Solar cells formed via aluminum electroplating
11682739 · 2023-06-20
Assignee
Inventors
Cpc classification
Y02P70/50
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y02E10/50
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
H01L31/022458
ELECTRICITY
International classification
Abstract
Electroplating of aluminum may be utilized to form electrodes for solar cells. In contrast to expensive silver electrodes, aluminum allows for reduced cell cost and addresses the problem of material scarcity. In contrast to copper electrodes which typically require barrier layers, aluminum allows for simplified cell structures and fabrication steps. In the solar cells, point contacts may be utilized in the backside electrodes for increased efficiency. Solar cells formed in accordance with the present disclosure enable large-scale and cost-effective deployment of solar photovoltaic systems.
Claims
1. A method for electroplating of aluminum onto silicon, comprising: preparing an ionic liquid comprising aluminum chloride and an organic halide, the ionic liquid having a molar ratio of aluminum chloride:organic halide greater than 1; pre-baking the ionic liquid at a temperature of between 100 degrees Celsius and 200 degrees Celsius for a period of between 30 minutes and 90 minutes to drive out residual moisture in the ionic liquid; cleaning a silicon substrate with at least one of hydrogen fluoride, hydrogen chloride, hydrogen peroxide, or ammonia hydroxide; depositing at least one of nickel or titanium onto a first side of the silicon substrate via a galvanostatic electroplating process forming a first layer of nickel or titanium, wherein the first layer of nickel or titanium has a thickness of between about 50 nanometers and about 99 nanometers and reduces the resistance of the silicon substrate or facilitates the adhesion of aluminum; depositing aluminum onto the first layer of nickel or titanium via a galvanostatic electroplating process incorporating the ionic liquid, wherein the depositing is performed with the ionic liquid at a temperature of between 111 degrees Celsius and 150 degrees Celsius; cleaning the silicon substrate with alcohol and deionized water; annealing the silicon substrate to reduce the resistivity of the electroplated aluminum; storing the ionic liquid under dry nitrogen in a dry nitrogen glove box; and reusing the ionic liquid to electroplate a second silicon substrate.
2. The method of claim 1, wherein the molar ratio is 3:2.
3. The method of claim 1, wherein the organic halide is 1-ethyl-3-methylimidazolium.
4. The method of claim 1, wherein the electroplating process utilizes a 2-electrode cell.
5. The method of claim 1, wherein the electroplating process utilizes a 3-electrode cell.
6. The method of claim 1, wherein the method further comprises: depositing at least one of nickel or titanium onto a second side of the silicon substrate via a galvanostatic electroplating process forming a second layer of nickel or titanium, wherein the second layer of nickel or titanium has a thickness of between about 50 nanometers and about 500 nanometers and reduces the resistance of the silicon substrate or facilitates the adhesion of aluminum; depositing aluminum onto the second layer of nickel or titanium via a galvanostatic electroplating process incorporating the ionic liquid, wherein the depositing is performed with the ionic liquid at a temperature of between 111 degrees Celsius and 150 degrees Celsius; cleaning the silicon substrate a second time with alcohol and deionized water; and annealing the silicon substrate a second time to reduce the resistivity of the electroplated aluminum.
7. The method of claim 1, wherein annealing the silicon substrate to reduce the resistivity of the electroplated aluminum comprises using a laser to locally heat the silicon substrate.
8. The method of claim 1, wherein annealing the silicon substrate to reduce the resistivity of the electroplated aluminum occurs in a dry nitrogen environment.
9. The method of claim 1, wherein annealing the silicon substrate to reduce the resistivity of the electroplated aluminum occurs in a vacuum environment.
10. The method of claim 1, wherein annealing the silicon substrate to reduce the resistivity of the electroplated aluminum occurs between about 200 degrees Celsius and about 450 degrees Celsius.
11. The method of claim 1, wherein the organic halide comprises 1-butyl-3-methylimidazolium.
12. The method of claim 1, wherein the organic halide comprises 1-methyl-3-ethylimidazolium.
13. The method of claim 1, wherein the organic halide comprises ethyl-pyridinium.
14. The method of claim 1, wherein the organic halide comprises n-(n-butyl) pyridinium.
15. The method of claim 1, wherein the silicon substrate comprises a textured silicon wafer of either n-type or p-type.
16. The method of claim 15, wherein the resistivity of the textured silicon wafer is between about 0.3 ohms-cm and about 10 ohms-cm.
