System and method for coupling lead-in conductor to insulated conductor

Description

RELATED PATENTS

This patent application incorporates by reference in its entirety each of U.S. Pat. Nos.

6,688,387 to Wellington et al.; 6,991,036 to Sumnu-Dindoruk et al.; 6,698,515 to Karanikas et al.; 6,880,633 to Wellington et al.; 6,782,947 to de Rouffignac et al.; 6,991,045 to Vinegar et al.; 7,073,578 to Vinegar et al.; 7,121,342 to Vinegar et al.; 7,320,364 to Fairbanks; 7,527,094 to McKinzie et al.; 7,584,789 to Mo et al.; 7,533,719 to Hinson et al.; 7,562,707 to Miller; 7,798,220 to Vinegar et al.; 8,636,323 to Prince-Wright et al.; 8,281,861 to Nguyen et al.; and 8,327,932 to Karanikas et al; and U.S. Patent Application Publication No. 2009-0189617 to Bums et al.

BACKGROUND

1. Field of the Invention

The present invention relates to systems for insulated conductors used in heater elements. More particularly, the invention relates to fittings to splice together insulated conductor cables and lead-in cables.

2. Description of Related Art

Hydrocarbons obtained from subterranean formations are often used as energy resources, as feedstocks, and as consumer products. Concerns over depletion of available hydrocarbon resources and concerns over declining overall quality of produced hydrocarbons have led to development of processes for more efficient recovery, processing and/or use of available hydrocarbon resources. In situ processes may be used to remove hydrocarbon materials from subterranean formations that were previously inaccessible and/or too expensive to extract using available methods. Chemical and/or physical properties of hydrocarbon material in a subterranean formation may need to be changed to allow hydrocarbon material to be more easily removed from the subterranean formation and/or increase the value of the hydrocarbon material. The chemical and physical changes may include in situ reactions that produce removable fluids, composition changes, solubility changes, density changes, phase changes, and/or viscosity changes of the hydrocarbon material in the formation.

Heaters may be placed in wellbores to heat a formation during an in situ process. There are many different types of heaters which may be used to heat the formation. Examples of in situ processes utilizing downhole heaters are illustrated in U.S. Pat. Nos. 2,634,961 to Ljungstrom; 2,732,195 to Ljungstrom; 2,780,450 to Ljungstrom; 2,789,805 to Ljungstrom; 2,923,535 to Ljungstrom; 4,886,118 to Van Meurs et al.; and 6,688,387 to Wellington et al., each of which is incorporated by reference as if fully set forth herein.

Mineral insulated (MI) cables (insulated conductors) for use in subsurface applications, such as heating hydrocarbon containing formations in some applications, are longer, may have larger outside diameters, and may operate at higher voltages and temperatures than what is typical in the MI cable industry. There are many potential problems during manufacture and/or assembly of long length insulated conductors.

For example, there are potential electrical and/or mechanical problems due to degradation over time of the electrical insulator used in the insulated conductor. There are also potential problems with electrical insulators to overcome during assembly of the insulated conductor heater. Problems such as core bulge or other mechanical defects may occur during assembly of the insulated conductor heater. Such occurrences may lead to electrical problems during use of the heater and may potentially render the heater inoperable for its intended purpose.

In addition, for subsurface applications, the joining of multiple MI cables may be needed to make MI cables with sufficient length to reach the depths and distances needed to heat the subsurface efficiently and to join segments with different functions, such as lead-in cables joined to heater sections. Such long heaters also require higher voltages to provide enough power to the farthest ends of the heaters.

Conventional MI cable splice designs are typically not suitable for voltages above 1000 volts, above 1500 volts, or above 2000 volts and may not operate for extended periods without failure at elevated temperatures, such as over 650° C. (about 1200° F.), over 700° C. (about 1290° F.), or over 800° C. (about 1470° F.). Such high voltage, high temperature applications typically require the compaction of the mineral insulant in the splice to be as close as possible to or above the level of compaction in the insulated conductor (MI cable) itself.

The relatively large outside diameter and long length of MI cables for some applications requires that the cables be spliced while oriented horizontally. There are splices for other applications of MI cables that have been fabricated horizontally. These techniques typically use a small hole through which the mineral insulation (such as magnesium oxide powder) is filled into the splice and compacted slightly through vibration and tamping. Such methods do not provide sufficient compaction of the mineral insulation or even allow any compaction of the mineral insulation, and are not suitable for making splices for use at the high voltages needed for these subsurface applications.

Thus, there is a need for splices of insulated conductors that are simple yet can operate at the high voltages and temperatures in the subsurface environment over long durations without failure. In addition, the splices may need higher bending and tensile strengths to inhibit failure of the splice under the weight loads and temperatures that the cables can be subjected to in the subsurface. Techniques and methods also may be utilized to reduce electric field intensities in the splices so that leakage currents in the splices are reduced and to increase the margin between the operating voltage and electrical breakdown. Reducing electric field intensities may help increase voltage and temperature operating ranges of the splices.

In addition, there may be problems with increased stress on the insulated conductors during assembly and/or installation into the subsurface of the insulated conductors. For example, winding and unwinding of the insulated conductors on spools used for transport and installation of the insulated conductors may lead to mechanical stress on the electrical insulators and/or other components in the insulated conductors. Thus, more reliable systems and methods are needed to reduce or eliminate potential problems during manufacture, assembly, and/or installation of insulated conductors.

SUMMARY

Embodiments described herein generally relate to systems, methods, and heaters for treating a subsurface formation. Embodiments described herein also generally relate to heaters that have novel components therein. Such heaters can be obtained by using the systems and methods described herein.

In certain embodiments, the invention provides one or more systems, methods, and/or heaters. In some embodiments, the systems, methods, and/or heaters are used for treating a subsurface formation.

In certain embodiments, a method for coupling a lead-in cable to an insulated conductor includes: exposing an end portion of a core of the insulated conductor by removing at least a portion of a jacket and an electrical insulator surrounding the end portion of the core; forming a recess in the electrical insulator at the end of the electrical insulator surrounding the end portion of the core; exposing an end portion of a conductor of the lead-in cable by removing at least a portion of a sheath and insulation surrounding the end portion of the conductor; coupling the end portion of the core to the end portion of the conductor; placing the end portion of the core and the end portion of the conductor in a body; coupling the body to the jacket of the insulated conductor such that the exposed portion of the core is enclosed within the body; coupling the body to the sheath of the lead-in cable such that the exposed portion of the conductor is enclosed within the body; and filling the body with electrically insulating material such that there are no voids or gaps inside the body.

In further embodiments, features from specific embodiments may be combined with features from other embodiments. For example, features from one embodiment may be combined with features from any of the other embodiments.

In further embodiments, treating a subsurface formation is performed using any of the methods, systems, power supplies, or heaters described herein.

In further embodiments, additional features may be added to the specific embodiments described herein.

BRIEF DESCRIPTION OF THE DRAWINGS

Features and advantages of the methods and apparatus of the present invention will be more fully appreciated by reference to the following detailed description of presently preferred but nonetheless illustrative embodiments in accordance with the present invention when taken in conjunction with the accompanying drawings.

FIG. 1 shows a schematic view of an embodiment of a portion of an in situ heat treatment system for treating a hydrocarbon containing formation.

FIG. 2 depicts an embodiment of an insulated conductor heat source.

FIG. 3 depicts an embodiment of an insulated conductor heat source.

FIG. 4 depicts an embodiment of an insulated conductor heat source.

FIG. 5 depicts a cross-sectional representation of an embodiment of a fitting used to couple a lead-in conductor and an insulated conductor.

FIG. 6 depicts an embodiment of a three leg lead-in cable with three lead-in conductors.

FIG. 7 depicts an embodiment of a prepared end portion of an insulated conductor.

FIG. 8 depicts an embodiment of a prepared end portion of a lead-in conductor.

While the invention is susceptible to various modifications and alternative forms, specific embodiments thereof are shown by way of example in the drawings and will herein be described in detail. The drawings may not be to scale. It should be understood that the drawings and detailed description thereto are not intended to limit the invention to the particular form disclosed, but to the contrary, the intention is to cover all modifications, equivalents and alternatives falling within the spirit and scope of the present invention as defined by the appended claims.

DETAILED DESCRIPTION

The following description generally relates to systems and methods for treating hydrocarbons in the formations. Such formations may be treated to yield hydrocarbon products, hydrogen, and other products.

“Alternating current (AC)” refers to a time-varying current that reverses direction substantially sinusoidally. AC produces skin effect electricity flow in a ferromagnetic conductor.

