NO20160544A1

NO20160544A1 - Downhole flow inhibition tool and method of unplugging a seat

Info

Publication number: NO20160544A1
Application number: NO20160544A
Authority: NO
Inventors: Zhiyue Xu; Michael H Johnson
Original assignee: Baker Hughes Inc
Priority date: 2013-10-01
Filing date: 2016-04-06
Publication date: 2016-04-06
Also published as: AU2014329957A1; GB2538622A; AU2014329957B2; CA2926044A1; CA2926044C; WO2015050678A1

Description

DOWNHOLE FLOW INHIBITION TOOL AND METHOD OF UNPLUGGING A SEAT

CROSS REFERENCE TO RELATED APPLICATIONS

[0001] This application claims the benefit of U.S. Application No. 14/043425, filed on October 1, 2013, which is incorporated herein by reference in its entirety.

BACKGROUND

[0002] In the drilling and completion industry it is often desirable to utilize what is known to the art as tripping balls, darts, (generically plugs) for a number of different operations requiring pressure up events. As is known to one of skill in the art, tripping balls are dropped at selected times to seat in a downhole ball seat and create a seal there. The seal that is created is often intended to be temporary. After the operation for which the tripping ball was dropped is completed, the ball is removed from the wellbore by methods such as reverse circulating the ball out of the well. Doing so, however, requires that the ball dislodge from the seat. At times balls can become stuck to a seat thereby preventing it from being circulated out of the well, thereby requiring more time consuming and costly methods of removing the ball, such as, through drilling the ball out, for example. Devices and methods that allow an operator to remove a ball without resorting to such a costly process would be well received by the art.

SUMMARY

[0003] Disclosed herein is a downhole flow inhibition tool. The tool includes at least a first component and a mating component at least a portion of one of the first component and the mating component is dissolvable in a target environment to reduce flow inhibition upon dissolution of the at least a portion.

[0004] Further disclosed herein is a method of unplugging a seat. The method includes dissolving at least a surface defined by a shell surrounding a core of a plug seated against the seat, unseating the plug from the seat, dimensioning the core to fit through the seat without necessarily dissolving the core, and passing the core through the seat.

BRIEF DESCRIPTION OF THE DRAWINGS

[0005] Referring now to the drawings wherein like elements are numbered alike in the several Figures:

[0006] FIG. 1 is a photomicrograph of a powder 10 as disclosed herein that has been embedded in an epoxy specimen mounting material and sectioned;

[0007] FIG. 2 is a schematic illustration of an exemplary embodiment of a powder particle 12 as it would appear in an exemplary section view represented by section 2-2 of FIG. 1;

[0008] FIG. 3 is a schematic illustration of a second exemplary embodiment of a powder particle 12 as it would appear in a second exemplary section view represented by section 2-2 of FIG. 1;

[0009] FIG. 4 is a schematic illustration of a third exemplary embodiment of a powder particle 12 as it would appear in a third exemplary section view represented by section 2-2 of FIG. 1;

[0010] FIG. 5 is a schematic illustration of a fourth exemplary embodiment of a powder particle 12 as it would appear in a fourth exemplary section view represented by section 2-2 of FIG. 1;

[0011] FIG. 6 is a schematic illustration of a second exemplary embodiment of a powder as disclosed herein håving a multi-modal distribution of particle sizes;

[0012] FIG. 7 is a schematic illustration of a third exemplary embodiment of a powder as disclosed herein håving a multi-modal distribution of particle sizes;

[0013] FIG. 8 is a flow chart of an exemplary embodiment of a method of making a powder as disclosed herein;

[0014] FIG. 9 is a photomicrograph of an exemplary embodiment of a powder compact as disclosed herein;

[0015] FIG. 10 is a schematic of illustration of an exemplary embodiment of a powder compact of FIG. 9 made using a powder håving single-layer coated powder particles as it would appear tåken along section 10-10;

[0016] FIG. 11 is a schematic illustration of an exemplary embodiment of a powder compact as disclosed herein håving a homogenous multi-modal distribution of particle sizes;

[0017] FIG. 12 is a schematic illustration of an exemplary embodiment of a powder compact as disclosed herein håving a non-homogeneous, multi-modal distribution of particle sizes;

[0018] FIG. 13 is a schematic illustration of an exemplary embodiment of a powder compact as disclosed herein formed from a first powder and a second powder and håving a homogenous multi-modal distribution of particle sizes;

[0019] FIG. 14 is a schematic illustration of an exemplary embodiment of a powder compact as disclosed herein formed from a first powder and a second powder and håving a non-homogeneous multi-modal distribution of particle sizes.

[0020] FIG. 15 is a schematic of illustration of another exemplary embodiment of the powder compact of FIG. 9 made using a powder håving multilayer coated powder particles as it would appear tåken along section 10-10;

[0021] FIG. 16 is a schematic cross-sectional illustration of an exemplary embodiment of a precursor powder compact;

[0022] FIG. 17 is a flow chart of an exemplary embodiment of a method of making a powder compact as disclosed herein;

[0023] FIG. 18 is a tab le that describes the particle core and metallic coating layer configurations for powder particles and powders used to make exemplary embodiments of powder compacts for testing as disclosed herein;

[0024] FIG. 19 a plot of the compressive strength of the powder compacts of FIG. 18 both dry and in an aqueous solution comprising 3% KC1;

[0025] FIG. 20 is a plot of the rate of corrosion (ROC) of the powder compacts of FIG. 18 in an aqueous solution comprising 3% KC1 at 200°F and room temperature;

[0026] FIG. 21 is a plot of the ROC of the powder compacts of FIG. 18 in 15% HC1;

[0027] FIG. 22 is a schematic illustration of a change in a property of a powder compact as disclosed herein as a function of time and a change in condition of the powder compact environment;

[0028] FIG. 23 is an electron photomicrograph of a fracture surface of a powder compact formed from a pure Mg powder;

[0029] FIG. 24 is an electron photomicrograph of a fracture surface of an exemplary embodiment of a powder metal compact as described herein;

[0030] FIG. 25 is a plot of compressive strength of a powder compact as a function the amount of a constituent (AI2O3) of the cellular nanomatrix;

[0031] FIG. 26 depicts a cross sectional view of a plug disclosed herein within a tubular; and

[0032] FIG. 27 depicts a cross sectional view of an alternate plug disclosed herein.

DETAILED DESCRIPTION

[0033] Lightweight, high-strength metallic materials are disclosed that may be used in a wide variety of applications and application environments, including use in various wellbore environments to make various selectably and controllably disposable or degradable lightweight, high-strength downhole tools 610, 710 (Figures 26 and 27) or other downhole components, as well as many other applications for use in both durable and disposable or degradable articles. Such downhole tools include, frac plugs, bridge plugs, wiper plugs, shear out plugs, debris barriers, atmospheric chamber discs, swabbing element protectors, sealbore protectors, screen protectors, beaded screen protectors, screen basepipe plugs, drill in stim liner plugs, ICD plugs, flapper valves, gaslift valves, Transmatic CEM™ plugs, 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, and cementing plugs.

[0034] These lightweight, high-strength and selectably and controllably degradable materials include fUlly-dense, sintered powder compacts formed from coated powder materials that include various lightweight particle cores and core materials håving various single layer and multilayer nanoscale coatings. These powder compacts are made from coated metallic powders that include various electrochemically-active (e.g., håving relatively higher standard oxidation potentials) lightweight, high-strength particle cores and core materials, such as electrochemically active metals, that are dispersed within a cellular nanomatrix formed from the various nanoscale metallic coating layers of metallic coating materials, and are particularly useful in wellbore applications. These powder compacts provide a unique and advantageous combination of mechanical strength properties, such as compression and shear strength, low density and selectable and controllable corrosion properties, particularly rapid and controlled dissolution in various wellbore fluids. For example, the particle core and coating layers of these powders may be selected to provide sintered powder compacts suitable for use as high strength engineered materials håving a compressive strength and shear strength comparable to various other engineered materials, including carbon, stainless and alloy steels, but which also have a low density comparable to various polymers, elastomers, low-density porous ceramics and composite materials. As yet another example, these powders and powder compact materials may be configured to provide a selectable and controllable degradation or disposal in response to a change in an environmental condition, such as a transition from a very low dissolution rate to a very rapid dissolution rate in response to a change in a property or condition of a wellbore proximate an article formed from the compact, including a property change in a wellbore fluid that is in contact with the powder compact. The selectable and controllable degradation or disposal characteristics described also allow the dimensional stability and strength of articles, such as wellbore tools or other components, made from these materials to be maintained until they are no longer needed, at which time a predetermined environmental condition, such as a wellbore condition, including wellbore fluid temperature, pressure or pH value, may be changed to promote their removal by rapid dissolution. These coated powder materials and powder compacts and engineered materials formed from them, as well as methods of making them, are described further below.

[0035] Referring to FIGS. 1-5, a metallic powder 10 includes a plurality of metallic, coated powder particles 12. Powder particles 12 may be formed to provide a powder 10, including free-flowing powder, that may be poured or otherwise disposed in all manner of forms or molds (not shown) håving all manner of shapes and sizes and that may be used to fashion precursor powder compacts 100 (FIG. 16) and powder compacts 200 (FIGS. 10-15), as described herein, that may be used as, or for use in manufacturing, various articles of manufacture, including various wellbore tools and components.

