psi. for a joint providing an average opening on the order of 0.01 inch. Yet, because of the tortuous path through which the fluid must flow, sand grains of much smaller dimensions than the average opening are filtered out.
At least three types of ends will fit yet provide adequate fiexure to avoid emplacement problems and, once in place, control the influx of sand into the well.
FIGURE 2 illustrates the preferred embodiment wherein the section terminates in a spherical end. Section 35 is rough cast having one protruding end 38 and one recessed end 39. Both the protruding end 38 and the recessed end 39 have approximately the same spherical radius of curvature. Thus, they conform when adjacent sections are stacked together as shown in FIGURE 1.
FIGURE 3 is a cross-sectional view of two sections conformably abutting in lap-type relationship. With this configuration, an inner protrusion 44 is adapted to fit conformably into a recessed cylindrical opening 45 of the adjacent section.
FIGURE 4 shows adjacent sections joined with a keyhole-type joint. Therein, diametrically opposed protruding keyhole ends 50 are provided with an enlargement 51 at the extremity of neck 52 on one end of section 53. At the other end of section 53 there is provided a conformable end illustrated at the bottom of section 55. There, an enlarged opening 56 adapted to fit enlargement 51 is provided at one end of notch 57 adapted to fit conformably with neck 52 of section 53. A retaining ring 60 (shown in dotted lines) may be clipped around the joints between rings 61 and 62 to prevent lateral movement. Ring 60 need not be resistant to high temperature since its function is necessary only during the setting operation. While the keyhole-type joint is more elaborate and more expensive than the spherical or laptype abutment, it has some advantages in that it can sustain slight tension.
When the liner 28 of articulated sections is arranged as illustrated in FIGURE 1, fluids flowing into the formation from the well, such as air injected during an insitu combustion process, must flow through the liner. Alternatively, as in a production well when hot hydrocarbons, gases, and oxygen are flowing into the well from the formation, they are constrained to flow through liner 28 into its interior where they pass to the surface by conduit 24. In this way, the majority of 'well equipment is isolated from the hot, corrosive fluids.
Conduit 24 should be constructed to heat and corrosion resistant material, such as titanium or stainless steel, when used in the production Well. Alternatively, it may be conventional tubing having a heat and corrosion resistant internal coating, such as a ceramic lining. It may be conventional tubing in the injection well.
Conduit 24 may be connected to liner 28 by cap 26. Cap 26 should be constructed of heat and corrosion resistant metallic alloys, such as those of stainless steel and titanium. Cap 26 is provided with an annular recess 30 adapted to fit conformably the top end of the section 36, and with threads 27 adapted to screw onto conduit 24. Cap 26 should be somewhat removed from the turbulent, high temperature zone adjacent formation 13, as shown in FIGURE 1. Obviously, other connecting means can be employed.
In placing liner 28 into a well, it is necessary .to thread individually the sections of the liner over either a wire line operated or tubing operated mandrel where the wellbore is known to be crooked. The flexibility of liner 28, with its articulated sections which abut one another to form joint means which permit relative lateral movement of these sections, is a particular advantage of the invention and enables it to be inserted into crooked wellbores. The mandrel and liner 28 are lowered into position onto plug 22 and adjacent formation 13 by conventional wire line equipment or tubing, whichever the operator chooses. The mandrel releases bottom support 37 and liner 28. The mandrel is Withdrawn before cap 26 and conduit 24 are put into position and heat resistant packer 20 set in place to isolate liner 28.
In a preferred embodiment of the invention, the articulated sections of refractory material are assembled within a preperforated, expendable metal conduit which facilitates emplacement when the well is known to be relatively straight. FIGURE 5 is a cross-sectional view of this preferred embodiment wherein the heat resistant liner has been emplaced in the preperforated metal liner. Therein, the articulated conduit sections as exemplified by section '70 hav-e been inserted into preperforated metal liner 71. This preperforated metal liner 71 is a conventional mild steel liner having preperforations such as shown at 73. Metal liner 71 is expendable and is used only in setting the heat resistant or refractory liner 28. Metal liner 71 will have closure 74 at its bottom end to support sections 70 of liner 28. Closure '74 rests on heat resistant packer 22 which may be, for example, a plug of high temperature oement. Metal liner 71 is connected to conduit 24 in communication with surface equipment. Where the diameter of the conduit 24, which may be, for example, tubing, is different from the diameter of liner 71, as will generally be the case, an appropriate cross-over connection 76 will be used to connect the two. Obviously, threaded or welded connections can be used conjunctively or alternatively. The top articulated section 70 may be sealed to liner 71 by high temperature cement 77 or other suitable material. With such a seal, heat resistant packer 20 may be set below threads 78. Alternatively, heat resistant packer 20 may be set above threads 78 as shown'in FIGURE 1. In either construction, packer 20 will force fluids to flow in the interior of conduit 24 and through liner 28.