“Coupled” means either a direct connection or an indirect connection (for example, one or more intervening connections) between one or more objects or components. The phrase “directly connected” means a direct connection between objects or components such that the objects or components are connected directly to each other so that the objects or components operate in a “point of use” manner.

A “formation” includes one or more hydrocarbon containing layers, one or more non-hydrocarbon layers, an overburden, and/or an underburden. “Hydrocarbon layers” refer to layers in the formation that contain hydrocarbons. The hydrocarbon layers may contain non-hydrocarbon material and hydrocarbon material. The “overburden” and/or the “underburden” include one or more different types of impermeable materials. For example, the overburden and/or underburden may include rock, shale, mudstone, or wet/tight carbonate. In some embodiments of in situ heat treatment processes, the overburden and/or the underburden may include a hydrocarbon containing layer or hydrocarbon containing layers that are relatively impermeable and are not subjected to temperatures during in situ heat treatment processing that result in significant characteristic changes of the hydrocarbon containing layers of the overburden and/or the underburden. For example, the underburden may contain shale or mudstone, but the underburden is not allowed to heat to pyrolysis temperatures during the in situ heat treatment process. In some cases, the overburden and/or the underburden may be somewhat permeable.

“Formation fluids” refer to fluids present in a formation and may include pyrolyzation fluid, synthesis gas, mobilized hydrocarbons, and water (steam). Formation fluids may include hydrocarbon fluids as well as non-hydrocarbon fluids. The term “mobilized fluid” refers to fluids in a hydrocarbon containing formation that are able to flow as a result of thermal treatment of the formation. “Produced fluids” refer to fluids removed from the formation.

A “heat source” is any system for providing heat to at least a portion of a formation substantially by conductive and/or radiative heat transfer. For example, a heat source may include electrically conducting materials and/or electric heaters such as an insulated conductor, an elongated member, and/or a conductor disposed in a conduit. A heat source may also include systems that generate heat by burning a fuel external to or in a formation. The systems may be surface burners, downhole gas burners, flameless distributed combustors, and natural distributed combustors. In some embodiments, heat provided to or generated in one or more heat sources may be supplied by other sources of energy. The other sources of energy may directly heat a formation, or the energy may be applied to a transfer medium that directly or indirectly heats the formation. It is to be understood that one or more heat sources that are applying heat to a formation may use different sources of energy. Thus, for example, for a given formation some heat sources may supply heat from electrically conducting materials, electric resistance heaters, some heat sources may provide heat from combustion, and some heat sources may provide heat from one or more other energy sources (for example, chemical reactions, solar energy, wind energy, biomass, or other sources of renewable energy). A chemical reaction may include an exothermic reaction (for example, an oxidation reaction). A heat source may also include an electrically conducting material and/or a heater that provides heat to a zone proximate and/or surrounding a heating location such as a heater well.

A “heater” is any system or heat source for generating heat in a well or a near wellbore region. Heaters may be, but are not limited to, electric heaters, burners, combustors that react with material in or produced from a formation, and/or combinations thereof.

“Hydrocarbons” are generally defined as molecules formed primarily by carbon and hydrogen atoms. Hydrocarbons may also include other elements such as, but not limited to, halogens, metallic elements, nitrogen, oxygen, and/or sulfur. Hydrocarbons may be, but are not limited to, kerogen, bitumen, pyrobitumen, oils, natural mineral waxes, and asphaltites. Hydrocarbons may be located in or adjacent to mineral matrices in the earth. Matrices may include, but are not limited to, sedimentary rock, sands, silicilytes, carbonates, diatomites, and other porous media. “Hydrocarbon fluids” are fluids that include hydrocarbons. Hydrocarbon fluids may include, entrain, or be entrained in non-hydrocarbon fluids such as hydrogen, nitrogen, carbon monoxide, carbon dioxide, hydrogen sulfide, water, and ammonia.

An “in situ conversion process” refers to a process of heating a hydrocarbon containing formation from heat sources to raise the temperature of at least a portion of the formation above a pyrolysis temperature so that pyrolyzation fluid is produced in the formation.

An “in situ heat treatment process” refers to a process of heating a hydrocarbon containing formation with heat sources to raise the temperature of at least a portion of the formation above a temperature that results in mobilized fluid, visbreaking, and/or pyrolysis of hydrocarbon containing material so that mobilized fluids, visbroken fluids, and/or pyrolyzation fluids are produced in the formation.

“Insulated conductor” refers to any elongated material that is able to conduct electricity and that is covered, in whole or in part, by an electrically insulating material.

“Nitride” refers to a compound of nitrogen and one or more other elements of the Periodic Table. Nitrides include, but are not limited to, silicon nitride, boron nitride, or alumina nitride.

“Perforations” include openings, slits, apertures, or holes in a wall of a conduit, tubular, pipe or other flow pathway that allow flow into or out of the conduit, tubular, pipe or other flow pathway.

“Pyrolysis” is the breaking of chemical bonds due to the application of heat. For example, pyrolysis may include transforming a compound into one or more other substances by heat alone. Heat may be transferred to a section of the formation to cause pyrolysis.

“Pyrolyzation fluids” or “pyrolysis products” refers to fluid produced substantially during pyrolysis of hydrocarbons. Fluid produced by pyrolysis reactions may mix with other fluids in a formation. The mixture would be considered pyrolyzation fluid or pyrolyzation product. As used herein, “pyrolysis zone” refers to a volume of a formation (for example, a relatively permeable formation such as a tar sands formation) that is reacted or reacting to form a pyrolyzation fluid.

“Thickness” of a layer refers to the thickness of a cross section of the layer, wherein the cross section is normal to a face of the layer.

The term “wellbore” refers to a hole in a formation made by drilling or insertion of a conduit into the formation. A wellbore may have a substantially circular cross section, or another cross-sectional shape. As used herein, the terms “well” and “opening,” when referring to an opening in the formation may be used interchangeably with the term “wellbore.”

A formation may be treated in various ways to produce many different products. Different stages or processes may be used to treat the formation during an in situ heat treatment process. In some embodiments, one or more sections of the formation are solution mined to remove soluble minerals from the sections. Solution mining minerals may be performed before, during, and/or after the in situ heat treatment process. In some embodiments, the average temperature of one or more sections being solution mined may be maintained below about 120° C.

In some embodiments, one or more sections of the formation are heated to remove water from the sections and/or to remove methane and other volatile hydrocarbons from the sections. In some embodiments, the average temperature may be raised from ambient temperature to temperatures below about 220° C. during removal of water and volatile hydrocarbons.

In some embodiments, one or more sections of the formation are heated to temperatures that allow for movement and/or visbreaking of hydrocarbons in the formation. In some embodiments, the average temperature of one or more sections of the formation are raised to mobilization temperatures of hydrocarbons in the sections (for example, to temperatures ranging from 100° C. to 250° C., from 120° C. to 240° C., or from 150° C. to 230° C.).

In some embodiments, one or more sections are heated to temperatures that allow for pyrolysis reactions in the formation. In some embodiments, the average temperature of one or more sections of the formation may be raised to pyrolysis temperatures of hydrocarbons in the sections (for example, temperatures ranging from 230° C. to 900° C., from 240° C. to 400° C. or from 250° C. to 350° C.).

Heating the hydrocarbon containing formation with a plurality of heat sources may establish thermal gradients around the heat sources that raise the temperature of hydrocarbons in the formation to desired temperatures at desired heating rates. The rate of temperature increase through the mobilization temperature range and/or the pyrolysis temperature range for desired products may affect the quality and quantity of the formation fluids produced from the hydrocarbon containing formation. Slowly raising the temperature of the formation through the mobilization temperature range and/or pyrolysis temperature range may allow for the production of high quality, high API gravity hydrocarbons from the formation. Slowly raising the temperature of the formation through the mobilization temperature range and/or pyrolysis temperature range may allow for the removal of a large amount of the hydrocarbons present in the formation as hydrocarbon product.

In some in situ heat treatment embodiments, a portion of the formation is heated to a desired temperature instead of slowly heating the temperature through a temperature range. In some embodiments, the desired temperature is 300° C., 325° C., or 350° C. Other temperatures may be selected as the desired temperature.

Superposition of heat from heat sources allows the desired temperature to be relatively quickly and efficiently established in the formation. Energy input into the formation from the heat sources may be adjusted to maintain the temperature in the formation substantially at a desired temperature.

Mobilization and/or pyrolysis products may be produced from the formation through production wells. In some embodiments, the average temperature of one or more sections is raised to mobilization temperatures and hydrocarbons are produced from the production wells. The average temperature of one or more of the sections may be raised to pyrolysis temperatures after production due to mobilization decreases below a selected value. In some embodiments, the average temperature of one or more sections may be raised to pyrolysis temperatures without significant production before reaching pyrolysis temperatures. Formation fluids including pyrolysis products may be produced through the production wells.