[0036] Each of the metallic, coated powder particles 12 of powder 10 includes a particle core 14 and a metallic coating layer 16 disposed on the particle core 14. The particle core 14 includes a core material 18. The core material 18 may include any suitable material for forming the particle core 14 that provides powder particle 12 that can be sintered to form a lightweight, high-strength powder compact 200 håving selectable and controllable dissolution characteristics. Suitable core materials include electrochemically active metals håving a standard oxidation potential greater than or equal to that of Zn, including as Mg, Al, Mn or Zn or a combination thereof. These electrochemically active metals are very reactive with a number of common wellbore fluids, including any number of ionic fluids or highly polar fluids, such as those that contain various chlorides. Examples include fluids comprising potassium chloride (KO), hydrochloric acid (HO), calcium chloride (CaCb), calcium bromide (Calfø) or zinc bromide (Znlfø). Core material 18 may also include other metals that are less electrochemically active than Zn or non-metallic materials, or a combination thereof. Suitable non-metallic materials include ceramics, composites, glasses or carbon, or a combination thereof. Core material 18 may be selected to provide a high dissolution rate in a predetermined wellbore fluid, but may also be selected to provide a relatively low dissolution rate, including zero dissolution, where dissolution of the nanomatrix material causes the

particle core 14 to be rapidly undermined and liberated from the particle compact at the

interface with the wellbore fluid, such that the effective rate of dissolution of particle compacts made using particle cores 14 of these core materials 18 is high, even though core material 18 itself may have a low dissolution rate, including core materials 20 that may be substantially insoluble in the wellbore fluid.

[0037] With regard to the electrochemically active metals as core materials 18, including Mg, Al, Mn or Zn, these metals may be used as pure metals or in any combination with one another, including various alloy combinations of these materials, including binary, tertiary, or quaternary alloys of these materials. These combinations may also include composites of these materials. Further, in addition to combinations with one another, the Mg, Al, Mn or Zn core materials 18 may also include other constituents, including various alloying additions, to alter one or more properties of the particle cores 14, such as by improving the strength, lowering the density or altering the dissolution characteristics of the core material 18.

[0038] Among the electrochemically active metals, Mg, either as a pure metal or an alloy or a composite material, is particularly useful, because of its low density and ability to

form high-strength alloys, as well as its high degree of electro chemical activity, since it has a standard oxidation potential higher than Al, Mn or Zn. Mg alloys include all alloys that have Mg as an alloy constituent. Mg alloys that combine other electrochemically active metals, as described herein, as alloy constituents are particularly useful, including binary Mg-Zn, Mg-Al and Mg-Mn alloys, as well as tertiary Mg-Zn-Y and Mg-Al-X alloys, where X includes Zn, Mn, Si, Ca or Y, or a combination thereof. These Mg-Al-X alloys may include, by weight, up to about 85% Mg, up to about 15% Al and up to about 5% X. Particle core 14 and core material 18, and particularly electrochemically active metals including Mg, Al, Mn or Zn, or combinations thereof, may also include a rare earth element or combination of rare earth elements. As used herein, rare earth elements include Sc, Y, La, Ce, Pr, Nd or Er, or a combination of rare earth elements. Where present, a rare earth element or combinations of rare earth elements may be present, by weight, in an amount of about 5% or less.

[0039] Particle core 14 and core material 18 have a melting temperature (Tp). As used herein, Tp includes the lowest temperature at which incipient melting or liquation or other forms of partial melting occur within core material 18, regardless of whether core material 18 comprises a pure metal, an alloy with multiple phases håving different melting temperatures or a composite of materials håving different melting temperatures.

[0040] Particle cores 14 may have any suitable particle size or range of particle sizes or distribution of particle sizes. For example, the particle cores 14 may be selected to provide an average particle size that is represented by a normal or Gaussian type unimodal distribution around an average or mean, as illustrated generally in FIG. 1. In another example, particle cores 14 may be selected or mixed to provide a multimodal distribution of particle sizes, including a plurality of average particle core sizes, such as, for example, a homogeneous bimodal distribution of average particle sizes, as illustrated generally and schematically in FIG. 6. The selection of the distribution of particle core size may be used to determine, for example, the particle size and interparticle spacing 15 of the particles 12 of powder 10. In an exemplary embodiment, the particle cores 14 may have a unimodal distribution and an average particle diameter of about 5(xm to about 300(xm, more particularly about 80(xmto about 120(xm, and even more particularly about 100(xm.

[0041] Particle cores 14 may have any suitable particle shape, including any regular or irregular geometric shape, or combination thereof. In an exemplary embodiment, particle cores 14 are substantially spheroidal electrochemically active metal particles. In another exemplary embodiment, particle cores 14 are substantially irregularly shaped ceramic particles. In yet another exemplary embodiment, particle cores 14 are carbon or other nanotube structures or hollow glass microspheres.

[0042] Each of the metallic, coated powder particles 12 of powder 10 also includes a metallic coating layer 16 that is disposed on particle core 14. Metallic coating layer 16 includes a metallic coating material 20. Metallic coating material 20 gives the powder particles 12 and powder 10 its metallic nature. Metallic coating layer 16 is a nanoscale coating layer. In an exemplary embodiment, metallic coating layer 16 may have a thickness of about 25nm to about 2500nm. The thickness of metallic coating layer 16 may vary over the surface of particle core 14, but will preferably have a substantially uniform thickness over the surface of particle core 14. Metallic coating layer 16 may include a single layer, as illustrated in FIG. 2, or a plurality of layers as a multilayer coating structure, as illustrated in FIGS. 3-5 for up to four layers. In a single layer coating, or in each of the layers of a multilayer coating, the metallic coating layer 16 may include a single constituent chemical element or compound, or may include a plurality of chemical elements or compounds. Where a layer includes a plurality of chemical constituents or compounds, they may have all manner of homogeneous or heterogeneous distributions, including a homogeneous or heterogeneous distribution of metallurgical phases. This may include a graded distribution where the relative amounts of the chemical constituents or compounds vary according to respective constituent profiles across the thickness of the layer. In both single layer and multilayer coatings 16, each of the respective layers, or combinations of them, may be used to provide a predetermined property to the powder particle 12 or a sintered powder compact formed therefrom. For example, the predetermined property may include the bond strength of the metallurgical bond between the particle core 14 and the coating material 20; the interdiffusion characteristics between the particle core 14 and metallic coating layer 16, including any interdiffusion between the layers of a multilayer coating layer 16; the interdiffusion characteristics between the various layers of a multilayer coating layer 16; the interdiffusion characteristics between the metallic coating layer 16 of one powder particle and that of an adjacent powder particle 12; the bond strength of the metallurgical bond between the metallic coating layers of adjacent sintered powder particles 12, including the outermost layers of multilayer coating layers; and the electrochemical activity of the coating layer 16.

[0043] Metallic coating layer 16 and coating material 20 have a melting temperature (Tc). As used herein, Tcincludes the lowest temperature at which incipient melting or liquation or other forms of partial melting occur within coating material 20, regardless of whether coating material 20 comprises a pure metal, an alloy with multiple phases each håving different melting temperatures or a composite, including a composite comprising a plurality of coating material layers håving different melting temperatures.

[0044] Metallic coating material 20 may include any suitable metallic coating material 20 that provides a sinterable outer surface 21 that is configured to be sintered to an adjacent powder particle 12 that also has a metallic coating layer 16 and sinterable outer surface 21. In powders 10 that also include second or additional (coated or uncoated) particles 32, as described herein, the sinterable outer surface 21 of metallic coating layer 16 is also configured to be sintered to a sinterable outer surface 21 of second particles 32. In an exemplary embodiment, the powder particles 12 are sinterable at a predetermined sintering temperature (Ts) that is a function of the core material 18 and coating material 20, such that sintering of powder compact 200 is accomplished entirely in the solid state and where Tsis less than Tp and Tc. Sintering in the solid state limits particle core 14/metallic coating layer 16 interactions to solid state diffusion processes and metallurgical transport phenomena and limits growth of and provides control over the resultant interface between them. In contrast, for example, the introduction of liquid phase sintering would provide for rapid interdiffusion of the particle core 14/metallic coating layer 16 materials and make it difficult to limit the growth of and provide control over the resultant interface between them, and thus interfere with the formation of the desirable microstructure of particle compact 200 as described herein.

[0045] In an exemplary embodiment, core material 18 will be selected to provide a core chemical composition and the coating material 20 will be selected to provide a coating chemical composition and these chemical compositions will also be selected to differ from one another. In another exemplary embodiment, the core material 18 will be selected to provide a core chemical composition and the coating material 20 will be selected to provide a coating chemical composition and these chemical compositions will also be selected to differ from one another at their interface. Differences in the chemical compositions of coating material 20 and core material 18 may be selected to provide different dissolution rates and selectable and controllable dissolution of powder compacts 200 that incorporate them making them selectably and controllably dissolvable. This includes dissolution rates that differ in response to a changed condition in the wellbore, including an indirect or direct change in a wellbore fluid. In an exemplary embodiment, a powder compact 200 formed from powder 10 håving chemical compositions of core material 18 and coating material 20 that make compact 200 is selectably dissolvable in a wellbore fluid in response to a changed wellbore condition that includes a change in temperature, change in pressure, change in flow rate, change in pH or change in chemical composition of the wellbore fluid, or a combination thereof. The selectable dissolution response to the changed condition may result from actual chemical reactions or processes that promote different rates of dissolution, but also encompass changes in the dissolution response that are associated with physical reactions or processes, such as changes in wellbore fluid pressure or flow rate.

