Patent Publication Number: US-11658286-B2

Title: Nanocomposite electrode materials for use in high temperature and high pressure rechargeable batteries

Description:
CROSS REFERENCE TO RELATED APPLICATIONS 
     This application is a continuation of U.S. patent application Ser. No. 15/866,113, filed Jan. 9, 2018, the disclosure of which is hereby incorporated by reference herein in its entirety. 
    
    
     FIELD 
     The present disclosure relates generally to nanocomposites, and more particularly to electrode materials for rechargeable batteries (for example, lithium-ion batteries, lithium-sulfur batteries, or both) designed to tolerate operation at conditions of high temperature and high pressure. 
     BACKGROUND 
     Rechargeable batteries are used to power a broad range of consumer devices such as electric vehicles and portable electronic devices. However, these batteries are susceptible to failure and can be unsafe under “abuse conditions” such as when the rechargeable batteries are overcharged, over-discharged, or operated at high temperature and high pressure. For example, when operated at a temperature that is greater than a critical temperature, a rechargeable battery can undergo thermal runaway. During thermal runaway, high temperatures trigger a chain of exothermic reactions in the battery, causing the battery&#39;s temperature to increase rapidly. Thermal runaway can cause battery failure, damage to devices, and harm to users. During thermal runaway, rechargeable batteries such as lithium-ion and lithium-sulfur batteries can be prone to fire and explosion because the electrode materials (for example, anode and cathode materials) can be highly reactive and are unstable. Even when thermal runaway does not occur, electrode materials used in rechargeable batteries can suffer from performance decay when operated at high temperatures. For example, lithium-based and silicon-based anode materials can suffer from a loss of capacity when operated at high temperatures. Accordingly, there is a need for improved electrode materials which are resistant to thermal runaway and are safe, reliable, and stable when operated at conditions of high temperature and high pressure. 
     SUMMARY 
     Presented in the present disclosure are nanocomposites and rechargeable batteries which are resistant to thermal runaway and can be used as safe, reliable, and stable electrode materials for rechargeable batteries operated at high temperature and high pressure. The nanocomposites include a plurality of transition metal oxide nanoparticles, a plurality of ultrathin sheets of a first two-dimensional (2D) material, and a plurality of ultrathin sheets of a second (and different) 2D material, which act in synergy to provide an improved thermal stability, an increased surface area, and enhanced electrochemical properties to the nanocomposites. For example, rechargeable batteries that include the nanocomposites as an electrode material have an enhanced performance and stability over a broad temperature range from room temperature to high temperatures (for example, about 100° C.). These batteries may fill an important need by providing a safe and reliable power source for devices operated at high temperatures and pressures such as the downhole equipment used in the oil industry. 
     The present disclosure encompasses the recognition that including a second thermally stable two-dimensional (2D) material (for example, hexagonal boron nitride) in a nanocomposite may not only improve the thermal stability of the nanocomposite but also improve the electrochemical performance of the nanocomposite when it is used as an electrode material. Thus, the nanocomposite described in the present disclosure can be used to simultaneously prevent thermal runaway events and enhance a battery&#39;s overall electrochemical performance. The 2D materials may include a 2D carbon material (for example, graphene, graphene oxide, or reduced graphene oxide), a 2D nitride (for example, hexagonal boron nitride), a 2D metal chalcogenide (for example, MoS 2 , SnS 2 , TiS 2 , WS 2 , MoSe 2 , or WSe 2 ), a 2D oxide (for example, TiO 2 , ZnO, MnO 2 , or a perovskite), a 2D hybrid material (for example, MoS 2 /graphene or MoSe 2 /MnO 2 ), or combinations of these. 
     Without wishing to be bound to any particular theory, it is thought that, in certain embodiments, the second thermally stable 2D material (for example, hexagonal boron nitride) acts in synergy with the other 2D material (for example, reduced graphene oxide) and the plurality of transition metal oxide nanoparticles in the nanocomposite to enhance (i) the thermal stability, (ii) the mechanical properties (for example, strength), (iii) the physical properties (for example, the specific surface area), (iv) and the electrochemical properties (for example, the specific capacity, coulombic efficiency, and cycling performance) of the corresponding electrode material. For example, the first 2D material may be less susceptible to restacking and loss of active surface area during operation in the presence of a second (and different) 2D material over a broad temperature range and at high pressure. This results in an increased operating life and improved tolerance to high temperatures and high pressure. Moreover, without wishing to be bound to any particular theory, it is thought that the second 2D material may act as a “substrate” for the first 2D material and effectively increase its carrier mobility and thus improve its electrochemical properties as an electrode material over a broad range of temperatures and under conditions of high pressure. 
     In certain embodiments, the nanocomposites described in the present disclosure may perform better, be more stable, and cost less than conventional electrode materials. For example, the nanocomposites described in the present disclosure may be stable at high temperatures (of about 100° C. or greater) and may have consistent electrochemical properties even after 1,000 or more charge/discharge cycles at about 100° C. For example, the nanocomposites described in the present disclosure may not suffer from the characteristic capacity decay of silicon-based anodes after a few charge/discharge cycles at high temperature. For example, the methods described in the present disclosure are based on hydrothermal microwave irradiation and thus may be less costly than existing methods to prepare conventional electrode materials. 
     In certain embodiments, the rechargeable batteries (for example, lithium-ion batteries and lithium-sulfur batteries) described in the present disclosure are safer than conventional batteries when operated at high temperature. For example, dendritic lithium, which is a major cause of thermal runaway events in conventional anode materials, does not form in the nanocomposites described in the present disclosure. For example, short circuit(s) may not occur at high temperatures in the batteries described in the present disclosure, and the batteries may not undergo thermal runaway at temperatures of about 100° C. or greater. Accordingly, the nanocomposites and the rechargeable batteries described in the present disclosure can be used in safe energy-storage devices and in devices operated at high temperatures and pressure. For example, the rechargeable batteries described in the present disclosure can be used in the oil industry to power downhole equipment such as that used to monitor conditions (for example, of temperature and pressure) in oil wells and other oil-related applications where high temperatures and pressures are encountered. 
     In one aspect, the present disclosure is directed to a nanocomposite that includes (a) a plurality of transition metal oxide (for example, cobalt oxide) nanoparticles, (b) a plurality of ultrathin sheets of a first two-dimensional (2D) material, and (c) a plurality of ultrathin sheets of a second 2D material. The second 2D material is of a different type than the first 2D material. 
     In certain embodiments, the first 2D material is a member selected from the group consisting of a 2D carbon material (for example, graphene, graphene oxide, or reduced graphene oxide), a 2D nitride (for example, functionalized boron nitride or hexagonal boron nitride), a 2D metal chalcogenide (for example, MoS 2 , SnS 2 , TiS 2 , WS 2 , MoSe 2 , or WSe 2 ), a 2D oxide (for example, TiO 2 , ZnO, MnO 2 , or a perovskite), and a 2D hybrid material (for example, MoS 2 /graphene or MoSe 2 /MnO 2 ). 
     In certain embodiments, the second 2D material is a member selected from the group consisting of a 2D carbon material (for example, graphene, graphene oxide, or reduced graphene oxide), a 2D nitride (for example, functionalized boron nitride or hexagonal boron nitride), a 2D metal chalcogenide (for example, MoS 2 , SnS 2 , TiS 2 , WS 2 , MoSe 2 , or WSe 2 ), a 2D oxide (for example, TiO 2 , ZnO, MnO 2 , or a perovskite), a 2D hybrid material (for example, MoS 2 /graphene or MoSe 2 /MnO 2 ). 
     In certain embodiments, the first 2D material is graphene or reduced graphene oxide. 
     In certain embodiments, the second 2D material is a member selected from the group consisting of hexagonal boron nitride, boron nitride, and functionalized boron nitride. For example, boron nitride may be functionalized via chemical oxidation, functionalized via hydrothermal microwave irradiation, or both. 
     In certain embodiments, a weight percent of the plurality of ultrathin sheets of the first 2D material is in a range from 0.1% to 20%. This weight percent is based on the total weight of the plurality of transition metal oxide nanoparticles, the plurality of ultrathin sheets of the first 2D material, and the plurality of ultrathin sheets of the second 2D material. 
     In certain embodiments, a weight percent of the plurality of ultrathin sheets of the second 2D material is in a range from 0.1% to 50%. This weight percent is based on the total weight of the plurality of transition metal oxide nanoparticles, the plurality of ultrathin sheets of the first 2D material, and the plurality of ultrathin sheets of the second 2D material. 
     In certain embodiments, the nanocomposite has a component weight ratio (x:y:z) in a range from (1:0.001:0.001) to (1:0.67:1.67), where x is the plurality of transition metal oxide nanoparticles, y is the plurality of ultrathin sheets of the first 2D material, and z is the plurality of ultrathin sheets of the second 2D material. 
     In certain embodiments, at least a portion of the plurality of transition metal nanoparticles has an average particle size of less than 300 nanometers (nm). For example, the size of the transition metal nanoparticles may be determined using scanning electron microscopy. 
     In certain embodiments, at least a portion of the plurality of transition metal nanoparticles has an average particle size in a range from 30 nm to 45 nm. 
     In certain embodiments, at least a portion of the plurality of transition metal nanoparticles has a particle-size distribution with a standard deviation of 2 nm. 
     In certain embodiments, at least a portion of the plurality of transition metal nanoparticles has an approximately rectangular prism shape. For example, the shape of the transition metal nanoparticles may be determined using scanning electron microscopy. 
     In certain embodiments, at least a portion of the plurality of transition metal oxide nanoparticles comprise cobalt oxide (for example, Co 3 O 4 ). 
     In certain embodiments, at least a portion of the cobalt oxide has a cubic-spinel crystal structure. For example, the crystal structure may be determined based on an intensity or a relative intensity of a peak in an X-ray diffraction (XRD) pattern of the plurality of transition metal oxide nanoparticles. For example, the crystal structure may be determined based on an interplanar spacing measured with Selected Area Electron Diffraction (SAED) analysis. 
     In certain embodiments, at least a portion of the plurality of ultrathin sheets of the first 2D material and at least a portion of the plurality of ultrathin sheets of the second 2D material has an average sheet thickness of less than 20 nm. For example, the thickness of the ultrathin sheets may be determined using scanning electron microscopy. 
     In certain embodiments, at least a portion of the plurality of ultrathin sheets of the first 2D material and at least a portion of the plurality of ultrathin sheets of the second 2D material have an average sheet thickness in a range from 5 nm to 20 nm 
