Oil and natural gas wells often utilize wellbore components or tools that, due to their function, are only required to have limited service lives that are considerably less than the service life of the well. After a component or tool service function is complete, it must be removed or disposed of in order to recover the original size of the fluid pathway for use, including hydrocarbon production, CO2 sequestration, etc. Disposal of components or tools has conventionally been done by milling or drilling the component or tool out of the wellbore, which are generally time consuming and expensive operations.
Recently, self-disintegrating downhole tools have been developed. Instead of milling or drilling operations, these tools can be removed by dissolution of engineering materials using various wellbore fluids. One challenge for the self-disintegrating downhole tools is that the disintegration process can start as soon as the conditions in the well allow the corrosion reaction of the engineering material to start. Thus the disintegration period is not controllable as it is desired by the users but rather ruled by the well conditions and product properties. For certain applications, the uncertainly associated with the disintegration period can cause difficulties in well operations and planning. An uncontrolled disintegration can also delay well productions. Therefore, the development of downhole tools that can be disintegrated on-demand is very desirable.
A downhole assembly includes a matrix material and a unit in contact with the matrix material. The unit includes a core having an energetic material, an activator disposed in direct contact with the core, and at least one layer disposed on the core. The activator includes a triggering system having an igniter and a pre-set timer connected in an electrical circuit. The igniter is inactive in an open condition of the electrical circuit, and, after a pre-set time period, the pre-set timer closes the electrical circuit and the igniter is activated.
A method of controllably removing a downhole article of a downhole assembly, the method including: setting a timer of the downhole article for a first time period, the downhole article including a degradable-on-demand material having a matrix material and a unit in contact with the matrix material, the unit including a core formed of an energetic material, a triggering system in direct contact with the core, and at least one layer on the core, the energetic material configured to generate energy upon activation to facilitate the degradation of the downhole article; disposing the downhole assembly in a downhole environment; performing a downhole operation using the downhole article during a second time period shorter than the first time period; activating the energetic material at the end of the first time period using an igniter of the triggering system; and degrading the downhole article.
A downhole assembly including: a tubing string having a flowbore; and, a fluid loss control flapper pivotally connected to the tubing string at a hinge, the flapper formed of a degradable-on-demand material including: a matrix material; and, a unit in contact with the matrix material, the unit including: a core comprising an energetic material; and, an activator disposed in direct contact with the core, the activator including a triggering system having an igniter and a pre-set timer connected in an electrical circuit; wherein the igniter is inactive in an open condition of the electrical circuit, and, after a pre-set time period, the pre-set timer closes the electrical circuit and the igniter is activated.
A frac plug including at least one component formed of a degradable-on-demand material including: a matrix material; and, a unit in contact with the matrix material, the unit including: a core including an energetic material; and, an activator disposed in direct contact with the core, the activator including a triggering system having an igniter and a pre-set timer connected in an electrical circuit; wherein the igniter is inactive in an open condition of the electrical circuit, and, after a pre-set time period, the pre-set timer closes the electrical circuit and the igniter is activated.
The following descriptions should not be considered limiting in any way. With reference to the accompanying drawings, like elements are numbered alike:
The disclosure provides a multilayered unit that can be embedded in a downhole article, attached to a downhole article, or disposed between two adjacent components of a downhole assembly. The downhole article or downhole assembly containing the multilayered unit has controlled degradation, including partial or full disintegration, in a downhole environment. The controlled degradation, and more particularly the controlled disintegration, is implemented through integrating a high-strength matrix material with energetic material that can be triggered on demand for rapid tool disintegration.
The multilayered unit includes a core comprising an energetic material and an activator; a support layer disposed on the core; and a protective layer disposed on the support layer, wherein the support layer and the protective layer each independently comprises a polymeric material, a metallic material, or a combination comprising at least one of the foregoing, provided that the support layer is compositionally different from the protective layer.
The multilayered unit can have various shapes and dimensions. In an embodiment, the multilayered unit has at least one stress concentration location to promote disintegration. As used herein, a stress concentration location refers to a location in an object where stress is concentrated. Examples of stress concentration locations include but are not limited to sharp corners, notches, or grooves. The multilayered unit can have a spherical shape or an angular shape such as a triangle, rhombus, pentagon, hexagon, or the like. The multilayered unit can also be a rod or sheet. The matrix around the multilayered unit can also have stress concentration locations.