[0046] In an exemplary embodiment of a powder 10, particle core 14 includes Mg, Al, Mn or Zn, or a combination thereof, as core material 18, and more particularly may include pure Mg and Mg alloys, and metallic coating layer 16 includes Al, Zn, Mn, Mg, Mo, W, Cu, Fe, Si, Ca, Co, Ta, Re, or Ni, or an oxide, nitride or a carbide thereof, or a combination of any of the aforementioned materials as coating material 20.

[0047] In another exemplary embodiment of powder 10, particle core 14 includes Mg, Al, Mn or Zn, or a combination thereof, as core material 18, and more particularly may include pure Mg and Mg alloys, and metallic coating layer 16 includes a single layer of Al or Ni, or a combination thereof, as coating material 20, as illustrated in FIG. 2. Where metallic coating layer 16 includes a combination of two or more constituents, such as Al and Ni, the combination may include various graded or co-deposited structures of these materials where the amount of each constituent, and hence the composition of the layer, varies across the thickness of the layer, as also illustrated in FIG. 2.

[0048] In yet another exemplary embodiment, particle core 14 includes Mg, Al, Mn or Zn, or a combination thereof, as core material 18, and more particularly may include pure Mg and Mg alloys, and coating layer 16 includes two layers as core material 20, as illustrated in FIG. 3. The first layer 22 is disposed on the surface of particle core 14 and includes Al or Ni, or a combination thereof, as described herein. The second layer 24 is disposed on the surface of the first layer and includes Al, Zn, Mg, Mo, W, Cu, Fe, Si, Ca, Co, Ta, Re or Ni, or a combination thereof, and the first layer has a chemical composition that is different than the chemical composition of the second layer. In general, first layer 22 will be selected to provide a strong metallurgical bond to particle core 14 and to limit interdiffusion between the particle core 14 and coating layer 16, particularly first layer 22. Second layer 24 may be selected to increase the strength of the metallic coating layer 16, or to provide a strong metallurgical bond and promote sintering with the second layer 24 of adjacent powder particles 12, or both. In an exemplary embodiment, the respective layers of metallic coating layer 16 may be selected to promote the selective and controllable dissolution of the coating layer 16 in response to a change in a property of the wellbore, including the wellbore fluid, as described herein. However, this is only exemplary and it will be appreciated that other selection criteria for the various layers may also be employed. For example, any of the respective layers may be selected to promote the selective and controllable dissolution of the coating layer 16 in response to a change in a property of the wellbore, including the wellbore fluid, as described herein. Exemplary embodiments of a two-layer metallic coating layers 16 for use on particles cores 14 comprising Mg include first/second layer combinations comprising Al/Ni and Al/W.

[0049] In still another embodiment, particle core 14 includes Mg, Al, Mn or Zn, or a combination thereof, as core material 18, and more particularly may include pure Mg and Mg alloys, and coating layer 16 includes three layers, as illustrated in FIG. 4. The first layer 22 is disposed on particle core 14 and may include Al or Ni, or a combination thereof. The second layer 24 is disposed on first layer 22 and may include Al, Zn, Mg, Mo, W, Cu, Fe, Si, Ca, Co, Ta, Re or Ni, or an oxide, nitride or a carbide thereof, or a combination of any of the aforementioned second layer materials. The third layer 26 is disposed on the second layer 24 and may include Al, Mn, Fe, Co, Ni or a combination thereof. In a three-layer configuration, the composition of adjacent layers is different, such that the first layer has a chemical composition that is different than the second layer, and the second layer has a chemical composition that is different than the third layer. In an exemplary embodiment, first layer 22 may be selected to provide a strong metallurgical bond to particle core 14 and to limit

interdiffusion between the particle core 14 and coating layer 16, particularly first layer 22. Second layer 24 may be selected to increase the strength of the metallic coating layer 16, or

to limit interdiffusion between particle core 14 or first layer 22 and outer or third layer 26, or to promote adhesion and a strong metallurgical bond between third layer 26 and first layer 22, or any combination of them. Third layer 26 may be selected to provide a strong metallurgical bond and promote sintering with the third layer 26 of adjacent powder particles 12. However, this is only exemplary and it will be appreciated that other selection criteria for the various layers may also be employed. For example, any of the respective layers may be selected to promote the selective and controllable dissolution of the coating layer 16 in response to a change in a property of the wellbore, including the wellbore fluid, as described herein. An exemplary embodiment of a three-layer coating layer for use on particles cores comprising Mg include first/second/third layer combinations comprising AI/AI2O3/AI.

[0050] In still another embodiment, particle core 14 includes Mg, Al, Mn or Zn, or a combination thereof, as core material 18, and more particularly may include pure Mg and Mg alloys, and coating layer 16 includes four layers, as illustrated in FIG. 5. In the four layer configuration, the first layer 22 may include Al or Ni, or a combination thereof, as described herein. The second layer 24 may include Al, Zn, Mg, Mo, W, Cu, Fe, Si, Ca, Co, Ta, Re or Ni or an oxide, nitride, carbide thereof, or a combination of the aforementioned second layer materials. The third layer 26 may also include Al, Zn, Mg, Mo, W, Cu, Fe, Si, Ca, Co, Ta, Re or Ni, or an oxide, nitride or carbide thereof, or a combination of any of the aforementioned third layer materials. The fourth layer 28 may include Al, Mn, Fe, Co, Ni or a combination thereof. In the four layer configuration, the chemical composition of adjacent layers is different, such that the chemical composition of first layer 22 is different than the chemical composition of second layer 24, the chemical composition is of second layer 24 different than the chemical composition of third layer 26, and the chemical composition of third layer 26 is different than the chemical composition of fourth layer 28. In an exemplary embodiment, the selection of the various layers will be similar to that described for the three-layer configuration above with regard to the inner (first) and outer (fourth) layers, with the second and third layers available for providing enhanced interlayer adhesion, strength of the overall metallic coating layer 16, limited interlayer diffusion or selectable and controllable dissolution, or a combination thereof. However, this is only exemplary and it will be appreciated that other selection criteria for the various layers may also be employed. For example, any of the respective layers may be selected to promote the selective and controllable dissolution of the coating layer 16 in response to a change in a property of the wellbore, including the wellbore fluid, as described herein.

[0051] The thickness of the various layers in multi-layer configurations may be apportioned between the various layers in any manner so long as the sum of the layer thicknesses provide a nanoscale coating layer 16, including layer thicknesses as described herein. In one embodiment, the first layer 22 and outer layer (24, 26, or 28 depending on the number of layers) may be thicker than other layers, where present, due to the desire to provide sufficient material to promote the desired bonding of first layer 22 with the particle core 14, or the bonding of the outer layers of adjacent powder particles 12, during sintering of powder compact 200.

[0052] Powder 10 may also include an additional or second powder 30 interspersed in the plurality of powder particles 12, as illustrated in FIG. 7. In an exemplary embodiment, the second powder 30 includes a plurality of second powder particles 32. These second powder particles 32 may be selected to change a physical, chemical, mechanical or other property of a powder particle compact 200 formed from powder 10 and second powder 30, or a combination of such properties. In an exemplary embodiment, the property change may include an increase in the compressive strength of powder compact 200 formed from powder 10 and second powder 30. In another exemplary embodiment, the second powder 30 may be selected to promote the selective and controllable dissolution of in particle compact 200 formed from powder 10 and second powder 30 in response to a change in a property of the wellbore, including the wellbore fluid, as described herein. Second powder particles 32 may be uncoated or coated with a metallic coating layer 36. When coated, including single layer or multilayer coatings, the coating layer 36 of second powder particles 32 may comprise the same coating material 40 as coating material 20 of powder particles 12, or the coating material 40 may be different. The second powder particles 32 (uncoated) or particle cores 34 may include any suitable material to provide the desired benefit, including many metals. In an exemplary embodiment, when coated powder particles 12 comprising Mg, Al, Mn or Zn, or a combination thereof are employed, suitable second powder particles 32 may include Ni, W, Cu, Co or Fe, or a combination thereof. Since second powder particles 32 will also be configured for solid state sintering to powder particles 12 at the predetermined sintering temperature (Ts), particle cores 34 will have a melting temperature Tap and any coating layers 36 will have a second melting temperature Tac, where Tsis less than Tap and Tac- It will also be appreciated that second powder 30 is not limited to one additional powder particle 32 type (i.e., a second powder particle), but may include a plurality of additional powder particles 32 (i.e., second, third, fourth, etc. types of additional powder particles 32) in any number.

[0053] Referring to FIG. 8, an exemplary embodiment of a method 300 of making a metallic powder 10 is disclosed. Method 300 includes forming 310 a plurality of particle cores 14 as described herein. Method 300 also includes depositing 320 a metallic coating layer 16 on each of the plurality of particle cores 14. Depositing 320 is the process by which coating layer 16 is disposed on particle core 14 as described herein.

[0054] Forming 310 of particle cores 14 may be performed by any suitable method for forming a plurality of particle cores 14 of the desired core material 18, which essentially comprise methods of forming a powder of core material 18. Suitable powder forming methods include mechanical methods; including machining, milling, impacting and other mechanical methods for forming the metal powder; chemical methods, including chemical decomposition, precipitation from a liquid or gas, solid-solid reactive synthesis and other chemical powder forming methods; atomization methods, including gas atomization, liquid and water atomization, centrifugal atomization, plasma atomization and other atomization methods for forming a powder; and various evaporation and condensation methods. In an exemplary embodiment, particle cores 14 comprising Mg may be fabricated using an atomization method, such as vacuum spray forming or inert gas spray forming.