In some embodiments, the average temperature of one or more sections may be raised to temperatures sufficient to allow synthesis gas production after mobilization and/or pyrolysis. In some embodiments, hydrocarbons may be raised to temperatures sufficient to allow synthesis gas production without significant production before reaching the temperatures sufficient to allow synthesis gas production. For example, synthesis gas may be produced in a temperature range from about 400° C. to about 1200° C., about 500° C. to about 1100° C., or about 550° C. to about 1000° C. A synthesis gas generating fluid (for example, steam and/or water) may be introduced into the sections to generate synthesis gas. Synthesis gas may be produced from production wells.

Solution mining, removal of volatile hydrocarbons and water, mobilizing hydrocarbons, pyrolyzing hydrocarbons, generating synthesis gas, and/or other processes may be performed during the in situ heat treatment process. In some embodiments, some processes may be performed after the in situ heat treatment process. Such processes may include, but are not limited to, recovering heat from treated sections, storing fluids (for example, water and/or hydrocarbons) in previously treated sections, and/or sequestering carbon dioxide in previously treated sections.

FIG. 1 depicts a schematic view of an embodiment of a portion of the in situ heat treatment system for treating the hydrocarbon containing formation. The in situ heat treatment system may include barrier wells 200. Barrier wells are used to form a barrier around a treatment area. The barrier inhibits fluid flow into and/or out of the treatment area. Barrier wells include, but are not limited to, dewatering wells, vacuum wells, capture wells, injection wells, grout wells, freeze wells, or combinations thereof. In some embodiments, barrier wells 200 are dewatering wells. Dewatering wells may remove liquid water and/or inhibit liquid water from entering a portion of the formation to be heated, or to the formation being heated. In the embodiment depicted in FIG. 1, the barrier wells 200 are shown extending only along one side of heat sources 202, but the barrier wells typically encircle all heat sources 202 used, or to be used, to heat a treatment area of the formation.

Heat sources 202 are placed in at least a portion of the formation. Heat sources 202 may include heaters such as insulated conductors, conductor-in-conduit heaters, surface burners, flameless distributed combustors, and/or natural distributed combustors. Heat sources 202 may also include other types of heaters. Heat sources 202 provide heat to at least a portion of the formation to heat hydrocarbons in the formation. Energy may be supplied to heat sources 202 through supply lines 204. Supply lines 204 may be structurally different depending on the type of heat source or heat sources used to heat the formation. Supply lines 204 for heat sources may transmit electricity for electric heaters, may transport fuel for combustors, or may transport heat exchange fluid that is circulated in the formation. In some embodiments, electricity for an in situ heat treatment process may be provided by a nuclear power plant or nuclear power plants. The use of nuclear power may allow for reduction or elimination of carbon dioxide emissions from the in situ heat treatment process.

When the formation is heated, the heat input into the formation may cause expansion of the formation and geomechanical motion. The heat sources may be turned on before, at the same time, or during a dewatering process. Computer simulations may model formation response to heating. The computer simulations may be used to develop a pattern and time sequence for activating heat sources in the formation so that geomechanical motion of the formation does not adversely affect the functionality of heat sources, production wells, and other equipment in the formation.

Heating the formation may cause an increase in permeability and/or porosity of the formation. Increases in permeability and/or porosity may result from a reduction of mass in the formation due to vaporization and removal of water, removal of hydrocarbons, and/or creation of fractures. Fluid may flow more easily in the heated portion of the formation because of the increased permeability and/or porosity of the formation. Fluid in the heated portion of the formation may move a considerable distance through the formation because of the increased permeability and/or porosity. The considerable distance may be over 1000 m depending on various factors, such as permeability of the formation, properties of the fluid, temperature of the formation, and pressure gradient allowing movement of the fluid. The ability of fluid to travel considerable distance in the formation allows production wells 206 to be spaced relatively far apart in the formation.

Production wells 206 are used to remove formation fluid from the formation. In some embodiments, production well 206 includes a heat source. The heat source in the production well may heat one or more portions of the formation at or near the production well. In some in situ heat treatment process embodiments, the amount of heat supplied to the formation from the production well per meter of the production well is less than the amount of heat applied to the formation from a heat source that heats the formation per meter of the heat source. Heat applied to the formation from the production well may increase formation permeability adjacent to the production well by vaporizing and removing liquid phase fluid adjacent to the production well and/or by increasing the permeability of the formation adjacent to the production well by formation of macro and/or micro fractures.

More than one heat source may be positioned in the production well. A heat source in a lower portion of the production well may be turned off when superposition of heat from adjacent heat sources heats the formation sufficiently to counteract benefits provided by heating the formation with the production well. In some embodiments, the heat source in an upper portion of the production well may remain on after the heat source in the lower portion of the production well is deactivated. The heat source in the upper portion of the well may inhibit condensation and reflux of formation fluid.

In some embodiments, the heat source in production well 206 allows for vapor phase removal of formation fluids from the formation. Providing heating at or through the production well may: (1) inhibit condensation and/or refluxing of production fluid when such production fluid is moving in the production well proximate the overburden, (2) increase heat input into the formation, (3) increase production rate from the production well as compared to a production well without a heat source, (4) inhibit condensation of high carbon number compounds (C6 hydrocarbons and above) in the production well, and/or (5) increase formation permeability at or proximate the production well.

Subsurface pressure in the formation may correspond to the fluid pressure generated in the formation. As temperatures in the heated portion of the formation increase, the pressure in the heated portion may increase as a result of thermal expansion of in situ fluids, increased fluid generation and vaporization of water. Controlling rate of fluid removal from the formation may allow for control of pressure in the formation. Pressure in the formation may be determined at a number of different locations, such as near or at production wells, near or at heat sources, or at monitor wells.

In some hydrocarbon containing formations, production of hydrocarbons from the formation is inhibited until at least some hydrocarbons in the formation have been mobilized and/or pyrolyzed. Formation fluid may be produced from the formation when the formation fluid is of a selected quality. In some embodiments, the selected quality includes an API gravity of at least about 20°, 30°, or 40°. Inhibiting production until at least some hydrocarbons are mobilized and/or pyrolyzed may increase conversion of heavy hydrocarbons to light hydrocarbons. Inhibiting initial production may minimize the production of heavy hydrocarbons from the formation. Production of substantial amounts of heavy hydrocarbons may require expensive equipment and/or reduce the life of production equipment.

In some hydrocarbon containing formations, hydrocarbons in the formation may be heated to mobilization and/or pyrolysis temperatures before substantial permeability has been generated in the heated portion of the formation. An initial lack of permeability may inhibit the transport of generated fluids to production wells 206. During initial heating, fluid pressure in the formation may increase proximate heat sources 202. The increased fluid pressure may be released, monitored, altered, and/or controlled through one or more heat sources 202. For example, selected heat sources 202 or separate pressure relief wells may include pressure relief valves that allow for removal of some fluid from the formation.

In some embodiments, pressure generated by expansion of mobilized fluids, pyrolysis fluids or other fluids generated in the formation may be allowed to increase although an open path to production wells 206 or any other pressure sink may not yet exist in the formation. The fluid pressure may be allowed to increase towards a lithostatic pressure. Fractures in the hydrocarbon containing formation may form when the fluid approaches the lithostatic pressure. For example, fractures may form from heat sources 202 to production wells 206 in the heated portion of the formation. The generation of fractures in the heated portion may relieve some of the pressure in the portion. Pressure in the formation may have to be maintained below a selected pressure to inhibit unwanted production, fracturing of the overburden or underburden, and/or coking of hydrocarbons in the formation.

After mobilization and/or pyrolysis temperatures are reached and production from the formation is allowed, pressure in the formation may be varied to alter and/or control a composition of formation fluid produced, to control a percentage of condensable fluid as compared to non-condensable fluid in the formation fluid, and/or to control an API gravity of formation fluid being produced. For example, decreasing pressure may result in production of a larger condensable fluid component. The condensable fluid component may contain a larger percentage of olefins.

In some in situ heat treatment process embodiments, pressure in the formation may be maintained high enough to promote production of formation fluid with an API gravity of greater than 20°. Maintaining increased pressure in the formation may inhibit formation subsidence during in situ heat treatment. Maintaining increased pressure may reduce or eliminate the need to compress formation fluids at the surface to transport the fluids in collection conduits to treatment facilities.