     In certain embodiments, at least a portion of the plurality of ultrathin sheets of the first 2D material and at least a portion of the plurality of ultrathin sheets of the second 2D material have an average sheet thickness in a range from 5 nm to 10 nm. 
     In certain embodiments, the nanocomposite has a specific surface area in a range from 10 square meters per gram (m 2 /g) to 500 m 2 /g. For example, the specific surface area may be a Brunauer-Emmett-Teller (BET) specific surface area measured via a nitrogen adsorption/desorption isotherm. In certain embodiments, the nanocomposite has a specific surface area in a range from 10 m 2 /g to 200 m 2 /g. 
     In certain embodiments, the nanocomposite further comprises (i) a binding agent (for example, polyvinylidene fluoride), (ii) a conductive additive (for example, carbon black), or both of (i) and (ii). 
     In certain embodiments, a summed weight percent of the binding agent and the conductive additive in the nanocomposite is in a range from 5% to 20%. For example, the summed weight percent of the binding agent and the conductive additive may be about 10%. The summed weight percent is based on the total weight of (i) the plurality of transition metal oxide nanoparticles, (ii) the plurality of ultrathin sheets of the first 2D material, (iii) the plurality of ultrathin sheets of the second 2D material, and (iv) any binding agent, conductive additive, or both present in the nanocomposite. For example, the amount of the binding agent in the nanocomposite may be zero; the amount of conductive additive in the nanocomposite may be zero; or the nanocomposite may contain both the binding agent and the conductive additive. 
     In certain embodiments, the nanocomposite is a film with a thickness in a range from 50 micrometers (μm) to 200 μm. For example, film thickness may be measured using profilometry or scanning electron microscopy. 
     In certain embodiments, the nanocomposite is a film with a thickness in a range from 10 μm to 20 μm. 
     In certain embodiments, the nanocomposite also includes sulfur. For example, the nanocomposite also includes elemental sulfur, a sulfur-containing salt, a sulfur-containing and lithium-containing salt, a sulfur/graphene composite, or combinations of these. 
     In certain embodiments, the weight percent of sulfur is in a range from 40% to 80%. For example, the weight percent of sulfur may be from 60% to 80% or from 70% to 80%. The weight percent is based on the total weight of (i) the plurality of transition metal oxide nanoparticles, (ii) the plurality of ultrathin sheets of the first 2D material, (iii) the plurality of ultrathin sheets of the second 2D material, (iv) any binding agent, conductive additive, or both present in the nanocomposite, and (v) the sulfur. 
     In one aspect, the present disclosure is directed to a lithium-ion battery that includes an anode. The anode includes the nanocomposite described previously. 
     In certain embodiments, the lithium-ion battery also includes a cathode (for example, lithium metal or a lithium metal oxide); an electrolyte [for example, one or more lithium salts (for example, lithium hexafluorphosphate) dissolved in one or more organic solvents (for example, ethylene carbonate or dimethyl carbonate)]; and a separator (for example, a polypropylene membrane) between the anode and the cathode. 
     In certain embodiments, at about 25° C., the lithium-ion battery has a specific capacity (for example, specific charge/discharge capacity) in a range from 600 milliamp-hours per gram (mAh/g) (for example, 651.4 mAh/g) to at least 800 mAh/g (for example, 816.5 mAh/g). For example, the specific capacity may be measured at a current density of about 200 milliamps per gram (mA/g)). At about 100° C., the lithium-ion battery has a specific capacity (for example, charge/discharge capacity) in a range from 1 to 5 mAh/g (for example, a specific charge capacity of 1 mAh/g and a specific discharge capacity of 2 mAh/g. For example, the specific capacity may be measured at a current density of about 100 mA/g. 
     In certain embodiments, after 100 charge/discharge cycles at about 100° C. or after 1000 charge/discharge cycles at about 100° C., the lithium-ion battery retains at least 90% of its specific capacity compared to an initial specific charge capacity in a first charge cycle at about 100° C. 
     In certain embodiments, after 100 charge/discharge cycles at about 100° C. or after 1000 charge/discharge cycles at about 100° C., a coulombic efficiency of the lithium-ion battery is 90% or greater at 100° C. 
     In one aspect, the present disclosure is directed to a lithium-sulfur battery that includes a cathode. The cathode includes the nanocomposite described previously. 
     In certain embodiments, the lithium-sulfur batter also includes an anode (for example, lithium metal); an electrolyte [for example, one or more lithium salts (for example, bis(trifluoromethane)sulfonimide lithium salt (LiTFSI)) in an organic solvent (for example, 1,2-dimethoxyethane (DME) or 1,3-dioxolane (DOL))]]; and a separator (for example, a polypropylene membrane) between the anode and the cathode. 
     In one aspect, the present disclosure is directed to a method of preparing a nanocomposite. The method includes preparing a plurality of transition metal oxide nanoparticles and a plurality of ultrathin reduced graphene oxide sheets by applying microwave irradiation to a volume of a first solvent comprising a transition metal-containing salt [for example, cobalt (II) acetate tetrahydrate (Co(C 2 H 3 O 2 ) 2 ), cobalt nitrate, or cobalt chloride] and graphene oxide. For example, microwave irradiation may be applied at a temperature of at least 140° C. Microwave irradiation may be applied at a temperature in a range from 140° C. to 220° C. Microwave irradiation may, for example, be applied at 180° C. Microwave irradiation may be applied at, for example, a microwave power of at least 900 watts (W). Microwave irradiation may be applied at a microwave power in range from 900 W to 1800 W. Microwave irradiation may be applied at a pressure of at least 150 pounds per square inch (psi) or, for example, at a pressure in a range from 150 psi to 350 psi. The concentration of the transition metal-containing salt is in a range from 0.01 moles per liter (mol/L) to 0.5 mol/L. The method includes preparing a plurality of ultrathin boron nitride sheets by (i) oxidizing boron nitride in a volume of a second solvent (for example, a mixture of H 2 O 2  and H 2 SO 4 ) and (ii) applying microwave irradiation to the volume of the second solvent (for example, for 15 minutes at a temperature in a range from 120° C. to 180° C., at a microwave power of 900 W, and at a pressure of 150 psi). The method includes contacting together (i) at least a portion of the plurality of transition metal oxide nanoparticles, (ii) at least a portion of the plurality of ultrathin reduced graphene oxide sheets, and (iii) at least a portion of the plurality of ultrathin boron nitride sheets in a volume of a third solvent, thereby preparing a nanocomposite mixture. The method includes drying the nanocomposite mixture (for example, for about 12 hours at 60° C.), thereby preparing a nanocomposite. 
     In certain embodiments, the method includes, following drying the nanocomposite mixture, contacting together the nanocomposite mixture with sulfur (for example, elemental sulfur, a sulfur-containing salt, a sulfur-containing and lithium-containing salt, a sulfur/graphene composite, or combinations of these). For example, the weight percent of sulfur may be in a range from 50% to 80%, from 60% to 80%, or from 70% to 80%. The weight percent is based on the total weight of the nanocomposite. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWING 
       The foregoing and other objects, aspects, features, and advantages of the present disclosure will become more apparent and better understood by referring to the following description taken in conjunction with the accompanying drawings, in which: 
         FIG.  1 A  is a block diagram showing a method for preparing a nanocomposite, according to an illustrative embodiment; 
         FIG.  1 B  is a block diagram showing a method for preparing graphene oxide, according to an illustrative embodiment; 
         FIG.  1 C  is a block diagram showing a method for preparing a transition metal oxide/first 2D material sample, according to an illustrative embodiment; 
         FIG.  1 D  is a block diagram showing a method for preparing a second 2D material, according to an illustrative embodiment; 
         FIG.  1 E  is a block diagram showing a method for combining the transition metal oxide/first 2D material sample with the second 2D material, according to an illustrative embodiment; 
         FIG.  2 A  is a block diagram showing a nanocomposite, according to an illustrative embodiment; 
         FIG.  2 B  is a block diagram showing a nanocomposite comprising a plurality of ultrathin reduced graphene oxide sheets, a plurality of cobalt oxide nanoparticles, and a plurality of ultrathin boron nitride sheets, according to an illustrative embodiment; 
         FIG.  3 A  is a block diagram showing a lithium-ion battery, according to an illustrative embodiment; 
         FIG.  3 B  is a block diagram showing a lithium-sulfur battery, according to an illustrative embodiment; 
         FIG.  4    is a plot of X-Ray diffraction (XRD) patterns for example Co 3 O 4  nanoparticles (curve a), an example Co 3 O 4 /RGO sample (curve b), an example Co 3 O 4 /h-BN sample (curve c), and an example Co 3 O 4 /RGO/h-BN nanocomposite (curve d), according to an illustrative embodiment; 
         FIG.  5    is a plot of the Raman spectra of example Co 3 O 4  nanoparticles, an example Co 3 O 4 /RGO sample, an example Co 3 O 4 /h-BN sample, and an example Co 3 O 4 /RGO/h-BN sample, according to an illustrative embodiment; 
         FIG.  6 A  is a scanning electron micrograph of example Co 3 O 4  nanoparticles, according to an illustrative embodiment; 
         FIG.  6 B  is a scanning electron micrograph of an example Co 3 O 4 /RGO sample, according to an illustrative embodiment; 
         FIG.  6 C  is a scanning electron micrograph of an example Co 3 O 4 /h-BN sample, according to an illustrative embodiment; 
         FIG.  6 D  is a scanning electron micrograph of an example Co 3 O 4 /RGO/h-BN sample, according to an illustrative embodiment; 
         FIG.  7    is a plot of thermogravimetric analysis (TGA) curves for different example samples, according to an illustrative embodiment; 
         FIG.  8    is a first derivative plot (DTG curves) of the TGA curves shown in  FIG.  7    for different example samples, according to an illustrative embodiment; 
         FIG.  9 A  is a plot of the nitrogen adsorption-desorption isotherm for example Co 3 O 4  nanoparticles, according to an illustrative embodiment; 
         FIG.  9 B  is a plot of the nitrogen adsorption-desorption isotherm for an example Co 3 O 4 /RGO sample, according to an illustrative embodiment; 
         FIG.  9 C  is a plot of the nitrogen adsorption-desorption isotherm for an example Co 3 O 4 /h-BN sample, according to an illustrative embodiment; 
         FIG.  9 D  is a plot of the nitrogen adsorption-desorption isotherm for an example Co 3 O 4 /RGO/h-BN nanocomposite, according to an illustrative embodiment; 
         FIG.  10 A  is a plot of curves of voltage versus specific capacity for lithium-ion batteries prepared with different anode materials, according to an illustrative embodiment; 
         FIG.  10 B  is a Nyquist plot of the imaginary impedance (Z″) versus the real impedance (Z) for lithium-ion batteries prepared with different anode materials, according to an illustrative embodiment; 
         FIG.  11    is a plot of the specific capacity versus charge/discharge cycle number for an example battery with an anode that includes a Co 3 O 4 /RGO/h-BN nanocomposite for 100 charge/discharge cycles at room temperature (about 25° C.), according to an illustrative embodiment; 
         FIG.  12    is a plot of the specific capacity versus charge/discharge cycle number for an example battery with an anode that includes a Co 3 O 4 /RGO/h-BN nanocomposite for 100 charge/discharge cycles at about 100° C., according to an illustrative embodiment; and 
         FIG.  13    is a plot of the specific capacity versus charge/discharge cycle number for an example battery with an anode that includes a Co 3 O 4 /RGO/h-BN nanocomposite for 1,000 charge/discharge cycles at about 100° C., according to an illustrative embodiment. 
     