The energetic material comprises a thermite, a thermate, a solid propellant fuel, or a combination comprising at least one of the foregoing. The thermite materials include a metal powder (a reducing agent) and a metal oxide (an oxidizing agent), where choices for a reducing agent include aluminum, magnesium, calcium, titanium, zinc, silicon, boron, and combinations including at least one of the foregoing, for example, while choices for an oxidizing agent include boron oxide, silicon oxide, chromium oxide, manganese oxide, iron oxide, copper oxide, lead oxide and combinations including at least one of the foregoing, for example.
Thermate materials comprise a metal powder and a salt oxidizer including nitrate, chromate and perchlorate. For example thermite materials include a combination of barium chromate and zirconium powder; a combination of potassium perchlorate and metal iron powder; a combination of titanium hydride and potassium perchlorate, a combination of zirconium hydride and potassium perchlorate, a combination of boron, titanium powder, and barium chromate, or a combination of barium chromate, potassium perchlorate, and tungsten powder.
Solid propellant fuels may be generated from the thermate compositions by adding a binder that meanwhile serves as a secondary fuel. The thermate compositions for solid propellants include, but not limited to, perchlorate and nitrate, such as ammonium perchlorate, ammonium nitrate, and potassium nitrate. The binder material is added to form a thickened liquid and then cast into various shapes. The binder materials include polybutadiene acrylonitrile (PBAN), hydroxyl-terminated polybutadiene (HTPB), or polyurethane. An exemplary solid propellant fuel includes ammonium perchlorate (NH4ClO4) grains (20 to 200 μm) embedded in a rubber matrix that contains 69-70% finely ground ammonium perchlorate (an oxidizer), combined with 16-20% fine aluminum powder (a fuel), held together in a base of 11-14% polybutadiene acrylonitrile or hydroxyl-terminated polybutadiene (polybutadiene rubber matrix). Another example of the solid propellant fuels includes zinc metal and sulfur powder.
As used herein, the activator is a device that is effective to generate spark, electrical current, or a combination thereof to active the energetic material. The activator can be triggered by a preset timer, characteristic acoustic waves generated by perforations from following stages, a pressure signal from fracking fluid, or an electrochemical signal interacting with the wellbore fluid. Other known methods to activating an energetic material can also be used.
The multilayered unit has a support layer to hold the energetic materials together. The Support layer can also provide structural integrity to the multilayered unit.
The multilayered unit has a protective layer so that the multilayered unit does not disintegrate prematurely during the material fabrication process. In an embodiment, the protective layer has a lower corrosion rate than the support layer when tested under the same testing conditions. The support layer and the protective layer each independently include a polymeric material, a metallic material, or a combination comprising at least one of the foregoing. The polymeric material and the metallic material can corrode once exposed to a downhole fluid, which can be water, brine, acid, or a combination comprising at least one of the foregoing. In an embodiment, the downhole fluid includes potassium chloride (KCl), hydrochloric acid (HCl), calcium chloride (CaCl2), calcium bromide (CaBr2) or zinc bromide (ZnBr2), or a combination comprising at least one of the foregoing.
In an embodiment, the support layer comprises the metallic material, and the protective layer comprises the polymeric material. In another embodiment, the support layer comprises the polymeric material, and the protective layer comprises the metallic material. In yet another embodiment, both the support layer and the protective layer comprise a polymeric material. In still another embodiment, both the support layer and the protective layer comprise a metallic material.
Exemplary polymeric materials include a polyethylene glycol, a polypropylene glycol, a polyglycolic acid, a polycaprolactone, a polydioxanone, a polyhydroxyalkanoate, a polyhydroxybutyrate, a copolymer thereof, or a combination comprising at least one of the foregoing.
The metallic material can be a corrodible metallic material, which includes a metal, a metal composite, or a combination comprising at least one of the foregoing. As used herein, a metal includes metal alloys.