[0055] Depositing 320 of metallic coating layers 16 on the plurality of particle cores 14 may be performed using any suitable deposition method, including various thin film deposition methods, such as, for example, chemical vapor deposition and physical vapor deposition methods. In an exemplary embodiment, depositing 320 of metallic coating layers 16 is performed using fluidized bed chemical vapor deposition (FBCVD). Depositing 320 of the metallic coating layers 16 by FBCVD includes flowing a reactive fluid as a coating medium that includes the desired metallic coating material 20 through a bed of particle cores 14 fluidized in a reactor vessel under suitable conditions, including temperature, pressure and flow rate conditions and the like, sufficient to induce a chemical reaction of the coating medium to produce the desired metallic coating material 20 and induce its deposition upon the surface of particle cores 14 to form coated powder particles 12. The reactive fluid selected will depend upon the metallic coating material 20 desired, and will typically comprise an organometallic compound that includes the metallic material to be deposited, such as nickel tetracarbonyl (Ni(CO)4), tungsten hexafluoride (WFe), and triethyl aluminum (C6H15AI), that is transported in a carrier fluid, such as helium or argon gas. The reactive fluid, including carrier fluid, causes at least a portion of the plurality of particle cores 14 to be suspended in the fluid, thereby enabling the entire surface of the suspended particle cores 14 to be exposed to the reactive fluid, including, for example, a desired organometallic constituent, and enabling deposition of metallic coating material 20 and coating layer 16 over the entire surfaces of particle cores 14 such that they each become enclosed forming coated particles 12 håving metallic coating layers 16, as described herein. As also described herein, each metallic coating layer 16 may include a plurality of coating layers. Coating material 20 may be deposited in multiple layers to form a multilayer metallic coating layer 16 by repeating the step of depositing 320 described above and changing 330 the reactive fluid to provide the desired metallic coating material 20 for each subsequent layer, where each subsequent layer is deposited on the outer surface of particle cores 14 that already include any previously deposited coating layer or layers that make up metallic coating layer 16. The metallic coating materials 20 of the respective layers (e.g., 22, 24, 26, 28, etc.) may be different from one another, and the differences may be provided by utilization of different reactive media that are configured to produce the desired metallic coating layers 16 on the particle cores 14 in the fluidize bed reactor.

[0056] As illustrated in FIGS. 1 and 9, particle core 14 and core material 18 and metallic coating layer 16 and coating material 20 may be selected to provide powder particles 12 and a powder 10 that is configured for compaction and sintering to provide a powder compact 200 that is lightweight (i.e., håving a relatively low density), high-strength and is selectably and controllably removable from a wellbore in response to a change in a wellbore property, including being selectably and controllably dissolvable in an appropriate wellbore fluid, including various wellbore fluids as disclosed herein. Powder compact 200 includes a substantially-continuous, cellular nanomatrix 216 of a nanomatrix material 220 håving a plurality of dispersed particles 214 dispersed throughout the cellular nanomatrix 216. The substantially-continuous cellular nanomatrix 216 and nanomatrix material 220 formed of sintered metallic coating layers 16 is formed by the compaction and sintering of the plurality of metallic coating layers 16 of the plurality of powder particles 12. The chemical composition of nanomatrix material 220 may be different than that of coating material 20 due to diffusion effects associated with the sintering as described herein. Powder metal compact 200 also includes a plurality of dispersed particles 214 that comprise particle core material 218. Dispersed particle cores 214 and core material 218 correspond to and are formed from the plurality of particle cores 14 and core material 18 of the plurality of powder particles 12 as the metallic coating layers 16 are sintered together to form nanomatrix 216. The chemical composition of core material 218 may be different than that of core material 18 due to diffusion effects associated with sintering as described herein.

[0057] As used herein, the use of the term substantially-continuous cellular nanomatrix 216 does not connote the major constituent of the powder compact, but rather refers to the minority constituent or constituents, whether by weight or by volume. This is distinguished from most matrix composite materials where the matrix comprises the majority constituent by weight or volume. The use of the term substantially-continuous, cellular nanomatrix is intended to describe the extensive, regular, continuous and interconnected nature of the distribution of nanomatrix material 220 within powder compact 200. As used herein, "substantially-continuous" describes the extension of the nanomatrix material throughout powder compact 200 such that it extends between and envelopes substantially all of the dispersed particles 214. Substantially-continuous is used to indicate that complete continuity and regular order of the nanomatrix around each dispersed particle 214 is not required. For example, defects in the coating layer 16 over particle core 14 on some powder particles 12 may cause bridging of the particle cores 14 during sintering of the powder compact 200, thereby causing localized discontinuities to result within the cellular nanomatrix 216, even though in the other portions of the powder compact the nanomatrix is substantially continuous and exhibits the structure described herein. As used herein, "cellular" is used to indicate that the nanomatrix defines a network of generally repeating, interconnected, compartments or cells of nanomatrix material 220 that encompass and also interconnect the dispersed particles 214. As used herein, "nanomatrix" is used to describe the size or scale of the matrix, particularly the thickness of the matrix between adjacent dispersed particles 214. The metallic coating layers that are sintered together to form the nanomatrix are themselves nanoscale thickness coating layers. Since the nanomatrix at most locations, other than the intersection of more than two dispersed particles 214, generally comprises the interdiffusion and bonding of two coating layers 16 from adjacent powder particles 12 håving nanoscale thicknesses, the matrix formed also has a nanoscale thickness (e.g., approximately two times the coating layer thickness as described herein) and is thus described as a nanomatrix. Further, the use of the term dispersed particles 214 does not connote the minor constituent of powder compact 200, but rather refers to the majority constituent or constituents, whether by weight or by volume. The use of the term dispersed particle is intended to convey the discontinuous and discrete distribution of particle core material 218 within powder compact 200.

[0058] Powder compact 200 may have any desired shape or size, including that of a cylindrical billet or bar that may be machined or otherwise used to form useful articles of manufacture, including various wellbore tools and components. The pressing used to form precursor powder compact 100 and sintering and pressing processes used to form powder compact 200 and deform the powder particles 12, including particle cores 14 and coating layers 16, to provide the full density and desired macroscopic shape and size of powder compact 200 as well as its microstructure. The microstructure of powder compact 200 includes an equiaxed configuration of dispersed particles 214 that are dispersed throughout and embedded within the substantially-continuous, cellular nanomatrix 216 of sintered coating layers. This microstructure is somewhat analogous to an equiaxed grain microstructure with a continuous grain boundary phase, except that it does not require the use of alloy constituents håving thermodynamic phase equilibria properties that are capable of producing such a structure. Rather, this equiaxed dispersed particle structure and cellular nanomatrix 216 of sintered metallic coating layers 16 may be produced using constituents where thermodynamic phase equilibrium conditions would not produce an equiaxed structure. The equiaxed morphology of the dispersed particles 214 and cellular network 216 of particle layers results from sintering and deformation of the powder particles 12 as they are compacted and interdiffuse and deform to fill the interparticle spaces 15 (FIG. 1). The sintering temperatures and pressures may be selected to ensure that the density of powder compact 200 achieves substantially full theoretical density.

[0059] In an exemplary embodiment as illustrated in FIGS. 1 and 9, dispersed particles 214 are formed from particle cores 14 dispersed in the cellular nanomatrix 216 of sintered metallic coating layers 16, and the nanomatrix 216 includes a solid-state metallurgical bond 217 or bond layer 219, as illustrated schematically in FIG. 10, extending between the dispersed particles 214 throughout the cellular nanomatrix 216 that is formed at a sintering temperature (Ts), where Tsis less than Tcand Tp. As indicated, solid-state metallurgical bond 217 is formed in the solid state by solid-state interdiffusion between the coating layers 16 of adjacent powder particles 12 that are compressed into touching contact during the compaction and sintering processes used to form powder compact 200, as described herein. As such, sintered coating layers 16 of cellular nanomatrix 216 include a solid-state bond layer 219 that has a thickness (t) defined by the extent of the interdiffusion of the coating materials 20 of the coating layers 16, which will in turn be defined by the nature of the coating layers 16, including whether they are single or multilayer coating layers, whether they have been selected to promote or limit such interdiffusion, and other factors, as described herein, as well as the sintering and compaction conditions, including the sintering time, temperature and pressure used to form powder compact 200.

[0060] As nanomatrix 216 is formed, including bond 217 and bond layer 219, the chemical composition or phase distribution, or both, of metallic coating layers 16 may change. Nanomatrix 216 also has a melting temperature (Tm). As used herein, Tm includes the lo west temperature at which incipient melting or liquation or other forms of partial melting will occur within nanomatrix 216, regardless of whether nanomatrix material 220 comprises a pure metal, an alloy with multiple phases each håving different melting temperatures or a composite, including a composite comprising a plurality of layers of various coating materials håving different melting temperatures, or a combination thereof, or otherwise. As dispersed particles 214 and particle core materials 218 are formed in conjunction with nanomatrix 216, diffusion of constituents of metallic coating layers 16 into the particle cores 14 is also possible, which may result in changes in the chemical composition or phase distribution, or both, of particle cores 14. As a result, dispersed particles 214 and particle core materials 218 may have a melting temperature (Tdp) that is different than Tp. As used herein, Tdp includes the lowest temperature at which incipient melting or liquation or other forms of partial melting will occur within dispersed particles 214, regardless of whether particle core material 218 comprise a pure metal, an alloy with multiple phases each håving different melting temperatures or a composite, or otherwise. Powder compact 200 is formed at a sintering temperature (Ts), where Tsis less than Tc,Tp, Tm and Td<p.>

[0061] Dispersed particles 214 may comprise any of the materials described herein for particle cores 14, even though the chemical composition of dispersed particles 214 may be different due to diffusion effects as described herein. In an exemplary embodiment, dispersed particles 214 are formed from particle cores 14 comprising materials håving a standard oxidation potential greater than or equal to Zn, including Mg, Al, Zn or Mn, or a combination thereof, may include various binary, tertiary and quaternary alloys or other combinations of these constituents as disclosed herein in conjunction with particle cores 14. Of these materials, those håving dispersed particles 214 comprising Mg and the nanomatrix 216 formed from the metallic coating materials 16 described herein are particularly useful. Dispersed particles 214 and particle core material 218 of Mg, Al, Zn or Mn, or a combination thereof, may also include a rare earth element, or a combination of rare earth elements as disclosed herein in conjunction with particle cores 14.