Maintaining increased pressure in a heated portion of the formation may surprisingly allow for production of large quantities of hydrocarbons of increased quality and of relatively low molecular weight. Pressure may be maintained so that formation fluid produced has a minimal amount of compounds above a selected carbon number. The selected carbon number may be at most 25, at most 20, at most 12, or at most 8. Some high carbon number compounds may be entrained in vapor in the formation and may be removed from the formation with the vapor. Maintaining increased pressure in the formation may inhibit entrainment of high carbon number compounds and/or multi-ring hydrocarbon compounds in the vapor. High carbon number compounds and/or multi-ring hydrocarbon compounds may remain in a liquid phase in the formation for significant time periods. The significant time periods may provide sufficient time for the compounds to pyrolyze to form lower carbon number compounds.

Generation of relatively low molecular weight hydrocarbons is believed to be due, in part, to autogenous generation and reaction of hydrogen in a portion of the hydrocarbon containing formation. For example, maintaining an increased pressure may force hydrogen generated during pyrolysis into the liquid phase within the formation. Heating the portion to a temperature in a pyrolysis temperature range may pyrolyze hydrocarbons in the formation to generate liquid phase pyrolyzation fluids. The generated liquid phase pyrolyzation fluids components may include double bonds and/or radicals. Hydrogen (H₂) in the liquid phase may reduce double bonds of the generated pyrolyzation fluids, thereby reducing a potential for polymerization or formation of long chain compounds from the generated pyrolyzation fluids. In addition, H₂may also neutralize radicals in the generated pyrolyzation fluids. H₂in the liquid phase may inhibit the generated pyrolyzation fluids from reacting with each other and/or with other compounds in the formation.

Formation fluid produced from production wells 206 may be transported through collection piping 208 to treatment facilities 210. Formation fluids may also be produced from heat sources 202. For example, fluid may be produced from heat sources 202 to control pressure in the formation adjacent to the heat sources. Fluid produced from heat sources 202 may be transported through tubing or piping to collection piping 208 or the produced fluid may be transported through tubing or piping directly to treatment facilities 210. Treatment facilities 210 may include separation units, reaction units, upgrading units, fuel cells, turbines, storage vessels, and/or other systems and units for processing produced formation fluids. The treatment facilities may form transportation fuel from at least a portion of the hydrocarbons produced from the formation. In some embodiments, the transportation fuel may be jet fuel, such as JP-8.

An insulated conductor may be used as an electric heater element of a heater or a heat source. The insulated conductor may include an inner electrical conductor (core) surrounded by an electrical insulator and an outer electrical conductor (jacket). The electrical insulator may include mineral insulation (for example, magnesium oxide) or other electrical insulation.

In certain embodiments, the insulated conductor is placed in an opening in a hydrocarbon containing formation. In some embodiments, the insulated conductor is placed in an uncased opening in the hydrocarbon containing formation. Placing the insulated conductor in an uncased opening in the hydrocarbon containing formation may allow heat transfer from the insulated conductor to the formation by radiation as well as conduction. Using an uncased opening may facilitate retrieval of the insulated conductor from the well, if necessary.

In some embodiments, an insulated conductor is placed within a casing in the formation; may be cemented within the formation; or may be packed in an opening with sand, gravel, or other fill material. The insulated conductor may be supported on a support member positioned within the opening. The support member may be a cable, rod, or a conduit (for example, a pipe). The support member may be made of a metal, ceramic, inorganic material, or combinations thereof. Because portions of a support member may be exposed to formation fluids and heat during use, the support member may be chemically resistant and/or thermally resistant.

Ties, spot welds, and/or other types of connectors may be used to couple the insulated conductor to the support member at various locations along a length of the insulated conductor. The support member may be attached to a wellhead at an upper surface of the formation. In some embodiments, the insulated conductor has sufficient structural strength such that a support member is not needed. The insulated conductor may, in many instances, have at least some flexibility to inhibit thermal expansion damage when undergoing temperature changes.

In certain embodiments, insulated conductors are placed in wellbores without support members and/or centralizers. An insulated conductor without support members and/or centralizers may have a suitable combination of temperature and corrosion resistance, creep strength, length, thickness (diameter), and metallurgy that will inhibit failure of the insulated conductor during use.

FIG. 2 depicts a perspective view of an end portion of an embodiment of insulated conductor 212. Insulated conductor 212 may have any desired cross-sectional shape such as, but not limited to, round (depicted in FIG. 2), triangular, ellipsoidal, rectangular, hexagonal, or irregular. In certain embodiments, insulated conductor 212 includes core 214, electrical insulator 216, and jacket 218. Core 214 may resistively heat when an electrical current passes through the core. Alternating or time-varying current and/or direct current may be used to provide power to core 214 such that the core resistively heats.

In some embodiments, electrical insulator 216 inhibits current leakage and arcing to jacket 218. Electrical insulator 216 may thermally conduct heat generated in core 214 to jacket 218. Jacket 218 may radiate or conduct heat to the formation. In certain embodiments, insulated conductor 212 is 1000 m or more in length. Longer or shorter insulated conductors may also be used to meet specific application needs. The dimensions of core 214, electrical insulator 216, and jacket 218 of insulated conductor 212 may be selected such that the insulated conductor has enough strength to be self supporting even at upper working temperature limits. Such insulated conductors may be suspended from wellheads or supports positioned near an interface between an overburden and a hydrocarbon containing formation without the need for support members extending into the hydrocarbon containing formation along with the insulated conductors.

Insulated conductor 212 may be designed to operate at power levels of up to about 1650 watts/meter or higher. In certain embodiments, insulated conductor 212 operates at a power level between about 500 watts/meter and about 1150 watts/meter when heating a formation. Insulated conductor 212 may be designed so that a maximum voltage level at a typical operating temperature does not cause substantial thermal and/or electrical breakdown of electrical insulator 216. Insulated conductor 212 may be designed such that jacket 218 does not exceed a temperature that will result in a significant reduction in corrosion resistance properties of the jacket material. In certain embodiments, insulated conductor 212 may be designed to reach temperatures within a range between about 650° C. and about 900° C. Insulated conductors having other operating ranges may be formed to meet specific operational requirements.

FIG. 2 depicts insulated conductor 212 having a single core 214. In some embodiments, insulated conductor 212 has two or more cores 214. For example, a single insulated conductor may have three cores. Core 214 may be made of metal or another electrically conductive material. The material used to form core 214 may include, but not be limited to, nichrome, copper, nickel, carbon steel, stainless steel, and combinations thereof. In certain embodiments, core 214 is chosen to have a diameter and a resistivity at operating temperatures such that its resistance, as derived from Ohm's law, makes it electrically and structurally stable for the chosen power dissipation per meter, the length of the heater, and/or the maximum voltage allowed for the core material.

In some embodiments, core 214 is made of different materials along a length of insulated conductor 212. For example, a first section of core 214 may be made of a material that has a significantly lower resistance than a second section of the core. The first section may be placed adjacent to a formation layer that does not need to be heated to as high a temperature as a second formation layer that is adjacent to the second section. The resistivity of various sections of core 214 may be adjusted by having a variable diameter and/or by having core sections made of different materials.

Electrical insulator 216 may be made of a variety of materials. Commonly used powders may include, but are not limited to, MgO, Al₂O₃, Zirconia, BeO, different chemical variations of Spinels, and combinations thereof. MgO may provide good thermal conductivity and electrical insulation properties. The desired electrical insulation properties include low leakage current and high dielectric strength. A low leakage current decreases the possibility of thermal breakdown and the high dielectric strength decreases the possibility of arcing across the insulator. Thermal breakdown can occur if the leakage current causes a progressive rise in the temperature of the insulator leading also to arcing across the insulator.

Jacket 218 may be an outer metallic layer or electrically conductive layer. Jacket 218 may be in contact with hot formation fluids. Jacket 218 may be made of material having a high resistance to corrosion at elevated temperatures. Alloys that may be used in a desired operating temperature range of jacket 218 include, but are not limited to, 304 stainless steel, 310 stainless steel, Incoloy® 800, and Inconel® 600 (Inco Alloys International, Huntington, West Va., U.S.A.). The thickness of jacket 218 may have to be sufficient to last for three to ten years in a hot and corrosive environment. A thickness of jacket 218 may generally vary between about 1 mm and about 2.5 mm. For example, a 1.3 mm thick, 310 stainless steel outer layer may be used as jacket 218 to provide good chemical resistance to sulfidation corrosion in a heated zone of a formation for a period of over 3 years. Larger or smaller jacket thicknesses may be used to meet specific application requirements.

