US20140166471A1 - Depositing lithium metal oxide on a battery substrate - Google Patents
Depositing lithium metal oxide on a battery substrate Download PDFInfo
- Publication number
- US20140166471A1 US20140166471A1 US14/089,019 US201314089019A US2014166471A1 US 20140166471 A1 US20140166471 A1 US 20140166471A1 US 201314089019 A US201314089019 A US 201314089019A US 2014166471 A1 US2014166471 A1 US 2014166471A1
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- Prior art keywords
- sputtering
- magnetron
- chamber
- substrate
- targets
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- 239000000758 substrate Substances 0.000 title claims abstract description 110
- 238000000151 deposition Methods 0.000 title claims abstract description 43
- 229910021450 lithium metal oxide Inorganic materials 0.000 title claims abstract description 13
- 238000000034 method Methods 0.000 claims abstract description 84
- 238000004544 sputter deposition Methods 0.000 claims abstract description 67
- 238000005477 sputtering target Methods 0.000 claims abstract description 36
- 229910000625 lithium cobalt oxide Inorganic materials 0.000 claims description 20
- BFZPBUKRYWOWDV-UHFFFAOYSA-N lithium;oxido(oxo)cobalt Chemical compound [Li+].[O-][Co]=O BFZPBUKRYWOWDV-UHFFFAOYSA-N 0.000 claims description 20
- 230000004907 flux Effects 0.000 claims description 10
- 239000000203 mixture Substances 0.000 claims description 5
- 230000002093 peripheral effect Effects 0.000 claims description 5
- QTHKJEYUQSLYTH-UHFFFAOYSA-N [Co]=O.[Ni].[Li] Chemical compound [Co]=O.[Ni].[Li] QTHKJEYUQSLYTH-UHFFFAOYSA-N 0.000 claims description 4
- CASZBAVUIZZLOB-UHFFFAOYSA-N lithium iron(2+) oxygen(2-) Chemical compound [O-2].[Fe+2].[Li+] CASZBAVUIZZLOB-UHFFFAOYSA-N 0.000 claims description 4
- 229910002102 lithium manganese oxide Inorganic materials 0.000 claims description 4
- VLXXBCXTUVRROQ-UHFFFAOYSA-N lithium;oxido-oxo-(oxomanganiooxy)manganese Chemical compound [Li+].[O-][Mn](=O)O[Mn]=O VLXXBCXTUVRROQ-UHFFFAOYSA-N 0.000 claims description 4
- URIIGZKXFBNRAU-UHFFFAOYSA-N lithium;oxonickel Chemical compound [Li].[Ni]=O URIIGZKXFBNRAU-UHFFFAOYSA-N 0.000 claims description 4
- 229910052723 transition metal Inorganic materials 0.000 claims description 4
- 150000003624 transition metals Chemical class 0.000 claims description 4
- 239000010408 film Substances 0.000 description 138
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- 230000008021 deposition Effects 0.000 description 32
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 24
- 239000010409 thin film Substances 0.000 description 16
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 14
- 239000001301 oxygen Substances 0.000 description 14
- 229910052760 oxygen Inorganic materials 0.000 description 14
- 238000003776 cleavage reaction Methods 0.000 description 13
- 230000007017 scission Effects 0.000 description 13
- 238000000137 annealing Methods 0.000 description 12
- 229910052786 argon Inorganic materials 0.000 description 12
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 12
- 238000004140 cleaning Methods 0.000 description 10
- 239000010445 mica Substances 0.000 description 10
- 229910052618 mica group Inorganic materials 0.000 description 10
- 239000013078 crystal Substances 0.000 description 9
- 229910032387 LiCoO2 Inorganic materials 0.000 description 8
- 239000010410 layer Substances 0.000 description 8
- 238000004519 manufacturing process Methods 0.000 description 8
- 239000003792 electrolyte Substances 0.000 description 7
- 238000010438 heat treatment Methods 0.000 description 7
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 6
- 230000007547 defect Effects 0.000 description 6
- 238000005137 deposition process Methods 0.000 description 6
- 239000000463 material Substances 0.000 description 6
- 229910052697 platinum Inorganic materials 0.000 description 6
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- 229910012914 LiCoOx Inorganic materials 0.000 description 5
- 150000002500 ions Chemical class 0.000 description 5
- 229910052751 metal Inorganic materials 0.000 description 5
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- GNTDGMZSJNCJKK-UHFFFAOYSA-N divanadium pentaoxide Chemical compound O=[V](=O)O[V](=O)=O GNTDGMZSJNCJKK-UHFFFAOYSA-N 0.000 description 4
- -1 for example Chemical class 0.000 description 4
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 3
- 238000002441 X-ray diffraction Methods 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
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- 239000000919 ceramic Substances 0.000 description 3
- 229910001882 dioxygen Inorganic materials 0.000 description 3
- 238000011065 in-situ storage Methods 0.000 description 3
- 238000001755 magnetron sputter deposition Methods 0.000 description 3
- 238000005240 physical vapour deposition Methods 0.000 description 3
- 239000011241 protective layer Substances 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- 229910012305 LiPON Inorganic materials 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 2
- 229920003182 Surlyn® Polymers 0.000 description 2
- 230000004913 activation Effects 0.000 description 2
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- 230000007613 environmental effect Effects 0.000 description 2
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 2
- 229910052737 gold Inorganic materials 0.000 description 2
- 239000010931 gold Substances 0.000 description 2
- FUJCRWPEOMXPAD-UHFFFAOYSA-N lithium oxide Chemical class [Li+].[Li+].[O-2] FUJCRWPEOMXPAD-UHFFFAOYSA-N 0.000 description 2
- 229910001947 lithium oxide Inorganic materials 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- 229910001200 Ferrotitanium Inorganic materials 0.000 description 1
- 239000002200 LIPON - lithium phosphorus oxynitride Substances 0.000 description 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- HBBGRARXTFLTSG-UHFFFAOYSA-N Lithium ion Chemical compound [Li+] HBBGRARXTFLTSG-UHFFFAOYSA-N 0.000 description 1
- 229910014892 LixPOyNz Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910003092 TiS2 Inorganic materials 0.000 description 1