The insertion of heat resistant liner 28 within metal liner 71 obviously presents no problems in lengths of less than one joint of metal liner. Where it must be longer and thus not readily handled by the rig available, the liner is assembled for emplacement as follows. The first joint of preperforated liner 71 having inserted within it a section of liner 28 is partially lowered into wellbore 10 and held in place. A second joint of preperforated metal liner 71 having inserted inside it another section of liner 28 is positioned directly above the first. By way of example only, a piece of strap steel welded across the bottom end of the second joint will hold the second section of internal liner 28 satisfactorily during such positioning. Because liner 28 is not too heavy, it can be held manually while the strap steel is cut from across the open end of the second length of metal liner 71. The second length of liner 28 is then lowered onto the first length, and the second length of metal liner 71 is lowered onto and welded to the first length of liner 71. In this manner, any desired length liner can be assembled and lowered into the wellbore.
The invention has been described with particularly with respect to recovery of oil from subsurface reservoirs. It can of course be used in analogous circumstances such as recovering shale oil from oil shale and hydrocarbons from tar sands. Other modifications of the invention will readily occur to one skilled in the art. It is intended to cover such modifications and uses as fall within the scope of the appended claims.
What is claimed is:
1. A well liner adapted for use in oxidizing atmospheres at temperatures above 800 F. which comprises stacked, articulated conduit sections of a refractory material, said sections having protruding and recessed ends and conformably abutting one to another toform joint means providing flexibility in permitting lateral movement of said sections individually and maintaining said sections in fluid permeable, sand impermeable relationship.
2. The well liner of claim 1 wherein said refractory material is fused alumina.
3. A well liner adapted for use in oxidizing atmospheres at temperatures above 800 F. which comprises stacked, permeable, articulated, cylindrical conduit sections of a refractory material, said sections having protruding and recessed ends and conformably abutting one to another to form joint means providing flexibility in permitting lateral movement of said sections individual-1y and maintaining said sections in fluid permeable, sand impermeable relationship.
4. The well liner of claim 3 wherein said sections each have a protruding spherical end and a recessed spherical end.
5. The well liner of claim 3 wherein said sections each have a protruding keyhole end and a recessed keyhole end.
6. A well liner adapted for use in oxidizing atmospheres at temperatures above 800 P. which comprises permeable, articulated, cylindrical conduit sections of a refractory material stacked within a preperforated, expendable metal conduit closed at its bottom end, said sections having protruding and recessed ends and conformably abutting one to another to form joint means providing flexibility in permitting lateral movement of said sections individually and maintaining said sections in fluid permeable, sand impermeable relationship.
7. The well liner of claim 6 wherein said sections each have a protruding lap-type end and a recessed lap-type end.
8. A well adapted for use in recovering hydrocarbons from a subsurface formation by thermal methods wherein flow of hot, oxidizing fluids will be encountered, which comprises a wellbore penetrating the formation; a liner comprised of stacked, articulated, cylindrical conduit sections of refractory material, said sections having protruding and recessed ends and conformably abutting one to another to form joint means providing flexibility in permitting lateral movement of said sections individually and maintaining said sections in fluid permeable, sand impermeable relationship disposed within the borehole; conduit means connected to said liner and communicating with the surface; and sealing plugs located within the borehole near the top and bottom of the formation supporting said liner and isolating the interior of said conduit, said liner, and said formation from the remainder of the wellbore and well in such manner that any fluid flow between surface and subsurface formation will be via said isolated interior, and through said liner.
9. The well of claim 8 wherein a heat resistant metallic cap connects said liner to said conduit.
10. The well liner of claim 1 wherein said refractory material is refractory cement.
11. The well liner of claim 1 wherein said refractory material is fused quartz.
References Cited by the Examiner UNITED STATES PATENTS 1,292,992 2/1919 Bartram 285332.1 2,170,181 8/1939 Allen et al. 285-231 2,335,558 11/1943 Young 166-235 2,687,282 8/1954 Sanders -320 2,973,813 3/1961 Parker 166-11 3,134,435 5/1964 Wyllie 166-39 3,149,671 9/1964 Alexander 166-228 CHARLES E. OCONNELL, Primary Examiner.
I. A. LElPINK, Assistant Examiner,
UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent Non 3,280,911 October 25, 1966 Lloyd K, Strange et all It is hereby certified that error appears in the above numbered patent requiring correction and that the said Letters Patent should read as corrected below.
Column 2, line 20, for "by" read be column 3, line 22, for "6 Q 28 M c of read 6C8 mcfr. line 72, for "to" read of column 5, line 5, for "particularly" read particularity M a Signed and sealed this 22nd day of August 1967 (SEAL) Attest:
ERNEST W. SW'IDER EDWARD J. BRENNER Athesting Officer Commissioner of Patents