One or more insulated conductors may be placed within an opening in a formation to form a heat source or heat sources. Electrical current may be passed through each insulated conductor in the opening to heat the formation. Alternately, electrical current may be passed through selected insulated conductors in an opening. The unused conductors may be used as backup heaters. Insulated conductors may be electrically coupled to a power source in any convenient manner. Each end of an insulated conductor may be coupled to lead-in cables that pass through a wellhead. Such a configuration typically has a 180° bend (a “hairpin” bend) or turn located near a bottom of the heat source. An insulated conductor that includes a 180° bend or turn may not require a bottom termination, but the 180° bend or turn may be an electrical and/or structural weakness in the heater. Insulated conductors may be electrically coupled together in series, in parallel, or in series and parallel combinations. In some embodiments of heat sources, electrical current may pass into the conductor of an insulated conductor and may be returned through the jacket of the insulated conductor by connecting core 214 to jacket 218 (shown in FIG. 2) at the bottom of the heat source.

In some embodiments, three insulated conductors 212 are electrically coupled in a 3-phase wye configuration to a power supply. FIG. 3 depicts an embodiment of three insulated conductors in an opening in a subsurface formation coupled in a wye configuration. FIG. 4 depicts an embodiment of three insulated conductors 212 that are removable from opening 220 in the formation. No bottom connection may be required for three insulated conductors in a wye configuration. Alternately, all three insulated conductors of the wye configuration may be connected together near the bottom of the opening. The connection may be made directly at ends of heating sections of the insulated conductors or at ends of cold pins (less resistive sections) coupled to the heating sections at the bottom of the insulated conductors. The bottom connections may be made with insulator filled and sealed canisters or with epoxy filled canisters. The insulator may be the same composition as the insulator used as the electrical insulation.

Three insulated conductors 212 depicted in FIGS. 3 and 4 may be coupled to support member 222 using centralizers 224. Alternatively, insulated conductors 212 may be strapped directly to support member 222 using metal straps. Centralizers 224 may maintain a location and/or inhibit movement of insulated conductors 212 on support member 222. Centralizers 224 may be made of metal, ceramic, or combinations thereof. The metal may be stainless steel or any other type of metal able to withstand a corrosive and high temperature environment. In some embodiments, centralizers 224 are bowed metal strips welded to the support member at distances less than about 6 m. A ceramic used in centralizer 224 may be, but is not limited to, Al₂O₃, MgO, or another electrical insulator. Centralizers 224 may maintain a location of insulated conductors 212 on support member 222 such that movement of insulated conductors is inhibited at operating temperatures of the insulated conductors. Insulated conductors 212 may also be somewhat flexible to withstand expansion of support member 222 during heating.

Support member 222, insulated conductor 212, and centralizers 224 may be placed in opening 220 in hydrocarbon layer 226. Insulated conductors 212 may be coupled to bottom conductor junction 228 using cold pin 230. Bottom conductor junction 228 may electrically couple each insulated conductor 212 to each other. Bottom conductor junction 228 may include materials that are electrically conducting and do not melt at temperatures found in opening 220. Cold pin 230 may be an insulated conductor having lower electrical resistance than insulated conductor 212.

Lead-in conductor 232 may be coupled to wellhead 234 to provide electrical power to insulated conductor 212. Lead-in conductor 232 may be made of a relatively low electrical resistance conductor such that relatively little heat is generated from electrical current passing through the lead-in conductor. In some embodiments, the lead-in conductor is a rubber or polymer insulated stranded copper wire. In some embodiments, the lead-in conductor is a mineral insulated conductor with a copper core. Lead-in conductor 232 may couple to wellhead 234 at surface 236 through a sealing flange located between overburden 238 and surface 236. The sealing flange may inhibit fluid from escaping from opening 220 to surface 236.

In certain embodiments, lead-in conductor 232 is coupled to insulated conductor 212 using transition conductor 240. Transition conductor 240 may be a less resistive portion of insulated conductor 212. Transition conductor 240 may be referred to as “cold pin” of insulated conductor 212. Transition conductor 240 may be designed to dissipate about one-tenth to about one-fifth of the power per unit length as is dissipated in a unit length of the primary heating section of insulated conductor 212. Transition conductor 240 may typically be between about 1.5 m and about 15 m, although shorter or longer lengths may be used to accommodate specific application needs. In an embodiment, the conductor of transition conductor 240 is copper. The electrical insulator of transition conductor 240 may be the same type of electrical insulator used in the primary heating section. A jacket of transition conductor 240 may be made of corrosion resistant material.

In certain embodiments, transition conductor 240 is coupled to lead-in conductor 232 by a splice or other coupling joint. Splices may also be used to couple transition conductor 240 to insulated conductor 212. Splices may have to withstand a temperature equal to half of a target zone operating temperature. Density of electrical insulation in the splice should in many instances be high enough to withstand the required temperature and the operating voltage.

In some embodiments, as shown in FIG. 3, packing material 242 is placed between overburden casing 244 and opening 220. In some embodiments, reinforcing material 246 may secure overburden casing 244 to overburden 238. Packing material 242 may inhibit fluid from flowing from opening 220 to surface 236. Reinforcing material 246 may include, for example, Class G or Class H Portland cement mixed with silica flour for improved high temperature performance, slag or silica flour, and/or a mixture thereof. In some embodiments, reinforcing material 246 extends radially a width of from about 5 cm to about 25 cm.

As shown in FIGS. 3 and 4, support member 222 and lead-in conductor 232 may be coupled to wellhead 234 at surface 236 of the formation. Surface conductor 248 may enclose reinforcing material 246 and couple to wellhead 234. Embodiments of surface conductors may extend to depths of approximately 3 m to approximately 515 m into an opening in the formation. Alternatively, the surface conductor may extend to a depth of approximately 9 m into the formation. Electrical current may be supplied from a power source to insulated conductor 212 to generate heat due to the electrical resistance of the insulated conductor. Heat generated from three insulated conductors 212 may transfer within opening 220 to heat at least a portion of hydrocarbon layer 226.

Heat generated by insulated conductors 212 may heat at least a portion of a hydrocarbon containing formation. In some embodiments, heat is transferred to the formation substantially by radiation of the generated heat to the formation. Some heat may be transferred by conduction or convection of heat due to gases present in the opening. The opening may be an uncased opening, as shown in FIGS. 3 and 4. An uncased opening eliminates cost associated with thermally cementing the heater to the formation, costs associated with a casing, and/or costs of packing a heater within an opening. In addition, heat transfer by radiation is typically more efficient than by conduction, so the heaters may be operated at lower temperatures in an open wellbore. Conductive heat transfer during initial operation of a heat source may be enhanced by the addition of a gas in the opening. The gas may be maintained at a pressure up to about 27 bars absolute. The gas may include, but is not limited to, carbon dioxide and/or helium. An insulated conductor heater in an open wellbore may advantageously be free to expand or contract to accommodate thermal expansion and contraction. An insulated conductor heater may advantageously be removable or redeployable from an open wellbore.

In certain embodiments, an insulated conductor heater assembly is installed or removed using a spooling assembly. More than one spooling assembly may be used to install both the insulated conductor and a support member simultaneously. Alternatively, the support member may be installed using a coiled tubing unit. The heaters may be un-spooled and connected to the support as the support is inserted into the well. The electric heater and the support member may be un-spooled from the spooling assemblies. Spacers may be coupled to the support member and the heater along a length of the support member. Additional spooling assemblies may be used for additional electric heater elements.

Temperature limited heaters may be in configurations and/or may include materials that provide automatic temperature limiting properties for the heater at certain temperatures. Examples of temperature limited heaters may be found in U.S. Patent Nos. 6,688,387 to Wellington et al.; 6,991,036 to Sumnu-Dindoruk et al.; 6,698,515 to Karanikas et al.; 6,880,633 to Wellington et al.; 6,782,947 to de Rouffignac et al.; 6,991,045 to Vinegar et al.; 7,073,578 to Vinegar et al.; 7,121,342 to Vinegar et al.; 7,320,364 to Fairbanks; 7,527,094 to McKinzie et al.; 7,584,789 to Mo et al.; 7,533,719 to Hinson et al.; 7,562,707 to Miller; 7,841,408 to Vinegar et al.; 8,636,323 to Prince-Wright et al.; 8,281,861 to Nguyen et al.; and U.S. Patent Application Publication No. 2009-0189617 to Burns et al., each of which is incorporated by reference as if fully set forth herein. Temperature limited heaters are dimensioned to operate with AC frequencies (for example, 60 Hz AC) or with modulated DC current.