17. The method of claim 1, wherein the silicon substrate is operative as a counter electrode, wherein a first aluminum wire is operative as a working electrode, and wherein a second aluminum wire is operative as a reference electrode.
18. The method of claim 17, wherein the method further comprises: cleaning the first and second aluminum wires with 37% hydrochloric acid; and rinsing the first and second aluminum wires with deionized water, wherein the first and second aluminum wires are of at least 99.99% purity.
19. The method of claim 18, wherein the method further comprises storing the electrodes in a dry nitrogen glove box.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) With reference to the following description and accompanying drawings:
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DETAILED DESCRIPTION
(21) The following description is of various exemplary embodiments only, and is not intended to limit the scope, applicability or configuration of the present disclosure in any way. Rather, the following description is intended to provide a convenient illustration for implementing various embodiments including the best mode. As will become apparent, various changes may be made in the function and arrangement of the elements described in these embodiments without departing from principles of the present disclosure.
(22) For the sake of brevity, conventional techniques for materials deposition, electroplating, silicon solar cell fabrication, and the like may not be described in detail herein. Furthermore, the connecting lines shown in various figures contained herein are intended to represent exemplary functional relationships and/or physical couplings between various elements. It should be noted that many alternative or additional functional relationships or physical connections may be present in a practical silicon solar cell and/or method for electroplating of aluminum.
(23) Prior solar cells suffer from various deficiencies. For example, many solar cells utilize silver for an electrode or electrodes. However, silver is increasing in expense and decreasing in availability. A common alternative, copper, requires barrier layers and/or protective layers, increasing complexity and cost. In contrast, these and other shortcomings of prior approaches may be overcome by utilizing principles of the present disclosure, for example as illustrated in various exemplary embodiments. For example, by utilizing electroplating of aluminum, silicon solar cells having acceptable performance (for example, power conversion efficiency above 15%) and reduced cost (for example, cost reductions of $0.1/Wp or greater) may be achieved.
(24) The annual production of photovoltaic solar cells was ˜30 GWp in 2012, with ˜90% of them produced on silicon wafers. The front finger electrode in wafer-silicon solar cells is typically made of silver. Silver provides several advantages over other metals as the front finger electrode, such as low electrical resistivity and resistance to oxidation. However, there are a number of problems on the horizon for silver as an electrode in wafer-silicon solar cells. One is the rising price of silver, which fluctuated between $15 and $45 per ounce between summer 2010 and late 2014. During price peaks, it is estimated that the silver electrode adds up to ˜$0.12/Wp to the cost of wafer-silicon solar cells. The fluctuating price also makes cost control difficult for solar cell manufacturers. Another problem is the limited reserve of silver on this planet. The known reserve of silver on this planet, according to U.S. Geological Survey, is about 540,000 metric tons. Several analyses have been published in the last few years about resource limitations to wafer-silicon solar cells due to the limited availability of silver. It is estimated that even if all the silver reserve were used exclusively for wafer-silicon solar cells, the total amount of energy these solar cells could produce would be limited to only about 1-2% of the projected energy demands in 2100.
(25) In order to reduce the cost of wafer-silicon solar cells and enable large scale (for example, terawatt-scale) deployment, the silver electrode in wafer-silicon solar cells will desirably be replaced with a low-cost earth-abundant metal. Copper has been investigated extensively in recent years for this purpose, with industrial-type wafer-silicon solar cells with electroplated copper electrodes having been demonstrated with efficiency above 20%.
(26) However, prior approaches have failed to suitably investigate aluminum as another metal candidate for this purpose. It is revealing to compare copper and aluminum as possible substitutes for silver in wafer-silicon solar cells. The biggest advantage of copper is its low resistivity, which is almost the same as that of silver. In comparison, the resistivity of aluminum is ˜75% higher than silver. Typically, to reduce the resistive loss in an aluminum finger electrode, either a denser aluminum layer or a higher aspect ratio has to be achieved for the aluminum finger. On the other hand, there are several advantages of aluminum over copper as an electrode in wafer-silicon solar cells. Aluminum can be placed in direct contact with silicon as an electrode. In contrast, copper in direct contact with silicon is detrimental to the electrical properties of silicon, resulting in reduced efficiencies in wafer-silicon solar cells. For copper to serve as an electrode on silicon, a barrier layer (such as nickel) is typically placed between copper and silicon to prevent copper from going into the silicon.