Exemplary corrodible metallic materials include zinc metal, magnesium metal, aluminum metal, manganese metal, an alloy thereof, or a combination comprising at least one of the foregoing. In addition to zinc, magnesium, aluminum, manganese, or alloys thereof, the corrodible material can further comprise a cathodic agent such as Ni, W, Mo, Cu, Fe, Cr, Co, an alloy thereof, or a combination comprising at least one of the foregoing to adjust the corrosion rate of the corrodible material. The corrodible material (anode) and the cathodic agent are constructed on the microstructural level to form μm-scale galvanic cells (micro-galvanic cells) when the material are exposed to an electrolytic fluid such as downhole brines. The cathodic agent has a standard reduction potential higher than −0.6 V. The net cell potential between the corrodible material and cathodic agent is above 0.5 V, specifically above 1.0 V.
Magnesium alloy is specifically mentioned. Magnesium alloys suitable for use include alloys of magnesium with aluminum (Al), cadmium (Cd), calcium (Ca), cobalt (Co), copper (Cu), iron (Fe), manganese (Mn), nickel (Ni), silicon (Si), silver (Ag), strontium (Sr), thorium (Th), tungsten (W), zinc (Zn), zirconium (Zr), or a combination comprising at least one of these elements. Particularly useful alloys include magnesium alloyed with Ni, W, Co, Cu, Fe, or other metals. Alloying or trace elements can be included in varying amounts to adjust the corrosion rate of the magnesium. For example, four of these elements (cadmium, calcium, silver, and zinc) have to mild-to-moderate accelerating effects on corrosion rates, whereas four others (copper, cobalt, iron, and nickel) have a still greater effect on corrosion. Exemplary commercial magnesium alloys which include different combinations of the above alloying elements to achieve different degrees of corrosion resistance include but are not limited to, for example, those alloyed with aluminum, strontium, and manganese such as AJ62, AJ50x, AJ51x, and AJ52x alloys, and those alloyed with aluminum, zinc, and manganese such as AZ91A-E alloys.
As used herein, a metal composite refers to a composite having a substantially-continuous, cellular nanomatrix comprising a nanomatrix material; a plurality of dispersed particles comprising a particle core material that comprises Mg, Al, Zn or Mn, or a combination thereof, dispersed in the cellular nanomatrix; and a solid-state bond layer extending throughout the cellular nanomatrix between the dispersed particles. The matrix comprises deformed powder particles formed by compacting powder particles comprising a particle core and at least one coating layer, the coating layers joined by solid-state bonding to form the substantially-continuous, cellular nanomatrix and leave the particle cores as the dispersed particles. The dispersed particles have an average particle size of about 5 μm to about 300 μm. The nanomatrix material comprises Al, Zn, Mn, Mg, Mo, W, Cu, Fe, Si, Ca, Co, Ta, Re or Ni, or an oxide, carbide or nitride thereof, or a combination of any of the aforementioned materials. The chemical composition of the nanomatrix material is different than the chemical composition of the particle core material.
The corrodible metallic material can be formed from coated particles such as powders of Zn, Mg, Al, Mn, an alloy thereof, or a combination comprising at least one of the foregoing. The powder generally has a particle size of from about 50 to about 150 micrometers, and more specifically about 5 to about 300 micrometers, or about 60 to about 140 micrometers. The powder can be coated using a method such as chemical vapor deposition, anodization or the like, or admixed by physical method such cryo-milling, ball milling, or the like, with a metal or metal oxide such as Al, Ni, W, Co, Cu, Fe, oxides of one of these metals, or the like. The coating layer can have a thickness of about 25 nm to about 2,500 nm. Al/Ni and Al/W are specific examples for the coating layers. More than one coating layer may be present. Additional coating layers can include Al, Zn, Mg, Mo, W, Cu, Fe, Si, Ca, Co, Ta, or Re. Such coated magnesium powders are referred to herein as controlled electrolytic materials (CEM). The CEM materials are then molded or compressed forming the matrix by, for example, cold compression using an isostatic press at about 40 to about 80 ksi (about 275 to about 550 MPa), followed by forging or sintering and machining, to provide a desired shape and dimensions of the disintegrable article. The CEM materials including the composites formed therefrom have been described in U.S. Pat. Nos. 8,528,633 and 9,101,978.