    
    
     The features and advantages of the present disclosure will become more apparent from the detailed description set forth in the following when taken in conjunction with the drawings, in which like reference characters identify corresponding elements throughout. In the drawings, like reference numbers generally indicate identical elements, functionally similar elements, or structurally similar elements. 
     Definitions 
     About, Approximately: As used in the present disclosure, the terms “about” and “approximately,” in reference to a number, are used to include numbers that fall within a range of 20%, 10%, 5%, 1%, or 0.5% in either direction of (greater than or less than) the number unless otherwise stated or otherwise evident from the context (except where such number would exceed 100% of a possible value). 
     Anode: As used in the present disclosure, the term “anode” refers to the negative electrode of a battery. Oxidation reactions occurs at the anode. 
     Carrier Mobility: As used in the present disclosure, the term “carrier mobility” refers to a metric of how quickly an electron or hole can be transported through a material in the presence of an electric field. For example, an electrode with an increased carrier mobility tends to have an increased conductivity and improved electrochemical properties compared to an electrode with a decreased carrier mobility. 
     Cathode: As used in the present disclosure, the term “cathode” refers to the positive electrode of a battery. Reduction reactions occur at the cathode. 
     Capacity, specific capacity, specific charge capacity: As used in the present disclosure, the term “capacity” means the product of the discharge current (for example, in amps (A) or milliamps (mA)) and the discharge time (for example, in hours (h)) for a battery at a given load. For example, a “capacity” may be expressed in amp-hours (Ah) or milliamp-hours (mAh). As used in the present disclosure, the term “specific capacity” means the product of the discharge current and the discharge time of a battery at a given load for a given weight of electrode material (for example, for a given weight of nanocomposite used as an anode material in a battery). For example, a “specific capacity” may be expressed in amp-hours per gram (Ah/g) or milliamp-hours per gram (mAh/g). In certain embodiments, “specific capacity” is referred to as “specific discharge capacity.” As used in the present disclosure, the term “specific charge capacity” means the product of the charge current and the charge time for a battery at a given load for a given weight of electrode material (for example, for a given weight of nanocomposite used as an anode material). For example, a “specific charge capacity” may be expressed in Ah/g or mAh/g. 
     Charge/discharge cycle, Cycle: As used in the present disclosure, the terms “charge/discharge cycle” and “cycle” refer to the process of charging, discharging, or both a battery. For example, a single “charge/discharge cycle” includes charging and discharging a battery. In certain embodiments, a battery may be discharged either fully or partially during a discharge cycle. For example, 100%, 90%, 80%, 70%, or less of a battery&#39;s capacity may be discharged during a discharge cycle. Similarly, in certain embodiments, a battery may be charged either fully or partially during a charge cycle. For example, a battery may be charged to 100%, 90%, 80%, 70%, or less of its full capacity during a charge cycle. 
     Downhole equipment: As used in the present disclosure, the term “downhole equipment” refers to devices used to measure the conditions inside an oil well. For example, downhole equipment may include a pressure sensor for measuring the pressure inside an oil well or a temperature sensor for measuring the temperature inside an oil well. As used in the present disclosure, the term “oil well” means a boring (for example, a drilled hole or tunnel) in the earth that is designed to bring hydrocarbons (for example, oil) from an underground hydrocarbon reservoir to the surface. 
     Graphene oxide: As used in the present disclosure, the term “graphene oxide” refers to a material substantially composed of ultrathin sheets of a compound of carbon, oxygen, and hydrogen, where each sheet has a thickness defined by a monolayer of carbon rings (for example, a layer of carbon rings approximately one atom thick, with attached oxygen-containing moieties on the edges of the carbon rings, above the plane of carbon rings, below the plane of carbon rings, or combinations of these). In certain embodiments, the carbon, oxygen, and hydrogen may be present in variable ratios. Graphene oxide may be obtained, for example, by treating graphite with strong oxidizers. In certain embodiments, the graphene oxide may include a dopant; in certain embodiments there is no dopant. Examples of dopants include boron and nitrogen. 
     High Pressure: As used in the present disclosure, the term “high pressure” refers to a pressure of greater than atmospheric pressure (1 atmosphere). For example, an oil well is typically under conditions of high pressure during oil recovery because of the high temperature of the well, hydrostatic pressure from the column of water extending from the well bore to the oil-bearing formation, pressure induced by pumping fluid in and out of the reservoir, and internal sources of pressure such as from the gases and fluids in the reservoir. Examples of high pressure are, for example, at least 1 atmosphere, at least 10 pounds per square inch gauge (psig), at least 50 psig, at least 100 psig, at least 200 psig, at least 500 psig, at least 1000 psig, at least 2000 psig, at least 3000 psig, or at least 5000 psig. 
     High Temperature: As used in the present disclosure, the term “high temperature” refers to a temperature from about 80° C. to about 100° C. For example, an oil reservoir, during drilling or oil recovery, may have a temperature of 80° C. to 100° C. or greater. 
     Improve, Increase, Reduce, Decrease: As used in the present disclosure, the terms “improve”, “increase”, “reduce, “decrease”, or their grammatical equivalents, indicate values that are relative to a baseline or other reference measurement. In certain embodiments, an appropriate reference measurement may be or comprise a measurement under particular reference conditions (for example, at a temperature near an average ambient temperature) absent the presence of (for example, prior to) a particular change in these conditions (for example, a change in temperature). 
     Stable: As used in the present disclosure, the term “stable” refers to not substantially changing in physical properties or not substantially deteriorating in performance over a usable lifetime. For example, a stable nanocomposite does not undergo substantial physical changes during a predetermined useable lifetime of the product in which the nanocomposite is used. For example, a stable electrode for a rechargeable battery substantially retains its charge capacity after repeated use. 
     Substantially: As used in the present disclosure, the term “substantially” refers to the qualitative condition of exhibiting total or near-total extent or degree of a characteristic or property, where “near-total” means within 20%, 10%, 5%, 1%, or 0.5% of the total (in either direction). 
     Two-dimensional (2D) material: As used in the present disclosure, the term “2D material” refers to a material substantially composed of ultrathin sheets having a thickness defined by a monolayer approximately one atom thick. For example, graphene, reduced graphene oxide, hexagonal boron nitride, and the like are two-dimensional materials. In certain embodiments, the 2D material may include a dopant; in certain embodiments there is no dopant. Examples of dopants include carbon, boron, and nitrogen, 
     Thermal Stability: As used in the present disclosure, the term “thermal stability” refers to a measure of the extent to which a material is stable at high temperature. For example, an electrode material with a superior thermal stability will remain stable at high temperature, while an electrode material with an inferior thermal stability will likely undergo changes (for example, chemical or structural transformations) leading to decreased performance. 
     Ultrathin: As used in the present disclosure, the term “ultrathin” refers to having a thickness defined by a monolayer within one or two orders of magnitude of the thickness of a single atom. For example, a plurality of ultrathin sheet may have an average sheet thickness no greater than 20 nm, for example, in a range from 5 nm to 20 nm. In other embodiments, an ultrathin sheet may have an average thickness equal to the diameter of no greater than 10 atoms, no greater than 5 atoms, no greater than 3 atoms, no greater than 2 atoms, or about 1 atom. For example, an ultrathin sheet may have a thickness from about 0.3 nm to 1.5 nm. 
     DETAILED DESCRIPTION 
     It is contemplated that systems, architectures, devices, methods, and processes described in the present disclosure encompass variations and adaptations developed using information from the embodiments described in the present disclosure. Adaptation, modification, or both of the systems, architectures, devices, methods, and processes described in the present disclosure may be performed, as contemplated by this description. 
     Throughout the description, where articles, devices, systems, and architectures are described as having, including, or comprising specific components, or where processes and methods are described as having, including, or comprising specific steps, it is contemplated that, additionally, there are articles, devices, systems, and architectures of the present disclosure that consist essentially of, or consist of, the recited components, and that there are processes and methods according to the present disclosure that consist essentially of, or consist of, the recited processing steps. 
     It should be understood that the order of steps or order for performing certain action is immaterial so long as the disclosure remains operable. Moreover, two or more steps or actions may be conducted simultaneously. 
     The mention in the present disclosure of any publication, for example, in the Background section, is not an admission that the publication serves as prior art with respect to any of the claims presented in the present disclosure. The Background section is presented for purposes of clarity and is not meant as a description of prior art with respect to any claim. 
     Headers are provided for the convenience of the reader—the presence, placement, or both of a header is not intended to limit the scope of the subject matter described in the present disclosure. 