In certain embodiments, ferromagnetic materials are used in temperature limited heaters. Ferromagnetic material may self-limit temperature at or near the Curie temperature of the material and/or the phase transformation temperature range to provide a reduced amount of heat when a time-varying current is applied to the material. In certain embodiments, the ferromagnetic material self-limits temperature of the temperature limited heater at a selected temperature that is approximately the Curie temperature and/or in the phase transformation temperature range. In certain embodiments, the selected temperature is within about 35° C., within about 25° C., within about 20° C., or within about 10° C. of the Curie temperature and/or the phase transformation temperature range. In certain embodiments, ferromagnetic materials are coupled with other materials (for example, highly conductive materials, high strength materials, corrosion resistant materials, or combinations thereof) to provide various electrical and/or mechanical properties. Some parts of the temperature limited heater may have a lower resistance (caused by different geometries and/or by using different ferromagnetic and/or non-ferromagnetic materials) than other parts of the temperature limited heater. Having parts of the temperature limited heater with various materials and/or dimensions allows for tailoring the desired heat output from each part of the heater.

Temperature limited heaters may be more reliable than other heaters. Temperature limited heaters may be less apt to break down or fail due to hot spots in the formation. In some embodiments, temperature limited heaters allow for substantially uniform heating of the formation. In some embodiments, temperature limited heaters are able to heat the formation more efficiently by operating at a higher average heat output along the entire length of the heater. The temperature limited heater operates at the higher average heat output along the entire length of the heater because power to the heater does not have to be reduced to the entire heater, as is the case with typical constant wattage heaters, if a temperature along any point of the heater exceeds, or is about to exceed, a maximum operating temperature of the heater. Heat output from portions of a temperature limited heater approaching a Curie temperature and/or the phase transformation temperature range of the heater automatically reduces without controlled adjustment of the time-varying current applied to the heater. The heat output automatically reduces due to changes in electrical properties (for example, electrical resistance) of portions of the temperature limited heater. Thus, more power is supplied by the temperature limited heater during a greater portion of a heating process.

In certain embodiments, the system including temperature limited heaters initially provides a first heat output and then provides a reduced (second heat output) heat output, near, at, or above the Curie temperature and/or the phase transformation temperature range of an electrically resistive portion of the heater when the temperature limited heater is energized by a time-varying current. The first heat output is the heat output at temperatures below which the temperature limited heater begins to self-limit. In some embodiments, the first heat output is the heat output at a temperature about 50° C., about 75° C., about 100° C., or about 125° C. below the Curie temperature and/or the phase transformation temperature range of the ferromagnetic material in the temperature limited heater.

The temperature limited heater may be energized by time-varying current (alternating current or modulated direct current) supplied at the wellhead. The wellhead may include a power source and other components (for example, modulation components, transformers, and/or capacitors) used in supplying power to the temperature limited heater. The temperature limited heater may be one of many heaters used to heat a portion of the formation.

In certain embodiments, the temperature limited heater includes a conductor that operates as a skin effect or proximity effect heater when time-varying current is applied to the conductor. The skin effect limits the depth of current penetration into the interior of the conductor. For ferromagnetic materials, the skin effect is dominated by the magnetic permeability of the conductor. The relative magnetic permeability of ferromagnetic materials is typically between 10 and 1000 (for example, the relative magnetic permeability of ferromagnetic materials is typically at least 10 and may be at least 50, 100, 500, 1000 or greater). As the temperature of the ferromagnetic material is raised above the Curie temperature, or the phase transformation temperature range, and/or as the applied electrical current is increased, the magnetic permeability of the ferromagnetic material decreases substantially and the skin depth expands rapidly (for example, the skin depth expands as the inverse square root of the magnetic permeability). The reduction in magnetic permeability results in a decrease in the AC or modulated DC resistance of the conductor near, at, or above the Curie temperature, the phase transformation temperature range, and/or as the applied electrical current is increased. When the temperature limited heater is powered by a substantially constant current source, portions of the heater that approach, reach, or are above the Curie temperature and/or the phase transformation temperature range may have reduced heat dissipation. Sections of the temperature limited heater that are not at or near the Curie temperature and/or the phase transformation temperature range may be dominated by skin effect heating that allows the heater to have high heat dissipation due to a higher resistive load.

An advantage of using the temperature limited heater to heat hydrocarbons in the formation is that the conductor is chosen to have a Curie temperature and/or a phase transformation temperature range in a desired range of temperature operation. Operation within the desired operating temperature range allows substantial heat injection into the formation while maintaining the temperature of the temperature limited heater, and other equipment, below design limit temperatures. Design limit temperatures are temperatures at which properties such as corrosion, creep, and/or deformation are adversely affected. The temperature limiting properties of the temperature limited heater inhibit overheating or burnout of the heater adjacent to low thermal conductivity “hot spots” in the formation. In some embodiments, the temperature limited heater is able to lower or control heat output and/or withstand heat at temperatures above 25° C., 37° C., 100° C., 250° C., 500° C., 700° C., 800° C., 900° C., or higher up to 1131° C., depending on the materials used in the heater.

The temperature limited heater allows for more heat injection into the formation than constant wattage heaters because the energy input into the temperature limited heater does not have to be limited to accommodate low thermal conductivity regions adjacent to the heater. For example, in Green River oil shale there is a difference of at least a factor of 3 in the thermal conductivity of the lowest richness oil shale layers and the highest richness oil shale layers. When heating such a formation, substantially more heat is transferred to the formation with the temperature limited heater than with the conventional heater that is limited by the temperature at low thermal conductivity layers. The heat output along the entire length of the conventional heater needs to accommodate the low thermal conductivity layers so that the heater does not overheat at the low thermal conductivity layers and burn out. The heat output adjacent to the low thermal conductivity layers that are at high temperature will reduce for the temperature limited heater, but the remaining portions of the temperature limited heater that are not at high temperature will still provide high heat output. Because heaters for heating hydrocarbon formations typically have long lengths (for example, at least 10 m, 100 m, 300 m, 500 m, 1 km or more up to about 10 km), the majority of the length of the temperature limited heater may be operating below the Curie temperature and/or the phase transformation temperature range while only a few portions are at or near the Curie temperature and/or the phase transformation temperature range of the temperature limited heater.

The use of temperature limited heaters allows for efficient transfer of heat to the formation. Efficient transfer of heat allows for reduction in time needed to heat the formation to a desired temperature. For example, in Green River oil shale, pyrolysis typically requires 9.5 years to 10 years of heating when using a 12 m heater well spacing with conventional constant wattage heaters. For the same heater spacing, temperature limited heaters may allow a larger average heat output while maintaining heater equipment temperatures below equipment design limit temperatures. Pyrolysis in the formation may occur at an earlier time with the larger average heat output provided by temperature limited heaters than the lower average heat output provided by constant wattage heaters. For example, in Green River oil shale, pyrolysis may occur in 5 years using temperature limited heaters with a 12 m heater well spacing. Temperature limited heaters counteract hot spots due to inaccurate well spacing or drilling where heater wells come too close together. In certain embodiments, temperature limited heaters allow for increased power output over time for heater wells that have been spaced too far apart, or limit power output for heater wells that are spaced too close together. Temperature limited heaters also supply more power in regions adjacent the overburden and underburden to compensate for temperature losses in these regions.

Temperature limited heaters may be advantageously used in many types of formations. For example, in tar sands formations or relatively permeable formations containing heavy hydrocarbons, temperature limited heaters may be used to provide a controllable low temperature output for reducing the viscosity of fluids, mobilizing fluids, and/or enhancing the radial flow of fluids at or near the wellbore or in the formation. Temperature limited heaters may be used to inhibit excess coke formation due to overheating of the near wellbore region of the formation.

In some embodiments, the use of temperature limited heaters eliminates or reduces the need for expensive temperature control circuitry. For example, the use of temperature limited heaters eliminates or reduces the need to perform temperature logging and/or the need to use fixed thermocouples on the heaters to monitor potential overheating at hot spots.

The temperature limited heaters may be used in conductor-in-conduit heaters. In some embodiments of conductor-in-conduit heaters, the majority of the resistive heat is generated in the conductor, and the heat radiatively, conductively and/or convectively transfers to the conduit. In some embodiments of conductor-in-conduit heaters, the majority of the resistive heat is generated in the conduit.

In some embodiments, a relatively thin conductive layer is used to provide the majority of the electrically resistive heat output of the temperature limited heater at temperatures up to a temperature at or near the Curie temperature and/or the phase transformation temperature range of the ferromagnetic conductor. Such a temperature limited heater may be used as the heating member in an insulated conductor heater. The heating member of the insulated conductor heater may be located inside a sheath with an insulation layer between the sheath and the heating member.

Mineral insulated (MI) cables (insulated conductors) are used in certain embodiments to provide heat to subsurface formations that have large overburden depths. In such embodiments, the large overburden depths require long lead-in cables to be used in the overburden. Using insulated conductors with conductive cores (for example, copper cores) in the overburden may be expensive. Use of other, less expensive cables in the overburden may be challenging because of the difficulty in coupling the lead-in cables to insulated conductors used to heat the hydrocarbon containing formation below the overburden.

