The field of the disclosure relates generally to the formation of secondary batteries, and more specifically, methods of forming secondary battery assemblies following a pre-lithiation process.
In rocking-chair battery cells, both the positive electrode and the negative electrode of a secondary battery comprise materials into which a carrier ion, such as lithium, inserts and extracts. As the battery is discharged, carrier ions are extracted from the negative electrode and inserted into the positive electrode. As the battery is charged, the carrier ion is extracted from the positive electrode and inserted into the negative electrode.
After a lithium containing secondary battery is assembled, the assembled battery is typically subjected to a formation process. During the formation process, the battery is slowly charged and discharged one or more times. At least some known formation processes include a pre-lithiation process to add lithium to the battery. In some instances, it may be desirable to remove one or more auxiliary electrodes used in the pre-lithiation process to reduce the footprint and increase the energy density of the secondary battery following the pre-lithiation process.
One embodiment comprises a method of forming a lithium containing secondary battery including a population of unit cells, an electrode busbar, a counter-electrode busbar, a first terminal electrically connected to the electrode busbar, and a second terminal electrically connected to the counter-electrode busbar, wherein each unit cell of the population of unit cells comprises an electrode structure, a separator structure, and a counter-electrode structure. The method comprises positioning the lithium containing secondary battery within a pouch defined by an enclosure, trimming the enclosure to form a plurality of flaps, the plurality of flaps including a first side flap extending from the pouch at a first fold line, a second side flap extending from the pouch at a second fold line, and an end flap extending from the pouch at a third fold line, and attaching the first side flap and the second side flap to the pouch by folding each of the first and second side flaps about the respective first and second fold lines towards and into contact with the pouch. A portion of the first side flap extends beyond the pouch to define a first tab and a portion of the second side flap extends beyond the pouch to define a second tab. The method further includes attaching the end flap to the pouch by folding the end flap about the third fold line towards and into contact with the pouch, and attaching the first tab and the second tab to the end flap by folding each of the first tab and the second tab towards and into contact with the end flap.
Another embodiment comprises a method of forming a lithium containing secondary battery positioned within a pouch defined by an enclosure. The lithium containing battery includes a population of unit cells, an electrode busbar, a counter-electrode busbar, a first terminal electrically connected to the electrode busbar, and a second terminal electrically connected to the counter-electrode busbar, wherein each unit cell of the population of unit cells comprises an electrode structure, a separator structure, and a counter-electrode structure. The enclosure includes a plurality of flaps extending outward from the pouch, the plurality of flaps including a first side flap extending from the pouch at a first fold line, a second side flap extending from the pouch at a second fold line, and an end flap extending from the pouch at a third fold line. The method comprises applying a bonding agent to at least one of the first side flap and the pouch, to at least one of the second side flap and the pouch, and to at least one of the end flap and the pouch, folding the first side flap about the first fold line towards the pouch, wherein a portion of the first side flap extends beyond the pouch to define a first tab, folding the second side flap about the second fold line towards the pouch, wherein a portion of the second side flap extends beyond the pouch to define a second tab, compressing the first and second side flaps against the pouch, folding the end flap about the third fold line towards and into contact with the pouch, applying, after the end flap is folded into contact with the pouch, a bonding agent to at least one of the end flap and each of the first and second tabs, folding the first tab and the second tab towards and into contact with the end flap to connect the first and second tabs to the end flap, and compressing the end flap, the first tab, and the second tab against the pouch.
Another embodiment comprises a method of forming a lithium containing secondary battery including a population of unit cells, an electrode busbar, a counter-electrode busbar, a first terminal electrically connected to the electrode busbar, and a second terminal electrically connected to the counter-electrode busbar, wherein each unit cell of the population of unit cells comprises an electrode structure, a separator structure, and a counter-electrode structure. The method comprises positioning the lithium containing secondary battery within a pouch defined by an enclosure, positioning an auxiliary electrode within the pouch such that the auxiliary electrode is in contact with the lithium containing secondary battery, performing a buffer process on the lithium containing secondary battery whereby carrier ions from the auxiliary electrode are transferred to the lithium containing secondary battery, removing the auxiliary electrode from the pouch after the buffer process, sealing the enclosure with the secondary battery positioned within the pouch after the auxiliary electrode is removed from the pouch, trimming the sealed enclosure to form a plurality of flaps in the enclosure, wherein each flap extends outward from the pouch at a respective fold line, the plurality of flaps including a first side flap, a second side flap, and an end flap, attaching the first and second side flaps to the pouch by folding each of the first and second side flaps towards and into contact with the pouch, wherein a portion of the first side flap extends beyond the pouch to define a first tab, and a portion of the second side flap extends beyond the pouch to define a second tab, attaching the end flap to the pouch by folding the end flap towards and into contact with the pouch, and attaching the first tab and the second tab to the end flap by folding each of the first tab and the second tab towards and into contact with the end flap.
Another embodiment comprises a method of forming a lithium containing secondary battery including a population of unit cells, an electrode busbar, a counter-electrode busbar, a first terminal electrically connected to the electrode busbar, and a second terminal electrically connected to the counter-electrode busbar, wherein each unit cell of the population of unit cells comprises an electrode structure, a separator structure, and a counter-electrode structure. The method comprises positioning the lithium containing secondary battery within a pouch defined by an enclosure, where the enclosure includes a first enclosure layer and a second enclosure layer joined to the first enclosure layer, the pouch including a base defined by the first enclosure layer, a cover positioned opposite the base and defined by the second enclosure layer, a first sidewall extending from the base to the cover, a second sidewall positioned opposite the first sidewall and extending from the base to the cover, a first end wall extending from the first sidewall to the second sidewall and from the base to the cover, and a second end wall positioned opposite the first end wall and extending from the first sidewall to the second sidewall and from the base to the cover, wherein the first and second terminals of the secondary battery extend outward from the second end wall. The method further includes trimming the enclosure to form a plurality of flaps in the enclosure, wherein each flap extends outward from the pouch at a respective fold line and includes a first surface defined by the first enclosure layer and an opposing second surface defined by the second enclosure layer, the plurality of flaps including a first side flap extending from the first sidewall of the pouch at a first fold line, a second side flap extending from the second sidewall of the pouch at a second fold line, and an end flap extending from the first end wall of the pouch at a third fold line. The method further includes applying a bonding agent to at least one of the first surface of the first side flap and the pouch first sidewall, to at least one of the first surface of the second side flap and the pouch second sidewall, and to at least one of the first surface of the end flap and the first end wall, folding the first side flap about the first fold line towards and into contact with the pouch first sidewall, wherein a portion of the first side flap extends beyond the pouch first end wall to define a first tab, folding the second side flap about the second fold line towards and into contact with the pouch second sidewall, wherein a portion of the second side flap extends beyond the pouch first end wall to define a second tab, compressing the first side flap against the pouch first sidewall and the second side flap against the pouch second sidewall while heated at a first temperature for a first compression time, folding the end flap about the third fold line towards and into contact with the pouch first end wall, applying, after the end flap is folded into contact with the pouch first end wall, a bonding agent to at least one of the second surface of the end flap and the first surface of each of the first and second tabs, folding the first tab about a fourth fold line towards and into contact with the second surface of the end flap, folding the second tab about a fifth fold line towards and into contact with the second surface of the end flap, and compressing the end flap, the first tab, and the second tab against the pouch first end wall while heated at a second temperature for a second compression time.
Various refinements exist of the features noted in relation to the above-mentioned aspects. Further features may also be incorporated in the above-mentioned aspects. These refinements and additional features may exist individually or in any combination. For instance, various features discussed below in relation to any of the illustrated embodiments may be incorporated into any of the above-described aspects, alone or in any combination.
“A,” “an,” and “the” (i.e., singular forms) as used herein refer to plural referents unless the context clearly dictates otherwise. For example, in one instance, reference to “an electrode” includes both a single electrode and a plurality of similar electrodes.
“About” and “approximately” as used herein refers to plus or minus 10%, 5%, or 1% of the value stated. For example, in one instance, about 250 micrometers (μm) would include 225 μm to 275 μm. By way of further example, in one instance, about 1,000 μm would include 900 μm to 1,100 μm. Unless otherwise indicated, all numbers expressing quantities (e.g., measurements, and the like) and so forth used in the specification and claims are to be understood as being modified in all instances by the term “about.” Accordingly, unless indicated to the contrary, the numerical parameters set forth in the following specification and attached claims are approximations. Each numerical parameter should at least be construed in light of the number of reported significant digits and by applying ordinary rounding techniques.
“Anode” as used herein in the context of a secondary battery refers to the negative electrode in the secondary battery.
“Anode material” or “Anodically active” as used herein means material suitable for use as the negative electrode of a secondary battery
“Cathode” as used herein in the context of a secondary battery refers to the positive electrode in the secondary battery
“Cathode material” or “Cathodically active” as used herein means material suitable for use as the positive electrode of a secondary battery.
“Conversion chemistry active material” or “Conversion chemistry material” refers to a material that undergoes a chemical reaction during the charging and discharging cycles of a secondary battery.
“Counter-electrode” as used herein may refer to the negative or positive electrode (anode or cathode), opposite of the Electrode, of a secondary battery unless the context clearly indicates otherwise.
“Counter-electrode current collector” as used herein may refer to the negative or positive (anode or cathode) current collector, opposite of the Electrode current connector, of a secondary battery unless the context clearly indicates otherwise.
“Cycle” as used herein in the context of cycling of a secondary battery between charged and discharged states refers to charging and/or discharging a battery to move the battery in a cycle from a first state that is either a charged or discharged state, to a second state that is the opposite of the first state (i.e., a charged state if the first state was discharged, or a discharged state if the first state was charged), and then moving the battery back to the first state to complete the cycle. For example, a single cycle of the secondary battery between charged and discharged states can include, as in a charge cycle, charging the battery from a discharged state to a charged state, and then discharging back to the discharged state, to complete the cycle. The single cycle can also include, as in a discharge cycle, discharging the battery from the charged state to the discharged state, and then charging back to a charged state, to complete the cycle.
“Electrochemically active material” as used herein means anodically active or cathodically active material.