     The present disclosure encompasses a recognition of the synergistic effects of combining two different two-dimensional (2D) materials with a plurality of transition metal oxide nanoparticles. For example, a nanocomposite that includes a plurality of hexagonal boron nitride sheets, a plurality of reduced graphene oxide sheets, and a plurality of Co 3 O 4  nanoparticles may provide improved thermal properties and improved electrochemical properties when used as an electrode material in a rechargeable battery. For example, a nanocomposite in which the weight percent of the plurality of ultrathin reduced graphene oxide sheets is in a range from 0.1% to 20% and the weight percent of the plurality of ultrathin boron nitride sheets is in a range from 0.1% to 50% may exhibit an enhanced specific surface area, an improved specific charge/discharge capacity, and a stable cycling performance at both room temperature (for example, about 25° C.) and at high temperatures (for example, at about 100° C. or greater). 
     In certain embodiments, the batteries (for example, lithium-ion batteries or lithium-sulfur batteries) described in the present disclosure can be used to power downhole equipment which is used to measure conditions inside oil wells or during other oil operations, for example during oil discovery and recovery. For example, downhole equipment includes pressure and temperature sensors for measuring the pressure and temperature, respectively, in an oil well during drilling and oil recovery. For example, conditions in an oil well can be variable with temperatures in a range from 80° C. to 100° C. or greater. The ability to monitor these conditions allows drilling and oil recovery to be performed more effectively and for potential safety concerns (for example, caused by sudden increases in temperature, pressure, or both) to be identified early such that the risks of damage to equipment and human injury are greatly reduced. The rechargeable batteries described in the present disclosure may have improved safety, electrochemical properties, and stability compared to those of conventional batteries used to power downhole equipment. For example, the lithium-ion batteries and lithium-sulfur batteries described in the present disclosure provide lightweight power sources with an improved energy density, cycle life, and structural stability than batteries employing conventional electrode materials. 
     In certain embodiment, the rechargeable batteries described in the present disclosure obviate (or decrease) the need for complex engineering techniques and safety devices that may otherwise be used in an attempt to limit the likelihood of thermal runaway. For example, while safety devices may relieve high pressure in a battery to help prevent thermal runaway, such devices are not 100% effective or completely reliable. Instead, the rechargeable batteries described in the present disclosure provide a more cost-effective and safer option for preventing thermal runaway without relying on complex safety devices. 
     Nanocomposites 
     Preparing Precursor(s) to 2D Material(s) 
       FIG.  1 A  shows an illustrative example of a method  100  for preparing a nanocomposite, according to an illustrative embodiment. In certain embodiments, the method, optionally, begins with preparing a precursor to the first 2D material in Step  110 . As an illustrative example of this step,  FIG.  1 B  shows an example method  102  for preparing graphene oxide from graphite. 
     As shown in the illustrative example of  FIG.  1 B , graphite is oxidized in sulfuric acid (Step  112 ). The concentration of the graphite is about 5 milligrams per milliliter (mg/mL) or more. For example, the concentration of the added graphite may be in a range from about 5 mg/mL to about 20 mg/mL. The concentration of sulfuric acid is at least 1 mole per liter (mol/L). For example, the concentration of sulfuric acid may be in a range from 1 mol/L to 3 mol/L. 
     In Step  114 , potassium permanganate is added to the mixture that was prepared in Step  112 . Potassium permanganate is added to achieve a final concentration of potassium permanganate of at least 1 mol/L. For example, the concentration of the potassium permanganate may be in a range from 1 mol/L to 2 mol/L. In Step  114 , potassium permanganate is added to the mixture prepared in Step  112  at a volume ratio of 1:1 (volume potassium permanganate solution:volume of sulfuric acid solution). In certain embodiments, the mixture prepared in Step  112  may be cooled to 20° C. or less prior to the addition of potassium permanganate. 
     In Step  116 , the mixture prepared in Step  114  is stirred or mixed. For example, the mixture may be stirred for 5 minutes (min), 10 min, 30 min, 1 hour, 12 hours, or a similar time interval. For example, the mixture may be stirred mechanically, agitated with a magnetic stir bar, or exposed to ultrasonic irradiation. The method of stirring may be selected to correspond to the size of vessel used to prepare the mixture in Step  112  and Step  114 . Mixing or stirring in Step  116  may be performed at a temperature in a range from about 30° C. to 40° C. 
     Following Step  116 , the reaction was completed in Step  118 . For example, solids in the mixture are separated from the liquids (for example, via centrifugation and removal of the supernatant). The solids are then redispersed in a reaction fluid to complete the oxidation reaction. In certain embodiments, the reaction fluid may include hydrogen peroxide (H 2 O 2 ). The concentration of hydrogen peroxide in the reaction fluid is at least 0.1 mol/L. For example, the concentration of hydrogen peroxide may be in a range from 0.1 mol/L to 0.3 mol/L. In certain embodiments, the reaction fluid can include sodium percarbonate. Graphene oxide is produced after Step  118 . 
     After the reaction is completed in Step  118 , the solid product is separated from the reaction fluid and dried to obtain a graphene oxide powder in Step  120 . The material may be filtered using centrifugation, filter paper, vacuum filtration, or combinations of these. For example, the material may be dried at room temperature or at 50° C., 60° C., 70° C., or 80° C. to obtain a dry powder of graphene oxide. For example, the product may be dried for 1 hour, 2 hours, 6 hours, 12 hours, 24 hours, or similar intervals of time. 
     In certain embodiments, the preparation of graphene oxide may not be required. For example, graphene oxide may be purchased (for example, as a dry powder or dispersed in a fluid) and used as-received. In certain embodiments, graphene oxide sheets may be modified before use. For example, graphene oxide may be washed, purified, filtered, dried, or combinations of the same before further use. 
     Preparing Transition Metal Nanoparticles/2D Material 
     Returning to  FIG.  1 A , a sample that includes a plurality of transition metal oxide nanoparticles (TMO NPs) and a plurality of ultrathin sheets of a first 2D material (i.e., a TMO NPs/first 2D material sample) is prepared in Step  130  of example method  100 . The first 2D material can be a 2D carbon material (for example, graphene, graphene oxide, or reduced graphene oxide), a 2D nitride (for example, functionalized boron nitride or hexagonal boron nitride), a 2D metal chalcogenide (for example, MoS 2 , SnS 2 , TiS 2 , WS 2 , MoSe 2 , or WSe 2 ), a 2D oxide (for example, TiO 2 , ZnO, MnO 2 , or a perovskite), or a 2D hybrid material (for example, MoS 2 /graphene or MoSe 2 /MnO 2 ). For example, the first 2D material may be graphene or reduced graphene oxide. 
       FIG.  1 C  shows an illustrative example of method  104  for preparing a TMO NPs/first 2D material sample. In Step  132  of example method  104 , graphene oxide (for example, prepared in Step  104  of method  100  shown in  FIG.  1 A  or obtained otherwise) is added to a solution that includes a cobalt-containing salt. For example, the cobalt-containing salt may be cobalt (II) acetate tetrahydrate (Co(C 2 H 3 O 2 ) 2 ), cobalt nitrate, or cobalt chloride. The concentration of the cobalt-containing salt in the solution is in a range from 0.01 mol/L to 0.5 mol/L. The concentration of graphene oxide in the solution is in a range from 1 mg/mL to 3 mg/mL. For example, the concentration of graphene oxide in the solution may be 2 mg/mL. 
     In certain embodiments, the mixture obtained in Step  132  is stirred or mixed. The mixture is stirred for 5 min, 10 min, 30 min, 1 hour, 12 hours, or a similar interval of time. For example, the mixture may be stirred mechanically, agitated with a magnetic stir bar, or exposed to ultrasonic irradiation. For example, the method of stirring may be selected to correspond to the size of vessel used to prepare the Co 3 O 4 /RGO sample in Step  132 . 
     Step  134  of example method  104  includes the hydrothermal microwave irradiation of the mixture from Step  132 . In this step, the mixture is exposed to microwaves under a high pressure at a high temperature. For example, the mixture is heated (for example, in an autoclave) to a temperature of at least 140° C. For example, the mixture may be heated to a temperature in a range from 140° C. to 220° C. For example, the mixture may be heated to a temperature of 180° C. During Step  134 , the mixture is held in a vessel (for example, an autoclave) at a pressure of at least 150 psi. For example, the mixture may be held in a vessel at a pressure in a range from 150 psi to 350 psi. In Step  134 , the mixture is irradiated with microwaves at a power in a range from 900 W to 1800 W. For example, hydrothermal microwave irradiation may be performed for a reaction time in a range from 30 minutes to 60 minutes. 
     In Step  136 , the mixture is washed. For example, solids in the mixture are separated from the liquids based on density (for example, by centrifugation and removal of the supernatant). The solids are then redispersed in a washing fluid to remove residual materials from the solid product. This process may be repeated multiple times. The washing fluid may include distilled water, another solvent (for example, an organic solvent), one or more salts, an acid (for example, dilute hydrochloric acid), or combinations of these. 
     After the solid material is washed in Step  136 , it is separated from the washing fluid and dried to obtain a nanocomposite of the transition metal nanoparticles and the first 2D material in Step  138 . The material may be filtered using centrifugation, filter paper, vacuum filtration, or combinations of these. The material is dried at room temperature or at a temperature of 30° C., 40° C., 50° C., or 60° C. to obtain a dry powder of the TMO NPs/2D material. For example, the product may be dried for 1 hour, 2 hours, 6 hours, 12 hours, 24 hours, or similar intervals of time. 
     A scanning electron micrograph of example transition metal nanoparticles is shown in  FIG.  6 A . As shown in the micrograph, at least a portion of the plurality of transition metal nanoparticles have an average particle size of less than 300 nm. For example, at least a portion of the plurality of transition metal nanoparticles have an average particle size in a range from 30 nm to 45 nm and have a particle-size distribution with a standard deviation of 2 nm. Average particle size can be assessed, for example, using scanning electron microscopy. At least a portion of the plurality of transition metal nanoparticles may have an approximately rectangular prism shape like those shown in  FIG.  6 A . 