In an embodiment, the metallic material comprises Al, Mg, Zn. Mn, Fe, an alloy thereof, or a combination comprising at least one of the foregoing. In specific embodiments, the metallic material comprises aluminum alloy, magnesium alloy, zinc alloy, iron alloy, or a combination comprising at least one of the foregoing. In the instance wherein both the support layer and the protective layer comprise a metallic material, the metallic materials in the support layer and the protective layer are selected such that the support layer and the protective layer are easier to disintegrate when the energetic material is activated as compared to an otherwise identical unit except for containing only one metallic layer.
The core is present in an amount of about 5 to about 80 vol %, specifically about 15 to about 70 vol %; the support layer is present in an amount of about 20 to about 95 vol %, specifically about 30 to about 85; and the protective layer is present in an amount of about 0.1 to about 20 vol %, specifically about 1 to about 10 vol %, each based on the total volume of the multilayered unit.
The multilayered units can be embedded into different tools. The location and number of MLM units are selected to ensure that the whole tool can disintegrate into multiple pieces when the energetic material is activated. Thus in an embodiment, the disclosure provides a degradable article, and in particular a disintegrable article, comprising a matrix and a multilayered unit embedded therein. The matrix of the article can be formed from a corrodible metallic material as described herein. The matrix can further comprise additives such as carbides, nitrides, oxides, precipitates, dispersoids, glasses, carbons, or the like in order to control the mechanical strength and density of the articles if needed. In an embodiment, the matrix has pre-cracks including but not limited to pre-crack notches or pre-crack grooves around the multilayered unit to facilitate the quick degradation, and in particular the quick disintegration, of the article once the energetic material is activated.
Degradable articles, and in particular disintegrable articles, are not particularly limited. Exemplary articles include a ball, a ball seat, a fracture plug, a bridge plug, a wiper plug, shear out plugs, a debris barrier, an atmospheric chamber disc, a swabbing element protector, a sealbore protector, a screen protector, a beaded screen protector, a screen basepipe plug, a drill in stim liner plug, ICD plugs, a flapper valve, a gaslift valve, a transmatic CEM plug, float shoes, darts, diverter balls, shifting/setting balls, ball seats, sleeves, teleperf disks, direct connect disks, drill-in liner disks, fluid loss control flappers, shear pins or screws, cementing plugs, teleperf plugs, drill in sand control beaded screen plugs, HP beaded frac screen plugs, hold down dogs and springs, a seal bore protector, a stimcoat screen protector, or a liner port plug. In specific embodiments, the disintegrable article is a ball, a fracture plug, or a bridge plug.
A downhole assembly comprising a downhole article having a multilayered unit embedded therein is also provided. More than one component of the downhole article can be an article having embedded multilayered units.
The multilayered units can also be disposed on a surface of an article. In an embodiment, a downhole assembly comprises a first component and a multilayered unit disposed on a surface of the first component. The downhole assembly further comprises a second component, and the multilayer unit is disposed between the first and second components. The first component, the second component, or both can comprise corrodible metallic material as disclosed herein. Exemplary downhole assemblies include frac plugs, bridge plugs, and the like.
Referring to
A method of controllably removing a downhole article or a downhole assembly comprises disposing a downhole article or a downhole assembly as described herein in a downhole environment; performing a downhole operation; activating the energetic material; and degrading, including full or partially disintegrating, the downhole article. A downhole operation can be any operation that is performed during drilling, stimulation, completion, production, or remediation. A fracturing operation is specifically mentioned. To start an on-demand degradation process, one multilayered unit is triggered and other units will continue the rapid degradation process following a series of sequenced reactions. The sequenced reactions might be triggered by pre-set timers in different units. Alternatively, the energetic material in one unit is activated and reacts to generate heat, strain, vibration, an acoustic signal or the like, which can be sensed by an adjacent unit and activate the energetic material in the adjacent unit. The energetic material in the adjacent unit reacts and generates a signal that leads to the activation of the energetic material in an additional unit. The process repeats and sequenced reactions occur.