“Electrode” as used herein may refer to the negative or positive electrode (anode or cathode) of a secondary battery unless the context clearly indicates otherwise.
“Electrode current collector” as used herein may refer to the negative or positive (anode or cathode) current collector of a secondary battery unless the context clearly indicates otherwise.
“Electrode material” as used herein may refer to anode material or cathode material unless the context clearly indicates otherwise.
“Electrode structure” as used herein may refer to an anode structure (e.g., negative electrode structure) or a cathode structure (e.g., positive electrode structure) adapted for use in a battery unless the context clearly indicates otherwise.
“Capacity” or “C” as used herein refers to an amount of electric charge that a battery (or a sub-portion of a battery comprising one or more pairs of electrode structures and counter-electrode structures that form a bilayer) can deliver at a pre-defined voltage unless the context clearly indicates otherwise.
“Electrolyte” as used herein refers to a non-metallic liquid, gel, or solid material in which current is carried by the movement of ions adapted for use in a battery unless the context clearly indicates otherwise.
“Charged state” as used herein in the context of the state of a secondary battery refers to a state where the secondary battery is charged to at least 75% of its rated capacity unless the context clearly indicates otherwise. For example, the battery may be charged to at least 80% of its rated capacity, at least 90% of its rated capacity, and even at least 95% of its rated capacity, such as 100% of its rated capacity.
“Discharge capacity” as used herein in connection with a negative electrode means the quantity of carrier ions available for extraction from the negative electrode and insertion into the positive electrode during a discharge operation of the battery between a predetermined set of cell end of charge and end of discharge voltage limits unless the context clearly indicates otherwise.
“Discharged state” as used herein in the context of the state of a secondary battery refers to a state where the secondary battery is discharged to less than 25% of its rated capacity unless the context clearly indicates otherwise. For example, the battery may be discharged to less than 20% of its rated capacity, such as less than 10% of its rated capacity, and even less than 5% of its rated capacity, such as 0% of its rated capacity.
“Reversible coulombic capacity” as used herein in connection with an electrode (i.e., a positive electrode, a negative electrode or an auxiliary electrode) means the total capacity of the electrode for carrier ions available for reversible exchange with a counter electrode.
“Longitudinal axis,” “transverse axis,” and “vertical axis,” as used herein refer to mutually perpendicular axes (i.e., each are orthogonal to one another). For example, the “longitudinal axis,” “transverse axis,” and the “vertical axis” as used herein are akin to a Cartesian coordinate system used to define three-dimensional aspects or orientations. As such, the descriptions of elements of the disclosed subject matter herein are not limited to the particular axis or axes used to describe three-dimensional orientations of the elements. Alternatively stated, the axes may be interchangeable when referring to three-dimensional aspects of the disclosed subject matter.
“Composite material” or “Composite” as used herein refers to a material which comprises two or more constituent materials unless the context clearly indicates otherwise.
“Void fraction” or “Porosity” or “Void volume fraction” as used herein refers to a measurement of the voids (i.e., empty) spaces in a material, and is a fraction of the volume of voids over the total volume of the material, between 0 and 1, or as a percentage between 0% and 100%.
“Polymer” as used herein may refer to a substance or material consisting of repeating subunits of macromolecules unless the context clearly indicates otherwise.
“Microstructure” as used herein may refer to the structure of a surface of a material revealed by an optical microscope above about 25× magnification unless the context clearly indicates otherwise.
“Microporous” as used herein may refer to a material containing pores with diameters less than about 2 nanometers unless the context clearly indicates otherwise.
“Macroporous” as used herein may refer to a material containing pores with diameters greater than about 50 nanometers unless the context clearly indicates otherwise.
“Nanoscale” or “Nanoscopic scale” as used herein may refer to structures with a length scale in the range of about 1 nanometer to about 100 nanometers.
“Pre-lithiation” or “Pre-lithiate” as used herein may refer to the addition of lithium to the active lithium content of a lithium containing secondary battery as part of the formation process prior to battery operation to compensate for the loss of active lithium. “Pre-lithiation” or “Pre-lithiate” may also be referred to herein as a “buffer process.”
As illustrated in
Referring to
In one embodiment, a casing 116, which may be referred to as a constraint, may be applied over one or both of the X-Y surfaces of the secondary battery 100. In the embodiment shown in
In some embodiments, the casing 116 comprises a sheet having a thickness in the range of about 10 to about 100 micrometers (μm). In one embodiment, the casing 116 comprises a stainless-steel sheet (e.g., SS316) having a thickness of about 30 μm. In another embodiment, the casing 116 comprises an aluminum sheet (e.g., 7075-T6) having a thickness of about 40 μm. In another embodiment, the casing 116 comprises a zirconia sheet (e.g., Coorstek YZTP) having a thickness of about 30 μm. In another embodiment, the casing 116 comprises an E Glass UD/Epoxy 0 deg sheet having a thickness of about 75 μm. In another embodiment, the casing 116 comprises 12 μm carbon fibers at >50% packing density.
In this embodiment, the secondary battery 100 includes a first major surface 126 and a second major surface 127 that opposes the first major surface 126. The major surfaces 126, 127 of the secondary battery 100 may be substantially planar is some embodiments.
With reference to
In an alternative embodiment, the placement of the cathodically active material layer 106 and the anodically active material layer 104 may be swapped, such that the cathodically active material layers are toward the center and the anodically active material layers are distal to the cathodically active material layers. In one embodiment, a unit cell 200A includes, from left to right in stacked succession, the anode current collector 202, the anodically active material layer 104, the separator layer 108, the cathodically active material layer 106, and the cathode current collector 204. In an alternative embodiment, a unit cell 200B includes, from left to right in stacked succession, the separator layer 108, a first layer of the cathodically active material layer 106, the cathode current collector 204, a second layer of the cathodically active material layer 106, the separator layer 108, a first layer of the anodically active material layer 104, the anode current collector 202, a second layer of the anodically active material layer 104, and the separator layer 108.
In
A voltage difference V exists between adjacent cathode structures 206 and anode structures 207, with the adjacent structures considered a bilayer in some embodiments. Each bilayer has a capacity C determined by the makeup and configuration of the cathode structures 206 and the anode structures 207. In this embodiment, each bilayer produces a voltage difference of about 4.35 volts. In other embodiments, each bilayer has a voltage difference of about 0.5 volts, about 1.0 volts, about 1.5 volts, about 2.0 volts, about 2.5 volts, about 3.0 volts, about 3.5 volts, about 4.0 volts, 4.5 volts, about 5.0 volts, between 4 and 5 volts, or any other suitable voltage. During cycling between a charged state and a discharged state, the voltage may vary, for example, between about 2.5 volts and about 4.35 volts. The capacity C of a bilayer in this embodiment is about 3.5 milliampere-hour (mAh). In other embodiments, the capacity C of a bilayer is about 2 mAh, less than 5 mAh, or any other suitable capacity. In some embodiments, the capacity C of a bilayer may be up to about 10 mAh.
The cathode current collector 204 may comprise aluminum, nickel, cobalt, titanium, and tungsten, or alloys thereof, or any other material suitable for use as a cathode current collector layer. In general, the cathode current collector 204 will have an electrical conductivity of at least about 103 Siemens/cm. For example, in one such embodiment, the cathode current collector 204 will have a conductivity of at least about 104 Siemens/cm. By way of further example, in one such embodiment, the cathode current collector 204 will have a conductivity of at least about 105 Siemens/cm. In general, the cathode current collector 204, may comprise a metal such as aluminum, carbon, chromium, gold, nickel, NiP, palladium, platinum, rhodium, ruthenium, an alloy of silicon and nickel, titanium, or a combination thereof (see “Current collectors for positive electrodes of lithium-based batteries” by A. H. Whitehead and M. Schreiber, Journal of the Electrochemical Society, 152(11) A2105-A2113 (2005)). By way of further example, in one embodiment, the cathode current collector 204 comprises gold or an alloy thereof such as gold silicide. By way of further example, in one embodiment, the cathode current collector 204 comprise nickel or an alloy thereof such as nickel silicide.
The cathodically active material layer 106 may be an intercalation-type chemistry active material, a conversion chemistry active material, or a combination thereof.
Exemplary conversion chemistry materials useful in the present disclosure include, but are not limited to, S (or Li2S in the lithiated state), LiF, Fe, Cu, Ni, FeF2, FeOdF3.2d, FeF3, CoF3, CoF2, CuF2, NiF2, where 0≤d≤0.5, and the like.
Exemplary cathodically active material layers 106 also include any of a wide range of intercalation-type cathodically active materials. For example, for a lithium-ion battery, the cathodically active material may comprise a cathodically active material selected from transition metal oxides, transition metal sulfides, transition metal nitrides, lithium-transition metal oxides, lithium-transition metal sulfides, and lithium-transition metal nitrides may be selectively used. The transition metal elements of these transition metal oxides, transition metal sulfides, and transition metal nitrides can include metal elements having a d-shell or f-shell. Specific examples of such metal element are Sc, Y, lanthanoids, actinoids, Ti, Zr, Hf, V, Nb, Ta, Cr, Mo, W, Mn, Tc, Re, Fe, Ru, Os, Co, Rh, Ir, Ni, Pb, Pt, Cu, Ag, and Au. Additional cathodically active materials include LiCoO2, LiNi0.5Mn1.5O4, Li(NixCoyAlz)O2, LiFePO4, Li2MnO4, V2O5, molybdenum oxysulfides, phosphates, silicates, vanadates, sulfur, sulfur compounds, oxygen (air), Li(NixMnyCoz)O2, and combinations thereof.
In general, the cathodically active material layers 106 will have a thickness of at least about 20 μm. For example, in one embodiment, the cathodically active material layers 106 will have a thickness of at least about 40 μm. By way of further example, in one such embodiment, the cathodically active material layers 106 will have a thickness of at least about 60 μm. By way of further example, in one such embodiment, the cathodically active material layers 106 will have a thickness of at least about 100 μm. Typically, the cathodically active material layers 106 will have a thickness of less than about 90 μm or less than about 70 μm.