     At least a portion of the cobalt oxide has a cubic-spinel crystal structure. For example, a cubic-spinel crystal structure may be determined based on an intensity (or a relative intensity) of one or more peaks in an X-ray diffraction (XRD) pattern of the plurality of transition metal nanoparticles. For example, a cubic-spinel crystal structure may be determined based on an interplanar spacing measured with selected area electron diffraction (SAED) analysis. 
     The weight percent of the plurality of ultrathin sheets of the first 2D material may be in a range from 0.1% to 20%, where the weight percent is based on the total weight of the plurality of transition metal oxide nanoparticles, the plurality of ultrathin sheets of the first 2D material, and the plurality of ultrathin sheets of the second 2D material in the nanocomposite. 
     In certain embodiments, at least a portion of the plurality of ultrathin sheets of the first 2D material (for example, the reduced graphene oxide sheets) has an average sheet thickness of less than 20 nm. For example, at least a portion of the plurality of ultrathin sheets of the first 2D material (for example, the reduced graphene oxide sheets) may have an average sheet thickness in a range from 5 nm to 20 nm. For example, at least a portion of the plurality of ultrathin sheets of the first 2D material (for example, the reduced graphene oxide sheets) may have an average sheet thickness in a range from 5 nm to 10 nm. Average sheet thickness can be assessed, for example, using scanning electron microscopy. 
     Preparing Second 2D Material 
     Returning to  FIG.  1 A , a plurality of ultrathin sheets of a second 2D material are prepared in Step  150 . As an illustrative example of this step,  FIG.  1 D  shows example method  106  for preparing a plurality of functionalized boron nitride sheets. 
     In Step  152  of method  106 , boron nitride is oxidized. Boron nitride may be oxidized in a mixture of hydrogen peroxide and sulfuric acid. The mixture of hydrogen peroxide and sulfuric acid may have a volumetric ratio of hydrogen peroxide to sulfuric acid (H 2 O 2 :H 2 SO 4 ) in a range from 1:0.5 to 1:3. Boron nitride is added to this solution to achieve a concentration in a range from 0.5 mg/mL to 12 mg/mL. 
     Following Step  152 , the mixture may be stirred or mixed. For example, the mixture may be stirred for 5 min, 10 min, 30 min, 1 hour, 12 hours, or a similar interval of time. For example, the mixture may be stirred mechanically, agitated with a magnetic stir bar, exposed to ultrasonic irradiation, or combinations of these. For example, the method of stirring may be selected to correspond to the size of vessel used to prepare the plurality of ultrathin sheets of the second 2D material in method  106 . 
     Step  154  of example method  106  includes hydrothermal microwave irradiation of the mixture from Step  152 . In Step  154 , the mixture is exposed to microwaves under a high pressure at a high temperature. The mixture is heated (for example, in an autoclave) to a temperature of at least 140° C. For example, the mixture may be heated to a temperature in a range from 140° C. to 220° C. For example, the mixture may be heated to a temperature 180° C. During Step  154 , the mixture is held in a vessel (for example, an autoclave) at a pressure of at least 150 psi. For example, the mixture may be held in a vessel at a pressure in a range from 150 psi to 350 psi. In Step  154 , the mixture may be irradiated with microwaves at a power in a range from 900 W to 1800 W. Hydrothermal microwave irradiation in Step  154  may be performed for a reaction time in a range from 30 minutes to 60 minutes or more. 
     In Step  156 , the mixture is washed. For example, solids in the mixture may be separated from the liquids based on density (for example, by centrifugation and removal of the supernatant). The solids may then be redispersed in a washing fluid to remove residual materials from the solid product. This process may be repeated multiple times. The washing fluid may include distilled water, another solvent (for example, an organic solvent), one or more salts, an acid (for example, dilute hydrochloric acid), or combinations of these. 
     After the solid material is washed in Step  156 , it may be separated from the washing fluid and dried to obtain a functionalized boron nitride powder in Step  158 . The material may be filtered using centrifugation, filter paper, vacuum filtration, or combinations of these. For example, the material may be dried at room temperature or at a temperature of 30° C., 40° C., 50° C., or 60° C. to obtain a dry powder of the ultrathin sheets of the 2D material. For example, the product may be dried for 1 hour, 2 hours, 6 hours, 12 hours, 24 hours, or similar intervals of time. 
     The second 2D material can be a 2D carbon material (for example, graphene, graphene oxide, or reduced graphene oxide), a 2D nitride (for example, functionalized boron nitride or hexagonal boron nitride), a 2D metal chalcogenide (for example, MoS 2 , SnS 2 , TiS 2 , WS 2 , MoSe 2 , or WSe 2 ), a 2D oxide (for example, TiO 2 , ZnO, MnO 2 , or a perovskite), or a 2D hybrid material (for example, MoS 2 /graphene or MoSe 2 /MnO 2 ). For example, the second 2D material may be hexagonal boron nitride, boron nitride, or functionalized boron nitride (for example, functionalized via chemical oxidation (Step  152 ) and hydrothermal microwave irradiation (Step  154 ), as shown in  FIG.  1 D ). The weight percent of the plurality of ultrathin sheets of the second 2D material in the nanocomposite is in a range from 0.1% to 50%, where the weight percent is based on the total weight of the plurality of transition metal oxide nanoparticles, the plurality of ultrathin sheets of the first 2D material, and the plurality of ultrathin sheets of the second 2D material in the nanocomposite. 
     At least a portion of the plurality of ultrathin sheets of the second 2D material (for example, the functionalized boron nitride sheets) has an average sheet thickness of less than 20 nm. For example, at least a portion of the plurality of ultrathin sheets of the second 2D material may have an average sheet thickness in a range from 5 to 20 nm. For example, at least a portion of the plurality of ultrathin sheets of the second 2D material may have an average sheet thickness in a range from 5 to 10 nm. 
     Without wishing to be bound to any particular theory, it is thought that the thermal, mechanical, and chemical properties of the second 2D material (for example, hexagonal boron nitride) may provide benefits to the nanocomposite and batteries described in the present disclosure. For example, the superior thermal stability of hexagonal boron nitride compared to that of common carbon materials may help to prevent thermal runaway events. For example, the mechanical properties of hexagonal boron nitride and reduced graphene oxide may allow the nanocomposite to better accommodate changes in the volume of the transition metal oxide nanoparticles during charging and discharging. When a first 2D material and second 2D material are combined, the chemical properties of the second 2D material (for example, hexagonal boron nitride) may improve the carrier mobility (for example, electron mobility) of the first 2D material (for example, reduced graphene oxide) via a substrate effect. For example, a nanocomposite that includes both a first 2D material and a second 2D material may have an increased carrier mobility (and thus improved electrochemical properties) compared to that of a nanocomposite the includes only the first 2D material or second 2D material alone. 
     It is thought, without wishing to be bound to any particular theory, that the use of two different 2D materials (for example, reduced graphene oxide and hexagonal boron nitride) in the nanocomposite may prevent restacking of the 2D materials when the nanocomposite is used as an anode material. For example, the nanocomposites described in the present disclosure may be less prone to restacking during charging and discharging, resulting in the retention of desirable physical and electrochemical properties. For example, the nanocomposite retains its large surface area and its superior specific capacity even after many (for example, 1,000 or more) charge/discharge cycles. 
     Mixing Materials and Drying 
     Returning to  FIG.  1 A , the TMO NPs/first 2D material sample from Step  130  and the second 2D material from Step  150  are contacted together (for example, added to a solvent and mixed) in Step  170  of method  100 . For example, at least a portion of the transition metal oxide nanoparticles and at least a portion of the ultrathin sheets of the first 2D material prepared in Step  130  may be added to a volume of solvent along with at least a portion of the ultrathin sheets of the second 2D material prepared in Step  150 . As an illustrative example of this step,  FIG.  1 E  shows example method  108  for combining the materials prepared in Step  130  and Step  150  to form a nanocomposite. 
     As shown in  FIG.  1 E , the TMO NPs/first 2D material sample is dispersed in a solvent (Step  172 ). The solvent may be ethanol, distilled water, isopropyl alcohol, acetone, dimethylformamide, or combinations of these. The TMO NPs/first 2D material sample is added to the solvent at a concentration in a range from 1 mg/mL to 3 mg/mL. The mixture obtained in Step  172  may be stirred or mixed. For example, the mixture may be stirred for 5 min, 10 min, 30 min, 1 hour, 12 hours, or a similar interval of time. The mixture may be stirred mechanically, agitated with a magnetic stir bar, exposed to ultrasonic irradiation, or combinations of the same. The method of stirring may be selected to correspond to the size of vessel in which the TMO NPs/first 2D material are added to solvent in Step  172 . 
     In Step  174 , a plurality of sheets of the second 2D material (for example, from Step  150  of  FIG.  1 A ) are added to the mixture prepared in Step  172 . The second 2D material (for example, hexagonal boron nitride) may be dispersed in a fluid (for example, water, a salt solution, or a solvent), and this mixture may be added to the mixture from Step  172 . Alternatively, a dry powder of the second 2D material may be added to the mixture from Step  172 . The second 2D material is added to achieve a concentration of at least 1 mg/mL of the second 2D material in the mixture. For example, the concentration of the second 2D material in the mixture prepared in Step  174  may be in a range from 1 mg/mL to 3 mg/mL. 