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- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
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- 229910001416 lithium ion Inorganic materials 0.000 description 1
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- 230000014759 maintenance of location Effects 0.000 description 1
- 150000002736 metal compounds Chemical class 0.000 description 1
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- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 230000037361 pathway Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
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- 238000001552 radio frequency sputter deposition Methods 0.000 description 1
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- 239000000377 silicon dioxide Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
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Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M4/00—Electrodes
- H01M4/02—Electrodes composed of, or comprising, active material
- H01M4/04—Processes of manufacture in general
- H01M4/0402—Methods of deposition of the material
- H01M4/0421—Methods of deposition of the material involving vapour deposition
- H01M4/0423—Physical vapour deposition
- H01M4/0426—Sputtering
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/08—Oxides
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
- C23C14/35—Sputtering by application of a magnetic field, e.g. magnetron sputtering
- C23C14/352—Sputtering by application of a magnetic field, e.g. magnetron sputtering using more than one target
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/05—Accumulators with non-aqueous electrolyte
- H01M10/058—Construction or manufacture
- H01M10/0585—Construction or manufacture of accumulators having only flat construction elements, i.e. flat positive electrodes, flat negative electrodes and flat separators
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M4/00—Electrodes
- H01M4/02—Electrodes composed of, or comprising, active material
- H01M4/13—Electrodes for accumulators with non-aqueous electrolyte, e.g. for lithium-accumulators; Processes of manufacture thereof
- H01M4/139—Processes of manufacture
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M4/00—Electrodes
- H01M4/02—Electrodes composed of, or comprising, active material
- H01M4/13—Electrodes for accumulators with non-aqueous electrolyte, e.g. for lithium-accumulators; Processes of manufacture thereof
- H01M4/139—Processes of manufacture
- H01M4/1391—Processes of manufacture of electrodes based on mixed oxides or hydroxides, or on mixtures of oxides or hydroxides, e.g. LiCoOx
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Definitions
- a thin film battery typically comprises a substrate that supports a stack of thin films that can include one or more of a current collector, cathode, anode and electrolyte, the thin films typically having a thickness of less than 100 microns.
- the thin films can be formed on the substrate by conventional fabrication processes, such as for example, physical or chemical vapor deposition (PVD or CVD), oxidation, nitridation, electron beam evaporation, and electroplating processes.
- a lithium ion, thin film battery typically includes a cathode of a lithium-based material such as LiCoO x , and in these batteries, increasing the thickness of this cathode film increases the energy density of the battery.
- the thicker cathode film provides greater charge retention and faster charging and discharging rates. For example, specific energy levels of at least 250 Whr/L can be achieved using a cathode film having a thickness of 5 microns or higher, as for example is taught in commonly assigned U.S. patent application Ser. No. 11/007,362 entitled “THIN FILM BATTERY AND METHOD OF MANUFACTURE” which is incorporated by reference herein, and in its entirety.
- the cathode film can be deposited as an amorphous or microcrystalline film in a single pass deposition process, and thereafter, crystallized by heating the film; or deposited in a sequence of thin films to form a thicker cathode comprising a stack of films.
- conventional sputtering processes have several limitations, which include relatively slow cathode film deposition rates that make it economically difficult to manufacture thick cathode films.
- conventional radio frequency magnetron sputtering processes often result in deposition rates of around 0.2 microns per hour. Increasing the sputter deposition rates can result in plasma arcing which affects the quality of deposited films.
- These processes also require an impedance matching network to match the impedance of magnetron and power supply to increase plasma stability and efficiency. However, it is also often difficult to identify the correct impedance matching parameters.
- a method of depositing lithium metal oxide on a battery substrate in a sputtering chamber comprising (i) a substrate support, (ii) first and second sputtering targets each comprising a sputtering surface of lithium metal oxide and having a backside surface, and (iii) a first electrode about the backside surface of the first sputtering target and a second electrode about the backside surface of the second sputtering target.
- one or more substrates is placed on the substrate support, and sputtering gas is provided at a pressure in the sputtering chamber.
- the sputtering gas is energized by applying an alternating voltage of AC power to the first and second electrodes so that each electrode is alternately either an anode or a cathode, the alternating voltage being applied at a frequency of between about 10 and about 100 kHz.
- a time varying magnetic field is applied about each of the sputtering surfaces of the first and second targets.
- the deposition method uses first and second sputtering targets that each comprise lithium metal oxide comprising lithium cobalt oxide, lithium nickel oxide, lithium manganese oxide, lithium iron oxide, lithium cobalt nickel oxide, or a mixtures of transition metals.
- first and second sputtering targets can each consist essentially of lithium cobalt oxide.