The length LCE of the cathode structures 206 will vary depending upon the secondary battery 100 and its intended use. In general, however, each cathode structure 206 will typically have a length LCE in the range of about 5 millimeters (mm) to about 500 mm. For example, in one such embodiment, each cathode structure 206 has a length LCE of about 10 mm to about 250 mm. By way of further example, in one such embodiment each cathode structure 206 has a length LCE of about 25 mm to about 100 mm. According to one embodiment, the cathode structures 206 include one or more first electrode members having a first length, and one or more second electrode members having a second length that is different than the first length. In yet another embodiment, the different lengths for the one or more first electrode members and one or more second electrode members may be selected to accommodate a predetermined shape for an electrode assembly, such as an electrode assembly shape having a different lengths along one or more of the longitudinal and/or transverse axis, and/or to provide predetermined performance characteristics for the secondary battery 100.
The width WCE of the cathode structures 206 will also vary depending upon the secondary battery 100 and its intended use. In general, however, the cathode structures 206 will typically have a width WCE within the range of about 0.01 mm to 2.5 mm. For example, in one embodiment, the width WCE of each cathode structure 206 will be in the range of about 0.025 mm to about 2 mm. By way of further example, in one embodiment, the width WCE of each cathode structure 206 will be in the range of about 0.05 mm to about 1 mm. According to one embodiment, the cathode structures 206 include one or more first electrode members having a first width, and one or more second electrode members having a second width that is different than the first width. In yet another embodiment, the different widths for the one or more first electrode members and one or more second electrode members may be selected to accommodate a predetermined shape for the secondary battery 100, such as an assembly having a different widths along one or more of the longitudinal and/or transverse axis, and/or to provide predetermined performance characteristics for the secondary battery 100.
The height HCE of the cathode structures 206 will also vary depending upon the secondary battery 100 and its intended use. In general, however, the cathode structures 206 will typically have a height HCE within the range of about 0.05 mm to about 25 mm. For example, in one embodiment, the height HCE of each cathode structure 206 will be in the range of about 0.05 mm to about 5 mm. By way of further example, in one embodiment, the height HCE of each cathode structure 206 will be in the range of about 0.1 mm to about 1 mm. According to one embodiment, the cathode structures 206 include one or more first cathode members having a first height, and one or more second cathode members having a second height that is different than the first height. In yet another embodiment, the different heights for the one or more first cathode members and one or more second cathode members may be selected to accommodate a predetermined shape for the secondary battery 100, such as a shape having a different heights along one or more of the longitudinal and/or transverse axis, and/or to provide predetermined performance characteristics for the secondary battery 100.
In general, each cathode structure 206 has a length LCE that is substantially greater than its width WCE and substantially greater than its height HCE. For example, in one embodiment, the ratio of LCE to each of WCE and HCE is at least 5:1, respectively (that is, the ratio of LCE to WCE is at least 5:1, respectively and the ratio of LCE to HCE is at least 5:1, respectively), for each cathode structure 206. By way of further example, in one embodiment the ratio of LCE to each of WCE and HCE is at least 10:1 for each cathode structure 206. By way of further example, in one embodiment, the ratio of LCE to each of WCE and HCE is at least 15:1 for each cathode structure 206. By way of further example, in one embodiment, the ratio of LCE to each of WCE and HCE is at least 20:1 for each cathode structure 206.
In one embodiment, the ratio of the height HCE to the width WCE of the cathode structures 206 is at least 0.4:1, respectively. For example, in one embodiment, the ratio of HCE to WCE will be at least 2:1, respectively, for each cathode structure 206. By way of further example, in one embodiment, the ratio of HCE to WCE will be at least 10:1, respectively, for each cathode structure 206. By way of further example, in one embodiment, the ratio of HCE to WCE will be at least 20:1, respectively, for each cathode structure 206. Typically, however, the ratio of HCE to WCE will generally be less than 1,000:1, respectively, for each cathode structure 206. For example, in one embodiment, the ratio of HCE to WCE will be less than 500:1, respectively, for each cathode structure 206. By way of further example, in one embodiment, the ratio of HCE to WCE will be less than 100:1, respectively. By way of further example, in one embodiment, the ratio of HCE to WCE will be less than 10:1, respectively. By way of further example, in one embodiment, the ratio of HCE to WCE will be in the range of about 2:1 to about 100:1, respectively, for each cathode structure 206.
Referring again to
In general, the anodically active material layers 104 in the unit cell 200 may be selected from the group consisting of: (a) silicon (Si), germanium (Ge), tin (Sn), lead (Pb), antimony (Sb), bismuth (Bi), zinc (Zn), aluminum (Al), titanium (Ti), nickel (Ni), cobalt (Co), and cadmium (Cd); (b) alloys or intermetallic compounds of Si, Ge, Sn, Pb, Sb, Bi, Zn, Al, Ti, Ni, Co, or Cd with other elements; (c) oxides, carbides, nitrides, sulfides, phosphides, selenides, and tellurides of Si, Ge, Sn, Pb, Sb, Bi, Zn, Al, Ti, Fe, Ni, Co, V, or Cd, and their mixtures, composites, or lithium-containing composites; (d) salts and hydroxides of Sn; (e) lithium titanate, lithium manganate, lithium aluminate, lithium-containing titanium oxide, lithium transition metal oxide, ZnCo2O4; (f) particles of graphite and carbon; (g) lithium metal; and (h) combinations thereof.
Exemplary anodically active material layers 104 include carbon materials such as graphite and soft or hard carbons, or graphene (e.g., single-walled or multi-walled carbon nanotubes), or any of a range of metals, semi-metals, alloys, oxides, nitrides and compounds capable of intercalating lithium or forming an alloy with lithium. Specific examples of the metals or semi-metals capable of constituting the anode material include graphite, tin, lead, magnesium, aluminum, boron, gallium, silicon, Si/C composites, Si/graphite blends, silicon oxide (SiOx), porous Si, intermetallic Si alloys, indium, zirconium, germanium, bismuth, cadmium, antimony, silver, zinc, arsenic, hafnium, yttrium, lithium, sodium, graphite, carbon, lithium titanate, palladium, and mixtures thereof. In one exemplary embodiment, the anodically active material comprises aluminum, tin, or silicon, or an oxide thereof, a nitride thereof, a fluoride thereof, or other alloy thereof. In another exemplary embodiment, the anodically active material layers 104 comprise silicon or an alloy or oxide thereof.
In one embodiment, the anodically active material layers 104 are microstructured to provide a significant void volume fraction to accommodate volume expansion and contraction as lithium ions (or other carrier ions) are incorporated into or leave the anodically active material layers 104 during charging and discharging processes for the secondary battery 100. In general, the void volume fraction of (each of) the anodically active material layer 104 is at least 0.1. Typically, however, the void volume fraction of (each of) the anodically active material layer 104 is not greater than 0.8. For example, in one embodiment, the void volume fraction of (each of) the anodically active material layer 104 is about 0.15 to about 0.75. By way of the further example, in one embodiment, the void volume fraction of (each of) the anodically active material layer 104 is about 0.2 to about 0.7. By way of the further example, in one embodiment, the void volume fraction of (each of) the anodically active material layer 104 is about 0.25 to about 0.6.
Depending upon the composition of the microstructured anodically active material layers 104 and the method of their formation, the microstructured anodically active material layers 104 may comprise macroporous, microporous, or mesoporous material layers or a combination thereof, such as a combination of microporous and mesoporous, or a combination of mesoporous and macroporous. Microporous material is typically characterized by a pore dimension of less than 10 nanometer (nm), a wall dimension of less than 10 nm, a pore depth of 1 μm to 50 μm, and a pore morphology that is generally characterized by a “spongy” and irregular appearance, walls that are not smooth, and branched pores. Mesoporous material is typically characterized by a pore dimension of 10 nm to 50 nm, a wall dimension of 10 nm to 50 nm, a pore depth of 1 μm to 100 μm, and a pore morphology that is generally characterized by branched pores that are somewhat well defined or dendritic pores. Macroporous material is typically characterized by a pore dimension of greater than 50 nm, a wall dimension of greater than 50 nm, a pore depth of 1 μm to 500 μm, and a pore morphology that may be varied, straight, branched, or dendritic, and smooth or rough-walled. Additionally, the void volume may comprise open or closed voids, or a combination thereof. In one embodiment, the void volume comprises open voids, that is, the anodically active material layers 104 contain voids having openings at the lateral surface of the anodically active material layers through which lithium ions (or other carrier ions) can enter or leave. For example, lithium ions may enter the anodically active material layers 104 through the void openings after leaving the cathodically active material layers 106. In another embodiment, the void volume comprises closed voids, that is, the anodically active material layers 104 contain voids that are enclosed. In general, open voids can provide greater interfacial surface area for the carrier ions whereas closed voids tend to be less susceptible to SEI formation, while each provides room for the expansion of anodically active material layers 104 upon the entry of carrier ions. In certain embodiments, therefore, it is preferred that the anodically active material layers 104 comprise a combination of open and closed voids.
In one embodiment, the anodically active material layers 104 comprise porous aluminum, tin or silicon or an alloy, an oxide, or a nitride thereof. Porous silicon layers may be formed, for example, by anodization, by etching (e.g., by depositing precious metals such as gold, platinum, silver or gold/palladium on the surface of single crystal silicon and etching the surface with a mixture of hydrofluoric acid and hydrogen peroxide), or by other methods known in the art such as patterned chemical etching. Additionally, the porous anodically active material layers 104 will generally have a porosity fraction of at least about 0.1, but less than 0.8 and have a thickness of about 1 μm to about 100 μm. For example, in one embodiment, the anodically active material layers 104 comprise porous silicon, have a thickness of about 5 μm to about 100 μm, and have a porosity fraction of about 0.15 to about 0.75. By way of further example, in one embodiment, the anodically active material layers 104 comprise porous silicon, have a thickness of about 10 μm to about 80 μm, and have a porosity fraction of about 0.15 to about 0.7. By way of further example, in one such embodiment, the anodically active material layers 104 comprise porous silicon, have a thickness of about 20 μm to about 50 μm, and have a porosity fraction of about 0.25 to about 0.6. By way of further example, in one embodiment, the anodically active material layers 104 comprise a porous silicon alloy (such as nickel silicide), have a thickness of about 5 μm to about 100 μm, and have a porosity fraction of about 0.15 to about 0.75.
