Patent Application
20240049385
The subject matter disclosed herein relates to systems and methods for a smart carbon coating having one or more hard carbon-rich layers with one or more treated carbon regions. More specifically, the subject matter disclosed herein relates to a smart carbon coating, induced and created from a hard carbon material such as a diamond-like carbon coating, wherein by having one or more treated carbon regions with greatly different electrical properties the assessment of these electrical properties from the treated carbon portions determines at a surface coated with the smart carbon coating some changes in force, stress, pressure, displacement, strain, water (liquid, vapor including humidity), and/or the presence of material buildups, including scale deposits, among others.
A variety of equipment, for instances general pressure vessels and heavy pressurized structures, may be subjected to severe environmental and operational conditions, potentially leading to structural failures through a variety of progressive changes, including mechanical failures due to fatigue, corrosion in its various forms among uniform corrosion, stress-corrosion cracking, hydrogen-induced cracking, or other changes such as adherent scale buildups such as calcite deposits in water-producing conduits, among others. The equipment may include surface equipment deployed on land or floating infrastructures at normal atmospheric conditions, subsea equipment, deployed underwater under hydrostatic pressure, or downhole equipment used with subterranean reservoirs. For example, the equipment may include hydrocarbon extraction equipment used for the production of hydrocarbon streams (e.g., oil and/or gas) from a well. The equipment also may include sequestration equipment configured to inject and control the storage of fluids (e.g., liquid water, steam, gases such as carbon dioxide, hydrogen, among others) in a subterranean reservoir. For example, the sequestration equipment may be part of carbon capture and storage (CCS) infrastructures at surface, subsea or downhole. The foregoing equipment may include, for example, tubular components, hangers, valves, chokes, packers, pumps, or other associated fluid handling equipment required for the injection and storage of carbon (carbon dioxide). In any case, it may be difficult to monitor any gradual changes prior to any potential structural failures because the surfaces subject to the harsh conditions may be difficult to access, including positioned deep in a well. When a piece of equipment with one or several of its surfaces covered with one or more coatings, it is generally challenging, if not impractical, to determine the structural integrity of this coating regardless of the coating characteristics. A hard coating such as one comprising carbon and usually defined as a diamond-like carbon coating (DLC) may offer advantages in terms of wear resistance, reduced friction, anti-scaling, even anti-icing, and it may be highly desirable to enrich the coating with sensing capabilities so as to broadly sense, monitor, or ultimately conduct some prognostic health monitoring of equipment pieces.
A summary of certain embodiments disclosed herein is set forth below. It should be understood that these aspects are presented merely to provide the reader with a brief summary of these certain embodiments and that these aspects are not intended to limit the scope of this disclosure. Indeed, this disclosure may encompass a variety of aspects that may not be set forth below.
In certain embodiments, the present disclosure relates to a system. The system includes a substrate and a coating deposited onto a surface of the substrate. The coating includes a carbon rich layer deposited on the substrate. The carbon rich layer also includes a first carbon content characterized by its sp2 carbon and sp3 carbon. Further, the carbon rich layer includes one or more treated carbon regions. The one or more treated carbon regions include an electrically conductive carbon material having a second carbon content characterized by its sp2 carbon and sp3 carbon. The second carbon content of the treated region includes more sp2 carbon than the first carbon content.
In certain embodiments, the present disclosure relates to a system. The system includes a surface monitoring system that measures data indicative of a change in surface characteristics of a coating applied to a downhole component. The coating includes a carbon rich layer deposited on the substrate. The carbon rich layer also includes a first carbon content characterized by its sp2 carbon and sp3 carbon. Further, the carbon rich layer includes one or more treated carbon regions. The one or more treated carbon regions include an electrically conductive carbon material having a second carbon content including sp2 carbon and sp3 carbon. The second carbon content includes more sp2 carbon than the first carbon content. The system also includes a non-transitory machine-readable medium and executable by a processor to identify the change in the surface characteristics in response to the data and output an indication of the change.
In certain embodiments, the present disclosure relates to a method. The method includes applying one or more carbon rich layers to a substrate. The one or more carbon rich layers comprise a first carbon content characterized by its sp2 carbon and sp3 carbon. The method also includes treating a portion of the one or more carbon rich layers with a focused energy source to generate a pattern of electrically conductive carbon. The electrically conductive carbon comprises a second carbon content comprising more sp2 carbon than the first carbon content.
Various aspects of this disclosure may be better understood upon reading the following detailed description and upon reference to the drawings in which:
One or more specific embodiments will be described below. In an effort to provide a concise description of these embodiments, not all features of an actual implementation are described in the specification. It should be appreciated that in the development of any such actual implementation, as in any engineering or design project, numerous implementation-specific decisions must be made to achieve the developers' specific goals, such as compliance with system-related and business-related constraints, which may vary from one implementation to another. Moreover, it should be appreciated that such a development effort might be complex and time consuming, but would nevertheless be a routine undertaking of design, fabrication, and manufacture for those of ordinary skill having the benefit of this disclosure.