- each magnetron comprises a first magnet having a first magnetic flux or first magnetic field orientation, and a second magnet having a second magnetic flux or second magnetic field orientation.
- FIG. 1A is a sectional side view of an embodiment of a thin film battery comprising a battery cell on a substrate;
- FIG. 1B is a sectional side view of another embodiment of a battery comprising a first battery cell on a first surface of a substrate and a second battery cell on a second surface;
- FIG. 2 is a top plan view of a thin film battery showing a plurality of battery cells on a single surface of the substrate;
- FIG. 3A is a top plan schematic view of an embodiment of a twin magnetron deposition chamber
- FIG. 3B is a sectional side schematic view of the twin magnetron deposition chamber of FIG. 3A ;
- FIGS. 4A and 4B are plots of the X-ray diffraction pattern of a deposited lithium cobalt oxide film before and after annealing, respectively.
- FIG. 5 is a plot of the energy capacity versus current for an embodiment of a thin film battery.
- FIG. 1A An embodiment of a thin film battery 20 comprising a single battery cell 22 enclosed on one side by the substrate 24 , is illustrated in FIG. 1A .
- the battery 20 can also have single or multiple battery cells 22 a,b on opposing surfaces of a substrate 24 , as illustrated for example in FIG. 1B .
- FIG. 2 A further embodiment of a battery 20 comprising a plurality of battery cells 22 a - c on a planar surface 26 of a substrate 24 is illustrated in FIG. 2 .
- the battery cell 22 comprises a plurality of battery component films 30 .
- the battery component films 30 are typically formed on an adhesion layer 32 but can also be formed directly on the substrate 24 .
- the battery component films 30 cooperate to form a battery capable of receiving, storing, and discharging electrical energy.
- the films 30 can be employed in a number of different arrangements, shapes, and sizes.
- the battery component films 30 includes at least a pair of electrode films on either side of an electrolyte film 40 .
- the electrode films can include one or more of a cathode current collector film 34 , a cathode film 38 an anode film 42 , and an anode current collector film 44 , which are all inter-replaceable.
- the battery 20 can include (i) a pair of cathode and anode films or a pair of current collector films, (ii) both the anode/cathode films and the current collector films, or (iii) various combinations of these films, for example, a cathode film and an anode and anode current collector film but not a cathode current collector film, and so on.
- the exemplary versions of the battery 20 illustrated herein are provided to demonstrate features of the battery and to illustrate their processes of fabrication; however, it should be understood that these exemplary battery structures should not be used to limit the scope of the invention, and alternative battery structures as would be apparent to those of ordinary skill in the art are within the scope of the present invention.
- the battery 20 can include a first battery cell 22 a on a first planar surface 26 of the substrate 24 , and a second battery cell 22 b on a second planar surface 27 of the same substrate 24 .
- Each battery cell 22 a,b comprises a plurality of battery component films 30 a,b that include one or more adhesion films 32 a,b ; first or cathode current collector films 34 a,b ; cathode films 38 a,b ; electrolyte films 40 a,b ; anode films 42 a,b ; and second or anode current collector films 44 a,b .
- This version of the battery 20 with two opposing cells 22 a,b can be formed using the same processes used to form the battery 20 with the single cell 22 ( FIG. 1A ), by flipping over the substrate 24 to form the battery film components 30 b of the second battery cell 22 b , during or after processing of the first battery cell 30 a .
- the battery film components 30 b of the second battery cell 22 b can be formed simultaneously with the battery film components 30 a of cell 22 a , using chambers having multiple process zones, an exemplary version of which is described in copending U.S. patent application Ser. No. 11/681,754, filed Mar. 2, 2007, which is incorporated herein by reference and in it's entirety.
- the battery component films 30 are formed on a battery substrate 24 to fabricate a battery 20 in several fabrication steps, which can be performed separately or as a combination of steps.
- a suitable substrate 24 is selected, the substrate 24 being a dielectric having sufficient mechanical strength to support battery component films 30 , and typically having a surface suitable for the deposition of thin films.
- Suitable substrates 24 can be made from, for example, ceramics such as aluminum oxide or silicon dioxide; metals such as titanium and stainless steel; semiconductors such as silicon; or even polymers.
- One desirable substrate comprises a crystalline sheet formed by cleaving the planes of a cleavable crystalline structure.
- the cleavable crystalline structure splits along definite planes to create flat surfaces, and can include (i) basal cleavage crystals having cleavage planes parallel to the base of a crystal or to the plane of the lateral axes; (ii) cubic cleavage crystals having cleavage planes parallel to the faces of a cube, (iii) diagonal cleavage crystals which has cleavage planes parallel to a diagonal plane; (iv) lateral cleavage crystals which have cleavage planes parallel to the lateral planes; (v) octahedral, dodecahedral, or rhombohedral cleavage crystals in which cleavage occurs parallel to the faces of an octahedron, dodecahedron, or rhombohedron (respectively); and (vi) prismatic cleavage crystals in which cleavage occurs parallel to a vertical prism.
- the crystalline cleaving structure can be, for example, mica or graphite.
- Mica can be split into thin crystal sheets having thicknesses of less than about 100 microns or even less than about 25 microns, as described in a U.S. Pat. No. 6,632,563 “THIN FILM BATTERY AND METHOD OF MANUFACTURE”, filed on Sep. 9, 2000, which is incorporated by reference herein and in its entirety.
- an array of substrates 24 that each comprise a mica sheet is used in the fabrication process.