Claims (1)

1. A WELL-LINER ADAPTED FOR USE IN OXIDIZING ATMOSPHERES AT TEMPERATURES ABOVE 800* F. WHICH COMPRISES STACKED, ARTICULATED CONDUIT SECTIONS OF A REFRACTORY MATERIAL, SAID SECTIONS HAVING PROTRUDING AND RECESSED ENDS AND CONFORMABLY ABUTTING ONE TO ANOTHER TO FORM JOINT MEANS PROVIDING FLEXIBILITY IN PERMITTING LATERAL MOVEMENT OF SAID SECTIONS INDIVIDUAL AND MAINTAINING SAID SECTIONS IN FLUID PERMEABLE, SAND IMPERMEABLE RELATIONSHIP.
US330129A 1963-12-12 1963-12-12 Well liner with permeable joint Expired - Lifetime US3280911A (en)

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3366177A (en) * 1966-08-10 1968-01-30 Pan American Petroleum Corp Production of petroleum from unconsolidated formations
US3379252A (en) * 1965-11-29 1968-04-23 Phillips Petroleum Co Well completion for extreme temperatures
US3414055A (en) * 1966-10-24 1968-12-03 Mobil Oil Corp Formation consolidation using a combustible liner
US3461918A (en) * 1966-08-29 1969-08-19 Phillips Petroleum Co Corrosion protection
US4014387A (en) * 1974-01-11 1977-03-29 Thyssen Plastik Anger Kg Apparatus and process for drawing water from a water-bearing strata
US4624319A (en) * 1984-12-18 1986-11-25 Jacques A. Van Der Borght Method and apparatus to improve well water quality
US4811790A (en) * 1987-08-27 1989-03-14 Mobil Oil Corporation Well bore device and method for sand control
US4969518A (en) * 1988-11-14 1990-11-13 Stren Company Reciprocating rod type downhole pump
US5118016A (en) * 1990-09-27 1992-06-02 Martin & Pagenstecher, Inc. Bottom pour tiles with self sealing joint for pouring liquid steel
US5696801A (en) * 1995-08-24 1997-12-09 Performance Contracting, Inc. Suction strainer with a internal core tube
US5935439A (en) * 1997-02-19 1999-08-10 Performance Contracting, Inc. Suction system with end supported internal core tube suction strainers
US20040206679A1 (en) * 2002-11-25 2004-10-21 Bleigh James M Strainer assembly
US20070267340A1 (en) * 2006-05-22 2007-11-22 Bleigh James M Hydrofoil-shaped suction strainer with an internal core tube