In another embodiment, the anodically active material layers 104 comprise fibers of aluminum, tin, or silicon, or an alloy thereof. Individual fibers may have a diameter (thickness dimension) of about 5 nm to about 10,000 nm and a length generally corresponding to the thickness of the anodically active material layers 104. Fibers (nanowires) of silicon may be formed, for example, by chemical vapor deposition or other techniques known in the art such as vapor liquid solid (VLS) growth and solid liquid solid (SLS) growth. Additionally, the anodically active material layers 104 will generally have a porosity fraction of at least about 0.1, but less than 0.8 and have a thickness of about 1 μm to about 200 μm. For example, in one embodiment, the anodically active material layers 104 comprise silicon nanowires, have a thickness of about 5 μm to about 100 μm, and a porosity fraction of about 0.15 to about 0.75. By way of further example, in one embodiment, the anodically active material layers 104 comprise silicon nanowires, have a thickness of about 10 μm to about 80 μm, and a porosity fraction of about 0.15 to about 0.7. By way of further example, in one such embodiment, the anodically active material layers 104 comprise silicon nanowires, have a thickness of about 20 μm to about 50 μm, and a porosity fraction of about 0.25 to about 0.6. By way of further example, in one embodiment, the anodically active material layers 104 comprise nanowires of a silicon alloy (such as nickel silicide), have a thickness of about 5 μm to about 100 μm, and a porosity fraction of about 0.15 to about 0.75.
In yet other embodiments, the anodically active material layers 104 are coated with a particulate lithium material selected from the group consisting of stabilized lithium metal particles, e.g., lithium carbonate-stabilized lithium metal powder, lithium silicate stabilized lithium metal powder, or other source of stabilized lithium metal powder or ink. The particulate lithium material may be applied on the anodically active material layers 104 by spraying, loading, or otherwise disposing the lithium particulate material onto the anodically active material layers 104 at a loading amount of about 0.05 mg/cm2 to 5 mg/cm2, e.g., about 0.1 mg/cm2 to 4 mg/cm2, or even about 0.5 mg/cm2 to 3 mg/cm2. The average particle size (D50) of the lithium particulate material may be 5 μm to 200 μm, e.g., about 10 μm to 100 μm, 20 μm to 80 μm, or even about 30 μm to 50 μm. The average particle size (D50) may be defined as a particle size corresponding to 50% in a cumulative volume-based particle size distribution curve. The average particle size (D50) may be measured, for example, using a laser diffraction method.
In one embodiment, the anode current collector 202, has an electrical conductance that is substantially greater than the electrical conductance of its associated anodically active material layers 104. For example, in one embodiment, the ratio of the electrical conductance of the anode current collector 202 to the electrical conductance of the anodically active material layers 104 is at least 100:1 when there is an applied current to store energy in the secondary battery 100 or an applied load to discharge the secondary battery 100. By way of further example, in some embodiments, the ratio of the electrical conductance of the anode current collector 202 to the electrical conductance of the anodically active material layers 104 is at least 500:1 when there is an applied current to store energy in the secondary battery 100 or an applied load to discharge the secondary battery 100. By way of further example, in some embodiments, the ratio of the electrical conductance of the anode current collector 202 to the electrical conductance of the anodically active material layers 104 is at least 1000:1 when there is an applied current to store energy in the secondary battery 100 or an applied load to discharge the secondary battery 100. By way of further example, in some embodiments, the ratio of the electrical conductance of the anode current collector 202 to the electrical conductance of the anodically active material layers 104 is at least 5000:1 when there is an applied current to store energy in the secondary battery 100 or an applied load to discharge the secondary battery 100. By way of further example, in some embodiments, the ratio of the electrical conductance of the anode current collector 202 to the electrical conductance of the anodically active material layers 104 is at least 10,000:1 when there is an applied current to store energy in the secondary battery 100 or an applied load to discharge the secondary battery 100.
The length LE of the anode structures 207 will vary depending upon the secondary battery 100 and its intended use. In general, however, the anode structures 207 will typically have a length LE in the range of about 5 millimeter (mm) to about 500 mm. For example, in one such embodiment, the anode structures 207 have a length LE of about 10 mm to about 250 mm. By way of further example, in one such embodiment, the anode structures 207 have a length LE of about 25 mm to about 100 mm. According to one embodiment, the anode structure 207 include one or more first electrode members having a first length, and one or more second electrode members having a second length that is different than the first length. In yet another embodiment, the different lengths for the one or more first electrode members and the one or more second electrode members may be selected to accommodate a predetermined shape for the secondary battery 100, such as a shape having a different lengths along one or more of the longitudinal and/or transverse axis, and/or to provide predetermined performance characteristics for the secondary battery 100.
The width WE of the anode structures 207 will also vary depending upon the secondary battery 100 and its intended use. In general, however, each anode structure 207 will typically have a width WE within the range of about 0.01 mm to 2.5 mm. For example, in one embodiment, the width WE of each anode structure 207 will be in the range of about 0.025 mm to about 2 mm. By way of further example, in one embodiment, the width WE of each anode structure 207 will be in the range of about 0.05 mm to about 1 mm. According to one embodiment, the anode structures 207 include one or more first electrode members having a first width, and one or more second electrode members having a second width that is different than the first width. In yet another embodiment, the different widths for the one or more first electrode members and one or more second electrode members may be selected to accommodate a predetermined shape for the secondary battery 100, such as a shape having a different widths along one or more of the longitudinal and/or transverse axis, and/or to provide predetermined performance characteristics for the secondary battery 100.
The height HE of the anode structures 207 will also vary depending upon the secondary battery 100 and its intended use. In general, however, the anode structures 207 will typically have a height HE within the range of about 0.05 mm to about 25 mm. For example, in one embodiment, the height HE of each anode structure 207 will be in the range of about 0.05 mm to about 5 mm. By way of further example, in one embodiment, the height HE of each anode structure 207 will be in the range of about 0.1 mm to about 1 mm. According to one embodiment, the anode structures 207 include one or more first electrode members having a first height, and one or more second electrode members having a second height that is different than the first height. In yet another embodiment, the different heights for the one or more first electrode members and one or more second electrode members may be selected to accommodate a predetermined shape for the secondary battery 100, such as a shape having a different heights along one or more of the longitudinal and/or transverse axis, and/or to provide predetermined performance characteristics for the secondary battery 100.
In general, the anode structures 207 each have a length LE that is substantially greater than each of its width WE and its height HE. For example, in one embodiment, the ratio of LE to each of WE and HE is at least 5:1, respectively (that is, the ratio of LE to WE is at least 5:1, respectively and the ratio of LE to HE is at least 5:1, respectively), for each anode structure 207. By way of further example, in one embodiment, the ratio of LE to each of WE and HE is at least 10:1. By way of further example, in one embodiment, the ratio of LE to each of WE and HE is at least 15:1. By way of further example, in one embodiment, the ratio of LE to each of WE and HE is at least 20:1, for each anode structure 207.
In one embodiment, the ratio of the height HE to the width WE of the anode structures 207 is at least 0.4:1, respectively. For example, in one embodiment, the ratio of HE to WE will be at least 2:1, respectively, for each anode structure 207. By way of further example, in one embodiment, the ratio of HE to WE will be at least 10:1, respectively. By way of further example, in one embodiment, the ratio of HE to WE will be at least 20:1, respectively. Typically, however, the ratio of HE to WE will generally be less than 1,000:1, respectively. For example, in one embodiment, the ratio of HE to WE will be less than 500:1, respectively. By way of further example, in one embodiment, the ratio of HE to WE will be less than 100:1, respectively. By way of further example, in one embodiment, the ratio of HE to WE will be less than 10:1, respectively. By way of further example, in one embodiment, the ratio of HE to WE will be in the range of about 2:1 to about 100:1, respectively, for each anode structure 207.
Referring again to
In general, the separator layers 108 will each have a thickness of at least about 4 μm. For example, in one embodiment, the separator layers 108 will have a thickness of at least about 8 μm. By way of further example, in one such embodiment, the separator layers 108 will have a thickness of at least about 12 μm. By way of further example, in one such embodiment, the separator layers 108 will have a thickness of at least about 15 μm. In some embodiments, the separator layers 108 will have a thickness of up to 25 μm, up to 50 or any other suitable thickness. Typically, however, the separator layers 108 will have a thickness of less than about 12 μm or less than about 10 μm.
In general, the material of the separator layers 108 may be selected from a wide range of material having the capacity to conduct carrier ions between the anodically active material layers 104 and the cathodically active material layers 106 of the unit cell 200. For example, the separator layers 108 may comprise a microporous separator material that may be permeated with a liquid, non-aqueous electrolyte. Alternatively, the separator layers 108 may comprise a gel or solid electrolyte capable of conducting carrier ions between the anodically active material layers 104 and the cathodically active material layers 106 of the unit cell 200.
In one embodiment, the separator layers 108 may comprise a polymer-based electrolyte. Exemplary polymer electrolytes include PEO-based polymer electrolytes and polymer-ceramic composite electrolytes.
In another embodiment, the separator layers 108 may comprise an oxide-based electrolyte. Exemplary oxide-based electrolytes include lithium lanthanum titanate (Li0.34La0.56TiO3), Al-doped lithium lanthanum zirconate (Li6.24La3Zr2Al0.24O11.98), Ta-doped lithium lanthanum zirconate (Li6.4La3Zr1.4Ta0.6O12), and lithium aluminum titanium phosphate (Li1.4Al0.4Ti1.6(PO4)3).
In another embodiment, the separator layers 108 may comprise a solid electrolyte. Exemplary solid electrolytes include sulfide-based electrolytes such as lithium tin phosphorus sulfide (Li1SnP2Si2), lithium phosphorus sulfide (β-Li3PS4), and lithium phosphorus sulfur chloride iodide (Li6PS5Cl0.9I0.1).
In some embodiments, the separator layers 108 may comprise a solid-state lithium ion conducting ceramic, such as a lithium-stuffed garnet.