As generally discussed above, certain equipment, such as downhole components (e.g., tubular components, hangers, valves, chokes, packers, pumps, etc.) may be operated under severe conditions that challenge the safe operational limits of the equipment during its intended life span. For instances, these conditions may be generating elevated mechanical stresses on the equipment, and/or be associated to fluids or chemicals that may cause a detrimental chemical or electrochemical change to surfaces of the equipment, which may result in damage or end-of-life failure. To decrease risk of equipment damage and failure, it is presently recognized that it may be advantageous to provide a coating onto one or more surfaces. This coating may be considered as a protective coating and may be particularly resistant to wear and abrasion when it is hard, lubricious, and adherent to the substrate. Additionally, this coating may be such that it is capable to detect an otherwise non-measurable change in a coating property, the latter resulting from chemical (including electrochemical) and/or mechanical changes (e.g., due to force, stress, pressure, displacement, strain, water, humidity, fluids in contact with an interior and/or exterior surface of the equipment, and the like) to the surface of the coating. Moreover, it may be advantageous to produce or generate such a smart coating by functionalizing a carbon rich-coating, having a suitable hardness (e.g., having a Vickers hardness greater than 750 HVN, greater than 900 HVN, greater than 1050 HVN, greater than 1200 HVN, greater than 1350 HVN, or greater than 1500 HVN) with a circuitry capable of producing a detectable signal due to chemical or mechanical changes to a surface of a downhole component, such as force, pressure, displacement, stress, water, strain, humidity, presence of material buildups including scale deposits. The stress may be directly applied, or be the result of another event; for instance, shocks, scale adhesion, thermal change, etc., or chemical interactions.
Accordingly, the present disclosure is directed to techniques for generating and utilizing a smart carbon coating (e.g., smart carbon rich coating) having at least one carbon rich layer having a treated carbon rich portion. In general, the treated carbon rich portion may be formed by laser-treatment, or otherwise treating the non-conductive carbon rich layer, such that the treated carbon rich portion becomes more electrically conductive (e.g., having a lower sheet electrical resistance) than the carbon rich layer (e.g., an untreated portion of the carbon rich layer). For example, the carbon rich layer may be treated with an illumination source such as a laser source, such by irradiating a surface of one or more layers of the carbon rich layer with a suitable exposure of a laser an electrically conductive carbon materials (e.g., graphene, graphite, and others) is formed. By generating the electrically conductive materials, the smart coating is characterized by some improved electrical conductance (e.g., resulting from a reduced sheet electrical resistance) as compared to not treating the carbon rich layer. That is, the treated carbon rich portion includes electrically conductive carbon materials such that treated carbon rich portion is an electrically conductive carbon layer, while the untreated portion of the carbon rich layer is relatively less conductive or substantially a non-conductive carbon layer (e.g., formed of electrically insulating materials). For example, the treated carbon portion may be treated such that the sheet electrical resistance of the smart carbon coating includes the treated carbon rich portion has a sheet electrical resistance that is greater than 100 times less than, greater than 200 times less than, or greater than 300 times less than that of the untreated carbon rich layer. In any case, the electrical properties of the disclosed smart carbon coating may vary due to exposure of the equipment to certain conditions (e.g., strain, stress, fluids, humidity, scale deposition). Accordingly, the disclosed smart carbon coating may facilitate detecting exposure of the surface of the equipment (e.g., downhole components) to chemical and/or mechanical conditions, which result in one or more changes in the electrical properties of the smart carbon coating. In this way, the disclosed smart carbon coating may enable monitoring of equipment coated with the disclosed smart carbon coating to reduce a likelihood of the equipment working in an unexpected manner or otherwise failing.
With the foregoing in mind,
In the illustrated example of
It should be noted that the actuation subsystem 32 and the valve housing 30 may be configured to operate with or without use of fluid or electrical control lines extending from the surface into the wellbore 14. For example, electrical power and/or fluid pressure may be provided from the surface using one or more electrical generators, a power grid, batteries, pumps, or a combination thereof. Additionally, or alternatively, the actuation subsystem 32 may be powered by one or more local power supplies, such as a battery pack, at the location of the valve 22.
The illustrated embodiment of the closure device 12 includes the valve controller 34 that may be utilized to adjust the position of the components in the valve housing 30. The valve controller 34 controls and/or adjusts a position of the valve 22 between open and closed positions (e.g., via the actuation subsystem 32). For example, the valve controller 34 may control and/or adjust the valve 22 based on control signals and/or messages that are transmitted by a transmitter of a transmitter subsystem 38.
In some embodiments, the transmitter subsystem 38 may receive sensor measurements (e.g., temperature sensor measurements, pressure sensor measurements, flow-rate sensor measurements, fluid composition measurements such as salinity levels, other parameters relating to the formation of scale deposits, or any combination thereof). The sensor measurements may be directed by surface sensors, downhole sensors, or completion sensors to the transmitter subsystem 38 via any suitable telemetry (e.g., via electrical signals pulsed through the geological formation 16 or via mud pulse telemetry). In some embodiments, the transmitter subsystem 38 may receive inputs from a user interface (e.g., a graphical user interface) controlled by an operator. The transmitter subsystem 38 may process the sensor measurements and/or user inputs to determine a condition within the wellbore 14 or at the surface and determine whether to adjust the position of the valve 22 based on the condition of the wellbore 14 and/or the surface.