- Each mica sheet can be a rectangle which is sized, for example, having dimensions from about 10 mm to about 200 mm.
- the substrate 24 of mica or other materials can optionally be annealed to temperatures sufficiently high to clean the deposition surface, such as the cleavage plane surface, by burning-off contaminants and impurities, such as organic materials, water, dust, and other materials formed or deposited on the planar surfaces 26 , 27 of the substrate 24 ; or even heated to temperatures high enough to remove any water of crystallization present within the substrate.
- the annealing temperatures can be from about 150 to about 600° C., even at least about 400° C., or even at least about 540° C.
- the annealing process can be conducted in an oxygen-containing gas, such as oxygen or air, or other gas environments, for about 10 to about 120 minutes, for example, about 60 minutes.
- the cleaning process can also be conducted in an oxygen plasma containing cleaning step. Suitable annealing and other cleaning processes are described, for example, in U.S. patent application Ser. No. 11/681,754 which is incorporated by reference herein and in its entirety.
- a plurality of battery component films 30 are deposited on the surfaces 26 , 27 of the substrate 24 to form battery cells 22 that can generate or store electrical charge.
- the component films 30 are typically formed using a PVD sputter deposition process, under controlled process conditions and in one or more sputtering chambers.
- one or more battery component films 30 are deposited onto the battery substrate 24 using a sputtering chamber 100 , as shown, for example, in FIGS. 3A and 3B .
- the chamber 100 comprises a circular sidewall 108 , a chamber ceiling 110 and a lower wall 112 which surrounds and encloses a process zone 114 .
- the chamber sidewall 108 can be electrically isolated from the chamber ceiling 110 and the lower wall 112 and can even be electrically grounded.
- the chamber walls are typically composed of stainless steel, steel or aluminum.
- the sputtering chamber 100 is separated from a loading chamber by a slit valve 115 for passage and transport of substrates 24 into and out of the chamber 100 .
- the slit valve 115 can lead to a dry box 117 for loading the substrates 24 .
- Substrates 24 are placed onto a substrate holding fixture which is then carried into the sputtering chamber by a conveyer, the substrate holding fixture is electrically isolated from the chamber walls.
- One or more substrate supports 104 , or 104 a,b are positioned about the peripheral edge of the chamber 100 for receiving substrates 24 .
- the substrate supports 104 or 104 a,b are oriented to face inward and towards a radially inward region 116 of the chamber 100 .
- the substrate supports 104 can be moved during sputter processing, thereby allowing the substrates 24 to be rotated about the periphery of the sputtering chamber 100 or even around a circumference that encloses the plurality of sputtering targets 102 a - d . Rotation of the substrates 24 during processing increases the deposition uniformity.
- the substrate support 104 is electrically isolated from the chamber sidewall 108 and sputtering targets 102 .
- the substrate supports 104 can be biased at a negative voltage relative to the plasma, or even relative to the time averaged potential of the cathodes.
- the negatively biased substrate support 104 serves to attract the positively charged ions and sputtered material from the plasma zone 114 .
- the substrate supports 104 are biased by a biasing power supply.
- the biasing power supply provides a pulsed DC voltage bias of from about ⁇ 5 to about ⁇ 200 V or even about ⁇ 40 V between the substrate supports 104 and the radially inward region 116 of the chamber 100 .
- the pulsed biasing voltage has a duty cycle of from about 10% to about 90%, or even about 30%.
- the substrate support 104 can also include a heater and heating control circuitry to maintain the substrate 24 at an appropriate processing temperature. In one version the substrate 24 is maintained at a temperature of from about 50 to about 200° C. during processing.
- a plurality of sputtering targets 102 are mounted in the radially inward region 116 of the chamber 100 .
- the sputtering targets 102 can comprise lithium metal oxide, such as for example, lithium cobalt oxide, lithium nickel oxide, lithium manganese oxide, lithium iron oxide, or even lithium oxides comprising mixtures of transition metals such as for example, lithium cobalt nickel oxide.
- the sputtered target material deposits onto a plurality of battery substrates 24 in the chamber.
- the targets 102 comprise an even number of targets such as for example two, four, six or even ten or more targets. In one version, the number of targets 102 and the size of the chamber 100 is scaleable to accommodate a larger batch of substrates 24 for processing.
- the sputtering targets 102 can be rectangular or cylindrical.
- the cylindrically shaped targets are mounted to cylindrically shaped magnetrons 106 .
- These magnetrons 106 can be configured to self-rotate during the deposition process, exposing fresh sputtering surface and reducing localized heating of the attached targets 102 , thereby increasing the target lifespan, in on-time plasma hours, by from 15% to 70%.
- One or more magnetrons 106 are provided in the radially inward region 116 of the chamber 100 .
- the magnetrons 106 are capable of generating a time varying magnetic field at a particular location in the chamber 100 .
- Each magnetron 106 comprises a set of rotatable magnets or electromagnets.
- the magnetron 106 can be a single structure or a set of structures.
- the magnetron 106 includes a first rotatable magnet assembly 146 a which is rotated behind a backside surface of a first sputtering target 102 a , and a second rotatable magnet assembly 146 b which is rotated behind the backside surface of a second sputtering target 102 b.
- the rotatable magnet assembly comprises a magnet that is capable of being rotated about a central axis.
- a first magnet 148 having a first magnetic flux or magnetic field orientation, and one or more peripheral magnets 150 having a second magnetic flux or magnetic field orientation are mounted to a support plate 152 .