In one embodiment, the separator layers 108 comprise a microporous separator material comprising a particulate material and a binder, with the microporous separator material having a porosity (void fraction) of at least about 20 vol. %. The pores of the microporous separator material will have a diameter of at least 50 Å and will typically fall within the range of about 250 Å to about 2,500 Å. The microporous separator material will typically have a porosity of less than about 75%. In one embodiment, the microporous separator material has a porosity (void fraction) of at least about 25 vol %. In one embodiment, the microporous separator material will have a porosity of about 35-55%.
The binder for the microporous separator material may be selected from a wide range of inorganic or polymeric materials. For example, in one embodiment, the binder is an organic material selected from the group consisting of silicates, phosphates, aluminates, aluminosilicates, and hydroxides such as magnesium hydroxide, calcium hydroxide, etc. For example, in one embodiment, the binder is a fluoropolymer derived from monomers containing vinylidene fluoride, hexafluoropropylene, tetrafluoropropene, and the like. In another embodiment, the binder is a polyolefin such as polyethylene, polypropylene, or polybutene, having any of a range of varying molecular weights and densities. In another embodiment, the binder is selected from the group consisting of ethylene-diene-propene terpolymer, polystyrene, polymethyl methacrylate, polyethylene glycol, polyvinyl acetate, polyvinyl butyral, polyacetal, and polyethyleneglycol diacrylate. In another embodiment, the binder is selected from the group consisting of methyl cellulose, carboxymethyl cellulose, styrene rubber, butadiene rubber, styrene-butadiene rubber, isoprene rubber, polyacrylamide, polyvinyl ether, polyacrylic acid, polymethacrylic acid, and polyethylene oxide. In another embodiment, the binder is selected from the group consisting of acrylates, styrenes, epoxies, and silicones. In another embodiment, the binder is a copolymer or blend of two or more of the aforementioned polymers.
The particulate material comprised by the microporous separator material may also be selected from a wide range of materials. In general, such materials have a relatively low electronic and ionic conductivity at operating temperatures and do not corrode under the operating voltages of the battery electrode or current collector contacting the microporous separator material. For example, in one embodiment, the particulate material has a conductivity for carrier ions (e.g., lithium) of less than 1×10−4 Siemens/cm (S/cm). By way of further example, in one embodiment, the particulate material has a conductivity for carrier ions of less than 1×10−5 S/cm. By way of further example, in one embodiment, the particulate material has a conductivity for carrier ions of less than 1×10−6 S/cm. Exemplary particulate materials include particulate polyethylene, polypropylene, a TiO2-polymer composite, silica aerogel, fumed silica, silica gel, silica hydrogel, silica xerogel, silica sol, colloidal silica, alumina, titania, magnesia, kaolin, talc, diatomaceous earth, calcium silicate, aluminum silicate, calcium carbonate, magnesium carbonate, or a combination thereof. For example, in one embodiment, the particulate material comprises a particulate oxide or nitride such as TiO2, SiO2, Al2O3, GeO2, B2O3, Bi2O3, BaO, ZnO, ZrO2, BN, Si3N4, and Ge3N4. See, for example, P. Arora and J. Zhang, “Battery Separators” Chemical Reviews 2004, 104, 4419-4462). In one embodiment, the particulate material will have an average particle size of about 20 nm to 2 μm, more typically 200 nm to 1.5 μm. In one embodiment, the particulate material will have an average particle size of about 500 nm to 1 μm.
In an alternative embodiment, the particulate material comprised by the microporous separator material may be bound by techniques such as sintering, binding, curing, etc. while maintaining the void fraction desired for electrolyte ingress to provide the ionic conductivity for the functioning of the battery.
In the secondary battery 100 (see
When a secondary battery is assembled, the amount of carrier ions available for cycling between the anode and the cathode is often initially provided in the cathode, because cathodically active materials, such as lithium cobalt oxide, are relatively stable in ambient air (e.g., they resist oxidation) compared to lithiated anode materials, such as lithiated graphite. When a secondary battery is charged for the first time, the carrier ions are extracted from the cathode and introduced into the anode. As a result, the anode potential is lowered significantly (toward the potential of the carrier ions), and the cathode potential is increased (to become even more positive). These changes in potential may give rise to parasitic reactions on both the cathode and the anode, but sometimes more severely on the anode. For example, a decomposition product comprising lithium (or other carrier ions) and electrolyte components, known as solid electrolyte interphase (SEI), may readily form on the surfaces of carbon anodes. These surfaces or covering layers are carrier ion conductors, which establish an ionic connection between the anode and the electrolyte and prevent the reactions from proceeding any further.
Although formation of the SEI layer is desired for the stability of a half-cell system comprising the anode and the electrolyte, a portion of the carrier ions introduced into the cells via the cathode is irreversibly bound and thus removed from cyclic operation, i.e., from the capacity available to the user. As a result, during the initial discharge, fewer carrier ions are returned to the cathode from the anode than was initially provided by the cathode during the initial charging operation, leading to irreversible capacity loss. During each subsequent charge and discharge cycle, the capacity losses resulting from mechanical and/or electrical degradation to the anode and/or the cathode tend to be much less per cycle, but even the relatively small carrier ion losses per cycle contribute significantly to reductions in energy density and cycle life as the battery ages. In addition, chemical and electrochemical degradation may also occur on the electrodes and cause capacity losses. To compensate for the formation of SEI (or another carrier ion-consuming mechanism such as mechanical and/or electrical degradation of the negative electrode), additional or supplementary carrier ions may be provided from an auxiliary electrode after formation of the battery.
In general, the positive electrode 208 of the secondary battery 100 (e.g., the collective population of the cathode structures 206 in the secondary battery 100) preferably has a reversible coulombic capacity that is matched to the discharge capacity of the negative electrode 209 (e.g., the collective population of the anode structures 207 in the secondary battery 100). Stated differently, the positive electrode 208 of the secondary battery 100 is sized to have a reversible coulombic capacity that corresponds to the discharge capacity of the negative electrode 209 which, in turn, is a function of the negative electrode 209 end of discharge voltage.
In some embodiments, the negative electrode 209 of the secondary battery 100 (e.g., the collective population of the anode structures 207 in the secondary battery 100) is designed to have a reversible coulombic capacity that exceeds the reversible coulombic capacity of the positive electrode 208. For example, in one embodiment, a ratio of the reversible coulombic capacity of the negative electrode 209 to the reversible coulombic capacity of the positive electrode 208 is at least 1.2:1, respectively. By way of further example, in one embodiment, a ratio of the reversible coulombic capacity of the negative electrode 209 to the reversible coulombic capacity of the positive electrode 208 is at least 1.3:1, respectively. By way of further example, in one embodiment, a ratio of the reversible coulombic capacity of the negative electrode 209 to the reversible coulombic capacity of the positive electrode 208 is at least 2:1, respectively. By way of further example, in one embodiment, a ratio of the reversible coulombic capacity of the negative electrode 209 to the reversible coulombic capacity of the positive electrode 208 is at least 3:1, respectively. By way of further example, a ratio of the reversible coulombic capacity of the negative electrode 209 to the reversible coulombic capacity of the positive electrode 208 is at least 4:1, respectively. By way of further example, a ratio of the reversible coulombic capacity of the negative electrode 209 to the reversible coulombic capacity of the positive electrode 208 is at least 5:1, respectively. Advantageously, the excess coulombic capacity of the negative electrode 209 provides a source of anodically active material to allow the secondary battery 100 to reversibly operate within a specified voltage that inhibits formation of crystalline phases (incorporating carrier ions) on the negative electrode 209 that reduce cycle-life of the negative electrode 209 as result of cycling.
As previously noted, the formation of SEI during the initial charge/discharge cycle reduces the amount of carrier ions available for reversible cycling. Mechanical and/or electrical degradation of the negative electrode 209 during cycling of the secondary battery 100 may further reduce the amount of carrier ions available for reversible cycling. To compensate for the formation of SEI (or another carrier ion-consuming mechanism such as mechanical and/or electrical degradation of the negative electrode), therefore, additional or supplementary carrier ions may be provided from an auxiliary electrode after formation of the secondary battery 100. In the embodiments of the present disclosure, the auxiliary electrode is used to electrochemically transfer additional carrier ions to the positive electrode 208 and/or the negative electrode 209 of the secondary battery 100 during and/or after formation. In one embodiment, the auxiliary electrode is removed after transferring the additional carrier ions to the secondary battery 100 in order to improve the energy density of the secondary battery in its final form.
Referring to
The auxiliary electrode 502 partially surrounds the secondary battery 100 in the buffer system 500, and contains a source of carrier ions to replenish the lost energy capacity of the secondary battery 100 after formation (i.e., to compensate for the loss of carrier ions upon the formation of SEI and other carrier ion losses in the first charge and/or discharge cycle of the secondary battery 100). In embodiments, the auxiliary electrode 502 may comprise a foil of the carrier ions in metallic form (e.g., a foil of lithium, magnesium, or aluminum), or any of the previously mentioned materials used for the cathodically active material layers 106 and/or the anodically active material layers 104 (see
Referring to
The separator 702 may comprise any of the materials previously described with respect to the separator layer 108 of the secondary battery 100. The separator 702 may be permeated with an electrolyte that serves as a medium to conduct carrier ions from the carrier ion supply layers 706 to the positive electrode 208 of the secondary battery 100 and/or the negative electrode 209 of the secondary battery. The electrolyte may comprise any of the materials previously described with respect to the secondary battery 100.
The separator 702 in this embodiment includes a first surface 802 and a second surface 803 that opposes the first surface 802. The surfaces 802, 803 of the separator 702 form major surfaces for the separator 702 and are disposed in the X-Y plane in
In one embodiment, the width 804 of the separator 702 is about 34 mm. In other embodiments, the width 804 of the separator is about 30 mm, about 35 mm, or another suitable value. In some embodiments, the width 804 of the separator 702 lies in a range of values of about 10 mm to about 200 mm, or some other suitable range that allows the separator 702 to function as described herein.
The separator 702, in one embodiment, has a length 808 that extends in a direction of the X-axis. In an embodiment, the length 808 of the separator 702 is about 72 mm. In other embodiments, the length 808 of the separator 702 is about 65 mm, about 70 mm, about 75 mm, or some other suitable value that allows the separator 702 to function as described herein. In some embodiments, the length 808 of the separator 702 lies in a range of values of about 30 mm to about 200 mm, or some other suitable range of values that allows the separator 702 to function as described herein.