To this end, the transmitter subsystem 38 may be any electronic data processing system that can be used to carry out various functions of the systems and methods described herein. For example, the transmitter subsystem 38 may include a processor 40 which may execute instructions stored in memory 42 and/or storage 44. As such, the memory 42 and/or the storage 44 of the transmitter subsystem 38 may be any suitable article of manufacture that can store the instructions. In some embodiments, the memory 42 is a tangible, non-transitory, machine-readable-medium that may store machine-readable instructions for the processor 40 to execute. The memory 42 may include ROM, flash memory, a hard drive, or any other suitable optical, magnetic, or solid-state storage medium, or a combination thereof. The memory 42 may store data, instructions, and any other suitable data. Additionally, the transmitter subsystem 38 may include an input/output (I/O) port 46, which may include interfaces coupled to various components such as input devices (e.g., keyboard, mouse), input/output (I/O) modules, sensors (e.g., surface sensors and/or downhole sensors), and the like. For example, the I/O port 46 may include a display (e.g., an electronic display) that may provide a visualization, a well log, or other operating parameters of the geological formation 16, the wellbore 14, or the surface to an operator, for example. In this embodiment, the transmitter subsystem 38 (e.g., data processing system) has been represented at the well site. However, all or part of the transmitter subsystem 38 (e.g., all or part of the processor, the display, the memory, etc.) may be situated remotely from the well site and configured to communicate with the well site via a network connection. It should be noted that, at least in some instances, all or part of the data processing system may be cloud-based.
As discussed herein, a smart carbon coating having one or more carbon rich layers may be applied to one or more surfaces of the downhole components to reduce, block, or generally inhibit the precipitation of scale onto surfaces of the downhole components, thereby reducing the possibility of blockage of fluid flow or the improper actuation of a mechanical component. Furthermore, the smart carbon coating may have improved mechanical resistance as compared to a substrate (e.g., a substrate of a downhole component), and thus the smart carbon coating may improve the longevity of the substrate.
It should be noted that the above discussions of
Furthermore, in embodiments where the disclosed smart carbon coating is applied onto a surface of a piston, it should be noted that the smart carbon coating may be configured to provide a relatively low friction coefficient under certain conditions, such as dry and normally unlubricated, or conversely lubricated conditions. For example, the smart carbon coating may be deposited on opposing surfaces (e.g., opposing contacting surfaces) or an entire circumference of multiple parts of the downhole component (e.g., a first part such as a piston and a second part such as a shaft including the piston). Additionally, the carbon rich layer may have a coefficient of friction less than approximately 0.30, 0.25, 0.20, 0.15, 0,10, or 0.05 against a metal under dry conditions, such as alloys of iron (steels, stainless steels, cast irons), nickel (superalloys), titanium, among others. Example alloys that may be used in accordance with the disclose techniques are included in certain standards such as ISO 15156, certain stainless steels, among martensitic stainless steels (e.g., 13Cr, modified 13Cr), duplex and superduplex stainless steels (22Cr, 25Cr) and nickel-based alloys such as Alloy 925, Alloy 718, among others. In certain applications, a polymer composite material that is non-interfering with downhole measurements; in others, a carbide component may be utilized to mitigate erosion. When applied to these components, the smart carbon coating may mitigate, prevent, or reduce scale formation as well as not reduce efficiency of operation of components that may be partially in contact during operation. Additionally, because of its ability to sense, the smart carbon coating may be able to detect a circumstance that would normally precede a failure, and as such prevent a failure from occurring.
At block 74, the process 62 includes depositing a carbon source 76 and one or more additional chemical components 78 (e.g., metallic sources 80 and/or non-metallic sources 82) onto the substrate 72 (e.g., the downhole component, such as those described with respect to
The substrate 72 may be part of a downhole component, such as a valve (e.g., ball valve, gate valve, or flapper valve), a packer, sliding sleeves, and a choke, as discussed with respect to
The carbon source 76 is a source including the carbon element and delivering this carbon element to one or more substrates. For example, the carbon source 76 may be a hydrocarbon gas such as methane, ethane, and/or ethyne, and/or a metal carbonyl. To produce elemental carbon that would deposit rapidly onto a target substrate, the carbon source gas may be ignited by an AC voltage, which may cause carbon and hydrogen atoms to recombine as a dense carbon rich layer onto the substrate.
The additional chemical components 78 generally include silicon and metallic sources 80 (e.g., transition metal sources, main-group metal sources) and nonmetallic sources 82. For example, the metallic sources 80 may include tungsten, titanium, chromium, nickel, iron, and/or cobalt, such as corresponding metal carbonyls, metal hydrides, metal halides, among others. The nonmetallic sources 82 may include silicon, oxygen, nitrogen, fluorine, and/or chlorine, such as silanes, metal halides, fluorine gas, nitrogen gas, ammonia, and alkylamines.
At block 88, the process 62 includes treating the coating 84 (including the carbon rich layers 66) with radiation or a focused energy source. In general, treating the coating 84 with radiation may include providing a suitable exposure of the coating 84 with a laser, thereby modifying or altering at least a portion of the carbon rich layers 66 to produce an induced pattern or circuitry including electrically conductive carbon materials 70. As referred to herein, an “induced circuitry” or “an induced pattern” refers to circuitry or pattern formed due to a modification (e.g., a chemical modification resulting from laser treatment) of a material. In general, the suitable exposure may include illuminating the coating 84 at certain exposure parameters, such as a particular power of the laser (e.g., between 5 Watts (W) and 10 W, between 10 W and 15 W, between 15 W and 20 W, between 20 W and 25 W, or greater than 25 W, a wavelength of the emission of the laser within a suitable wavelength range (e.g., between 180 and 400 nm, between 400 and 700 nm, between 700 nm and 1100 nm), a pulse duration of width (e.g., between 1 ms and 10 ms, between 1 ns and 10 ns, between 5 fs and 100 ps) and scan rate between 1 mm/s and 6000 mm/s. In any case, providing the suitable exposure of the coating 84 with the laser may generate a smart carbon coating 64 having a carbon rich layer 66 and an electrically conductive carbon material 70. Focusing the laser beam on the surface of the carbon rich layers 66 may form a pattern (e.g., an electric circuit) of the electrically conductive carbon by modifying the carbon content, thereby producing a different carbon species. It is presently recognized that tuning the exposure parameters may enable tuning of the carbon content and/or the thickness of the electrically conductive carbon material 70.