[0062] In another exemplary embodiment, dispersed particles 214 are formed from particle cores 14 comprising metals that are less electrochemically active than Zn or non-metallic materials. Suitable non-metallic materials include ceramics, glasses (e.g., hollow glass microspheres) or carbon, or a combination thereof, as described herein.

[0063] Dispersed particles 214 of powder compact 200 may have any suitable particle size, including the average particle sizes described herein for particle cores 14.

[0064] Dispersed particles 214 may have any suitable shape depending on the shape selected for particle cores 14 and powder particles 12, as well as the method used to sinter and compact powder 10. In an exemplary embodiment, powder particles 12 may be spheroidal or substantially spheroidal and dispersed particles 214 may include an equiaxed particle configuration as described herein.

[0065] The nature of the dispersion of dispersed particles 214 may be affected by the selection of the powder 10 or powders 10 used to make particle compact 200. In one exemplary embodiment, a powder 10 håving a unimodal distribution of powder particle 12 sizes may be selected to form powder compact 200 and will produce a substantially homogeneous unimodal dispersion of particle sizes of dispersed particles 214 within cellular nanomatrix 216, as illustrated generally in FIG. 9. In another exemplary embodiment, a plurality of powders 10 håving a plurality of powder particles with particle cores 14 that have the same core materials 18 and different core sizes and the same coating material 20 may be selected and uniformly mixed as described herein to provide a powder 10 håving a homogenous, multimodal distribution of powder particle 12 sizes, and may be used to form powder compact 200 håving a homogeneous, multimodal dispersion of particle sizes of dispersed particles 214 within cellular nanomatrix 216, as illustrated schematically in FIGS. 6 and 11. Similarly, in yet another exemplary embodiment, a plurality of powders 10 håving a plurality of particle cores 14 that may have the same core materials 18 and different core sizes and the same coating material 20 may be selected and distributed in a non-uniform manner to provide a non-homogenous, multimodal distribution of powder particle sizes, and may be used to form powder compact 200 håving a non-homogeneous, multimodal dispersion of particle sizes of dispersed particles 214 within cellular nanomatrix 216, as illustrated schematically in FIG. 12. The selection of the distribution of particle core size may be used to determine, for example, the particle size and interparticle spacing of the dispersed particles 214 within the cellular nanomatrix 216 of powder compacts 200 made from powder 10.

[0066] As illustrated generally in FIGS. 7 and 13, powder metal compact 200 may also be formed using coated metallic powder 10 and an additional or second powder 30, as described herein. The use of an additional powder 30 provides a powder compact 200 that also includes a plurality of dispersed second particles 234, as described herein, that are dispersed within the nanomatrix 216 and are also dispersed with respect to the dispersed particles 214. Dispersed second particles 234 may be formed from coated or uncoated second powder particles 32, as described herein. In an exemplary embodiment, coated second powder particles 32 may be coated with a coating layer 36 that is the same as coating layer 16 of powder particles 12, such that coating layers 36 also contribute to the nanomatrix 216. In another exemplary embodiment, the second powder particles 232 may be uncoated such that dispersed second particles 234 are embedded within nanomatrix 216. As disclosed herein, powder 10 and additional powder 30 may be mixed to form a homogeneous dispersion of dispersed particles 214 and dispersed second particles 234, as illustrated in FIG. 13, or to form a non-homogeneous dispersion of these particles, as illustrated in FIG. 14. The dispersed second particles 234 may be formed from any suitable additional powder 30 that is different from powder 10, either due to a compositional difference in the particle core 34, or coating layer 36, or both of them, and may include any of the materials disclosed herein for use as second powder 30 that are different from the powder 10 that is selected to form powder compact 200. In an exemplary embodiment, dispersed second particles 234 may include Fe, Ni, Co or Cu, or oxides, nitrides or carbides thereof, or a combination of any of the aforementioned materials.

[0067] Nanomatrix 216 is a substantially-continuous, cellular network of metallic coating layers 16 that are sintered to one another. The thickness of nanomatrix 216 will depend on the nature of the powder 10 or powders 10 used to form powder compact 200, as well as the incorporation of any second powder 30, particularly the thicknesses of the coating layers associated with these particles. In an exemplary embodiment, the thickness of nanomatrix 216 is substantially uniform throughout the microstructure of powder compact 200 and comprises about two times the thickness of the coating layers 16 of powder particles 12. In another exemplary embodiment, the cellular network 216 has a substantially uniform average thickness between dispersed particles 214 of about 50nm to about 5000nm.

[0068] Nanomatrix 216 is formed by sintering metallic coating layers 16 of adjacent particles to one another by interdiffusion and creation of bond layer 219 as described herein. Metallic coating layers 16 may be single layer or multilayer structures, and they may be selected to promote or inhibit diffusion, or both, within the layer or between the layers of metallic coating layer 16, or between the metallic coating layer 16 and particle core 14, or between the metallic coating layer 16 and the metallic coating layer 16 of an adjacent powder particle, the extent of interdiffusion of metallic coating layers 16 during sintering may be limited or extensive depending on the coating thicknesses, coating material or materials selected, the sintering conditions and other factors. Given the potential complexity of the interdiffusion and interaction of the constituents, description of the resulting chemical composition of nanomatrix 216 and nanomatrix material 220 may be simply understood to be a combination of the constituents of coating layers 16 that may also include one or more constituents of dispersed particles 214, depending on the extent of interdiffusion, if any, that occurs between the dispersed particles 214 and the nanomatrix 216. Similarly, the chemical composition of dispersed particles 214 and particle core material 218 may be simply understood to be a combination of the constituents of particle core 14 that may also include one or more constituents of nanomatrix 216 and nanomatrix material 220, depending on the extent of interdiffusion, if any, that occurs between the dispersed particles 214 and the nanomatrix 216.

[0069] In an exemplary embodiment, the nanomatrix material 220 has a chemical composition and the particle core material 218 has a chemical composition that is different from that of nanomatrix material 220, and the differences in the chemical compositions may be configured to provide a selectable and controllable dissolution rate, including a selectable transition from a very low dissolution rate to a very rapid dissolution rate, in response to a controlled change in a property or condition of the wellbore proximate the compact 200, including a property change in a wellbore fluid that is in contact with the powder compact 200, as described herein. Nanomatrix 216 may be formed from powder particles 12 håving single layer and multilayer coating layers 16. This design flexibility provides a large number of material combinations, particularly in the case of multilayer coating layers 16, that can be utilized to tailor the cellular nanomatrix 216 and composition of nanomatrix material 220 by controlling the interaction of the coating layer constituents, both within a given layer, as well as between a coating layer 16 and the particle core 14 with which it is associated or a coating layer 16 of an adjacent powder particle 12. Several exemplary embodiments that demonstrate this flexibility are provided below.

[0070] As illustrated in FIG. 10, in an exemplary embodiment, powder compact 200 is formed from powder particles 12 where the coating layer 16 comprises a single layer, and the resulting nanomatrix 216 between adjacent ones of the plurality of dispersed particles 214 comprises the single metallic coating layer 16 of one powder particle 12, a bond layer 219 and the single coating layer 16 of another one of the adjacent powder particles 12. The thickness (t) of bond layer 219 is determined by the extent of the interdiffusion between the single metallic coating layers 16, and may encompass the entire thickness of nanomatrix 216 or only a portion thereof. In one exemplary embodiment of powder compact 200 formed using a single layer powder 10, powder compact 200 may include dispersed particles 214 comprising Mg, Al, Zn or Mn, or a combination thereof, as described herein, and nanomatrix 216 may include 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, including combinations where the nanomatrix material 220 of cellular nanomatrix 216, including bond layer 219, has a chemical composition and the core material 218 of dispersed particles 214 has a chemical composition that is different than the chemical composition of nanomatrix material 216. The difference in the chemical composition of the nanomatrix material 220 and the core material 218 may be used to provide selectable and controllable dissolution in response to a change in a property of a wellbore, including a wellbore fluid, as described herein. In a further exemplary embodiment of a powder compact 200 formed from a powder 10 håving a single coating layer configuration, dispersed particles 214 include Mg, Al, Zn or Mn, or a combination thereof, and the cellular nanomatrix 216 includes Al or Ni, or a combination thereof.

[0071] As illustrated in FIG. 15, in another exemplary embodiment, powder compact 200 is formed from powder particles 12 where the coating layer 16 comprises a multilayer coating layer 16 håving a plurality of coating layers, and the resulting nanomatrix 216 between adjacent ones of the plurality of dispersed particles 214 comprises the plurality of layers (t) comprising the coating layer 16 of one particle 12, a bond layer 219, and the plurality of layers comprising the coating layer 16 of another one of powder particles 12. In FIG. 15, this is illustrated with a two-layer metallic coating layer 16, but it will be understood that the plurality of layers of multi-layer metallic coating layer 16 may include any desired number of layers. The thickness (t) of the bond layer 219 is again determined by the extent of the interdiffusion between the plurality of layers of the respective coating layers 16, and may encompass the entire thickness of nanomatrix 216 or only a portion thereof. In this embodiment, the plurality of layers comprising each coating layer 16 may be used to control interdiffusion and formation of bond layer 219 and thickness (t).