In one embodiment, the separator 702 has a thickness 810 that extends in the direction of the Z-axis. Generally, the thickness 810 is a distance from the first surface 802 of the separator 702 to (and including) the second surface 803 of the separator. In one embodiment, the thickness 810 of the separator 702 is about 0.025 mm. In other embodiments, the thickness 810 of the separator 702 is about 0.015 mm, about 0.02 mm, about 0.03 mm, about 0.035 mm, or some other suitable value. In some embodiments, the thickness 810 of the separator 702 lies in a range of values of about 0.01 mm to about 1.0 mm, or some other suitable range of values that allows the separator 702 to function as described herein.
The conductive layer 704 is electrically conductive, and may comprise a metal, a metalized film, an insulating base material with a conductive material applied thereto, or some other type of electrically conductive material. In some embodiments, the conductive layer 704 comprises copper. In other embodiments, the conductive layer 704 comprises aluminum or another metal. In this embodiment, the conductive layer 704 is electrically coupled with the conductive tab 508-2, which is also electrically conductive. The conductive tab 508-2 has a first end 812 disposed proximate to the conductive layer 704 and a second end 813 disposed distal to the conductive layer 704 that opposes the first end 812. The first end 812 of the conductive tab 508-2 is electrically coupled to the conductive layer 704. In some embodiments, the first end 812 of the conductive tab 508-2 is spot-welded to the conductive layer 704. In other embodiments, the first end 812 of the conductive tab 508-2 is soldered to the conductive layer 704. Generally, the conductive tab 508-2 may be affixed at the first end 812 to the conductive layer 704 using any suitable means that ensure a mechanical connection and an electrical connection to the conductive layer. The conductive tab 508-2 may comprise any type of electrically conductive material as desired. In one embodiment, the conductive tab 508-2 comprises a metal. In these embodiments, the conductive tab 508-2 may comprise nickel, copper, aluminum, or other suitable metals or metal alloys that allows the conductive tab 508-2 to function as described herein.
The conductive layer 704 in this embodiment includes a first surface 814 and a second surface 815 that opposes the first surface 814. The surfaces 814, 815 of the conductive layer 704 form major surfaces for the conductive layer 704 and are disposed in the X-Y plane in
In some embodiments, the width 816 of the conductive layer 704 lies in a range of values of about 5 mm to about 100 mm, or some other suitable range of values that allows the conductive layer 704 to function as described herein. The first surface 814 of the conductive layer 704 in this embodiment is segmented into a first region 818-1, disposed proximate to a first end 820 of the conductive layer 704, a second region 818-2, disposed proximate to a second end 821 of the conductive layer 704, and a third region 818-3 disposed between the first region 818-1 and the second region 818-2.
The conductive layer 704 has a length 822 that extends in a direction of the X-axis. In one embodiment, the length 822 of the conductive layer 704 is about 70 mm. In other embodiments, the length 822 of the conductive layer 704 is about 60 mm, about 65 mm, about 75 mm, or some other suitable value that allows the conductive layer 704 to function as described herein. In some embodiments, the length 822 of the conductive layer 704 lies in a range of values of about 30 mm to about 200 mm, or some other suitable range of values that allows the conductive layer 704 to function as described herein.
The conductive layer 704 has a thickness 824 that extends in a direction of the Z-axis. Generally, the thickness 824 is a distance from the first surface 814 of the conductive layer 704 to (and including) the second surface 815 of the conductive layer 704. In one embodiment, the thickness 824 of the conductive layer 704 is about 0.1 mm. In other embodiments, the thickness 824 of the conductive layer 704 is about 0.005 mm, about 0.15 mm, or about 0.2 mm. In some embodiments, the thickness 824 of the conductive layer 704 lies in a range of values of about 0.01 mm to about 1.0 mm, or any other suitable range for the thickness that allows the conductive layer 704 to function as described herein.
The carrier ion supply layers 706, which comprise a population of carrier ion supply layers 706 in an embodiment, comprise any carrier ion containing material previously described that may be utilized to supply carrier ions to the positive electrode 208 and/or the negative electrode 209 of the secondary battery 100. The carrier ion supply layers 706 may comprise one or more sources of lithium ions, sodium ions, potassium ions, calcium ions, magnesium ions, and aluminum ions. In this embodiment, the carrier ion supply layers 706 are disposed within the first region 818-1 and the second region 818-2 of the conductive layer 704. In some embodiments, the carrier ion supply layers 706 are also disposed in the third region 818-3 of the conductive layer 704.
The carrier ion supply layers 706 in this embodiment include a first surface 826 and a second surface 827 that opposes the first surface 826. The surfaces 826, 827 of the carrier ion supply layers 706 form major surfaces for the carrier ion supply layers 706 and are disposed in the X-Y plane in
The carrier ion supply layers 706, in one embodiment, have a length 830 that extends in a direction of the X-axis. In an embodiment, the length 830 of the carrier ion supply layers 706 are about 23 mm. In other embodiments, the length 830 of the carrier ion supply layers 706 are about 15 mm, about 20 mm, about 25 mm, or some other suitable length that allows the carrier ion supply layers 706 to function as described herein. In some embodiments, the length 830 of the carrier ion supply layers 706 lie in a range of values of about 10 mm to about 100 mm, or some other suitable range of values that allow the carrier ion supply layers 706 to function as described herein.
The carrier ion supply layers 706 each have a thickness 832 that extends in a direction of the Z-axis. Generally, the thickness 832 is a distance between the first surface 826 of the carrier ion supply layers 706 and the second surface 827 of the carrier ion supply layers 706. In one embodiment, the thickness 832 of the carrier ion supply layers 706 are about 0.13 mm. In other embodiments, the thickness 832 of the carrier ion supply layers 706 are about 0.005 mm, about 0.15 mm, or about 0.2 mm. In some embodiments, the thickness 832 of the carrier ion supply layers 706 lie in a range of values of about 0.01 mm to about 1.0 mm, or any other suitable range of values for the thickness 832 that allows the carrier ion supply layers 706 to function as described herein.
In this embodiment, the carrier ion supply layers 706 are separated from each other by a distance 834, corresponding to the third region 818-3. In one embodiment, the distance 834 is about 23 mm. In other embodiments, the distance 834 is about 15 mm, about 20 mm, about 25 mm, or about 30 mm. In some embodiments, the distance 834 lies in a range of values of about 10 mm to about 50 mm, or any other suitable range of values that allows the carrier ion supply layers 706 to function as described herein.
In one embodiment, the carrier ion supply layers 706 are sized to be capable of providing at least 15% of the reversible coulombic capacity of the positive electrode 208 of the secondary battery 100. For example, in one such embodiment, the carrier ion supply layers 706 are sized such that they contain sufficient carrier ions (e.g., lithium, magnesium, or aluminum ions) to provide at least 30% of the reversible coulombic capacity of the positive electrode 208 of the secondary battery 100. By way of further example, in one such embodiment, the carrier ion supply layers 706 are sized such that they contain sufficient carrier ions to provide at least 100% of the reversible coulombic capacity of the positive electrode 208 of the secondary battery 100. By way of further example, in one such embodiment, the carrier ion supply layers 706 are sized such that they contain sufficient carrier ions to provide at least 200% of the reversible coulombic capacity of the positive electrode 208 of the secondary battery 100. By way of further example, in one such embodiment, the carrier ion supply layers 706 are sized such that they contain sufficient carrier ions to provide at least 300% of the reversible coulombic capacity of the positive electrode 208 of the secondary battery 100. By way of further example, in one such embodiment, the carrier ion supply layers 706 are sized such that they contain sufficient carrier ions to provide about 100% to about 200% of the reversible coulombic capacity of the positive electrode 208 of the secondary battery 100.
During an assembly process for the auxiliary electrode 502, the separator 702 may be cut from stock material or prefabricated to achieve the width 804 and the length 808 as shown in
In other embodiments, the conductive layer 704 is prefabricated to include the carrier ion supply layers 706 arranged in the orientation depicted in
To continue the fabrication process of the auxiliary electrode 502, in one embodiment, the second portion 806 of the separator 702 is folded in the direction of an arrow 902 towards the left (about an axis parallel to the X-axis) in
In one embodiment, the separator 702 is bonded to itself along at least a portion of an outer perimeter 1002 of the separator using a hot melt process, a welding process, a bonding process, etc. In
In response to fabricating the auxiliary electrode 502, performing a fabrication process for the buffer system 500 (see
With the auxiliary electrode 502 oriented within the pouch 514 as depicted in
With the secondary battery 100 loaded onto the second region 818-2 of the auxiliary electrode 502 within the pouch 514, the auxiliary electrode 502 is folded in the direction of an arrow 1302 in order to position the first side 1004 of the first region 818-1 of the auxiliary electrode 502 in contact with the second major surface 127 of the secondary battery 100, the result of which is depicted in
With the secondary battery 100 sandwiched by the auxiliary electrode 502 within the pouch 514 as illustrated in
With the secondary battery 100 and the carrier ion supply layers 706 of the auxiliary electrode 502 (not visible in
Either prior to inserting the secondary battery 100 into the buffer system 500, or after, the secondary battery 100 is charged (e.g., via the electrical terminals 124, 125) by transferring carrier ions from the cathode structures 206 of the secondary battery to the anode structures 207 of the secondary battery. Charging may be discontinued when the positive electrode 208 of the secondary battery 100 reaches its the end-of-charge design voltage. During the initial charging cycle, SEI may form on the surfaces of the anode structures 207 of the secondary battery 100. To compensate for the loss of carrier ions to SEI, and to further provide additional carrier ions to mitigate the long term secondary reactions during cycling where carrier ions are lost due to side reactions, the positive electrode 208 and/or the negative electrode 209 of the secondary battery 100 may be replenished by applying a voltage across the auxiliary electrode 502 and the cathode structures 206 and/or the anode structures 207 (e.g., via the conductive tab 508-1 of the auxiliary electrode 502 and one of the electrical terminals 124, 125) to drive carrier ions from the carrier ion supply layers 706 of the auxiliary electrode 502 to the cathode structures 206 and/or the anode structures 207 of the secondary battery 100. Once the transfer of carrier ions from the auxiliary electrode 502 to the secondary battery 100 is complete, the negative electrode 209 of the secondary battery 100 is again charged, this time with carrier ions transferred from the cathode structures 206 of the secondary battery 100 to the anode structures 207 of the secondary battery.