In some embodiments, treating the coating, at block 88, may include creating one or more interconnects between a conductive pattern, engraved circuitry, or printed circuitry by depositing a conductive metal (e.g., copper, gold, silver) and/or applying an electrically conductive anchoring element, thereby forming a material acting as a pad. At least in some instances, creating the interconnects and treating the coating may be performed in a single similar chamber, such as a plasma vapor deposition (PVD) chamber, a chemical vapor deposition (CVD), or a plasma-assisted or enhanced chemical vapor deposition (PACVD, PECVD) chamber. Moreover, one or more additional layers of the carbon rich layer 66 may be applied to the smart coating 64, thereby forming a carbon rich layer 66 on top of the treated carbon region 68.
In certain embodiments, the carbon rich layer 66 includes one or more regions, areas, or locations having carbon content with a particular amount of (e.g., or otherwise being characterized) sp2 carbon and/or sp3 carbon. Furthermore, the carbon rich layer may include a suitable amount of sp2 and sp3 carbon to produce desired combinations of properties among, surface hardness, friction coefficient, contact angles, all generally having positive impacts for reducing a likelihood of scale precipitation (e.g., scale formation) and/or other deterioration on the surface of a coating. Carbon is stabilized in various multi-atomic structures with diverse atomic arrangements or configurations referred as allotropes: these includes amorphous carbon (a-C), graphite (with sp2 configuration) and tetrahedral amorphous carbon (ta-C) or defected diamond (with sp3 configuration). Carbon-rich layers include these allotropes in various proportions, among carbon and non-carbon phases. The treated carbon rich portion generally includes electrically conductive carbon materials formed by treating the carbon rich layer with a focused energy source such as an illumination source such as a laser. In some embodiments, the carbon rich layer 66 and/or the treated carbon region 68 may include one or more dispersed phases that include mixtures of carbon with elements from the one or more additional chemical components 78, such as metal carbides. In some embodiments, the carbon rich layer 66 and/or the treated carbon region 68 may include combinations of different elements from the additional chemical components 78, such as metal chalcogenides, as discussed in further detail herein.
The carbon rich layer 66 may include a suitable amount of sp2 and sp3 carbon to produce desired combinations of mechanical and/or electrical properties. In general, carbon is stabilized in various multi-atomic structures with diverse atomic arrangements or configurations referred as allotropes: these includes amorphous carbon (a-C), graphite (with sp2 configuration) and tetrahedral amorphous carbon (ta-C) or defected diamond (with sp3 configuration). Carbon-rich layers include these allotropes in various proportions, among carbon and non-carbon phases. In some embodiments, the carbon rich layer 66 may include diamond-like carbon. For example, the carbon rich layer 66 may have greater than 30% sp3 carbon, greater than 50% sp3 carbon, greater than 70% sp3 carbon, greater than 90% sp3 carbon.
Further, the carbon rich layer 66 may include a total thickness between 0.5 μm and 30 μm. For example, the total thickness of the carbon rich layer 66 may be between 50 μm and 30 μm, between 0.75 μm and 15 μm, between 1.0 μm and 5.0 μm, or between 1.25 μm and 2.5 μm. In certain embodiments, the total thickness of the carbon rich layer 66 may include both a thickness of one or more carbon rich layers and a thickness of one or more other layers deposited on the substrate 72, such as a top surface layer, a buffer layer (i.e., a layer introduced to accommodate (e.g., increase the binding strength of) the carbon-rich layer on the substrate), and a dispersed phase layer. For example, the carbon rich layer 66 may include a plurality of layers, which may include carbon rich layers and optionally non-carbon rich layers, collectively defining a total thickness of the carbon rich layer 66. Buffer layers may include metallic materials, and may also comprise transition-metals applied by PVD, CVD, PACVD, PECVD, plating, thermal spray or others. The buffer layer may also include non-metallic materials, including polymeric materials and ceramic materials. In order to accommodate a carbon-rich layer onto a surface of the substrate, these layers may include carbon-containing materials, such as tungsten carbide and fluoropolymer.
As discussed herein, the carbon rich layer 66 includes a treated carbon region 68 that is an electrically conductive carbon region formed of electrically conductive carbon materials 70. In general, the treated carbon region 68 is more electrically conductive (e.g., has a lower sheet electrical resistance) than the untreated portions of the carbon rich layer 66. For example, the sheet electrical resistance of the carbon rich layers 66 may be more than 100 times (i.e., 2 orders of magnitude), more than 250 times, more than 500 times, or more than 1000 times (i.e., 3 orders of magnitude), than the sheet electrical resistance of the treated carbon region 68. Put differently, the sheet electrical resistance of the treated carbon region 68 may be less than 1/100th, than that of the sheet electrical resistance of the carbon rich layers 66. Additionally, the treated carbon region 68 may have a generally higher amount of sp2 carbon. For example, the treated carbon region 68 may have increased sp2 carbon (e.g., greater than 30%, greater than 40%, greater than 50%), a relatively higher sp2/sp3 ratio (e.g., greater than 0.5, greater than 1.0, greater than 1.5), a relatively low sheet electrical resistance (e.g., less than 1000 Ω per sq.), or a combination thereof, as compared to the carbon rich layers 66 that are untreated.