Typically, a transition insulated conductor is coupled to the insulated conductor used for heating and then some other type of lead-in cable or conductor is coupled to the transition insulated conductor. Coupling the transition insulated conductor to the overburden (lead-in) cable may be challenging. Thus, there is a need for new developments in connection methods that allow inexpensive overburden cables to be coupled to insulated conductors (MI cables).

One possible embodiment for an overburden cable is an ESP (electric submersible pump) cable. For example, the overburden cable may be an electrical cable that meets the test requirements of API (American Petroleum Institute) recommended practice standard 11S6. As the insulation and core materials differ between this type of overburden cable and the insulated conductor, there is a need for a splice and associated method to couple the cable and conductor for use in a subsurface environment.

Such a splice may be simple yet can operate at the high voltages and raised temperatures in the subsurface environment over long durations without failure. In addition, the splice may need a higher bending and tensile strength to inhibit failure of the splice under the weight loads that the cables can be subjected to in the subsurface. The splice may also allow both the overburden cable and the insulated conductor to be installed using coiled tubing installation methods. Coiled tubing installation methods may include, but are not limited to, installation of the splice on the inside of the coiled tubing assembly or installation of the splice on the exterior of the coiled tubing assembly.

FIG. 5 depicts a cross-sectional representation of an embodiment of fitting 336 used to couple lead-in conductor 232 and insulated conductor 212. In certain embodiment, fitting 336 includes body 338 and cap 340. In certain embodiments, lead-in conductor 232 is used in the overburden of the formation. In some embodiments, lead-in conductor 232 is one leg of a three leg lead-in cable that may be used for supplying three-phase power to the subsurface heater (for example, the insulated conductor heater). In some embodiments, lead-in conductor 232 is a single phase lead-in cable that supplies single-phase power to the subsurface heater.

FIG. 6 depicts an embodiment of a three leg lead-in cable with three lead-in conductors 232. In some embodiments, lead-in conductor 232 is an electrical cable that meets the test requirements of API recommended practice standard 11S6. In some embodiments, lead-in conductor 232 is coupled to another electrical cable (another lead-in conductor or cable). For example, lead-in conductor 232 may be coupled to an electrical cable that meets the test requirements of API recommended practice standard 11S6. In some embodiments, all or a portion of lead-in conductor 232 is placed inside a conduit (for example, a stainless steel conduit). In some embodiments, lead-in conductor 232 is one leg of a duel (two) leg lead-in conductor that may be used for supplying single-phase power to the subsurface heater. In certain embodiments, insulated conductor 212 is a transition insulated conductor (for example, core 214 is a highly conductive core such as a copper core). In some embodiments, insulated conductor 212 is able to carry voltages of about 600V to 5000V or higher. Insulated conductor 212 may be one leg of a three-leg (three-phase) heater used to provide heat to the subsurface formation. For three-phase (three-leg) connections, each leg of a lead-in cable may be connected to a leg of an insulated conductor heater. For single-phase (dual-leg) connections, each leg of a lead-in conductor may be connected to a leg of an insulated conductor heater.

Insulated conductor 212 may be prepared prior to coupling the insulated conductor to fitting 336. FIG. 7 depicts an embodiment of a prepared end portion of insulated conductor 212. In certain embodiments, end portions of jacket 218 and electrical insulator 216 are removed to expose core 214. In some embodiments, a shield and/or lead jacket is removed. In an embodiment, about 3″ (about 7.5 cm) of the end portions of jacket 218 and electrical insulator 216 are removed. In some embodiments, insulated conductor 212 is heated prior to removing the end portions of jacket 218 and electrical insulator 216. For example, insulated conductor 212 may be heated to a temperature between about 50° C. and about 75° C. (for example, about 60° C.) before removing the end portions of jacket 218 and electrical insulator 216.

After exposing core 214, recess 342 may be formed in electrical insulator 216 around the core. In an embodiment, recess 342 is a ½″ (about 1.2 cm) deep bore into electrical insulator 216. Forming of the recess may reduce stress to an acceptable level. In some embodiments, insulated conductor 212 is heated to an elevated temperature to prevent moisture from contaminating electrical insulator 216 in the insulated conductor during creation of recess 342. For example, insulated conductor 212 may be heated to a temperature between about 66° C. and about 120° C. Recess 342 may reduce electrical field intensities inside fitting 336.

In some embodiments, boot 343 is placed over end of insulated conductor 212 and into recess 342. Boot 343 may be molded to fit into recess 342 around core 214 and cover exposed electrical insulator 216 at end of insulated conductor 212. In some embodiments, a small air gap is left between boot 343 and electrical insulator 216 inside recess 342. The small air gap may allow for thermal expansion of core 214 and/or the electrical insulator. Boot 343 may be made of electrically insulating materials such as, but not limited to, EPDM rubber (ethylene propylene diene Monomer (M-class) rubber) available from Baker Hughes Centrilift (Claremore, Okla., U.S.A.). In some embodiments, boot 343 is coated with a lubricant (for example, a grease) before being inserted into recess 342. In certain embodiments, lubricant is silicone based lubricant or sealant such as, but not limited to, Dow Corning® 111 silicone compound. The combination of EPDM rubber and Dow Corning® 111 silicone compound for boot 343 may seal off the end of insulated conductor 212 at operating voltages up to about 10 kV and currents of at least about 300 A. Providing boot 343 into end of insulated conductor 212 may increase the operating temperature of fitting 336 by sealing off the end of the insulated conductor with thermally stable materials.

In certain embodiments, lead-in conductor 232 is prepared prior to coupling the lead-in cable to fitting 336. FIG. 8 depicts an embodiment of a prepared end portion of lead-in conductor 232. In certain embodiments, end portions of sheath 344 and insulation 346 are removed to expose conductor 348 of lead-in conductor 232. In an embodiment, about 3″ (about 7.5 cm) of the end portion of sheath 344 is removed and insulation 346 is cut back to expose about ½″ to about ¾″ (about 1.27 cm to about 1.9 cm) of conductor 348.

As shown in FIG. 8, conductor 348 may be coupled to one end of lug 350. Lug 350 may be, for example, a barrel connector or other mechanical connector such as a screw connector, a clamp, or a spring type connector). In some embodiments, lug 350 is a crimp type connector. In an embodiment, lug 350 is a barrel splice crimp connector. As shown in FIG. 5, the other end of lug 350 is coupled to core 214 of insulated conductor 212. Thus, lug 350 electrically couples conductor 348 and core 214. In other embodiments, conductor 348 and core 214 are coupled using another type of coupling.

As shown in FIG. 5, body 338 is coupled to jacket 218 of insulated conductor 212. Fitting 336 may be coupled to jacket 218 by welding the fitting to the jacket. In some embodiments, fitting 336 is coupled to jacket 218 using other methods known in the art (for example, a ferrule-type fitting or crimp-type coupling). In certain embodiments, jacket 218 is positioned in body 338 such that the end of the jacket aligns with the internal taper of the body. Aligning the internal taper with the end of the jacket reduces electrical field intensities inside fitting 336. In some embodiments, body 338 is placed over the end of insulated conductor 212 prior to coupling conductor 348 to core 214.

In certain embodiments, fitting 336 is filled with filling material 354. End cap 340 may be uncoupled from fitting 336 to allow filling material 354 to be provided (for example, poured, injected, or introduced) into the fitting. For example, end cap 340 may be uncoupled and slid down along lead-in conductor 232 to allow filling material 354 to be provided into the fitting. In some embodiments, filling material 354 is provided into the fitting 336 with the fitting and insulated conductor 212 in a substantially vertical position (a vertical or near-vertical position). Other positions between vertical and horizontal may also be possible. In some embodiments, filling material 354 is provided into fitting 336 with the fitting and end of insulated conductor 212 inside the fitting heated to an elevated temperature. For example, fitting 336 and end of insulated conductor 212 inside the fitting may be heated to a temperature between about 65° C. and about 95° C.

In certain embodiments, filling material 354 is provided into fitting 336 until a level of the filling material reaches a desired level. For example, filling material 354 may be provided until the filling material just begins to pour out through set screw openings 356. Providing filling material 354 to a level such that some filling material pours out through set screw openings 356 may ensure that there are no voids or gaps in the filling material or inside fitting 336.

In some embodiments, fitting 336 is left loose to allow filling material 354 to overflow out of the fitting. In some embodiments, fitting 336 includes a vent opening to allow filling material 354 to overflow out the vent opening. The vent opening may be plugged or sealed after filling fitting 336 with filling material 354.