In one embodiment, the amount of carrier ions transferred from the auxiliary electrode 502 to the secondary battery 100 during the buffer process is about 50% of the reversable columbic capacity of the positive electrode 208 of the secondary battery 100. In other embodiments, the amount of carrier ions transferred from the auxiliary electrode 502 to the secondary battery 100 during the buffer process is about 55%, about 60%, about 65%, about 70%, about 75%, about 80%, about 85%, about 90%, about 95%, or about 100% of the reversable columbic capacity of the positive electrode 208 of the secondary battery 100. In some embodiments, the amount of carrier ions transferred from the auxiliary electrode 502 to the secondary battery 100 lies in a range of values of about 1% to about 100% of the reversable columbic capacity of the positive electrode 208 of the secondary battery 100. In one particular embodiment, the negative electrode 209 of the secondary battery 100 has about 170% of the reversable columbic capacity of the positive electrode 208 of the secondary battery 100 stored as carrier ions when the secondary battery 100 is charged, and about 70% of the reversable columbic capacity of the positive electrode 208 of the secondary battery 100 stored as carrier ions when the secondary battery 100 is discharged. An excess of carrier ions at the negative electrode 209 of the secondary battery 100 provided during the buffer process provides a technical benefit of mitigating the loss of carrier ions at the secondary battery 100 due to SEI at initial formation. Further, an excess of carrier ions at the negative electrode 209 of the secondary battery 100 provided during the buffer process provides a technical benefit of mitigating the loss of carrier ions at the secondary battery 100 due to side reactions that deplete carrier ions in the secondary battery 100 as the secondary battery 100 is cycled during use, which reduces the capacity loss of the secondary battery 100 over time.
In some embodiments, transferring carrier ions from the auxiliary electrode 502 to the secondary battery 100 may occur concurrently with an initial formation of the secondary battery 100 (e.g., during the first charge of the secondary battery 100), and/or during a subsequent charge of the secondary battery 100 after initial formation. In these embodiments, carrier ions are transferred from the positive electrode 208 of the secondary battery 100 to the negative electrode 209 of the secondary battery 100. Concurrently with or based on a temporal delay or a temporal pattern, carrier ions are transferred from the auxiliary electrode 502 to the positive electrode 208 and/or the negative electrode 209 of the secondary battery 100.
In yet another embodiment, the positive electrode 208 may be replenished with carrier ions by simultaneously transferring carrier ions from the auxiliary electrode 502 to the positive electrode 208 of the secondary battery 100, while also transferring carrier ions from the positive electrode 208 of the secondary battery 100 to the negative electrode 209 of the secondary battery 100. Referring to
In one embodiment, without being limited by any particular theory, the carrier ions are transferred from the auxiliary electrode 502 to the positive electrode 208 of the secondary battery 100 as a part of the replenishment of the negative electrode 209 of the secondary battery 100 (as opposed to transferring from the auxiliary electrode 502 directly to the negative electrode 209 of the secondary battery), because the positive electrode 208 may be capable of more uniformly accepting carrier ions across the surface thereof, thus allowing the carrier ions to more uniformly participate in the transfer thereof between the positive electrode 208 and the negative electrode 209 of the secondary battery 100.
After the buffer process is performed on the secondary battery 100 utilizing the buffer system 500, the auxiliary electrode 502 may be removed from the buffer system 500 in order to improve the energy density of the secondary battery 100 in its final form. For example, after the buffer process, the carrier ion supply layers 706 (see
In this embodiment, the secondary battery 100 (see
The auxiliary electrode 502 (see
The auxiliary subassembly 516 is installed in the enclosure 504, where the electrical terminals 124, 125 of the secondary battery 100 and the electrically conductive tab 508 of the auxiliary electrode 502 electrically extend from the perimeter 506 of enclosure 504 (see step 1804, and
Carrier ions are transferred from the positive electrode 208 of the secondary battery 100 to the negative electrode 209 of the secondary battery 100 to at least partially charge the secondary battery 100 by applying a potential voltage across the electrical terminals 124, 125 (see step 1806). Charging may be discontinued when the positive electrode 208 of the secondary battery 100 reaches its the end-of-charge design voltage. During the initial charging cycle, SEI may form on the internal structural surfaces of the negative electrode 209 of the secondary battery 100.
To compensate for the loss of carrier ions to SEI, and to further provide additional carrier ions to mitigate the long term secondary reactions during cycling where carrier ions are lost due to side reactions, carrier ions are transferred from the carrier ion supply layers 706 of the auxiliary electrode 502 to the positive electrode 208 and/or the negative electrode 209 of the secondary battery 100 by applying a potential voltage across the electrically conductive tab 508 of the auxiliary electrode 502 and one or more of the electrical terminals 124, 125 of the secondary battery 100 (see step 1808,
In one embodiment, the amount of carrier ions transferred from the auxiliary electrode 502 to the secondary battery 100 is about 50% of the reversable columbic capacity of the positive electrode 208 of the secondary battery 100. In other embodiments, the amount of carrier ions transferred from the auxiliary electrode 502 to the secondary battery 100 is about 55%, about 60%, about 65%, about 70%, about 75%, about 80%, about 85%, about 90%, about 95%, or about 100% of the reversable columbic capacity of the positive electrode 208 of the secondary battery 100. In some embodiments, the amount of carrier ions transferred from the auxiliary electrode 502 to the secondary battery 100 lies in a range of values of about 1% to about 100% of the reversable columbic capacity of the positive electrode 208 of the secondary battery 100. In one particular embodiment, the negative electrode 209 of the secondary battery 100 has about 170% of the reversable columbic capacity of the positive electrode 208 of the secondary battery 100 stored as carrier ions when the secondary battery 100 is charged, and about 70% of the reversable columbic capacity of the positive electrode 208 of the secondary battery 100 stored as carrier ions when the secondary battery 100 is discharged. An excess of carrier ions at the negative electrode 209 of the secondary battery 100 provided during the buffer process provides a technical benefit of mitigating the loss of carrier ions at the secondary battery 100 due to SEI at initial formation. Further, an excess of carrier ions at the negative electrode 209 of the secondary battery 100 provided during the buffer process provides a technical benefit of mitigating the loss of carrier ions at the secondary battery 100 due to side reactions that deplete carrier ions in the secondary battery 100 as the secondary battery 100 is cycled during use, which reduces the capacity loss of the secondary battery 100 over time.
In some embodiments, transferring carrier ions from the auxiliary electrode 502 to the secondary battery 100 may occur concurrently with an initial formation of the secondary battery 100 (e.g., during the first charge of the secondary battery 100), and/or during a subsequent charge of the secondary battery 100 after initial formation. In these embodiments, carrier ions are transferred from the positive electrode 208 of the secondary battery 100 to the negative electrode 209 of the secondary battery 100. Concurrently with or based on a temporal delay or a temporal pattern, carrier ions are transferred from the auxiliary electrode 502 to the positive electrode 208 and/or the negative electrode 209 of the secondary battery 100.
Carrier ions are again transferred from the positive electrode 208 of the secondary battery 100 to the negative electrode 209 of the secondary battery 100 to charge the secondary battery 100 by applying a potential voltage across the electrical terminals 124, 125 of the secondary battery 100 until the negative electrode 209 has greater than 100% of the positive electrode 208 coulombic capacity stored as the carrier ions (see step 1810).
In yet another embodiment, the positive electrode 208 may be replenished with carrier ions by simultaneously transferring carrier ions from the auxiliary electrode 502 to the positive electrode 208 of the secondary battery 100, while also transferring carrier ions from the positive electrode 208 of the secondary battery 100 to the negative electrode 209 of the secondary battery 100. Referring to
In one embodiment, without being limited by any particular theory, the carrier ions are transferred from the auxiliary electrode 502 to the positive electrode 208 of secondary battery 100 as a part of the replenishment of the negative electrode 209 of the secondary battery 100 (as opposed to transferring from the auxiliary electrode 502 directly to the negative electrode 209 of the secondary battery 100), because the positive electrode 208 may be capable of more uniformly accepting carrier ions across the surface thereof, thus allowing the carrier ions to more uniformly participate in the transfer thereof between the positive electrode 208 and the negative electrode 209 of the secondary battery 100.
In some embodiments of the method 1800, the enclosure 504 is opened (see step 1902 of
Although installing the auxiliary subassembly 516 in the enclosure 504 as previously described with respect to step 1804 detailed above, one particular embodiment comprises installing the auxiliary subassembly 516 on the first enclosure layer 510 (see step 2002 of
The enclosure layers 510, 511 may be sealed along the sealing line 1602 (see
In embodiments where the first enclosure layer 510 includes the pouch 514, installing the auxiliary subassembly 516 within the enclosure 504 initially comprises placing the auxiliary subassembly 516 within the pouch 514 (see step 2102 of
In the example method 2200, the secondary battery 100 is positioned 2202 within the pouch 514 defined by the enclosure 504, and the auxiliary electrode 502 is positioned 2204 within the pouch 514 such that the auxiliary electrode 502 is in contact with the secondary battery 100. A buffer process, such as the buffer or pre-lithiation processes described herein, is performed 2206 on the lithium containing secondary battery to transfer carrier ions from the auxiliary electrode 502 to the lithium containing secondary battery 100.