Disintegrating the downhole article comprises breaking the downhole article into a plurality of discrete pieces. Advantageously, the discrete pieces can further corrode in the downhole fluid and eventually completely dissolve in the downhole fluid or become smaller pieces which can be carried back to the surface by wellbore fluids.
In one embodiment, the triggering system 112 includes an igniter 114 arranged to directly ignite the energetic material in the core 14. The igniter 114 may also directly ignite another material that then ignites the core 14. In either case, the core 14 is ignited. In the illustrated embodiment, the triggering system 112 further includes an electrical circuit 116. In
Various embodiments of the disclosure include a downhole article including: a matrix; and a multilayered unit disposed in the matrix, the multilayered unit including: a core comprising an energetic material and an activator; a support layer disposed on the core; and a protective layer disposed on the support layer, wherein the support layer and the protective layer each independently comprises a polymeric material, a metallic material, or a combination comprising at least one of the foregoing, provided that the support layer is compositionally different from the protective layer. In any prior embodiment or combination of embodiments, the multilayered unit has at least one stress concentration location. In any prior embodiment or combination of embodiments, the matrix has a pre-crack around the multilayered unit. In any prior embodiment or combination of embodiments, the activator is a device that is effective to generate spark, electrical current, or a combination thereof to active the energetic material. In any prior embodiment or combination of embodiments, the energetic material includes a thermite, a thermate, a solid propellant fuel, or a combination including at least one of the foregoing. In any prior embodiment or combination of embodiments, the metallic material includes Zn, Mg, Al, Mn, iron, an alloy thereof, or a combination comprising at least one of the foregoing. In any prior embodiment or combination of embodiments, the polymeric material comprises a polyethylene glycol, a polypropylene glycol, a polyglycolic acid, a polycaprolactone, a polydioxanone, a polyhydroxyalkanoate, a polyhydroxybutyrate, a copolymer thereof, or a combination including at least one of the foregoing. In any prior embodiment or combination of embodiments, the support layer includes the metallic material; and the protective layer includes the polymeric material. In any prior embodiment or combination of embodiments, the support layer includes the polymeric material; and the protective layer includes the metallic material. In any prior embodiment or combination of embodiments, the core is present in an amount of 5 to 80 vol %, the support layer is present in an amount of 20 to 95 vol %, and the protective layer is present in an amount of 0.1 to 20 vol %, each based on the total volume of the multilayered unit. In any prior embodiment or combination of embodiments, a downhole assembly includes the downhole article.
Various embodiments of the disclosure further include a downhole assembly including a first component and a multilayered unit disposed on a surface of the first component, the multilayered unit including: a core comprising an energetic material and an activator; a support layer disposed on the core; and a protective layer disposed on the support layer, wherein the support layer and the protective layer each independently includes a polymeric material, a metallic material, or a combination comprising at least one of the foregoing, provided that the support layer is compositionally different from the protective layer. In any prior embodiment or combination of embodiments, the downhole assembly further includes a second component, and the multilayer unit is disposed between the first and second components. In any prior embodiment or combination of embodiments, the activator is a device that is effective to generate spark, electrical current, or a combination thereof to active the energetic material. In any prior embodiment or combination of embodiments, the first component, the second component, or both include Zn, Mg, Al, Mn, an alloy thereof, or a combination comprising at least one of the foregoing. In any prior embodiment or combination of embodiments, the multilayered unit has at least one stress concentration location. In any prior embodiment or combination of embodiments, the polymeric material comprises a polyethylene glycol, a polypropylene glycol, a polyglycolic acid, a polycaprolactone, a polydioxanone, a polyhydroxyalkanoate, a polyhydroxybutyrate, a copolymer thereof, or a combination including at least one of the foregoing.
Various embodiments of the disclosure further include a method of controllably removing a downhole article, the method including: disposing a downhole article of any one of the previous embodiments in a downhole environment; performing a downhole operation; activating the energetic material; and disintegrating the downhole article. In any prior embodiment or combination of embodiments, disintegrating the downhole article comprises breaking the downhole article into a plurality of discrete pieces; and the method further includes corroding the discrete pieces in a downhole fluid. In any prior embodiment or combination of embodiments, activating the energetic material includes triggering the activator by a preset timer, a characteristic acoustic wave generated by a perforation from a following stage, a pressure signal from fracking fluid, an electrochemical signal interacting with a wellbore fluid, or a combination comprising at least one of the foregoing.