- the support plate 152 is rotated by an axle 154 that is powered by a motor (not shown).
- the ratio of the first magnetic flux to the second magnetic flux is at least about 1:2, for example, from about 1:3 to about 1:8, or even about 1:5. This allows the magnetic field from the peripheral magnets 150 to extend deeper into the chamber 100 .
- the second magnetic field orientation can be generated by positioning the peripheral magnets 150 so that their polarity direction is opposite to the polarity direction of the central magnets 150 .
- the first and second rotatable magnet assemblies 146 a,b are rotated at a rotational frequency of between about 0.005 and about 0.1 Hz, whereby a time varying magnetic field is provided about the surface of the first and second targets 102 .
- the magnetron 106 can also be connected to an AC power source 118 that provides an alternating voltage to excite the sputtering gas within the chamber 100 .
- the power source 118 serves to bias the twin magnetrons 106 a,b relative to each other.
- the first magnetron 106 a is on a negative potential relative to the second magnetron 106 b
- the first magnetron 106 a acts as the sputtering cathode
- the second magnetron 106 b acts as an anode.
- the magnetrons 106 are powered with an AC voltage that is between 200V and 1200V and has a power of between 1 kW and 20 kW.
- the magnetrons 106 can be mounted to the chamber ceiling 110 or lower wall 112 .
- a sputtering target is attached to each magnetron 106 .
- the magnetron 106 transmits the voltage to the attached sputtering target 102 , and the sputtering gas between the AC biased targets 102 is excited.
- the chamber 100 comprises twin magnetrons which are each connected to a target 102 .
- twin magnetrons 106 a,b are operated by a voltage or current maintained at a mid-frequency level, which is a frequency of from about 10 to about 100 kHz. It has been found that the mid-frequency sputtering process desirably reduces or eliminates co-excitation modes that would otherwise occur between the twin magnetrons 106 . Absence of the co-excitation mode results in reduced arcing of the sputtering targets 102 , thereby increasing the lifespan of the targets 102 , and also improving the quality of the deposited films. Arcing is often initiated by electrical breakdown of the insulating layer on the magnetron cathode.
- a mid-frequency power from a mid-frequency AC power source 118 reduces charging up of the insulating layer and resultant plasma process instabilities.
- targets 102 comprising lithium cobalt oxide
- sputtered films can be produced in this manner without arcing over almost the entire lifetime of the target 102 .
- higher power levels can be applied to the sputtering targets 102 .
- the deposition process is more continuous and results in high quality films and higher deposition throughput.
- the mid-frequency dual magnetron process provides a deposition rate of from about 0.2 to about 4 microns/hour.
- the chamber 100 also has a plurality of cathodes 120 , as shown for example in FIGS. 3A and 3B .
- Each cathode 120 is formed by binding a target 102 to a magnetron 106 , which provides an unbalanced magnetic field about the surface of the target 102 and results in a more continuous bombardment of the target during sputtering.
- the chamber 100 can further include a plurality of ion sources 122 that are capable of supplying ionized gas for in-situ active cleaning and activation of the substrates 24 .
- the ion sources 122 are located adjacent to the targets 102 .
- the ion sources 122 can be located within a radially inward region 116 of the chamber 100 , or even between the targets 102 .
- a cleaning gas is provided to the chamber 100 such as for example, argon and oxygen.
- a voltage is supplied between the radially inward region of the chamber 116 and the substrate supports 104 , such that the cleaning gas ions are drawn towards and bombard the surface of the substrate 24 .
- Typical ion-source cleaning processes are erosive to, and can decrease the lifespan of, the sputtering target 102 .
- a fixture (not shown) covering half of the surface of a target 102 can be rotated to first and second orientations within the chamber 100 . In the first orientation, the exposed part of the targets 102 face the substrates 24 for film deposition and in the second orientation, the exposed part of the targets 102 faces the center for in-situ active substrate cleaning, thereby decreasing target contamination.
- the chamber 100 is connected to a gas supply 123 , gas distributor 126 and gas exhaust 130 , which supply and control the pressure and concentration of process gas within the chamber 100 .
- the process gas mixture is controlled by first evacuating the chamber 100 and then introducing controlled amounts of process gas into the chamber 100 .
- the chamber 100 is evacuated to a pressure of less than about 5 ⁇ 10 ⁇ 5 Torr or even less than about 2 ⁇ 10 ⁇ 5 Torr prior to introduction of the sputtering gas.
- Sputtering process gas is introduced into the chamber and maintained at a pressure of from about 1.1 to about 15 mTorr.
- the sputtering gas comprises argon and oxygen.
- the argon provides stable plasma and oxygen can prevent oxygen loss in the targets or the deposited films during the process.
- the sputtering argon gas is maintained in the chamber 100 at a pressure of from about 1 to about 10 mTorr.
- the sputtering oxygen gas is maintained in the chamber 100 at a pressure of from about 0.1 to about 5 mTorr.
- the twin magnetrons are connected to a power source 118 , such as for example, an AC power supply 134 .
- the AC power supply 134 and provides an alternating voltage having a wave form that is approximately sinusoidal and that has a frequency in the mid-frequency range of between about 10 and about 100 kHz, or even about 40 kHz.
- the power supply 134 energizes the process gas by applying a voltage bias across the first and second magnetrons 106 a,b at a frequency of from about 10 to about 100 kHz, or even from about 20 to about 80 kHz.