     Step  176  of example method  108  includes the hydrothermal microwave irradiation of the mixture from Step  174 . The mixture from Step  174  is exposed to microwaves under a high pressure at a high temperature. The mixture is heated (for example, in an autoclave) to a temperature of at least 140° C. For example, the mixture may be heated to a temperature in a range from 140° C. to 220° C. For example, the mixture may be heated to a temperature 180° C. The mixture is held in a vessel (for example, an autoclave) at a pressure of at least 150 psi. For example, the mixture may be held in a vessel at a pressure in a range from 150 psi to 350 psi. The mixture is irradiated with microwaves at a power in a range from 900 W to 1800 W. Hydrothermal microwave irradiation may be performed for a reaction time in a range from 30 minutes to 60 minutes or more. 
     In Step  178 , the mixture is washed. Solids in the mixture are separated from the liquids based on density (for example, by centrifugation and removal of the supernatant). The solids are then dispersed in a washing fluid to remove residual materials from the solid product. This process may be repeated multiple times. The washing fluid may include distilled water, another solvent (for example, an organic solvent), one or more salts, an acid (for example, dilute hydrochloric acid), or combinations of these. 
     After the solid material is washed in Step  178 , it may be separated from the washing fluid and dried to obtain a powder of the final nanocomposite in Step  180 . The material may be filtered using centrifugation, filter paper, vacuum filtration, or combinations of these. For example, the material may be dried at room temperature or at a temperature of 30° C., 40° C., 50° C., or 60° C. to obtain a dry powder of the nanocomposite. For example, the product may be dried for 1 hour, 2 hours, 6 hours, 12 hours, 24 hours, or a similar interval of time. 
       FIG.  2 A  is a block diagram showing a nanocomposite  200 , according to an illustrative embodiment. For example, nanocomposite  200  includes a plurality of transition metal oxide nanoparticles  220 , a plurality of ultrathin sheets of a first two-dimensional (2D) material  210 , and a plurality of ultrathin sheets of a second two-dimensional (2D) material  230  where the second 2D material is of a different type than the first 2D material. An illustrative example of a nanocomposite  201  is shown in  FIG.  2 B . As shown in  FIG.  2 B , example nanocomposite  201  includes a plurality of reduced graphene oxide sheets  240 , a plurality of transition metal oxide nanoparticles  250 , and a plurality of hexagonal boron nitride sheets  260 . 
     The nanocomposite (for example, the nanocomposite from Step  180  of  FIG.  1 E ), may have a component weight ratio (x:y:z) in a range from (1:0.001:0.001) to (1:0.67:1.67), where x is the plurality of transition metal oxide nanoparticles, y is the plurality of ultrathin sheets of the first 2D material, and z is the plurality of ultrathin sheets of the second 2D material. 
     The nanocomposite (for example, obtained in Step  180  of  FIG.  1 E ) may have a specific surface area in a range from 10 m 2 /g to 500 m 2 /g. For example, the nanocomposite may have a specific surface area in a range from 10 m 2 /g to 200 m 2 /g. For example, the specific surface area may correspond to a Brunauer-Emmett-Teller (BET) specific surface area which is measured via a nitrogen adsorption-desorption isotherm (for example, as shown in the illustrative example of  FIG.  9 D ). 
     Lithium-Ion Batteries and Lithium-Sulfur Batteries 
     The nanocomposites described previously may be used as electrode materials in rechargeable batteries (for example, lithium-ion and lithium-sulfur batteries) designed to tolerate operation at high temperatures and high pressures.  FIG.  3 A  is a block diagram of example lithium-ion battery  300  designed for this purpose. Lithium-ion battery  300  also includes an anode material  320 , an electrolyte  330 , a separator  340 , and a cathode  350 . The anode includes an anode material  301 , which includes a TMO NPs/first 2D material/second 2D material nanocomposite  305  (for example, obtained in Step  180  of  FIG.  1 E ) and other additive(s)  310 . For example additive(s)  310  may include a binding agent, a conductive additive, or both. For example, the binding agent may be polyvinylidene fluoride or styrene butadiene. The conductive additive may, for example, be carbon black or a carbon nanotube-based conductive material. The solvent may, for example, be N-methyl-2-pyrrolidone or tetrahydrofuran. 
     A summed weight percent of additive(s)  310  (for example, a binding agent and a conductive additive) in the nanocomposite is in a range from 5% to 20% where the weight percent is based on the total weight of (i) the plurality of transition metal oxide nanoparticles, (ii) the plurality of ultrathin sheets of the first 2D material, (iii) the plurality of ultrathin sheets of the second 2D material, and (iv) any additive(s)  310  present in the nanocomposite. For example, the amount of the binding agent in the nanocomposite may be zero, or the amount of conductive additive in the nanocomposite may be zero. Alternatively, the nanocomposite may contain both the binding agent and the conductive additive. A summed weight percent of the binding agent and the conductive additive in the nanocomposite may be about 10%. 
     For lithium-ion battery  300 , cathode  350  may be, for example, a lithium metal or a lithium metal oxide. For lithium-ion battery  300 , electrolyte  330  may be, for example, one or more lithium salts dissolved in one or more organic solvents. For example, the one or more lithium salts may include lithium hexafluorphosphate. The organic solvents may include, for example, ethylene carbonate or dimethyl carbonate. Separator  340  may be a polypropylene membrane that is placed between the anode and the cathode. 
     In certain embodiments, the lithium-ion battery may exhibit an improved electrochemical performance at both room temperature (for example, at about of 25° C.) and at high temperatures (for example, of 100° C. or greater). For example, the lithium-ion battery may have a specific capacity (for example, specific charge/discharge capacity) in range from 60 mAh/g to 800 mAh/g or greater at about 25° C. For example, the lithium-ion battery may have a have a specific capacity (for example, specific charge/discharge capacity) in range from 1 mAh/g to 5 mAh/g or greater at about 100° C. 
     A lithium-ion battery that includes the nanocomposite described in the present disclosure may retain beneficial electrochemical characteristics after multiple charge/discharge cycles at both room temperature (for example, at about of 25° C.) and high temperatures (for example, of 100° C. or greater). For example, after 100 charge/discharge cycles at about 25° C. or 100° C., the lithium-ion battery may retain at least 90% of its specific capacity compared to an initial specific capacity measured in the first charge cycle at the same temperature. For example, after 1,000 charge/discharge cycles at about 25° C. or 100° C., the lithium-ion battery may retain at least 90% of its specific capacity compared to an initial specific charge capacity measured in the first charge cycle at the same temperature. For example, after 100 charge/discharge cycles at about 25° C. or 100° C., the coulombic efficiency of the lithium-ion battery may be 90% or greater. For example, after 1,000 charge/discharge cycles at about 25° C. or 100° C., the coulombic efficiency of the lithium-ion battery may be 90% or greater. 
     In certain embodiments, the nanocomposites described in the present disclosure can be used as a cathode material for lithium-sulfur batteries.  FIG.  3 B  shows an illustrative example of a lithium-sulfur battery  303 . Lithium-sulfur battery  303  includes cathode  325 , electrolyte  335 , separator  345 , and anode  355 . Cathode  325  includes a TMO NPs/first 2D material/second 2D material nanocomposite  305  (for example, obtained in Step  180  of  FIG.  1 E ) and other additive(s)  315 . To prepare a cathode material for lithium-sulfur batteries, the nanocomposite  302  may further include sulfur, for example, as one of additive(s)  315 . Nanocomposite  302  may include sulfur in the form of elemental sulfur, a sulfur-containing salt, a sulfur- and lithium-containing salt, a sulfur/graphene composite, or combinations of the same. 
     For a nanocomposite that includes sulfur, the weight percent of sulfur in the nanocomposite is in a range from 40% to 80% where the weight percent is based on total weight of (i) the plurality of transition metal oxide nanoparticles, (ii) the plurality of ultrathin sheets of the first 2D material, (iii) the plurality of ultrathin sheets of the second 2D material, (iv) any binding agent, conductive additive, or both present in the nanocomposite, and (v) the sulfur. For example, a weight percent of sulfur in the nanocomposite may be in a range from 60% to 80%. For example, a weight percent of sulfur in the nanocomposite may be in a range from 70% to 80%. 
     For lithium-sulfur battery  303 , anode  355  may be, for example, a lithium metal. For lithium-sulfur battery  303 , electrolyte  335  may be, for example, one or more lithium salts dissolved in one or more organic solvents. For example, the lithium salts may include bis(trifluoromethane)sulfonimide lithium salt (LiTFSI). For example, the organic solvents may include 1,2-dimethoxyethane (DME) or 1,3-dioxolane (DOL). Separator  345  may be a polypropylene membrane that is placed between the anode and the cathode. 
     In certain embodiments, the nanocomposite is a film with a thickness in a range from 50 μm to 200 μm. For example, the nanocomposite may be a film with a thickness in a range from 10 μm to 20 μm. A film of the nanocomposite may be prepared on a current collector such as a copper foil. For example, a homogeneous slurry of the nanocomposite (for example, the plurality of transition metal oxide nanoparticles, the plurality of ultrathin sheets of the first 2D material, the plurality of ultrathin sheets of the second 2D material, any binding agent, conductive additive, or both present in the nanocomposite, and any sulfur present in the nanocomposite) in a solvent may be spread on a copper foil and allowed to dry. 
     EXPERIMENTAL EXAMPLES 
     Example 1: X-Ray Diffraction and Raman Spectroscopy of Nanocomposites 
     In order to confirm the synergistic properties of the components, the properties of example nanocomposite (Co 3 O 4 /RGO/h-BN—sample d) were compared to those of transition metal nanoparticles alone (Co 3 O 4 —sample a), a composite of transition metal oxide nanoparticles with a first 2D material (Co 3 O 4 /RGO—sample b), and a composite of transition metal nanoparticles with a second 2D material (Co 3 O 4 /h-BN—sample c). Table 1 shows a summary of the nanocomposites that were studied and their compositions. 
     