Various embodiments of the disclosure further include a method of controllably removing a downhole assembly, the method including: disposing a downhole assembly of any one of the previous embodiments in a downhole environment; performing a downhole operation; activating the energetic material in the multilayered unit; and disintegrating the downhole assembly. In any prior embodiment or combination of embodiments, disintegrating the downhole assembly comprises breaking the downhole assembly into a plurality of discrete pieces; and the method further includes corroding the discrete pieces in a downhole fluid. In any prior embodiment or combination of embodiments, activating the energetic material comprises triggering the activator by a preset timer, a characteristic acoustic wave generated by a perforation from a following stage, a pressure signal from fracking fluid, an electrochemical signal interacting with a wellbore fluid, or a combination comprising at least one of the foregoing.
Set forth below are various embodiments of the disclosure.
A downhole assembly includes a matrix material; and, a unit in contact with the matrix material, the unit including: a core comprising an energetic material; an activator disposed in direct contact with the core, the activator including a triggering system having an igniter and a pre-set timer connected in an electrical circuit; and, at least one layer disposed on the core; wherein the igniter is inactive in an open condition of the electrical circuit, and, after a pre-set time period, the pre-set timer closes the electrical circuit and the igniter is activated.
The downhole assembly as in any prior embodiment or combination of embodiments, wherein the matrix material and the unit are packaged together in a self-contained downhole tool.
The downhole assembly as in any prior embodiment or combination of embodiments, wherein the electrical circuit further includes a battery, the battery arranged to provide electric current to set off the igniter in a closed condition of the circuit.
The downhole assembly as in any prior embodiment or combination of embodiments, wherein the timer includes a battery separate from the battery arranged to provide electric current to set off the igniter.
The downhole assembly as in any prior embodiment or combination of embodiments, wherein the matrix material is included in at least one component of a frac plug or in a flapper.
The downhole assembly as in any prior embodiment or combination of embodiments, further comprising a plurality of the units in contact with the matrix material.
The downhole assembly as in any prior embodiment or combination of embodiments, wherein the matrix material has a cellular nanomatrix, a plurality of dispersed particles dispersed in the cellular nanomatrix, and a solid-state bond layer extending through the cellular nanomatrix between the dispersed particles.
The downhole assembly as in any prior embodiment or combination of embodiments, wherein the unit is a multi-layered unit and the at least one layer includes a support layer disposed on the core; and a protective layer disposed on the support layer, wherein the support layer and the protective layer each independently comprises a polymeric material, a metallic material, or a combination comprising at least one of the foregoing, provided that the support layer is compositionally different from the protective layer.
The downhole assembly as in any prior embodiment or combination of embodiments, wherein the support layer comprises the metallic material; and the protective layer comprises the polymeric material.
The downhole assembly as in any prior embodiment or combination of embodiments, wherein the unit has at least one stress concentration location and/or the matrix has a pre-crack around the unit.
The downhole assembly as in any prior embodiment or combination of embodiments, wherein the energetic material comprises a thermite, a thermate, a solid propellant fuel, or a combination comprising at least one of the foregoing.
The downhole assembly as in any prior embodiment or combination of embodiments, wherein the at least one layer separates the matrix material from the unit.
The downhole assembly as in any prior embodiment or combination of embodiments, wherein the activator is disposed within the core.
A method of controllably removing a downhole tool, the method including setting the timer of the downhole assembly of any prior embodiment or combination of embodiments, for a first time period at a surface location; disposing the downhole assembly in a downhole environment; completing a downhole operation using the downhole tool within a second time period less than the first time period, the downhole tool formed at least partially of the matrix material; closing the electrical circuit upon completion of the first time period to activate the igniter; and activating the energetic material by the igniter and degrading the matrix material of the downhole tool.