The treated carbon rich portion 68 may include an electrically conductive pattern (e.g., electric circuit) that includes the electrically conductive carbon materials 70. The electrically conductive pattern may be utilized as a sensing substrate that is capable of detection a presence of fluids on the surface of the smart carbon rich coating, such as an electric circuit (e.g., printed circuitry) as described in more detail with respect to
In some embodiments, the smart carbon coating 64 and/or treated carbon region 68 may include a suitable amount of the electrically conductive carbon material 70 such that the sheet electrical resistance (Rs) in Ohms per square (Ω per sq.) of the smart carbon coating 64 is less than 1000 Ω per sq. For example, the suitable amount of the electrically conductive carbon material 70 may be such that the Rs of the smart carbon coating 64 is between approximately 10 to 1000 Ω per sq., 20 Ω per sq. to 500 Ω per sq., 30 Ω per sq. to 250 Ω per sq., 40 Ω per sq. to 200 Ω per sq., 50-150 Ω per sq. In some embodiments, the smart carbon coating 64 may include a suitable amount of the electrically conductive carbon material 70 such that the carbon content of the smart carbon coating 64 is greater than 30% sp2 carbon (e.g., amount of sp2 carbon/(amount of sp2 carbon+amount of spa carbon), greater than 40% sp2 carbon, greater than 50% sp2 carbon, greater than 60% sp2 carbon, greater than 70% sp2 carbon, greater than 80% sp2 carbon. In some embodiments, the smart carbon coating 64 may include a suitable amount of electrically conductive carbon material 70 such that the sp2/sp3 ratio of the smart coating is greater than 0.5, greater than 1.0, or greater than 1.5. For example, the smart carbon coating 64 may include a suitable amount of electrically conductive carbon material 70 such that the sp2/sp3 ratio of the smart coating is between 0.5 to 2.0, between 0.75 to 1.5, or between 1.0 to 1.25.
The electrically conductive carbon material 70 is generally a modified portion of the material within the carbon rich layer 66. In some embodiments, the electrically conductive carbon materials may include graphene, graphite, and other types of electrically conductive carbon materials. In some instances, the treated carbon region 68 may include a portion of the electrically conductive carbon material 70, such as one or more underlying layers of a less conductive carbon material or inventing portions of the less conductive carbon material in between any patterns (e.g., patterns formed of the electrically conductive carbon material 70, such as an electric circuit, a sensing circuit, and the like, as described with respect to
To illustrate how exposure to fluids, materials (e.g., scale), or stress applied to, reacting with, or otherwise in the presence of the smart carbon coating 64 may be detected (e.g., corrosive fluids, scale-forming fluids, abrasive fluids, and the like),
As discussed with respect to
The electrical monitoring system 96 generally includes one or more electrical sensors 104 that measure or detect the change in the electrical properties of the smart carbon coating 64 due to changes on a surface of the smart coating 64 (e.g., the electrically active carbon region 68 and/or the carbon rich layer 66). In some embodiments, the electrical sensors 104 may include electrical property sensors, multimeters, and other suitable devices capable of measuring a resistance of the smart coating 64, a change in current flowing through the smart carbon coating 64, a change in the dielectric constant of the smart carbon coating 64, and the like, that are indicative of the composition of the smart carbon coating 64. For example, the electrical monitoring system 96 may detect the change in the electrical properties of the smart carbon coating 64 due to a displacement, an elongation, a strain, a force, a stress, a pressure, a surface chemistry including environmental fluid, humidity, contaminants and combinations of such conditions, of the smart carbon coating 64. In general, the electrical monitoring system 96 may be capable detecting such changes inside (e.g., on an interior surface) or outside (e.g., on an exterior surface) of the downhole component that is coated with the smart carbon coating 64.
In any case, the sensor data (e.g., generated by the pressure sensor(s) 102 and electrical sensors 104) may be output to a computing device 108 (e.g., machine) having a processor 110, which may execute instructions stored in memory 112 and/or storage media, or based on inputs provided from a user via the input/output (I/O) device 114. The memory 112 and/or the storage media may be read-only memory (ROM), random-access memory (RAM), flash memory, an optical storage medium, or a hard disk drive, to name but a few examples. For example, in operation, the processor 110 may receive sensor data and/or the visual data, determine that the electrical properties of the smart carbon coating 64 have changed above a threshold indicating a potential of exposure to stress, strain, certain fluids (e.g., water and gases such as carbon dioxide, hydrogen sulfide, hydrogen, any combination thereof, and others), or scale deposition, and send an alert or suitable control signals to take a corrective action.