After the buffer process is performed 2206, the auxiliary electrode 502 is removed 2208 from the pouch 514. As described above, for example, the enclosure layers 510, 511 of the enclosure 504 may be cut or separated along separation lines 1702 (
The enclosure 504 may then be sealed (or resealed) 2210 with the secondary battery 100 positioned within the pouch 514 after the auxiliary electrode 502 is removed from the pouch 514. For example, the enclosure layers 510, 511 may be sealed 2210 along the final sealing line 1704 using any of the previously described processes for sealing the first enclosure layer 510 and the second enclosure layer 511 together. The sealed enclosure 504 may then be trimmed or cut 2212 along one or more final cut lines 1706, illustrated in
In this embodiment, the pouch 514 is shaped as a rectangular prism, and includes a planar, rectangular base 2302, a planar, rectangular cover 2304 (
As shown in
The plurality of flaps 2314 is formed during the sealing 2210 and/or trimming 2212 steps described above. More specifically, the size and shape of each flap 2314 may be set when the enclosure 504 is sealed and trimmed following removal of the auxiliary electrode 502. In the illustrated embodiment, each of the flaps 2314 is rectangular in shape, although other embodiments may have flaps shaped other than rectangular. In some embodiments, the step of trimming 2212 the enclosure 504 may include trimming the enclosure 504 such that each of the flaps 2314 has a width 2322 (
In the illustrated embodiment, the secondary battery assembly 2300 includes a first side flap 2328, a second side flap 2330, and an end flap 2332, although other embodiments may include additional or alternative flaps. The first side flap 2328 extends outward (in the X-direction as illustrated in
As shown in
After the bonding agent 2602 is applied, the first side flap 2328 is folded about the first fold line 2334 towards and into contact with the pouch first sidewall 2306 to connect the first side flap 2328 to the pouch first sidewall 2306, and the second side flap 2330 is folded about the second fold line 2336 towards and into contact with the pouch second sidewall 2308 to connect the second side flap 2330 to the pouch second sidewall 2308, as shown in
As shown in
As shown in
After the bonding agent 2802 is applied to the end flap 2332 and/or the pouch first end wall 2310, the end flap 2332 is folded about the third fold line 2338 towards and into contact with the pouch first end wall 2310 to connect the end flap 2332 to the pouch first end wall 2310, as shown in
When the end flap 2332 is folded towards and, optionally, into contact with the first end wall 2310 of the pouch 514, a portion of the first and second tabs 2702, 2704 may be folded along with the end flap 2332 because the end flap 2332 and first and second tabs 2702, 2704 are connected. As a result, an edge of each of the tabs 2702, 2704 may be oriented at an oblique angle relative to the other edges of the tabs 2702, 2704, as shown, for example, in
As shown in
After the bonding agent 3002 is applied, the first tab 2702 is folded about a fourth fold line 3102 towards and into contact with the second surface 2320 of the end flap 2332 to connect the first tab 2702 to the end flap 2332, and the second tab 2704 is folded about a fifth fold line 3104 towards and into contact with the second surface 2320 of the end flap 2332 to connect the second tab 2704 to the end flap 2332, as shown in
In some embodiments, the secondary battery assembly 2300 may be subjected to one or more compression and/or thermal processing steps to facilitate maintaining engagement between the flaps 2314 and the pouch 514. For example, the secondary battery assembly 2300 may be compressed and/or heated (simultaneously or in sequential steps) after one or more of the flaps 2314 are folded towards and, optionally, into contact with the pouch 514 to facilitate adhesion between the one or more flaps 2314 and the pouch 514, and/or to reduce or relieve internal stress or strain in the flaps 2314 (specifically within the material of the enclosure 504) resulting from deformation of the flaps 2314 during folding.
In some embodiments, for example, the first side flap 2328 is compressed against the pouch first sidewall 2306 and the second side flap 2330 is compressed against the pouch second sidewall 2308 after the first side flap 2328 is folded towards and, optionally, into contact with the pouch first sidewall 2306 and the second side flap 2330 is folded towards and, optionally, into contact with the pouch second sidewall 2308. The compressive force or pressure used to compress the first side flap 2328 against the pouch first sidewall 2306 and the second side flap 2330 against the pouch second sidewall 2308 may be any suitable force or pressure that facilitates maintaining engagement or connection between the first and second side flaps 2328, 2330 and the pouch 514. In some embodiments, the first and second side flaps 2328, 2330 are compressed against the pouch first sidewall 2306 and the pouch second sidewall 2308, respectively, by applying a compressive force across the pouch first sidewall 2306 and the pouch second sidewall 2308 equal to a pressure of at least 5 pounds per square inch (psi), at least 8 psi, at least 10 psi, at least 15 psi, at least 20 psi, at least 25 psi, at least 30 psi, at least 35 psi, between 5 psi and 50 psi, between 5 psi and 20 psi, between 10 psi and 40 psi, between 5 psi and 15 psi, or between 20 psi and 40 psi.
The first side flap 2328 and the second side flap 2330 may be compressed against the pouch 514 simultaneously or sequentially. Moreover, the secondary battery assembly 2300 may be heated prior to, during, or after the first side flap 2328 and the second side flap 2330 being compressed against the pouch 514. In one example embodiment, the first side flap 2328 is compressed against the pouch first sidewall 2306 and the second side flap 2330 is compressed against the pouch second sidewall 2308 while the secondary battery assembly 2300 is heated at a first compression temperature for a first compression time. The first compression temperature may be, for example and without limitation, in the range of 50° C. to 150° C., in the range of 70° C. to 150° C., in the range of 90° C. to 150° C., in the range of 90° C. to 140° C., in the range of 100° C. to 150° C., in the range of 90° C. to 130° C., in the range of 100° C. to 140° C., in the range of 110° C. to 150° C., in the range of 90° C. to 120° C., in the range of 100° C. to 130° C., in the range of 110° C. to 140° C., or in the range of 120° C. to 150° C. The first compression time may be, for example and without limitation, in the range of 10 seconds to 60 seconds, in the range of 10 seconds to 40 seconds, in the range of 20 seconds to 50 seconds, in the range of 30 seconds to 60 seconds, in the range of 10 seconds to 30 seconds, in the range of 15 seconds to 35 seconds, in the range of 20 seconds to 40 seconds, or in the range of 25 seconds to 45 seconds.
Additionally or alternatively, the end flap 2332, the first tab 2702, and the second tab 2704 may be compressed against the pouch first end wall 2310 after the end flap 2332 is folded towards and, optionally, into contact with the pouch first end wall 2310, and the first and second tabs 2702, 2704 are folded towards and, optionally, into contact with the end flap 2332. The compressive force or pressure used to compress the end flap 2332, the first tab 2702, and the second tab 2704 against the pouch first end wall 2310 may be any suitable force or pressure that facilitates maintaining engagement or connection between the end flap 2332 and the pouch first end wall 2310, and/or between the first and second tabs 2702, 2704 and the end flap 2332. In some embodiments, the end flap 2332 and the first and second tabs 2702, 2704 are compressed against the pouch first end wall 2310 by applying a compressive force across the pouch first end wall 2310 equal to a pressure of at least 2.5 psi, at least 3 psi, at least 4 psi, at least 5 psi, at least 10 psi, at least 15 psi, at least 20 psi, between 2.5 psi and 40 psi, between 2.5 psi and 30 psi, between 2.5 psi and 25 psi, between 3 psi and 30 psi, between 3 psi and 25 psi, between 4 psi and 40 psi, between 4 psi and 25 psi, between 5 psi and 40 psi, between 5 psi and 30 psi, between 5 psi and 25 psi, between 10 psi and 50 psi, between 10 psi and 40 psi, between 10 psi and 30 psi, between 10 psi and 25 psi, between 15 psi and 30 psi, or between 20 psi and 35 psi.
The end flap 2332, the first tab 2702, and the second tab 2704 may be compressed against the pouch first end wall 2310 simultaneously or sequentially. Moreover, the secondary battery assembly 2300 may be heated prior to, during, or after the end flap 2332, the first tab 2702, and the second tab 2704 being compressed against the pouch 514. In one example embodiment, the end flap 2332, the first tab 2702, and the second tab 2704 are compressed against the pouch first end wall 2310 while the secondary battery assembly 2300 is heated at a second compression temperature for a second compression time. The second compression temperature may be, for example and without limitation, in the range of 50° C. to 150° C., in the range of 70° C. to 150° C., in the range of 90° C. to 150° C., in the range of 90° C. to 140° C., in the range of 100° C. to 150° C., in the range of 90° C. to 130° C., in the range of 100° C. to 140° C., in the range of 110° C. to 150° C., in the range of 90° C. to 120° C., in the range of 100° C. to 130° C., in the range of 110° C. to 140° C., or in the range of 120° C. to 150° C. The second compression time may be, for example and without limitation, in the range of 10 seconds to 60 seconds, in the range of 10 seconds to 40 seconds, in the range of 20 seconds to 50 seconds, in the range of 30 seconds to 60 seconds, in the range of 10 seconds to 30 seconds, in the range of 15 seconds to 35 seconds, in the range of 20 seconds to 40 seconds, or in the range of 25 seconds to 45 seconds.
The compression and thermal processing steps described above may be performed on the secondary battery assembly 2300 using any suitable known compression fixture(s) and heating system(s). For example, a suitable compression fixture may include a pair of plates oriented parallel to one another, where at least one of the plates is fixed to a drive mechanism to move the plate towards and away from the other plate to apply a compressive load to an object positioned between the plates. The compression fixture or a portion thereof may be enclosed or positioned within a temperature-controlled environment such that the object compressed by the compression fixture may be heated at a desired temperature. Additionally, in some embodiments, the secondary battery assembly 2300 may be positioned and secured within a clamp, vice, or other compressive device prior to being subjected to the compression and/or thermal processing steps described herein. For example, the secondary battery assembly 2300 may be secured within a clamp that applies pressure in a direction orthogonal to a direction of the compressive force applied during the compression process to prevent or inhibit deformation of the secondary battery assembly 2300 in the direction orthogonal to the direction of the compressive force. In some embodiments, for example, the secondary battery assembly 2300 is placed in a clamp that applies a compressive force against the base 2302 and the cover 2304 (i.e., in the Z-direction, as illustrated in
The following embodiments are provided to illustrate various aspects of the present disclosure. The following embodiments are not intended to be limiting and therefore, the present disclosure further supports other aspects and/or embodiments not specifically provided below.
This written description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims.
This application claims priority to U.S. Provisional Patent Application No. 63/326,112, filed Mar. 31, 2022, the disclosure of which is hereby incorporated by reference in its entirety.
Number | Date | Country | |
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63326112 | Mar 2022 | US |