A method of controllably removing a downhole article of a downhole assembly, the method including: setting a timer of the downhole article for a first time period, the downhole article including a degradable-on-demand material having a matrix material and a unit in contact with the matrix material, the unit including a core formed of an energetic material, a triggering system in direct contact with the core, and at least one layer on the core, the energetic material configured to generate energy upon activation to facilitate the degradation of the downhole article; disposing the downhole assembly in a downhole environment; performing a downhole operation using the downhole article during a second time period shorter than the first time period; activating the energetic material at the end of the first time period using an igniter of the triggering system; and degrading the downhole article.
The method as in any prior embodiment or combination of embodiments, wherein the triggering system includes an electrical circuit that further includes the igniter and a battery, and at the end of the first time period, the timer closes the electrical circuit and the battery provides electric current to activate the igniter.
The method as in any prior embodiment or combination of embodiments, wherein the triggering system is disposed within the core.
A downhole assembly including: a tubing string having a flowbore; and, a fluid loss control flapper pivotally connected to the tubing string at a hinge, the flapper formed of a degradable-on-demand material including: a matrix material; and, a unit in contact with the matrix material, the unit including: a core comprising an energetic material; and, an activator disposed in direct contact with the core, the activator including a triggering system having an igniter and a pre-set timer connected in an electrical circuit; wherein the igniter is inactive in an open condition of the electrical circuit, and, after a pre-set time period, the pre-set timer closes the electrical circuit and the igniter is activated.
The downhole assembly as in any prior embodiment or combination of embodiments, further comprising at least one layer disposed on the core, the at least one layer separating the matrix material from the core.
The downhole assembly as in any prior embodiment or combination of embodiments, wherein the activator is disposed within the core, and the unit is disposed within the flapper.
A frac plug including at least one component formed of a degradable-on-demand material including: a matrix material; and, a unit in contact with the matrix material, the unit including: a core including an energetic material; and, an activator disposed in direct contact with the core, the activator including a triggering system having an igniter and a pre-set timer connected in an electrical circuit; wherein the igniter is inactive in an open condition of the electrical circuit, and, after a pre-set time period, the pre-set timer closes the electrical circuit and the igniter is activated.
The frac plug as in any prior embodiment or combination of embodiments, wherein the at least one component is at least one first component, and further comprising at least one second component formed of the matrix material, the at least one second component not including the unit, and the at least one second component in contact with the at least one first component.
All ranges disclosed herein are inclusive of the endpoints, and the endpoints are independently combinable with each other. As used herein, “combination” is inclusive of blends, mixtures, alloys, reaction products, and the like. All references are incorporated herein by reference in their entirety.
The use of the terms “a” and “an” and “the” and similar referents in the context of describing the invention (especially in the context of the following claims) are to be construed to cover both the singular and the plural, unless otherwise indicated herein or clearly contradicted by context. “Or” means “and/or.” The modifier “about” used in connection with a quantity is inclusive of the stated value and has the meaning dictated by the context (e.g., it includes the degree of error associated with measurement of the particular quantity). Further, it should further be noted that the terms “first,” “second,” and the like herein do not denote any order, quantity, or importance, but rather are used to distinguish one element from another.
The teachings of the present disclosure apply to downhole assemblies and downhole tools that may be used in a variety of well operations. These operations may involve using one or more treatment agents to treat a formation, the fluids resident in a formation, a wellbore, and/or equipment in the wellbore, such as production tubing. The treatment agents may be in the form of liquids, gases, solids, semi-solids, and mixtures thereof. Illustrative treatment agents include, but are not limited to, fracturing fluids, acids, steam, water, brine, anti-corrosion agents, cement, permeability modifiers, drilling muds, emulsifiers, demulsifiers, tracers, flow improvers etc. Illustrative well operations include, but are not limited to, hydraulic fracturing, stimulation, tracer injection, cleaning, acidizing, steam injection, water flooding, cementing, etc.
While the invention has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the claims. Also, in the drawings and the description, there have been disclosed exemplary embodiments of the invention and, although specific terms may have been employed, they are unless otherwise stated used in a generic and descriptive sense only and not for purposes of limitation, the scope of the invention therefore not being so limited.
The present application is a continuation-in-part of U.S. patent application Ser. No. 15/472,382, filed Mar. 29, 2017, which is hereby incorporated by reference in its entirety.
Number | Date | Country | |
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Parent | 15472382 | Mar 2017 | US |
Child | 15599101 | US |