- the voltage bias can also be applied at a power level of at least about 1 kW, or even at a power level of from about 3 kW to about 20 kW.
- the power supply 134 supplies a power density to the surface of the targets 102 that is at least 0.1 W/cm 2 or even between about 0.1 W/cm 2 and about 20 W/cm 2 .
- the chamber 100 is controlled by a controller 119 that comprises program code having instruction sets to operate components of the chamber 100 to process substrates 24 in the chamber 100 .
- the controller 119 can comprise a substrate positioning instruction set to operate a substrate transport mechanism to position a substrate 24 in the chamber 100 ; a gas flow control instruction set to operate the flow control valves 125 to set a flow of gas to the chamber 100 ; a gas pressure control instruction set to operate the exhaust 130 to maintain a pressure in the chamber 100 ; power supply control instruction sets such as a gas energizer control instruction set to operate the electrode power supply 134 to set a gas energizing power level and a DC power supply control instruction set to operate a DC power supply 121 to provide a DC voltage bias to the substrate support 104 ; a temperature control instruction set to control temperatures in the chamber 100 ; and a process monitoring instruction set to monitor the process in the chamber 100 , for example by monitoring temperatures or pressure via one or more sensors 137 that are within the chamber.
- the mid-frequency twin magnetron sputtering process is particularly efficient at deposition of lithium cobalt oxide films and can provide deposition rates of between 0.2 and 4 microns per hour.
- the sputtering rate is sensitive to adjustments in power, processing gas pressure and DC bias voltage.
- two or four LiCoO 2 targets are installed in the chamber.
- the substrate is placed in the chamber which is pumped down to below 5 ⁇ 10 ⁇ 5 Torr.
- a suitable substrate 24 comprises a 35 mm ⁇ 62 mm sheet of mica.
- Process gas such as for example, argon and oxygen, are introduced into the chamber 100 to serve as the sputtering gas.
- the sputtering gas comprising argon is maintained in the chamber 100 at a pressure from about 1 to about 10 mTorr and in one version about 2 mTorr, and oxygen is maintained at the pressure of from 0.1 to 5 mTorr and in one version about 0.75 m Torr.
- Sputtering is performed by applying an 0.1 to 20 W/cm 2 power density to each target 102 and a pulsed DC voltage bias of between ⁇ 5 and ⁇ 100 V or even about ⁇ 40 V between the substrate supports 104 and the radially inward region 116 of the chamber 100 .
- the duty cycle is between 10% and 90%, even at 30%.
- the substrate 24 is maintained at a temperature of from about 50 to about 200° C. during processing. In one version the voltage bias is applied for a sufficient time to deposit a lithium cobalt oxide film having a thickness of from about 0.25 to about 0.75 of the total thickness of a stack of films formed on the substrate 24 .
- the deposition rates obtained from the mid-frequency twin magnetron process were found to be higher than the deposition rates obtained by conventional sputtering processes, as illustrated by the following examples:
- LiCoO 2 targets were installed in the chamber 100 a mica substrate was placed in the chamber onto a substrate support 104 in the chamber 100 .
- the chamber 100 was pumped down to 2 ⁇ 10 ⁇ 5 Torr prior to introduction of the sputtering gas.
- Sputtering gas comprising argon and oxygen were introduced into the chamber 100 .
- the argon gas was maintained in the chamber 100 at a pressure of about 8.2 mTorr and the oxygen gas was maintained in the chamber 100 at a pressure of about 0.75 mTorr.
- Sputtering was performed by applying an oscillating voltage bias between the targets, the oscillation having a frequency of about 40 kHz.
- the power applied to each pair of targets was about 3 kW, and with a density of about 3.5 W/cm 2 .
- a pulsed DC voltage bias of about ⁇ 40 V was applied between the substrate support 104 and the radially inward region 116 of the chamber 100 with a duty cycle of about 30%.
- the substrate 24 was maintained at a temperature of about 120° C. during processing.
- the as-deposited lithium cobalt oxide film had a thickness of 3.5 microns after 5 hours deposition.
- the deposition rate was found to be about 0.7 microns per hour.
- the volume deposition rate per kilowatt hour was about 0.050 cm 3 /kW ⁇ hr.
- a single LiCoO 2 target was installed in the chamber and a substrate was placed onto a substrate support in the chamber.
- the chamber was pumped down to 1 ⁇ 10 ⁇ 5 Torr prior to introducing the sputtering gas.
- a process gas comprising argon and oxygen were introduced into the chamber.
- the argon gas was maintained in the chamber at a pressure of about 8.2 mTorr and the oxygen gas was maintained in the chamber at a pressure of about 0.75 mTorr.
- Sputtering was performed by applying an oscillating voltage bias to the target, with a frequency of about 13.5 MHz.
- a power density of 1.8 W/cm 2 was thereby applied to the target.
- the substrate 24 was maintained at a temperature of about 120° C. during processing.
- the as-deposited lithium cobalt oxide film had a thickness of 2 microns after 5 hours deposition.
- the deposition rate of the conventional RF system was found to be about 0.4 microns/hr.
- the volume deposition rate per kilowatt hour was about 0.016 cm 3 /kW ⁇ hr.
- the RF deposition process was limited in the amount of power that could be applied to the target because the system was prone to arcing at higher power densities.
- the volume deposition rate per kilowatt hour of the dual-magnetron mid-frequency process was found to be 3.1 times higher than the volume deposition rate per kilowatt hour of the RF process.