       
         
           
               
             
               
                 TABLE 1 
               
             
            
               
                   
               
               
                 Summary of materials studied and their compositions 
               
               
                 (weight percent based on total weight of the material). 
               
            
           
           
               
               
               
               
               
            
               
                   
                 Sample 
                 Co 3 O 4   
                 RGO 
                 h-BN 
               
               
                   
                   
               
            
           
           
               
               
               
               
               
            
               
                   
                 (a) Co 3 O 4   
                 100% 
                 — 
                 — 
               
               
                   
                 (b) Co 3 O 4 /RGO 
                 85% 
                 15% 
                 — 
               
               
                   
                 (c) Co 3 O 4 /h-BN 
                 85% 
                 — 
                 15% 
               
               
                   
                 (d) Co 3 O 4 /RGO/h-BN 
                 57% 
                 10% 
                 33% 
               
               
                   
                   
               
            
           
         
       
     
     XRD studies were performed on these samples with a Rigaku miniflex 600 X-ray diffractometer (Japan) using Cu Kα radiation (1.54430 angstrom (Å)) at 30 kilovolts (kV) and 40 milliamps (mA). XRD studies were first performed to identify characteristic peaks for Co 3 O 4 , reduced graphene oxide (RGO), and hexagonal boron nitride (h-BN). 
     The diffraction peaks of Co 3 O 4  were indexed to those of pure Co 3 O 4  with a cubic spinel structure (Joint Committee on Powder Diffraction Standards (JCPDS) card no. 76-1802). Peaks related to the presence of Co 3 O 4  are marked with an asterisk (*) in  FIG.  4    (as shown in the legend to  FIG.  4   ). The reduced graphene oxide (RGO) sheets exhibited a peak at about 2θ=23°, which was attributed to (002) RGO (as shown in the legend to FIG.  4 ). For the h-BN sheets, a peak was observed near 2θ=26°, which was attributed to (002) h-BN (as shown in the legend to  FIG.  4   ). 
     The XRD patterns for samples a, b, c, and d (see Table 1) are shown in  FIG.  4   . According to these results, each of the samples contained appropriate peaks for the components present in the corresponding sample. Both the Co 3 O 4  nanoparticles (sample a) and the Co 3 O 4 /RGO nanocomposite (sample b) exhibited a broad diffraction peak near 2θ=23° which corresponds to the (002) indicates the presence of RGO as shown in  FIG.  4   . 
     Raman spectroscopy was performed using an I-RAMAN® plus Raman spectrometer (USA) to determine the crystallographic structures of the different samples. The Raman spectra of samples a, b, c, and d are shown in  FIG.  5   . The Raman spectra of Co 3 O 4  (sample a) included bands at about 478 cm −1  (Eg), 521 cm −1  (F 2 g), 611 cm −1  (F 2 g), and 689 cm −1  (A 1g ), confirming the cubic spinel structure of Co 3 O 4 . The peak at 689 cm −1  (A 1 g) corresponded to octahedral sites in Co 3 O 4 , and the peaks at 478 cm −1  (Eg), 521 cm −1  (F 2 g), and 611 cm −1  (F 2 g) were attributed to the combined vibrations of tetrahedral sites and octahedral oxygen motion in Co 3 O 4 . 
     The nanocomposites containing RGO (samples b and d) exhibited peaks at 1327 cm −1  and 1584 cm −1 , which corresponded to the D band and G band of graphene, respectively. The D band may be associated with the breathing mode of k-point phonons with an A 1 g symmetry. The G band may be associated with an E 2 g phonon from sp 2  carbon atoms in the RGO. For the sample containing h-BN (sample c), a single peak was observed at 1365 cm −1 , corresponding to in-plane vibrations (E 2 g). 
     Example 2: Microstructure of Nanocomposites 
     The microscale morphologies of samples a, b, c, and d were observed using scanning electron microscopy (JEOL SEM (USA) and ZEISS FESEM (Germany)).  FIG.  6 A  is a scanning electron micrograph of example Co 3 O 4  nanoparticles (sample a). As shown in  FIG.  6 A , the Co 3 O 4  nanoparticles exhibited a rectangular prism shape. 
       FIG.  6 B  and  FIG.  6 C  show scanning electron micrographs of an example Co 3 O 4 /RGO sample (sample b) and an example Co 3 O 4 /h-BN sample (sample c), respectively. As shown in  FIG.  6 B , the Co 3 O 4 /RGO nanocomposite contained rectangular prism-shaped Co 3 O 4  nanoparticles on the surface of RGO sheets. These particles were nonporous and non-spherical. Similarly, as shown in  FIG.  6 C  rectangular prism-shaped Co 3 O 4  nanoparticles were observed on the surfaces of the h-BN sheets in the Co 3 O 4 /h-BN sample. 
       FIG.  6 D  shows a scanning electron micrograph of an example Co 3 O 4 /RGO/h-BN nanocomposite (sample d). The Co 3 O 4 /RGO/h-BN nanocomposite exhibited rectangular prism-shaped Co 3 O 4  nanoparticles that were anchored between the transparent h-BN sheets and RGO sheets. Accordingly, the Co 3 O 4  nanoparticles in the Co 3 O 4 /RGO/h-BN nanocomposite effectively prevented the sheets from restacking, providing space for the transport of electrolyte and ions in the final electrode materials and allowing the large surface area of the corresponding electrode to remain accessible to the electrolyte after multiple charge/discharge cycles. 
     Example 3: Thermal Properties 
     Thermogravimetric analysis (TGA) was performed to determine the thermal stability of samples a, b, c, and d at temperatures from 25° C. to 550° C. The resulting TGA curves—which are plots of weight (in percent of initial weight at the starting temperature) versus temperature—are shown in  FIG.  7   . Samples a, b, c, and d lost about 3.5%, 10%, 4%, and 5% of their initial weight, respectively, over the temperature range studied. The TGA curves can be divided into three temperature regions based on the extent of weight loss. In the first region (less than 100° C.), only 1% decomposition was observed for sample b (Co 3 O 4 /RGO). This weight loss was attributed to the removal of adsorbed water. 
     In the second temperature region (from 100° C. to 300° C.), sample c (Co 3 O 4 /h-BN) exhibited a weight loss of only about 2% at about 225° C. Meanwhile, sample b (Co 3 O 4 /RGO) exhibited a weight loss of about 4% at about 250° C. The weight losses for these samples in temperature region  2  were attributed to the decomposition of epoxy and hydroxyl groups in RGO and hydroxyl groups in h-BN. These results confirmed that the majority of oxygen-containing groups in the original graphene oxide were reduced to RGO during synthesis of the RGO sheets. Meanwhile, sample a (Co 3 O 4 ) exhibited a weight loss of only about 3% at about 300° C., and sample d (Co 3 O 4 /RGO/h-BN) remained relatively stable at 550° C. with a total loss of 5%. No peaks were observed for the decomposition of sample d. These results indicated that the oxygen-containing groups introduced to the h-BN sheets during the functionalized process no longer remained at a high temperature. 
     Derivative plots of the TGA curves (DTG curves) from  FIG.  7    are shown in  FIG.  8   . These plots show the change in weight over the change in temperature (dW/dT) of samples a, b, c, and d versus temperature. As shown in  FIG.  8   , the degradation of sample a (Co 3 O 4 ) began at about 300° C. For sample b (Co 3 O 4 /RGO), two degradation peaks were observed at about 250° C. and about 325° C. For sample c (Co 3 O 4 /h-BN), a single degradation peak was observed at an intermediate temperature of about 240° C. In contrast, sample d (Co 3 O 4 /RGO/h-BN) did not exhibit a sharp degradation peak. Instead, sample d only exhibited a low intensity peak beginning at about 350° C., indicating the superior thermal stability of the Co 3 O 4 /RGO/h-BN nanocomposite compared to those of the other samples (a, b, and c). The enhanced thermal stability of the Co 3 O 4 /RGO/h-BN nanocomposite compared to the other samples was attributed to the synergistic effects of RGO and h-BN. 
     Example 4: Surface Area of Nanocomposites 
     Specific surface areas of the samples were measured using the Brunauer-Emmett-Teller (BET) method.  FIG.  9 A  shows a nitrogen adsorption-desorption isotherm for sample a (Co 3 O 4 ). The BET specific surface area for the Co 3 O 4  nanoparticles was about 41 m 2 /g.  FIG.  9 B  shows a nitrogen adsorption-desorption isotherm for sample b (Co 3 O 4 /RGO). The BET specific surface area for the Co 3 O 4 /RGO sample was about 54 m 2 /g and was greater than that of the Co 3 O 4  nanoparticles alone.  FIG.  9 C  shows a nitrogen adsorption-desorption isotherm for sample c (Co 3 O 4 /h-BN). The BET specific surface area of the Co 3 O 4 /h-BN sample (12 m 2 /g) was less than that of all of the other samples.  FIG.  9 D  shows a nitrogen adsorption-desorption isotherm for sample d (Co 3 O 4 /RGO/h-BN). The BET specific surface area for the Co 3 O 4 /RGO/h-BN nanocomposite (about 191 m 2 /g) was greater than those of the other samples. Accordingly, the Co 3 O 4 /RGO/h-BN nanocomposite had the largest available surface area per weight of material. This increased surface area can facilitate charge transfer in electrode materials, for example, for lithium ion batteries or lithium-sulfur batteries. 
     The BET specific surface areas of each of samples a, b, c, and d are also presented in Table 2 alongside their electrochemical properties for comparison. 
     