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1292992A (en) * 1917-12-28 1919-02-04 George C Bartram Concrete pipe.
US2170181A (en) * 1937-06-11 1939-08-22 Morris C Allen Elastic pipe joint
US2335558A (en) * 1940-08-30 1943-11-30 Bruce B Young Well screen
US2687282A (en) * 1952-01-21 1954-08-24 Eastman Oil Well Survey Co Reaming bit structure for earth bores
US2973813A (en) * 1958-09-15 1961-03-07 Phillips Petroleum Co Process for controlling path in situ combustion front
US3134435A (en) * 1960-12-27 1964-05-26 Gulf Research Development Co Method for stabilizing an incompetent formation
US3149671A (en) * 1962-07-16 1964-09-22 Gem Oil Tool Company Inc Velocity joint and container

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1292992A (en) * 1917-12-28 1919-02-04 George C Bartram Concrete pipe.
US2170181A (en) * 1937-06-11 1939-08-22 Morris C Allen Elastic pipe joint
US2335558A (en) * 1940-08-30 1943-11-30 Bruce B Young Well screen
US2687282A (en) * 1952-01-21 1954-08-24 Eastman Oil Well Survey Co Reaming bit structure for earth bores
US2973813A (en) * 1958-09-15 1961-03-07 Phillips Petroleum Co Process for controlling path in situ combustion front
US3134435A (en) * 1960-12-27 1964-05-26 Gulf Research Development Co Method for stabilizing an incompetent formation
US3149671A (en) * 1962-07-16 1964-09-22 Gem Oil Tool Company Inc Velocity joint and container

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3379252A (en) * 1965-11-29 1968-04-23 Phillips Petroleum Co Well completion for extreme temperatures
US3366177A (en) * 1966-08-10 1968-01-30 Pan American Petroleum Corp Production of petroleum from unconsolidated formations
US3461918A (en) * 1966-08-29 1969-08-19 Phillips Petroleum Co Corrosion protection
US3414055A (en) * 1966-10-24 1968-12-03 Mobil Oil Corp Formation consolidation using a combustible liner
US4014387A (en) * 1974-01-11 1977-03-29 Thyssen Plastik Anger Kg Apparatus and process for drawing water from a water-bearing strata
US4624319A (en) * 1984-12-18 1986-11-25 Jacques A. Van Der Borght Method and apparatus to improve well water quality
US4811790A (en) * 1987-08-27 1989-03-14 Mobil Oil Corporation Well bore device and method for sand control
US4969518A (en) * 1988-11-14 1990-11-13 Stren Company Reciprocating rod type downhole pump
US5118016A (en) * 1990-09-27 1992-06-02 Martin & Pagenstecher, Inc. Bottom pour tiles with self sealing joint for pouring liquid steel
US5696801A (en) * 1995-08-24 1997-12-09 Performance Contracting, Inc. Suction strainer with a internal core tube
US5843314A (en) * 1995-08-24 1998-12-01 Performance Contracting, Inc. Suction strainer with an internal core tube
US5958234A (en) * 1995-08-24 1999-09-28 Performance Contracting, Inc. Suction strainer with an internal core tube
US6491818B2 (en) 1995-08-24 2002-12-10 Performance Contracting, Inc. Suction strainer with an internal core tube
US5935439A (en) * 1997-02-19 1999-08-10 Performance Contracting, Inc. Suction system with end supported internal core tube suction strainers
US20040206679A1 (en) * 2002-11-25 2004-10-21 Bleigh James M Strainer assembly
US20070267340A1 (en) * 2006-05-22 2007-11-22 Bleigh James M Hydrofoil-shaped suction strainer with an internal core tube

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