[0072] In one exemplary embodiment of a powder compact 200 made using powder particles 12 with multilayer coating layers 16, the compact includes dispersed particles 214 comprising Mg, Al, Zn or Mn, or a combination thereof, as described herein, and nanomatrix 216 comprises a cellular network of sintered two-layer coating layers 16, as shown in FIG. 3, comprising first layers 22 that are disposed on the dispersed particles 214 and a second layers 24 that are disposed on the first layers 22. First layers 22 include Al or Ni, or a combination thereof, and second layers 24 include Al, Zn, Mn, Mg, Mo, W, Cu, Fe, Si, Ca, Co, Ta, Re or Ni, or a combination thereof. In these configurations, materials of dispersed particles 214 and multilayer coating layer 16 used to form nanomatrix 216 are selected so that the chemical compositions of adjacent materials are different (e.g. dispersed particle/first layer and first layer/second layer).

[0073] In another exemplary embodiment of a powder compact 200 made using powder particles 12 with multilayer coating layers 16, the compact includes dispersed particles 214 comprising Mg, Al, Zn or Mn, or a combination thereof, as described herein, and nanomatrix 216 comprises a cellular network of sintered three-layer metallic coating layers 16, as shown in FIG. 4, comprising first layers 22 that are disposed on the dispersed particles 214, second layers 24 that are disposed on the first layers 22 and third layers 26 that are disposed on the second layers 24. First layers 22 include Al or Ni, or a combination thereof; second layers 24 include Al, Zn, Mn, Mg, Mo, W, Cu, Fe, Si, Ca, Co, Ta, Re or Ni, or an oxide, nitride or carbide thereof, or a combination of any of the aforementioned second layer materials; and the third layers include Al, Zn, Mn, Mg, Mo, W, Cu, Fe, Si, Ca, Co, Ta, Re or Ni, or a combination thereof. The selection of materials is analogous to the selection considerations described herein for powder compact 200 made using two-layer coating layer powders, but must also be extended to include the material used for the third coating layer.

[0074] In yet another exemplary embodiment of a powder compact 200 made using powder particles 12 with multilayer coating layers 16, the compact includes dispersed particles 214 comprising Mg, Al, Zn or Mn, or a combination thereof, as described herein, and nanomatrix 216 comprise a cellular network of sintered four-layer coating layers 16 comprising first layers 22 that are disposed on the dispersed particles 214; second layers 24 that are disposed on the first layers 22; third layers 26 that are disposed on the second layers 24 and fourth layers 28 that are disposed on the third layers 26. First layers 22 include Al or Ni, or a combination thereof; second layers 24 include Al, Zn, Mn, Mg, Mo, W, Cu, Fe, Si, Ca, Co, Ta, Re or Ni, or an oxide, nitride or carbide thereof, or a combination of any of the aforementioned second layer materials; third layers include Al, Zn, Mn, Mg, Mo, W, Cu, Fe, Si, Ca, Co, Ta, Re or Ni, or an oxide, nitride or carbide thereof, or a combination of any of the aforementioned third layer materials; and fourth layers include Al, Mn, Fe, Co or Ni, or a combination thereof. The selection of materials is analogous to the selection considerations described herein for powder compacts 200 made using two-layer coating layer powders, but must also be extended to include the material used for the third and fourth coating layers.

[0075] In another exemplary embodiment of a powder compact 200, dispersed particles 214 comprise a metal håving a standard oxidation potential less than Zn or a non-metallic material, or a combination thereof, as described herein, and nanomatrix 216 comprises a cellular network of sintered metallic coating layers 16. Suitable non-metallic materials include various ceramics, glasses or forms of carbon, or a combination thereof. Further, in powder compacts 200 that include dispersed particles 214 comprising these metals or non-metallic materials, nanomatrix 216 may include 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 as nanomatrix material 220.

[0076] Referring to FIG. 16, sintered powder compact 200 may comprise a sintered precursor powder compact 100 that includes a plurality of deformed, mechanically bonded powder particles as described herein. Precursor powder compact 100 may be formed by compaction of powder 10 to the point that powder particles 12 are pressed into one another, thereby deforming them and forming interparticle mechanical or other bonds 110 associated with this deformation sufficient to cause the deformed powder particles 12 to adhere to one another and form a green-state powder compact håving a green density that is less than the theoretical density of a fully-dense compact of powder 10, due in part to interparticle spaces 15. Compaction may be performed, for example, by isostatically pressing powder 10 at room temperature to provide the deformation and interparticle bonding of powder particles 12 necessary to form precursor powder compact 100.

[0077] Sintered and forged powder compacts 200 that include dispersed particles 214 comprising Mg and nanomatrix 216 comprising various nanomatrix materials as described herein have demonstrated an excellent combination of mechanical strength and low density that exemplify the lightweight, high-strength materials disclosed herein. Examples of powder compacts 200 that have pure Mg dispersed particles 214 and various nanomatrices 216 formed from powders 10 håving pure Mg particle cores 14 and various single and multilayer metallic coating layers 16 that include Al, Ni, W or AI2O3, or a combination thereof, and that have been made using the method 400 disclosed herein, are listed in a table as FIG. 18. These powders compacts 200 have been subjected to various mechanical and other testing, including density testing, and their dissolution and mechanical property degradation behavior has also beencharacterizedas disclosed herein. The results indicate that these materials may be configured to provide a wide range of selectable and controllable corrosion or dissolution behavior from very low corrosion rates to extremely high corrosion rates, particularly corrosion rates that are both lower and higher than those of powder compacts that do not incorporate the cellular nanomatrix, such as a compact formed from pure Mg powder through the same compaction and sintering processes in comparison to those that include pure Mg dispersed particles in the various cellular nanomatrices described herein. These powder compacts 200 may also be configured to provide substantially enhanced properties as compared to powder compacts formed from pure Mg particles that do not include the nanoscale coatings described herein. For example, referring to FIGS. 18 and 19, powder compacts 200 that include dispersed particles 214 comprising Mg and nanomatrix 216 comprising various nanomatrix materials 220 described herein have demonstrated room temperature compressive strengths of at least about 37 ksi, and have further demonstrated room temperature compressive strengths in excess of about 50 ksi, both dry and immersed in a solution of 3% KC1 at 200°F. In contrast, powder compacts formed from pure Mg powders have a compressive strength of about 20 ksi or less. Strength of the nanomatrix powder metal compact 200 can be further improved by optimizing powder 10, particularly the weight percentage of the nanoscale metallic coating layers 16 that are used to form cellular nanomatrix 216. For example, FIG. 25 shows the effect of varying the weight percentage (wt.%), i.e., thickness, of an alumina coating on the room temperature compressive strength of a powder compact 200 of a cellular nanomatrix 216 formed from coated powder particles 12 that include a multilayer (AI/AI2O3/AI) metallic coating layer 16 on pure Mg particle cores 14. In this example, optimal strength is achieved at 4 wt% of alumina, which represents an increase of 21% as compared to that of 0 wt% alumina.

[0078] Powder compacts 200 comprising dispersed particles 214 that include Mg and nanomatrix 216 that includes various nanomatrix materials as described herein have also demonstrated a room temperature sheer strength of at least about 20 ksi. This is in contrast with powder compacts formed from pure Mg powders which have room temperature sheer strengths of about 8 ksi.

[0079] Powder compacts 200 of the types disclosed herein are able to achieve an actual density that is substantially equal to the predetermined theoretical density of a compact material based on the composition of powder 10, including relative amounts of constituents of particle cores 14 and metallic coating layer 16, and are also described herein as being fully-dense powder compacts. Powder compacts 200 comprising dispersed particles that include Mg and nanomatrix 216 that includes various nanomatrix materials as described herein have demonstrated actual densities of about 1.738 g/cm<3>to about 2.50 g/cm<3>, which are substantially equal to the predetermined theoretical densities, differing by at most 4% from the predetermined theoretical densities.