(27) Moreover, oxidation of aluminum forms a dense protective aluminum oxide layer on the surface of aluminum, which prevents further oxidation of the underneath aluminum and makes aluminum electrodes stable over long terms and in all kinds of weather. In contrast, copper is more readily oxidized, especially in humid climates, making long-term reliability a concern for copper electrodes. A protective layer, such as tin, is often required to cover a copper electrode and improve its reliability. The barrier layer and the protective layer for copper, which are not required for aluminum, make the process more complicated and the cost higher for copper electrodes than aluminum electrodes.
(28) Prior approaches to utilize aluminum typically relied on expensive vacuum evaporation. In contrast, principles of the present disclosure contemplate wafer-silicon solar cell structures which are compatible with electroplated aluminum, for example as the front finger electrode. The back electrode may also be made of aluminum, which can be either electroplated or screen-printed. No silver is used as an electrode in these exemplary solar cell structures. The electroplating bath for aluminum may be an ionic liquid, or an organic solvent, or any suitable electroplating bath and/or process with a process temperature below 500° C. The electroplating process can be carried out in air or in dry air at a temperature between about 100° C. and 500° C. Moreover, the aluminum electrodes are in direct contact with silicon, both to n-type and p-type silicon. By replacing silver with aluminum in these solar cells, the cost of the cells may be reduced by up to $0.1/Wp or more, while the cells maintain a good efficiency above 15%. Accordingly, solar cells configured in accordance with principles of the present disclosure enable large-scale (for example, terawatt-scale) deployment of wafer-silicon solar cells at a significantly lower cost.
(29) In an exemplary embodiment, with initial reference to
(30) Typical ionic liquids are mixtures of aluminum chloride (AlCl.sub.3) and an organic halide (RX), such as 1-ethyl-3-methylimidazolium chloride (EMIC), 1-butyl-3-methylimidazolium chloride (BMIC), 1-methyl-3-ethylimidazolium chloride (MEIC), ethyl-pyridinium bromide (EPB), n-(n-butyl) pyridinium chloride (BPC), and the like. These ionic liquids exhibit adjustable Lewis acid-base properties, which vary with the molar ratio of AlCl.sub.3:RX. Ionic liquids with the molar ratio of AlCl.sub.3:RX>1 are acidic, and aluminum electroplating can be performed only under acidic conditions, in which the electroactive Al.sub.2Cl.sub.7.sup.− is reduced by the following reaction resulting in aluminum deposition:
4Al.sub.2Cl.sub.7.sup.−+3e.sup.−.fwdarw.Al+7AlCl.sub.4.sup.−
(31) Advantageously, in various exemplary embodiments a suitable ionic liquid is easy to prepare and relatively simple to handle under dry air, which prevents the ionic liquid from reacting with water. In various exemplary embodiments, the ionic liquid may be prepared and aluminum electroplating may be conducted both in a glove box with flowing dry nitrogen (N.sub.2). 1-ethyl-3-methylimidazolium tetrachloroaluminate ([EMIM]AlCl.sub.4) and anhydrous AlCl.sub.3 powder may be utilized.
(32) In various exemplary embodiments, an ionic liquid is prepared by mixing proper quantities of AlCl.sub.3 and [EMIM]AlCl.sub.4 in a suitable container, for example a dry 50 ml beaker, at or near ambient temperature. The molar quantity of AlCl.sub.3 is desirably larger than that of (EMIM)AlCl.sub.4 to enable aluminum deposition from the ionic liquid. After mixing, a pre-bake may be performed in which the obtained electrolyte is heated to a suitable temperature, for example between about 100° C. and about 200° C., for a suitable time, for example between about 30 minutes and about 90 minutes, in order to further drive out residual moisture in the electrolyte. Then, the temperature of the electrolyte is changed to a predetermined temperature for the electroplating, for example between about 20° C. and about 200° C., and more specifically between about 100° C. and about 150° C. The electrolyte may be utilized without further purification.