- the deposited film can be annealed to reduce or even eliminate point defects in the crystal lattice by heating the substrate 24 to a temperature that is sufficient for annealing for example, to a temperature of from about 200 to about 500° C.
- the substrate 24 can be annealed in-situ by direct heating from a temperature controlled substrate support 104 or by radiation heating from an infrared radiation source (not shown). In another embodiment, the substrate 24 is removed and annealed in a separate chamber or even outside the chamber environment.
- LiCoO x films deposited using a mid-frequency, dual magnetron process were found to anneal sufficiently well at a temperature of only about 400° C., as compared to a previous anneal temperature of about 540° C. for the conventionally deposited film. It is believed that this reduction in the temperature of annealing is because the as-deposited film contains fewer lattice defects. The reduction in lattice defects may be caused by a higher plasma density during the mid-frequency twin-magnetron deposition process, which may break down the sputtered material into smaller pieces.
- a LiCoO x film fabricated according to the present method and without an additional annealing step comprises LiCoO 2 which is crystalline with a strong (012) preferred orientation and with a smaller amount of (003) oriented grains.
- FIG. 4A shows a typical x-ray two theta diffraction pattern 138 of the as-deposited LiCoO 2 film.
- the large peak 140 located at a scattering angle of about 39°, and the smaller peak 142 , located at a scattering angle of about 19°, show that the film is highly crystalline and with a (012) and (003) preferred orientation.
- the substrate was slightly tilted when taking x-ray diffraction in order to suppress the diffraction peaks from an underlying mica substrate to better reveal the crystalline properties of the LiCoO 2 film. It is believed that the crystalline material was deposited due to a combination of plasma heating, oxygen activation and plasma enhanced nucleation and growth processes. The as deposited crystalline material was a good cathode material.
- the film formed on the substrate may be annealed at 150 to 600° C. to further improve the quality of the cathode film.
- An x-ray diffraction pattern 136 of crystalline LiCoO 2 film after annealing at 400° C. for 10 hours is shown in FIG. 4B .
- the larger intensity peak 148 located at a scattering angle of about 37.5° shows a strong (101) preferred orientation and the smaller intensity peak 150 , located at a scattering angle of about 40° shows a small amount of (012) oriented grains.
- the annealing step was found to increase the battery capacity by 10 to 20%, increase the charge and discharge current by more than 50%, and improve the resistance to moisture. It is believed that these attributes arise from the elimination of point defects and the reduction of electrical contact resistances in the cathode material.
- the area of the battery is 2.9 cm 2 .
- the mica substrate is 20 microns thick, and overall thickness of the battery is around 50 microns.
- the battery is sealed with Surlyn (epoxy) for temporary protection against the oxidizing environment.
- FIG. 5 shows the discharge curves of four test batteries, each comprising a LiCoO x film deposited by the method described above (with 400° C. annealing). The curves indicate that the higher the discharge current, the lower the capacity, which is consistent with previous data obtained from LiCoO x film batteries formed using an RF deposition process.
- This Surlyn sealed battery has an energy density of around 62.4 wh/l.
- the above methods or other deposition methods can be used to deposit one or more of the component films 30 , which in one embodiment include an adhesion film 32 .
- the adhesion film 32 is deposited on the planar surface 26 of the substrate 24 to improve adhesion of overlying battery component films 30 ( FIG. 1A ).
- the adhesion film 32 can comprise a metal or metal compound, such as for example, aluminum, cobalt, titanium, other metals, or their alloys or compounds thereof; or a ceramic oxide such as, for example, lithium cobalt oxide.
- Exemplary process conditions for deposition of a titanium adhesion film 32 comprise: argon maintained at a pressure of 2 mTorr; DC (direct current) sputtering plasma at a power level of 1 kW, a deposition time of 30 seconds, a titanium target size of 5 ⁇ 20 inches, and a target-to-substrate distance of 10 cm.
- argon maintained at a pressure of 2 mTorr
- the adhesion film 32 can be deposited on the substrate 24 not only to cover the area under the subsequently deposited battery cells 22 a - c and their battery component films 30 but also the area 36 extending beyond the battery component films 30 , as described in aforementioned U.S. patent application Ser. No. 11/681,754.
- the adhesion film 32 is typically deposited in a thickness of from about 100 to about 1500 angstroms.
- a cathode current collector film 34 is formed on the adhesion film 32 to collect the electrons during charge and discharge process.
- the cathode current collector film 34 typically comprises a conductor such as, for example, aluminum, platinum, silver or gold or even the same metal as the adhesion film 32 in a thickness that is sufficient to provide the desired electrical conductivity.
- the first current collector film 34 typically has a thickness that is from about 0.05 microns to about 2 microns.
- the cathode current collector film 34 a - c can be formed as a pattern of features 68 a - c , as illustrated in FIG. 2 , that each comprise a spaced apart discontinuous region that covers a small region of the adhesion film 32 .
- the features 68 a - c are over the covered regions 71 a - c of the adhesion film 32 , and adjacent to the features 68 a - c are exposed regions 70 a - c of the adhesion film 32 .
- a patterned mechanical mask is placed on top of the substrate 24 , and a first current collector film 34 of platinum is deposited by DC magnetron sputtering to form the features 68 a - c between the patterned mask regions.
- Exemplary process conditions for argon sputter deposition of a platinum cathode current collector film 34 a - c comprise a gas pressure of 5 mTorr to form a DC plasma at a power level of 40 Watts for 10 minutes.