[0080] Powder compacts 200 as disclosed herein may be configured to be selectively and controllably dissolvable in a wellbore fluid in response to a changed condition in a wellbore. Examples of the changed condition that may be exploited to provide selectable and controllable dissolvability include a change in temperature, change in pressure, change in flow rate, change in pH or change in chemical composition of the wellbore fluid, or a combination thereof. An example of a changed condition comprising a change in temperature includes a change in well bore fluid temperature. For example, referring to FIGS. 18 and 20, powder compacts 200 comprising dispersed particles 214 that include Mg and cellular nanomatrix 216 that includes various nanomatrix materials as described herein have relatively low rates of corrosion in a 3% KC1 solution at room temperature that ranges from about 0 to about 11 mg/cm<2>/hr as compared to relatively high rates of corrosion at 200°F that range from about 1 to about 246 mg/cm<2>/hr depending on different nanoscale coating layers 16. An example of a changed condition comprising a change in chemical composition includes a change in a chloride ion concentration or pH value, or both, of the wellbore fluid. For example, referring to FIGS. 18 and 21, powder compacts 200 comprising dispersed particles 214 that include Mg and nanomatrix 216 that includes various nanoscale coatings described herein demonstrate corrosion rates in 15% HC1 that range from about 4750 mg/cm<2>/hr to about 7432 mg/cm<2>/hr. Thus, selectable and controllable dissolvability in response to a changed condition in the wellbore, namely the change in the wellbore fluid chemical composition from KC1 to HC1, may be used to achieve a characteristic response as illustrated graphically in FIG. 22, which illustrates that at a selected predetermined critical service time (CST) a changed condition may be imposed upon powder compact 200 as it is applied in a given application, such as a wellbore environment, that causes a controllable change in a property of powder compact 200 in response to a changed condition in the environment in which it is applied. For example, at a predetermined CST changing a wellbore fluid that is in contact with powder contact 200 from a first fluid (e.g. KC1) that provides a first corrosion rate and an associated weight loss or strength as a function of time to a second wellbore fluid (e.g., HC1) that provides a second corrosion rate and associated weight loss and strength as a function of time, wherein the corrosion rate associated with the first fluid is much less than the corrosion rate associated with the second fluid. This characteristic response to a change in wellbore fluid conditions may be used, for example, to associate the critical service time with a dimension loss limit or a minimum strength needed for a particular application, such that when a wellbore tool or component formed from powder compact 200 as disclosed herein is no longer needed in service in the wellbore (e.g., the CST) the condition in the wellbore (e.g., the chloride ion concentration of the wellbore fluid) may be changed to cause the rapid dissolution of powder compact 200 and its removal from the wellbore. In the example described above, powder compact 200 is selectably dissolvable at a rate that ranges from about 0 to about 7000 mg/cm2/hr. This range of response provides, for example the ability to remove a 3 inch diameter ball formed from this material from a wellbore by altering the wellbore fluid in less than one hour. The selectable and controllable dissolvability behavior described above, coupled with the excellent strength and low density properties described herein, define a new engineered dispersed particle-nanomatrix material that is configured for contact with a fluid and configured to provide a selectable and controllable transition from one of a first strength condition to a second strength condition that is lower than a functional strength threshold, or a first weight loss amount to a second weight loss amount that is greater than a weight loss limit, as a function of time in contact with the fluid. The dispersed particle-nanomatrix composite is characteristic of the powder compacts 200 described herein and includes a cellular nanomatrix 216 of nanomatrix material 220, a plurality of dispersed particles 214 including particle core material 218 that is dispersed within the matrix. Nanomatrix 216 ischaracterized bya solid-state bond layer 219 which extends throughout the nanomatrix. The time in contact with the fluid described above may include the CST as described above. The CST may include a predetermined time that is desired or required to dissolve a predetermined portion of the powder compact 200 that is in contact with the fluid. The CST may also include a time corresponding to a change in the property of the engineered material or the fluid, or a combination thereof. In the case of a change of property of the engineered material, the change may include a change of a temperature of the engineered material. In the case where there is a change in the property of the fluid, the change may include the change in a fluid temperature, pressure, flow rate, chemical composition or pH or a combination thereof. Both the engineered material and the change in the property of the engineered material or the fluid, or a combination thereof, may be tailored to provide the desired CST response characteristic, including the rate of change of the particular property (e.g., weight loss, loss of strength) both prior to the CST (e.g., Stage 1) and after the CST (e.g., Stage 2), as illustrated in FIG. 22.

[0081] Referring to FIG. 17, a method 400 of making a powder compact 200. Method 400 includes forming 410 a coated metallic powder 10 comprising powder particles 12 håving particle cores 14 with nanoscale metallic coating layers 16 disposed thereon, wherein the metallic coating layers 16 have a chemical composition and the particle cores 14 have a chemical composition that is different than the chemical composition of the metallic coating material 16. Method 400 also includes forming 420 a powder compact by applying a predetermined temperature and a predetermined pressure to the coated powder particles sufficient to sinter them by solid-phase sintering of the coated layers of the plurality of the coated particle powders 12 to form a substantially-continuous, cellular nanomatrix 216 of a nanomatrix material 220 and a plurality of dispersed particles 214 dispersed within nanomatrix 216 as described herein.

[0082] Forming 410 of coated metallic powder 10 comprising powder particles 12 håving particle cores 14 with nanoscale metallic coating layers 16 disposed thereon may be performed by any suitable method. In an exemplary embodiment, forming 410 includes applying the metallic coating layers 16, as described herein, to the particle cores 14, as described herein, using fluidized bed chemical vapor deposition (FBCVD) as described herein. Applying the metallic coating layers 16 may include applying single-layer metallic coating layers 16 or multilayer metallic coating layers 16 as described herein. Applying the metallic coating layers 16 may also include contro Iling the thickness of the individual layers as they are being applied, as well as controlling the overall thickness of metallic coating layers 16. Particle cores 14 may be formed as described herein.

[0083] Forming 420 of the powder compact 200 may include any suitable method of forming a fully-dense compact of powder 10. In an exemplary embodiment, forming 420 includes dynamic forging of a green-density precursor powder compact 100 to apply a predetermined temperature and a predetermined pressure sufficient to sinter and deform the powder particles and form a fully-dense nanomatrix 216 and dispersed particles 214 as described herein. Dynamic forging as used herein means dynamic application of a load at temperature and for a time sufficient to promote sintering of the metallic coating layers 16 of adjacent powder particles 12, and may preferably include application of a dynamic forging load at a predetermined loading rate for a time and at a temperature sufficient to form a sintered and fully-dense powder compact 200. In an exemplary embodiment, dynamic forging included: 1) heating a precursor or green-state powder compact 100 to a predetermined solid phase sintering temperature, such as, for example, a temperature sufficient to promote interdiffusion between metallic coating layers 16 of adjacent powder particles 12; 2) holding the precursor powder compact 100 at the sintering temperature for a predetermined hold time, such as, for example, a time sufficient to ensure substantial uniformity of the sintering temperature throughout the precursor compact 100; 3) forging the precursor powder compact 100 to full density, such as, for example, by applying a predetermined forging pressure according to a predetermined pressureSchedule or ramp rate sufficient to rapidly achieve full density while holding the compact at the predetermined sintering temperature; and 4) cooling the compact to room temperature. The predetermined pressure and predetermined temperature applied during forming 420 will include a sintering temperature, Ts, and forging pressure, Pf, as described herein that will ensure solid-state sintering and deformation of the powder particles 12 to form fully-dense powder compact 200, including solid-state bond 217 and bond layer 219. The steps of heating to and holding the precursor powder compact 100 at the predetermined sintering temperature for the predetermined time may include any suitable combination of temperature and time, and will depend, for example, on the powder 10 selected, including the materials used for particle core 14 and metallic coating layer 16, the size of the precursor powder compact 100, the heating method used and other factors that influence the time needed to achieve the desired temperature and temperature uniformity within precursor powder compact 100. In the step of forging, the predetermined pressure may include any suitable pressure and pressure application schedule or pressure ramp rate sufficient to achieve a fully-dense powder compact 200, and will depend, for example, on the material properties of the powder particles 12 selected, including temperature dependent stress/strain characteristics (e.g., stress/strain rate characteristics), interdiffusion and metallurgical thermodynamic and phase equilibria characteristics, dislocation dynamics and other material properties. For example, the maximum forging pressure of dynamic forging and the forging schedule (i.e., the pressure ramp rates that correspond to strain rates employed) may be used to tailor the mechanical strength and toughness of the powder compact. The maximum forging pressure and forging ramp rate (i.e., strain rate) is the pressure just below the compact cracking pressure, i.e., where dynamic recovery processes are unable to relieve strain energy in the compact microstructure without the formation of a crack in the compact. For example, for applications that require a powder compact that has relatively higher strength and lower toughness, relatively higher forging pressures and ramp rates may be used. If relatively higher toughness of the powder compact is needed, relatively lower forging pressures and ramp rates may be used.

[0084] For certain exemplary embodiments of powders 10 described herein and precursor compacts 100 of a size sufficient to form many wellbore tools and components, predetermined hold times of about 1 to about 5 hours may be used. The predetermined sintering temperature, Ts, will preferably be selected as described herein to avoid melting of either particle cores 14 and metallic coating layers 16 as they are transformed during method 400 to provide dispersed particles 214 and nanomatrix 216. For these embodiments, dynamic forging may include application of a forging pressure, such as by dynamic pressing to a maximum of about 80 ksi at pressure ramp rate of about 0.5 to about 2 ksi/second.

[0085] In an exemplary embodiment where particle cores 14 included Mg and metallic coating layer 16 included various single and multilayer coating layers as described herein, such as various single and multilayer coatings comprising Al, the dynamic forging was performed by sintering at a temperature, Ts, of about 450°C to about 470 °C for up to about 1 hour without the application of a forging pressure, followed by dynamic forging by application of isostatic pressures at ramp rates between about 0.5 to about 2 ksi/second to a maximum pressure, Ps, of about 30 ksi to about 60 ksi, which resulted in forging cycles of 15 seconds to about 120 seconds. The short duration of the forging cycle is a significant advantage as it limits interdiffusion, including interdiffusion within a given metallic coating layer 16, interdiffusion between adjacent metallic coating layers 16 and interdiffusion between metallic coating layers 16 and particle cores 14, to that needed to form metallurgical bond 217 and bond layer 219, while also maintaining the desirable equiaxed dispersed particle 214 shape with the integrity of cellular nanomatrix 216 strengthening phase. The duration of the dynamic forging cycle is much shorter than the forming cycles and sintering times required for conventional powder compact forming processes, such as hot isostatic pressing (HIP), pressure assisted sintering or diffusion sintering.