In some embodiments, the processor 110 of the surface monitoring system 90 may send suitable control signals to a controller 116 (e.g., an external controller) of the subterranean well system 10. In general, the subterranean well system 10 may include machine components or downhole components that control one or more oil and gas operations, as described in
In this way, by enabling the surface monitoring system 90 to monitor and control operation of a subterranean well system 10, the surface monitoring system 90 may be utilized in maintenance or machine health monitoring operations. That is, the surface monitoring system 90 may be capable of receiving data (e.g., the sensor data, the visual data, or both), making a determination about a state or condition of the smart carbon coating 64 (e.g., whether the smart carbon coating 64 has been exposed to an amount of water and other fluids above a threshold), and outputting alerts and control signals that may modify the operation of the subterranean well system 10, such as alerting a user that a component including the smart carbon coating 64 needs to be replaced, halting operations, adjusting a fluid flow via one or more valves, and the like.
The controller 116 associated with the subterranean well system 10 includes a processor 120, which may execute instructions stored in memory 122 and/or storage media 44, or based on inputs provided from a user via the input/output (I/O) device 124. The processor 120 may execute instructions stored in memory 122 and/or storage media, or based on inputs provided from a user via the input/output (I/O) device 124. The memory 122 and/or the storage media 44 may be read-only memory (ROM), random-access memory (RAM), flash memory, an optical storage medium, or a hard disk drive, to name but a few examples. At least in some instances, the processor 110 of the computing device 108 of the surface monitoring system 90 may send the control signals directly to the subterranean well system 10 instead of sending control signals to an external processor (e.g., the processor 120 of the controller 116).
To illustrate one embodiment of the treated carbon region 68 of the smart carbon coating 64,
Additionally, the second pattern 130b of electrically conductive carbon material 70 includes multiple sections or strips 133 of the electrically conductive carbon material 70 arranged along (e.g., parallel with) the second axis 142 (e.g., transverse axis). For example, the first and second axes 132 and 142 may be oriented crosswise (e.g., perpendicular or between 45 to 90 degrees) relative to one another. In the illustrated embodiment, each strip 133 of the electrically conductive carbon material 70 has a length 134 and a width 136. Similar to the first pattern 130a, each strip 133 in the second pattern 130b may be a linear strip, a curved strip, a wavy strip, a multi-angled or zigzagging strip, or any suitable shape. For example, each strip 133 in the second pattern 130b may extend linearly along the second axis 142, wherein the strip 133 has a uniform width 136 along an entirety of the length 134. Additionally, adjacent strips 133 of the electrically conductive carbon material 70 are separated by a distance 140 (e.g., lateral distance in the direction of first axis 132). It should be noted that while only two strips 133 of the electrically conductive carbon material 70 are shown within the second pattern 130b, the smart carbon coating 64 may include three, four, five, six, seven, eight, nine, ten, or more strips 133 of the electrically conductive carbon material 70, each having a respective length 134 and width 136. Furthermore, while only two patterns 130 of the electrically conductive carbon material 70 are shown in
To illustrate another embodiment of the treated carbon region 68 of the smart carbon coating 64,
The pad region 152b is physically and electrically coupled to a second sensing array pattern region 154b of the electrically conductive carbon material 70. The second sensing array pattern region 154b includes a second length 156b (e.g., section or strip) of the electrically conductive carbon material 70 that extends along the first axis 132 and includes multiple branches 158b that extend along the second axis 142. As illustrated, the branches 158b are substantially parallel to each other and the second axis 142. The pad region 152b and the second sensing array pattern region 154b (e.g., including the second length 156b and the branches 158b) are formed of electrically conductive carbon material and, as such, form a continuous electrically conductive pattern.
In the illustrated embodiment, the first sensing array pattern region 154a and the second sensing array pattern region 154b are not physically coupled to each other. Instead, and as illustrated, the first sensing array pattern region 154a and the second sensing array pattern region 154b are separated by intermediate portions of the carbon rich layer 66. As shown, the branches 158a and 158b form an overlapping pattern 160, where the branches 158a and 158b are separated by intermediate portions of the carbon rich layer 66 and overlap along the second axis 142. As illustrated, the overlapping pattern 160 has the branches 158a and 158b arranged in an alternating configuration, wherein one of the branches 158a extends along the second axis 142 between each adjacent pair of the branches 158b. In the illustrated embodiment, the overlapping pattern 160 has an alternating sequence of one branch 158b, one branch 158a, one branch 158b, one branch 158a, one branch 158b, one branch 158a, one branch 158b, one branch 158a, one branch 158b, one branch 158a, one branch 158b, one branch 158a, one branch 158b, one branch 158a, one branch 158b, and one branch 158a, wherein the branches 158a and 158b are parallel and overlap along the second axis 142. In general, the carbon rich layer 66 is generally less conductive than the electrically conductive carbon material 70. As such, if a voltage is applied to the pad region 152a, current may not flow between the first sensing array pattern region 154a and the second sensing array pattern region 154b. However, if a fluid that is more conductive than the carbon rich layer 66 is deposited onto the sensing pattern 150, current may flow between the first sensing array pattern region 154a and the second sensing array pattern region 154b. Accordingly, the sensing pattern 150 shown in
To illustrate another embodiment of the treated carbon region 68 of the smart carbon coating 64,
To illustrate another embodiment of the smart carbon coating 64,
In the illustrated embodiment, the pad region 192b is physically and electrically coupled to a second sensing array pattern region 194b of the electrically conductive carbon material 70. The second sensing array pattern region 194b includes a second curved length 196b (e.g., section or strip) of the electrically conductive carbon material 70 that extends along the first axis 132 and includes multiple branches 198b that extend along the second axis 142. The branches 198b are substantially parallel to each other and the second axis 142. The pad region 192b and the second sensing array pattern region 194b (e.g., including the second curved length 196b and the branches 198b) are formed of electrically conductive carbon material 70 and, as such, form a continuous electrically conductive pattern.