       
         
           
               
             
               
                 TABLE 2 
               
             
            
               
                   
               
               
                 Specific charge/discharge capacities and BET 
               
               
                 surface areas of samples studied. 
               
            
           
           
               
               
               
               
            
               
                   
                 Current 
                   
                 BET 
               
               
                   
                 density 
                 Specific charge/discharge 
                 surface area 
               
               
                 Sample 
                 (mA/g) 
                 capacity (mAh/g) 
                 (m 2 /g) 
               
               
                   
               
            
           
           
               
               
               
               
            
               
                 Co 3 O 4   
                 200 
                 6/3 
                 41 
               
               
                 Co 3 O 4 /RGO 
                 200 
                 300/280 
                 54 
               
               
                 Co 3 O 4 /h-BN 
                 200 
                 19/5  
                 12 
               
               
                 Co 3 O 4 /RGO/h-BN 
                 200 
                 651/817 
                 191 
               
               
                   
               
            
           
         
       
     
     Example 5: Electrochemical Properties of Nanocomposites at Room Temperature 
     An anode material was prepared from each of samples a, b, c, and d. Batteries were assembled using these anode materials for electrochemical studies. In this experimental example, the working electrode was fabricated by mixing 90 weight percent (wt. %) of the sample (a, b, c, or d), 5 wt. % of the conductive agent carbon black, and 5 wt. % of the binding agent polyvinylidene fluoride in N-methyl-2-pyrrolidone solvent at a concentration of 100 mg/10 mL. A homogenous slurry of this mixture was obtained and spread as a film on a copper foil substrate, which acted as a current collector. This film was then allowed to dry at 60° C. under vacuum. Each working electrode contained about 1 mg of the corresponding sample (a, b, c, or d). The working electrode was then punched into disks, each with a diameter of about 14 millimeters (mm). 
     A polypropylene membrane (Celgard 2325, Celgard, Inc., USA) was used as a separator in the battery along with a lithium metal (purity 99.9%) counter electrode. The electrolyte was 1 mol/L lithium hexafluorophosphate (LiPF 6 ) in a 1:1 by volume mixture of ethylene carbonate (EC) and dimethyl carbonate (DMC). 
     The electrochemical performances of the assembled coin cell lithium-ion batteries were tested at both room temperature (at about 25° C.) and at a high temperature (at about 100° C.). Galvanostatic charge/discharge measurements were performed using the assembled batteries at a current density of 200 mA/g for a single cycle.  FIG.  10 A  shows the results of these measurements as plots of voltage versus specific capacity for lithium-ion batteries that included samples a, b, c, and d as anode materials. A battery that included the Co 3 O 4 /RGO/h-BN nanocomposite (sample d) exhibited increased charge and discharge capacities of 651 mAh/g and 817 mAh/g, respectively. A battery that included Co 3 O 4 /RGO (sample b) had the second largest charge and discharge capacities of 300 mAh/g and 280 mAh/g, respectively. Meanwhile, the charge and discharge capacities of a battery with Co 3 O 4 /h-BN (sample c) were only 19 mAh/g and 5 mAh/g, respectively, and a battery with a Co 3 O 4  anode material had the lowest charge and discharge capacities of only 6 mAh/g and 4 mAh/g, respectively. These electrochemical properties are reported in Table 2. 
       FIG.  10 B  is a Nyquist plot of the imaginary impedance (Z″) versus the real impedance (Z) for lithium-ion batteries that included samples a, b, c, and d as anode materials. The plots in  FIG.  10 B  correspond to the first charging cycle for these batteries. In each plot, a depressed semicircle was observed in the high-frequency region (for example, at smaller values of Z on the x axis) which was attributed to the resistance of the solid electrolyte interphase (SEI) layer (R SEI ). In the medium frequency region (for example, at intermediate values of Z on the x axis), a broad arc was observed which was attributed to the charge-transfer resistance (R ct ) of Li +  at the electrode/electrolyte interface. In the low frequency region (for example, at larger values of Z on the x axis), an inclined line was observed which was attributed to Warburg resistance (R w ). According to the results shown in  FIG.  10 B , the battery with an anode material that included the Co 3 O 4 /RGO/h-BN nanocomposite had the lowest resistance. 
     Example 6: Electrochemical Properties of Nanocomposites at 100° C. 
     The cycling performance of coin cell lithium-ion batteries with anodes that included the Co 3 O 4 /RGO/h-BN nanocomposite were tested at both room temperature (at about 25° C.) and at a high temperature of about 100° C. 
       FIG.  11    is a plot of the specific capacity versus charge/discharge cycle number for the battery with an anode that includes the Co 3 O 4 /RGO/h-BN nanocomposite (sample d) for 100 cycles at about 25° C. The batteries exhibited stable cycle performances and approximately 100% coulombic efficiencies at 25° C. 
       FIG.  12    and  FIG.  13    are plots of the specific capacity versus charge/discharge cycle number for batteries with an anode that includes a Co 3 O 4 /RGO/h-BN nanocomposite (sample d) for 100 and 1,000 charge/discharge cycles, respectively, at about 100° C. The batteries exhibited stable cycle performances and approximately 100% coulombic efficiencies at 100° C. These results were in agreement with the improved thermal stability of sample d as determined from the TGA plots and DTG plots shown in  FIG.  7    and  FIG.  8   , respectively. 
     Accordingly, the results shown in  FIG.  11   ,  FIG.  12   , and  FIG.  13    confirm that the Co 3 O 4 /RGO/h-BN nanocomposite is a stable anode material for use at both room temperature (at about 25° C.) and at high temperatures (about 100° C.). 
     Elements of different implementations described in the present disclosure may be combined to form other implementations not specifically set forth previously. Elements may be left out of the processes described in the present disclosure without adversely affecting their operation. In addition, the logic flows depicted in the figures do not necessarily require the particular order shown, or sequential order, to achieve desirable results. Various separate elements may be combined into one or more individual elements to perform the functions described in the present disclosure. 
     Throughout the description, where nanocomposites, materials, and systems are described as having, including, or comprising specific components, or where processes and methods are described as having, including, or comprising specific steps, it is contemplated that, additionally, there are apparatus, and systems of the present disclosure that consist essentially of, or consist of, the recited components, and that there are processes and methods according to the present disclosure that consist essentially of, or consist of, the recited processing steps. 
     It should be understood that the order of steps or order for performing certain action is immaterial so long as the approach described in the present disclosure remains operable. Moreover, two or more steps or actions may be conducted simultaneously. 
     While the approach described in the present disclosure has been particularly shown and described with reference to specific preferred embodiments, it should be understood by those skilled in the art that various changes in form and detail may be made therein without departing from the spirit and scope of the disclosure as defined by the appended claims.