(33) In various exemplary embodiments, a two-electrode electrochemical cell may be employed to carry out electroplating. In other exemplary embodiments, a three-electrode electrochemical cell may be used. A textured silicon wafer, either n-type or p-type, with resistivity between 0.3-10 ohms-cm may be used as the cathode (2-electrode cell) or counter electrode (3-electrode cell). Prior to electroplating, the silicon wafer may be dipped in diluted hydrofluoric acid (HF) to remove native oxide. Aluminum wires of suitable purity, for example 99.99% purity, may be used as the anode (2-electrode cell) or working and reference electrodes (3-electrode cell). The aluminum electrode is utilized as a sacrificial electrode. Electrodes may be cleaned with a short dip in 37% hydrochloric acid (HCl), followed by a deionized water rinse. After the cleaning, electrodes may be assembled and then transferred to a dry nitrogen glove box or other suitable working location. A schematic of an exemplary electroplating system is illustrated in
(34) In various exemplary embodiments, deposition of aluminum may be performed at room temperature or slightly above room temperature, or more broadly, between about 20° C. and about 200° C. The electrolyte may be stirred, for example at a constant speed. A suitable electroplating technique may be utilized, for example galvanostatic electrolysis having a current of between about 10 mA/cm.sup.2 and about 20 mA/cm.sup.2 (and preferably, about 15 mA/cm.sup.2). In some exemplary embodiments, a thin seed layer of nickel or titanium may be deposited first, before aluminum electroplating, to reduce the resistance of the silicon wafer, which helps aluminum electroplating.
(35) In various exemplary embodiments, post-deposition cleaning of the silicon wafer is desirable. After each deposition, excess ionic liquid may be removed from the silicon wafer by washing in alcohol. Then, the wafer may be rinsed, for example with deionized water, and dried, for example with nitrogen. Post-deposition annealing under different ambient conditions, for example from vacuum to dry nitrogen to air, and between about 200° C. and about 450° C., may also be conducted to further reduce the resistivity of the electroplated aluminum.
(36) In various exemplary embodiments, pre-deposition cleaning of the silicon wafer may be desirable. For example, the wafer may be cleaned with one or more of hydrogen fluoride, hydrogen chloride, hydrogen peroxide, ammonia hydroxide, and/or the like or mixtures of the same.
(37) In various exemplary embodiments, pre-electroplating deposition of a layer of nickel, titanium, and/or the like on the silicon wafer, for example a layer having a thickness of between about 50 nanometers and about 500 nanometers, may be desirable to reduce the resistance of the silicon wafer and/or to facilitate adhesion of aluminum.
(38) It will be appreciated that after multiple electroplating runs, the concentration of aluminum in the electrolyte remains largely unchanged, because the aluminum electrode continuously supplies aluminum ions to the electrolyte during deposition. In this manner, the electrolyte may be reused multiple times, provided it was stored under dry nitrogen such as in a dry nitrogen glove box, making the electroplating process more environmentally friendly.
(39) Characterization of exemplary aluminum devices constructed in accordance with principles of the present disclosure are illustrated in
(40) In various exemplary embodiments, with reference again to
(41) Principles of the present disclosure contemplate wafer-silicon solar cell structures which are compatible with electroplated aluminum, for example as the front finger electrode. The back aluminum electrode can be electroplated or screen-printed. Certain exemplary cell structures are schematically illustrated in
(42) With reference now to
(43) In various exemplary embodiments, with continued reference to
(44) After the high temperature firing, the front silicon nitride layer is patterned for the front finger electrode. The patterning can be realized by laser ablation, photolithography, or any other suitable patterning technique. Electroplating of aluminum is then performed for the front side of the wafer, as described herein. The silicon wafer is then heated to a moderate temperature, which is typically between 100° C. and 500° C., for the formation of the front electrical contact. The lower annealing temperature for the front electrode prevents aluminum from doping the front side n-type silicon. After the second metal annealing step, the cell is completed.