[0086] Method 400 may also optionally include forming 430 a precursor powder compact by compacting the plurality of coated powder particles 12 sufficiently to deform the particles and form interparticle bonds to one another and form the precursor powder compact 100 prior to forming 420 the powder compact. Compacting may include pressing, such as isostatic pressing, of the plurality of powder particles 12 at room temperature to form precursor powder compact 100. Compacting 430 may be performed at room temperature. In an exemplary embodiment, powder 10 may include particle cores 14 comprising Mg and forming 430 the precursor powder compact may be performed at room temperature at an isostatic pressure of about 10 ksi to about 60 ksi.

[0087] Method 400 may optionally also include intermixing 440 a second powder 30 into powder 10 as described herein prior to the forming 420 the powder compact, or forming 430 the precursor powder compact.

[0088] Without being limited by theory, powder compacts 200 are formed from coated powder particles 12 that include a particle core 14 and associated core material 18 as well as a metallic coating layer 16 and an associated metallic coating material 20 to form a substantially-continuous, three-dimensional, cellular nanomatrix 216 that includes a nanomatrix material 220 formed by sintering and the associated diffusion bonding of the respective coating layers 16 that includes a plurality of dispersed particles 214 of the particle core materials 218. This unique structure may include metastable combinations of materials that would be very difficult or impossible to form by solidification from a melt håving the same relative amounts of the constituent materials. The coating layers and associated coating materials may be selected to provide selectable and controllable dissolution in a predetermined fluid environment, such as a wellbore environment, where the predetermined fluid may be a commonly used wellbore fluid that is either injected into the wellbore or extracted from the wellbore. As will be further understood from the description herein, controlled dissolution of the nanomatrix exposes the dispersed particles of the core materials. The particle core materials may also be selected to also provide selectable and controllable dissolution in the wellbore fluid. Alternately, they may also be selected to provide a particular mechanical property, such as compressive strength or sheer strength, to the powder compact 200, without necessarily providing selectable and controlled dissolution of the core materials themselves, since selectable and controlled dissolution of the nanomatrix material surrounding these particles will necessarily release them so that they are carried away by the wellbore fluid. The microstructural morphology of the substantially-continuous, cellular nanomatrix 216, which may be selected to provide a strengthening phase material, with dispersed particles 214, which may be selected to provide equiaxed dispersed particles 214, provides these powder compacts with enhanced mechanical properties, including compressive strength and sheer strength, since the resulting morphology of the nanomatrix/dispersed particles can be manipulated to provide strengthening through the processes that are akin to traditional strengthening mechanisms, such as grain size reduction, solution hardening through the use of impurity atoms, precipitation or age hardening and strength/work hardening mechanisms. The nanomatrix/dispersed particle structure tends to limit dislocation movement by virtue of the numerous particle nanomatrix interfaces, as well as interfaces between discrete layers within the nanomatrix material as described herein. This is exemplified in the fracture behavior of these materials, as illustrated in FIGS. 23 and 24. In FIG. 23, a powder compact 200 made using uncoated pure Mg powder and subjected to a shear stress sufficient to induce failure demonstrated intergranular fracture. In contrast, in FIG. 24, a powder compact 200 made using powder particles 12 håving pure Mg powder particle cores 14 to form dispersed particles 214 and metallic coating layers 16 that includes Al to form nanomatrix 216 and subjected to a shear stress sufficient to induce failure demonstrated transgranular fracture and a substantially higher fracture stress as described herein. Because these materials have high-strength characteristics, the core material and coating material may be selected to utilize low density materials or other low density materials, such as low-density metals, ceramics, glasses or carbon, that otherwise would not provide the necessary strength characteristics for use in the desired applications, including wellbore tools and components.

[0089] Illustrated in FIG. 26, is an embodiment of the downhole tool 610 or component that is a tripping ball also described herein as a plug. Although the plug 610 is illustrated as a ball other shapes are contemplated such as conical, elliptical, etc. The plug 610 is configured to seatingly engage with a seat 614. The seat 614 illustrated herein includes a conical surface 618 sealingly engaged with a tubular 622. Seating engagement of the plug 610 with the seat 614 allows the body 612 to seal to the seat 614 thereby permitting pressure to be built thereagainst. The body 612 has an outer surface 626 that is configured to dissolve upon exposure to an environment 630 that is anticipated during deployment of the plug 610. This dissolution can include corrosion, for example, in applications wherein the outer surface 626 is part of an electrochemical cell. The dissolution of the outer surface 626 allows the body 612, when it has become stuck, wedged or lodged to the seat 614, to be dislodged and unsealed therefrom. This dislodging can be due, at least in part, to a decrease in frictional engagement between the plug 610 and the seat 614 as the body 612 begins to dissolve. Additionally, the dislodging is due to dimensional changes of the plug 610 as the body 612 dissolves initially from the outer surface 626.

[0090] The ability to dislodge the plug 610 from the seat 614 is particularly helpful in instances where the plug 610 has become wedged into an opening 634 of the seat 614. The severity of such wedging can be significant in cases where the body 612 has become deformed due to forces urging the plug 610 against the seat 614. Such deformation can cause a portion 638 of the body 612 to extend into the opening 634, thereby increasing frictional engagement between the portion 638 and a dimension 642 of the opening 634.

[0091] In applications for use in the drilling and completion industries, as discussed above, wherein the plug 610 is a tripping ball the ball will be exposed to a downhole environment 630. The downhole environment 630 may include high temperatures, high pressures, and wellbore fluids, such as, caustic chemicals, acids, bases and brine solutions, for example. By making the body 612 of a material 646 that degrades in strength in the environment 630, the body 612 can be made to effectively dissolve in response to exposure to the downhole environment 630. The initiation of dissolution or disintegration of the body 612 can begin at the outer surface 626 as the strength of the outer surface 626 decreases first and can propagate to the balance of the body 612. Possible choices for the material 646 include but are not limited to Magnesium, polymeric adhesives such as structural methacrylate adhesive, powder metal compact, high strength dissolvable Material such as the powder 10 (discussed in detail above in this specification), etc.

[0092] The body 612 and the outer surface 626 of the plug 610 in the embodiment of FIG. 26 are both made of the material 646. As such, dissolution of the material 646 can leave both the body 612 and the outer surface 626 in small pieces that are not detrimental to further operation of the well, thereby negating the need to either pump the body 612 out of the tubular 622 or run a tool within the wellbore to drill or mill the body 612 into pieces small enough to remove hindrance therefrom.

[0093] Referring to FIG. 27, an alternate embodiment of a plug disclosed herein is illustrated at 710. Unlike the plug 610 the plug 710 has a body 712 made of at least two different materials. The body 712 includes a core 716 made of a first material 717 and a shell 720 made of a second material 721. Since, in this embodiment, an outer surface 726 that actually contacts the seat 614 is only on the shell 720, only the second material 721 needs to be dissolvable in the target environment 630. In contrast, the first material 717 may or may not be dissolvable in the environment 630.

[0094] If the first material 717 is not dissolvable it may be desirable to make a greatest dimension 724 of the core 716 less than the dimension 642 of the seat 614 to permit the core 716 to pass therethrough after dissolution of the shell 720. In so doing the core 716 can be run, or allowed to drop down, out of a lower end of the tubular 622 instead of being pumped upward to remove it therefrom.

[0095] As introduced above, materials that may be utilized for the plugs 610, 710 are described herein as lightweight, high-strength metallic materials that may be used in a wide variety of applications and application environments, including use in various wellbore environments to make various selectably and controllably disposable or degradable lightweight, high-strength downhole tools or other downhole components, as well as many other applications for use in both durable and disposable or degradable articles.

[0096] 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. Moreover, the use of the terms first, second, etc. do not denote any order or importance, but rather the terms first, second, etc. are used to distinguish one element from another. Furthermore, the use of the terms a, an, etc. do not denote a limitation of quantity, but rather denote the presence of at least one of the referenced item.

Claims

1. Downhole flow inhibition tool comprising at least a first component and a mating component at least a portion of one of the first component and the mating component being dissolvable in a target environment to reduce flow inhibition upon dissolution of the at least a portion.

2. The downhole flow inhibition tool of claim 1, wherein the first component is dissolvable.

3. The downhole flow inhibition tool of claim 2, wherein the first component is made of a powder metal compact.

4. The downhole flow inhibition tool of claim 3, wherein the powder metal compact includes: 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.

5. The downhole flow inhibition tool of claim 4, wherein the particle core material comprises Mg-Zn, Mg-Zn, Mg-Al, Mg-Mn, or Mg-Zn-Y.

6. The downhole flow inhibition tool of claim 4, wherein the dispersed particles further comprise a rare earth element.

7. The downhole flow inhibition tool of claim 1, wherein the first component is a plug.

8. The downhole flow inhibition tool of claim 1, wherein the first component includes a shell and a core.

9. The downhole flow inhibition tool of claim 8, wherein the core is dissolvable.

10. The downhole flow inhibition tool of claim 1, wherein the downhole flow inhibition tool is selected from the group consisting of frac plugs, bridge plugs, wiper plugs, shear out plugs, debris barriers, atmospheric chamber discs, swabbing element protectors, sealbore protectors, screen protectors, beaded screen protectors, screen basepipe plugs, drill in stim liner plugs, ICD plugs, flapper valves, gaslift valves, transmatic CEM™ plugs, 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 and cementing plugs.

11. A method of unplugging a seat, comprising: dissolving at least a surface defined by a shell surrounding a core of a plug seated against the seat; unseating the plug from the seat; dimensioning the core to fit through the seat without necessarily dissolving the core; and passing the core through the seat.

12. The method of unplugging a seat of claim 11, further comprising dissolving the core after it has passed through the seat.