In the illustrated embodiment, the first sensing array pattern region 194a and the second sensing array pattern region 194b are not physically coupled to each other. Instead, and as illustrated, the first sensing array pattern region 194a and the second sensing array pattern region 194b are separated by intermediate portions of the carbon rich layer 66. Furthermore, as shown, the branches 198a and 198b form an overlapping pattern 200, where the branches 198a and 198b are separated by intermediate portions of the carbon rich layer 66 and overlap along the second axis 142. As illustrated, the overlapping pattern 200 has the branches 198a and 198b arranged in an alternating configuration, wherein one of the branches 198a extends along the second axis 142 between each adjacent pair of the branches 198b. In the illustrated embodiment, the overlapping pattern 200 has an alternating sequence of one branch 198b, one branch 198a, one branch 198b, one branch 198a, one branch 198b, one branch 198a, and so forth, wherein the branches 198a and 198b are parallel and overlap along the second axis 142. Additionally, each branch 198a coupled to the first curved length 196a extends toward without contacting the second curved length 196b (e.g., with a first spacing 202a), while each branch 198b coupled to the second curved length 196b extends toward without contacting the first curved length 196a (e.g., with a second spacing 202b). The spacing 202a and the spacing 202b may be the same or substantially the same for each of the branches 198a and 198b. Additionally, the branches 198a and 198b may vary in length along the second axis 142 depending on the position along the first and second curved lengths 196a and 196b, wherein the length of the branches 198a and 198b in middle portions 204a and 204b of the respective first and second curved lengths 196a and 196b is greater than the length of the branches 198a and 198b in end portions 206a and 206b of the respective first and second curved lengths 196a and 196b. In general, the carbon rich layer 66 is generally less conductive than the electrically conductive carbon material 70. As such, if a voltage is applied to the pad region 192a, current may not flow between the first sensing region 194a and the second sensing region 194b. However, if a fluid that is more conductive than the carbon rich layer 66 is deposited onto the sensing pattern 190, current may flow between the first sensing region 194a and the second sensing region 194b. Accordingly, the sensing pattern 190 shown in
To illustrate another embodiment of the treated carbon region 68 of the smart carbon coating 64,
To further illustrate various embodiments of the carbon rich layer 66, Table 1 provides example embodiments of the carbon rich layer 66 produced by a PACVD process, wherein the carbon rich layer 66 has different carbon contents, among others. It should be noted that although the examples are produced by a PACVD process, other suitable processes such as chemical vapor deposition (CVD), physical vapor deposition (PVD), plasma-assisted/plasma-enhanced CVD (PACVD, PECVD), plasma-based ion implantation and deposition (PBII&D), ionized evaporation (IE), sputtering (SP) or others may be used to produce the carbon rich layer 66. For example, an embodiments of the carbon rich layer 66 may have a sp3 carbon content greater than 40%, greater than 45%, greater than 50%, between 40%-60%. Additionally, or alternatively, example embodiments of the carbon rich layer 66 may have a carbon content with a sp2/sp3 ratio less than 1.5, less than 1.0, less than 0.8, less than 0.7, less than 0.6, or between 1.5-0.6, between 1.5-1.0, between 1.0-0.6, and other ranges represented in Table 1. In examples presented in Table 1, the carbon rich layers were produced with a range of thickness between approximately 0.2 μm and 30 μm, and fall under a broad range of designations. These carbon rich layers include hydrogen and silicon. Some of the carbon-rich layers are single layered and other double-layered. As a result of their different deposition process parameters and compositional differences, carbon layers with average Vickers hardness between 925 and 1550 were produced, indirectly causing a range of desirable coefficient of frictions. Because of the carbon film thickness, hardness was converted from Berkovich nano- and micro-indentation tests conducted with a hardness indenter and reported as average of a minimum of ten measurements. A friction coefficient was measured against a standard stainless-steel ball under dry and dynamic conditions as per a procedure modified from ASTM G99. To quantify or determine the relative amounts of sp2 carbon and sp3 carbon, suitable techniques such as X-ray Photoelectron Spectroscopy (XPS) may be used.
The ratios of sp2/sp3 were measured by X-ray Photoelectron Spectroscopy (XPS). The C1s XPS peak was recorded from the surface of the carbon rich layer. The C1s peak was deconvoluted to four Gaussian peaks attributed to sp3 (˜284.5 eV), sp2 (˜285.1 eV), C—O (˜286.8 eV) and C═O (˜288.4 eV). The sp2/sp3 and sp2/(sp3+sp3) were calculated based on their peak areas.
As described herein, treating the carbon rich layers 66 with a laser may produce a treated carbon region 68 having an increased sp2 content relative to the carbon rich layers 66. Table 2 shows exemplary results from laser treating the carbon coating 84, illustrating the increased sp2 content. In Table 2, the sheet electrical resistance is reported as an average of at least 6 consecutive measurements. Sheet electrical resistance was measured using R-check Four Point Sheet Resistance Meter (EDTM). In order to make the measurements consistent from a power level to another, as shown in Table 2, the laser treatment was pre-programmed to create parallel and overlapping treated lines eventually forming a well-defined square region of 645 mm2, that is a treated region with a total area large enough for reliable sheet electrical resistance measurements.