(45) With reference now to
(46) In various exemplary embodiments, with continued reference to
(47) After the high temperature firing, the front silicon nitride layer is patterned for the front finger electrode. The patterning can be realized by laser ablation, photolithography, or any other suitable patterning technique. Electroplating of aluminum is then performed for the front side of the wafer, as described herein. The silicon wafer is then heated to a moderate temperature, which is typically between 100° C. and 500° C., for the formation of the front electrical contact. The low annealing temperature for the front electrode prevents aluminum from doping the front side n-type silicon. After the second metal annealing step, the cell is completed.
(48) With reference now to
(49) In various exemplary embodiments, with continued reference to
(50) Aluminum metallization can be performed in two steps. In two-step aluminum deposition, aluminum is deposited on the backside by screen printing or electroplating. In a second step, the front silicon nitride layer is patterned for the front finger electrode. The patterning can be realized by laser ablation, photolithography, or any other suitable patterning technique. Electroplating of aluminum is then performed for the front side of the wafer, as described herein. The silicon wafer is then heated to a moderate temperature, which is typically between 100° C. and 500° C., for the formation of the front and back electrical contacts. After metal annealing, the cell is completed.
(51) With reference now to
(52) With reference now to
(53) In various exemplary embodiments, with continued reference to
(54) Aluminum metallization can be performed in two steps. In a first step, the front aluminum oxide/silicon nitride stack is patterned for the front finger electrode. The patterning can be realized by laser ablation, photolithography, or any other suitable patterning technique. Electroplating of aluminum is then performed for the front side of the wafer, as described herein. In a second step, aluminum is deposited on the backside by screen printing or electroplating. The silicon wafer is then heated to a moderate temperature, which is typically between 100° C. and 500° C., for the formation of the front and back electrical contacts. After metal annealing, the cell is completed.
(55) With reference now to
(56) With reference now to
(57) Turning now to
(58) With specific reference to
(59) In this exemplary embodiment, SiN.sub.x and Al.sub.2O.sub.3 coating is utilized. An about 50 nm to about 100 nm thick SiN.sub.x layer is deposited on the front side of the wafer (i.e., the phosphorus-diffused side), for example by plasma-enhanced chemical vapor deposition or the like. On the backside of the wafer, an about 5 nm to about 50 nm thick Al.sub.2O.sub.3 layer is deposited by atomic layer deposition. Alternatively, on the backside of the wafer, an about 5 nm to about 50 nm thick SiO.sub.2 layer may be deposited via plasma-enhanced chemical vapor deposition, thermal oxidation, and/or the like. Moreover, the sequence of the front side SiN.sub.x layer and the backside SiO.sub.2 or Al.sub.2O.sub.3 layer may be switched, as desired.
(60) A suitable method may be utilized to form the backside contact. For example, laser annealing may be utilized. In this approach, an aluminum layer is screen-printed onto the backside of the wafer. After firing between about 550° C. and about 800° C. for the screen-printed aluminum, a laser may be utilized to locally heat the backside of the wafer through the aluminum layer. Laser annealing allows the aluminum layer to penetrate the SiO.sub.2 or Al.sub.2O.sub.3 layer, and forms a heavily-doped p+ region under the laser spot. An array of p+ regions may be created by moving the laser spot across the back surface; the regions provide a localized p+ emitter for the solar cell. Alternatively, lithographic patterning may be utilized to created holes in the SiO.sub.2 or Al.sub.2O.sub.3 layer. An aluminum layer is then screen-printed on the patterned SiO.sub.2 or Al.sub.2O.sub.3. The wafer is then fired at between about 600° C. and about 800° C. to form a localized p+ emitter in the cell.
(61) Front metallization may be accomplished via a suitable method, for example laser ablation or lithography. In laser ablation, a laser is employed to remove SiN.sub.x from the contact area on the front side of the cell. In lithography, lithographic patterning is utilized to create openings in the SiN.sub.x layer. Aluminum electroplating may then be performed on the patterned SiN.sub.x layer, either directly on silicon or preferentially on a seed layer of nickel. When nickel is utilized, a nickel layer of between about 100 nm to about 400 nm is electroplated into the openings in the SiN.sub.x layer, and then an aluminum layer of between about 5 microns and about 25 microns is electroplated onto the nickel seed layer. A final annealing below 500° C. completes the fabrication process for the exemplary cell.