Filling material 354 is an electrically insulating material. Filling material 354 may be a malleable or ductile electrical insulant. Filling material 354 may need to withstand operating temperatures in excess of about 105° C. In certain embodiments, filling material 354 is a resin, an epoxy or epoxy-based electrical insulant. For example, filling material 354 may be Scotchcast™ 2130 polyurethane resin available from 3M™ Company (St. Paul, Minn., U.S.A.) or another insulating material (such as an epoxy or silicone material) suitable for operating up to temperatures in a range between about 230° C. and about 260° C.

After filling material 354 is provided into fitting 336, tubing 352 may be slid down sheath 344 such that at least part of the tubing is inside body 338. Tubing 352 may be, for example, a section of stainless steel tubing cut a desired length. Tubing 352 may fit snugly over the outside diameter of the end of sheath 344. In some embodiments, grease or another lubricant is placed on sheath 344 to allow tubing 352 to slide over the end of the sheath. In some embodiments, tubing 352 is placed over the end of sheath 344 prior to coupling conductor 348 to core 214. In some embodiments, tubing 352 is placed on sheath 344 prior to adding filling material 354 into fitting 336.

With tubing 352 in position inside body 338, end cap 340 and connector 358 may be slid into position in body 338. End cap 340 may be secured inside body 338 using set screws in set screw openings 356. In some embodiments, filling material 354 may move out of fitting through 356 when end cap 340 is moved into body 338. As noted above for tubing 352, end cap 340 and connector 358 may be placed on lead-in conductor 232 prior to coupling conductor 348 to core 214. End cap 340, connector 358, and tubing 352 may be temporarily moved away from fitting 336 to allow assembly of components within and around the fitting.

Filling material 354 may be allowed to cure with end cap 340 in place on fitting 336. In some embodiments, filling material 354 is allowed to cure at ambient temperature. In some embodiments, filling material 354 is cured with some heating. For example, filling material 354 may be cured at temperatures above about 35° C. up to temperatures of about 135° C. Filling material 354 may substantially fill the entire interior of fitting 336 without any gaps or voids inside the fitting. Filling material 354 may substantially fill recess 342 such that there are no gaps or voids inside the recess.

Connector 358 may be used to couple the assembly of lead-in conductor 232, insulated conductor 212, and fitting 336 to a mechanical support for the assembly. For example, connector 358 may be coupled to a support conduit. The support conduit may surround lead-in conductor 232 or be a separate support conduit. The mechanical support may support the weight of insulated conductor 212 below the assembly for a hanging heater assembly.

In certain embodiments, lead-in conductor 232, insulated conductor 212, and fitting 336 are one leg of a three leg subsurface heater assembly. Thus, there may be two similar legs (lead-in cable, insulated conductor, and fitting) to complete the three leg subsurface heater assembly. In some embodiments, the locations of the splice fittings in the three legs are staggered to reduce an overall diameter of the heater assembly. All three legs of the heater assembly may be placed in a coiled tubing installation conduit for installation into a subsurface wellbore. In some embodiments, lead-in conductor 232, insulated conductor 212, and fitting 336 are one leg of a single-phase subsurface heater assembly. Thus, there may be a similar leg for returning power from the subsurface.

It is to be understood the invention is not limited to particular systems described which may, of course, vary. It is also to be understood that the terminology used herein is for the purpose of describing particular embodiments only, and is not intended to be limiting. As used in this specification, the singular forms “a”, “an” and “the” include plural referents unless the content clearly indicates otherwise. Thus, for example, reference to “a core” includes a combination of two or more cores and reference to “a material” includes mixtures of materials.

In this patent, certain U.S. patents, U.S. patent applications, and other materials (for example, articles) have been incorporated by reference. The text of such U.S. patents, U.S. patent applications, and other materials is, however, only incorporated by reference to the extent that no conflict exists between such text and the other statements and drawings set forth herein. In the event of such conflict, then any such conflicting text in such incorporated by reference U.S. patents, U.S. patent applications, and other materials is specifically not incorporated by reference in this patent.

Further modifications and alternative embodiments of various aspects of the invention will be apparent to those skilled in the art in view of this description. Accordingly, this description is to be construed as illustrative only and is for the purpose of teaching those skilled in the art the general manner of carrying out the invention. It is to be understood that the forms of the invention shown and described herein are to be taken as the presently preferred embodiments. Elements and materials may be substituted for those illustrated and described herein, parts and processes may be reversed, and certain features of the invention may be utilized independently, all as would be apparent to one skilled in the art after having the benefit of this description of the invention. Changes may be made in the elements described herein without departing from the spirit and scope of the invention as described in the following claims.

Claims

1. A method for coupling a lead-in cable to an insulated conductor, comprising: exposing an end portion of a core of the insulated conductor by removing at least a portion of a jacket and an electrical insulator surrounding the end portion of the core;forming a recess in the electrical insulator at the end of the electrical insulator surrounding the end portion of the core;exposing an end portion of a conductor of the lead-in cable by removing at least a portion of a sheath and insulation surrounding the end portion of the conductor;coupling the end portion of the core to the end portion of the conductor;placing the end portion of the core and the end portion of the conductor in a body;coupling the body to the jacket of the insulated conductor such that the exposed portion of the core is enclosed within the body;coupling the body to the sheath of the lead-in cable such that the exposed portion of the conductor is enclosed within the body; andfilling the body with electrically insulating material such that there are no voids or gaps inside the body.
2. The method of claim 1, wherein the electrically insulating material comprises electrically insulating resin.
3. The method of claim 2, further comprising allowing the resin to cure.
4. The method of claim 1, further comprising placing a section of stainless steel tubing over the end portion of the conductor and at least a portion of the sheath of the lead-in cable.
5. The method of claim 1, further comprising filling the body with the electrically insulating material with the insulated conductor in a substantially vertical position.
6. The method of claim 1, further comprising coupling the end portion of the core to the end portion of the conductor with a mechanical connector.
7. The method of claim 1, further comprising placing a boot into the recess in the electrical insulator, wherein the boot covers the end of the electrical insulator.
8. The method of claim 7, wherein the boot seals the end of the insulated conductor around the core.
9. The method of claim 1, wherein filling the body with the electrically insulating material substantially fills the recess in the electrical insulator.
10. A method for coupling a lead-in cable to an insulated conductor, comprising: exposing an end portion of a core of the insulated conductor by removing at least a portion of a jacket and an electrical insulator surrounding the end portion of the core;forming a recess in the electrical insulator at the end of the electrical insulator surrounding the end portion of the core, wherein at least a portion of the core is exposed in the recess;exposing an end portion of a conductor of the lead-in cable by removing at least a portion of a sheath and insulation surrounding the end portion of the conductor;coupling the end portion of the core to the end portion of the conductor;placing the end portion of the core and the end portion of the conductor in a body;coupling the body to the jacket of the insulated conductor such that the exposed portion of the core is enclosed within the body;coupling the body to the sheath of the lead-in cable such that the exposed portion of the conductor is enclosed within the body; andfilling the body with electrically insulating material such that there are no voids or gaps inside the body.
11. The method of claim 10, wherein the electrically insulating material comprises electrically insulating resin.
12. The method of claim 11, further comprising allowing the resin to cure.
13. The method of claim 10, further comprising placing a section of stainless steel tubing over the end portion of the conductor and at least a portion of the sheath of the lead-in cable.
14. The method of claim 10, further comprising filling the body with the electrically insulating material with the insulated conductor in a substantially vertical position.
15. The method of claim 10, further comprising coupling the end portion of the core to the end portion of the conductor with a mechanical connector.
16. The method of claim 10, further comprising placing a boot into the recess in the electrical insulator, wherein the boot covers the end of the electrical insulator.
17. The method of claim 16, wherein the boot seals the end of the insulated conductor around the core.
18. The method of claim 10, wherein filling the body with the electrically insulating material substantially fills the recess in the electrical insulator.

PRIORITY CLAIM

This patent application claims priority to U.S. Provisional Patent Application Ser. No. 61/391,408 entitled “SYSTEM AND METHOD FOR COUPLING LEAD-IN CONDUCTOR TO INSULATED CONDUCTOR” to Burns et al. filed on Oct. 8, 2010; and U.S. Provisional Patent No. 61/473,599 entitled “SYSTEM AND METHOD FOR COUPLING LEAD-IN CONDUCTOR TO INSULATED CONDUCTOR” to Burns et al. filed on Apr. 8, 2011, all of which are incorporated by reference in their entirety.

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Related Publications (1)

	Number	Date	Country
	20120110845 A1	May 2012	US

Provisional Applications (2)

	Number	Date	Country
	61391408	Oct 2010	US
	61473599	Apr 2011	US

System and method for coupling lead-in conductor to insulated conductor

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