In this example, a 20 W, 450 nm laser was specifically used to form the treated carbon region 68. As shown in Table 2, increasing the laser power reduces the sheet electrical resistance of the carbon coating 84 required to produce the smart carbon coating 64. Furthermore, increasing the laser power increased the relative sp2, which is shown by the increased sp2 percentage and sp2/sp3 a ratio. For example, forming the treated carbon region 68 may conveniently reduce the sheet electrical resistance by less than 1/100 of the sheet electrical resistance of the untreated carbon layers 66. In Table 2, with 70 percent laser power, sheet electrical resistance is as low as 1/400.
To illustrate operation of the embodiments of components of the surface monitoring system 90 described in
At block 232, the surface monitoring system 90 may acquire property data using the electrical monitoring system 96. For example, in an embodiment where the surface monitoring system 90 includes the electrical monitoring system 96, the surface monitoring system 90 may activate electrodes to cause the electrodes of the electrical monitoring system 96 to induce a current (e.g., by applying a voltage) across the smart carbon coating 64 and the electrical monitoring system 96 may acquire data indicative of the electrical property of the smart carbon coating 64 based on the current provided to the one or more smart carbon coating 64. For example, the surface monitoring system 90 may determine a magnitude of the change in the electrical property (e.g., based on a relative change). At block 234, the surface monitoring system 90 may determine whether the substrate 64 has been exposed to fluids, stress (e.g., stress exceeding a threshold), an amount of scale (e.g., a mass of scale), a pressure induced by fluids or a solid material in the like, based on the electrical property data. In some embodiments, the surface monitoring system 90 may determine whether the substrate 64 needs maintenance, or needs to be replaced, based on the electrical property data. For example, the surface monitoring system 90 may determine a change in resistance, and/or other properties as discussed herein, indicative of exposure of a mechanical component having the smart carbon coating 64 to one or more fluids, such as water, carbon dioxide, sour gas, hydrogen, among others. In general, the surface monitoring system 90 may compare the electrical property (e.g., or a corresponding mechanical property such as pressure, as described with respect to
At block 236, the surface monitoring system 90 may generate a damage output (e.g., a mechanical component damage output and/or a component damage output). In general, the damage output may include an audible and/or visual alert (e.g., a notification displayed on a computing device, such as a laptop, mobile device, tablet, or otherwise) or cause a component of the subterranean well system 10 to modify operation. For example, the damage output may be a control signal or activation signal that causes a device utilizing the mechanical component coated with the smart carbon coating 64 to stop operating or change operation or position. As another non-limiting example, the control signal may cause a drill to stop drilling, a valve to open or close, and/or a fluid flow rate to change. In some embodiments, the damage output may be an indication or alert displayed on a computing device, indicating a likelihood that a mechanical component (e.g., a fluid handling component, a well closure component, a mineral extraction component, a hydrocarbon extraction component, a sequestration component, or any combination thereof) has been exposed to fluids. In some embodiments, the notification may indicate a magnitude of the exposure to fluids, material or otherwise that includes a mechanical and/or chemical change of the smart carbon coating 64 (e.g. based on the change in the electrical properties). For example, the alert may warn a user that the mechanical component was likely damaged as well as the extent of the damage (e.g., determined based on a magnitude change or the location of the change in electrical properties) and/or a time period when the vehicle was likely damaged. In some embodiments, the surface monitoring system 90 may determine an estimated time period for subsequent use of the mechanical component coated with the smart carbon coating 64 prior to inspection, repair, or replacement. For example, the surface monitoring system 90 may use a reference table (e.g., storing relationships between a magnitude of exposure and a time for replacement or maintenance) stored in a memory and the magnitude of the exposure to determine the estimate time period. As such, the surface monitoring system 90 may include the estimated time period in the notification or alert.
To illustrate an embodiment of the smart carbon coating monitoring system of
Accordingly, the present disclosure relates to a smart carbon coating 64 that includes carbon rich layer 66 with a treated carbon region 68 with an improved ability to prevent, mitigate, or block scale formation (e.g., scale precipitation) on various equipment, such as downhole components. As discussed herein, it is presently recognized that improved scale mitigation is achieved with a carbon rich layer 66 having one or more regions with a carbon content greater than 40 percent sp3 carbon and/or a sp2/sp3 ratio of the carbon content is less than 1.5, wherein the improved scale mitigation is substantially better than coatings with a carbon content with less than 40 percent sp3 carbon. Furthermore, the treated carbon region 68 may have a relatively low sheet electrical resistance, and thus, function as a circuit on the surface of the smart carbon coating 64 that may be used for detecting exposure of the smart carbon coating 64 or a machine component coated with the smart carbon coating 64 to certain fluids.
This written description uses examples to disclose the subject matter, including the best mode, and also to enable any person skilled in the art to practice the subject matter, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the subject matter is defined by the claims and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal language of the claims.
The techniques presented and claimed herein are referenced and applied to material objects and concrete examples of a practical nature that demonstrably improve the present technical field and, as such, are not abstract, intangible or purely theoretical. Further, if any claims appended to the end of this specification contain one or more elements designated as “means for [perform]ing [a function] . . . ” or “step for [perform]ing [a function] . . . ”, it is intended that such elements are to be interpreted under 35 U.S.C. 112(f). However, for any claims containing elements designated in any other manner, it is intended that such elements are not to be interpreted under 35 U.S.C. 112(f).