(62) Turning now to
(63) In this exemplary embodiment, SiN.sub.x and Al.sub.2O.sub.3 coating is utilized. An about 50 nm to about 100 nm thick SiN.sub.x layer is deposited on the front side of the wafer (i.e., the phosphorus-diffused side), for example by plasma-enhanced chemical vapor deposition or the like. On the backside of the wafer, an about 5 nm to about 50 nm thick Al.sub.2O.sub.3 layer is deposited by atomic layer deposition. Alternatively, on the backside of the wafer, an about 5 nm to about 50 nm thick SiO.sub.2 layer may be deposited via plasma-enhanced chemical vapor deposition, thermal oxidation, and/or the like. Moreover, the sequence of the front side SiN.sub.x layer and the backside SiO.sub.2 or Al.sub.2O.sub.3 layer may be switched, as desired.
(64) A suitable method may be utilized to form the backside contact. For example, laser annealing may be utilized. In this approach, an aluminum layer is screen-printed onto the backside of the wafer. After firing between about 550° C. and about 800° C. for the screen-printed aluminum, a laser may be utilized to locally heat the backside of the wafer through the aluminum layer. Laser annealing allows the aluminum layer to penetrate the SiO.sub.2 or Al.sub.2O.sub.3 layer and forms a heavily-doped p+ region under the laser spot. An array of p+ regions may be created by moving the laser spot across the back surface; the regions provide a localized p+ back surface field for the solar cell. Alternatively, lithographic patterning may be utilized to create holes in the SiO.sub.2 or Al.sub.2O.sub.3 layer. An aluminum layer is then screen-printed on the patterned SiO.sub.2 or Al.sub.2O.sub.3. The wafer is then fired at between about 600° C. and about 800° C. to form a localized p+ back surface field in the cell.
(65) Front metallization may be accomplished via a suitable method, for example laser ablation or lithography. In laser ablation, a laser is employed to remove SiN.sub.x from the contact area on the front side of the cell. In lithography, lithographic patterning is utilized to create openings in the SiN.sub.x layer. Aluminum electroplating may then be performed on the patterned SiN.sub.x layer, either directly on silicon or preferentially on a seed layer of nickel. When nickel is utilized, a nickel layer of between about 100 nm to about 400 nm is electroplated into the openings in the SiN.sub.x layer, and then an aluminum layer of between about 5 microns and about 25 microns is electroplated onto the nickel seed layer. A final annealing below 500° C. completes the fabrication process for the exemplary cell.
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(67) While the principles of this disclosure have been shown in various embodiments, many modifications of structure, arrangements, proportions, the elements, materials and components, used in practice, which are particularly adapted for a specific environment and operating requirements may be used without departing from the principles and scope of this disclosure. These and other changes or modifications are intended to be included within the scope of the present disclosure.
(68) The present disclosure has been described with reference to various embodiments. However, one of ordinary skill in the art appreciates that various modifications and changes can be made without departing from the scope of the present disclosure. Accordingly, the specification is to be regarded in an illustrative rather than a restrictive sense, and all such modifications are intended to be included within the scope of the present disclosure. Likewise, benefits, other advantages, and solutions to problems have been described above with regard to various embodiments. However, benefits, advantages, solutions to problems, and any element(s) that may cause any benefit, advantage, or solution to occur or become more pronounced are not to be construed as a critical, required, or essential feature or element.
(69) When a phrase similar to “at least one of A, B, or C” or “at least one of A, B, and C” is used in the claims, the phrase is intended to mean any of the following: (1) at least one of A; (2) at least one of B; (3) at least one of C; (4) at least one of A and at least one of B; (5) at least one of B and at least one of C; (6) at least one of A and at least one of C; or (7) at least one of A, at least one of B, and at least one of C.
(70) As used herein, the terms “comprises,” “comprising,” or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Also, as used herein, the terms “coupled,” “coupling,” or any other variation thereof, are intended to cover a physical connection, an electrical connection, a magnetic connection, an optical connection, a communicative connection, a functional connection, and/or any other connection.