- the adhesion film with its covered regions 71 a - c below the patterned features 68 a - c and exposed surface regions 70 a - d is then exposed to an oxygen-containing environment and heated to temperatures of from about 200° C. to about 600° C., for example, about 400° C., for about an hour, to oxidize the exposed regions 70 a - d of titanium that surround the deposited platinum features but not the titanium regions covered and protected by the platinum features.
- the resultant structure advantageously, includes not only the non-exposed covered regions 71 a - c of adhesion film 32 below the features 68 a - c of the current collector film 38 , but also oxygen-exposed or oxidized regions 70 a - d which form non-conducting regions that electrically separate the plurality of battery cells 22 a - c formed on the same substrate 24 .
- a cathode film 38 comprising an electroactive material is then formed over the current collector film 34 .
- the cathode film 38 is composed of lithium metal oxide, such as for example, lithium cobalt oxide, lithium nickel oxide, lithium manganese oxide, lithium iron oxide, or even lithium oxides comprising mixtures of transition metals such as for example, lithium cobalt nickel oxide.
- Other types of cathode films 38 that may be used comprise amorphous vanadium pentoxide, crystalline V 2 O 5 or TiS 2 .
- the cathode film 38 comprises crystalline lithium cobalt oxide, which in one version, has the stoichiometric formula of LiCoO 2 .
- the cathode film 38 can be fabricated in a single continuous deposition step or using a multiple sequential deposition and stress reducing annealing step that is performed at a temperature of between about 150 and 600° C.
- the cathode film 38 or cathode film stack has a thickness of at least about 5 microns, or even at least about 10 microns.
- the cathode film 38 is deposited using a twin-magnetron, mid-frequency sputtering process, as described above.
- the twin-magnetron mid-frequency process is particularly well suited for deposition of the cathode film 38 because of it's comparatively high sputtering rates for lithium metal oxides.
- the cathode film 38 can also be annealed in a defect reducing step to temperatures of from about 150 to about 700° C., for example, by about 400° C., to further improve the quality of the cathode film 38 by reducing the amount of defects.
- the electrolyte film 40 is formed over the cathode film 38 .
- the electrolyte film 40 can be, for example, an amorphous lithium phosphorus oxynitride film, also known as a LiPON film.
- the LiPON has the stoichiometric form Li x PO y N z in an x:y:z ratio of about 2.9:3.3:0.46.
- the electrolyte film 40 has a thickness of from about 0.1 micron to about 5 microns. This thickness is suitably large to provide sufficiently high ionic conductivity and suitably small to reduce ionic pathways to minimize electrical resistance and reduce stress.
- the anode film 42 can be the same material as the cathode film 38 , as already described.
- a suitable thickness is from about 0.1 micron to about 20 microns.
- anode film 42 is made from lithium which is also sufficiently conductive to also serve as the anode current collector film, and in this version the anode film 42 and anode current collector film 44 are the same.
- the anode current collector film 44 is formed on the anode film 42 , and comprises the same material as the cathode current collector film 34 to provide a conducting surface from which electrons may be dissipated or collected from the anode film 42 .
- the anode current collector film 44 comprises a non-reactive metal such as silver, gold, platinum, in a thicknesses of from about 0.05 microns to about 5 microns.
- the protective layer comprises a plurality of polymer and ceramic layers that are superimposed on each other.
- a portion of the cathode current collector film 34 or anode current collector film 44 that extends out from under a battery cell 22 forms a contact portion that is used to connect the battery cell 22 or the battery 20 to the external environment. This contact portion is coated with an electrically conducting barrier layer.
- the layers can protect the battery cell 22 during pulsed laser cutting of the individual battery cells from an array of cells formed on a larger mica substrate.
- the electrically conducting barrier layer is formed in a thickness sufficiently large to prevent the pulsed laser beam from penetrating therethrough.
- the thin film battery 20 can also be fabricated to provide a plurality of battery cells 22 a - c on a single substrate 24 .
- the battery cells 22 a - c can be arranged horizontally across a single substrate surface 26 or fabricated on the front surface 26 and backside surface 27 of a battery substrate 24 to substantially increase the energy density and capacity of the battery cell 22 .
- Suitable battery configurations, protective layers, and packaging, are described in for example, U.S. patent application Ser. No. 11/090,408, filed on Mar. 25, 2005, entitled “THIN FILM BATTERY WITH PROTECTIVE PACKAGING” by Krasnov et al., which is incorporated by reference herein and in its entirety.
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Abstract
A method of depositing lithium metal oxide on a battery substrate in a sputtering chamber comprising a substrate support, first and second sputtering targets each comprising lithium metal oxide, and first and second electrodes about the backside surfaces of the first and second sputtering targets respectively. In the method, a substrate is placed on the substrate support, sputtering gas maintained at a pressure and energized by applying an alternating voltage of AC power to the first and second electrodes so that each electrode is alternately either an anode or a cathode. The alternating voltage can be applied within a frequency range while also applying a time varying magnetic field about each of the surfaces of the first and second targets.
Description
- The present application is a continuation of U.S. patent application Ser. No. 11/849,959, filed on Sep. 4, 2007, which is incorporated herein by reference in its entirety.
- Thin film batteries are used to supply energy in applications requiring a small size, high specific energy or density, or resistance to environmental degradation. Common applications include, for example, portable electronics, medical devices, and outer space systems. A thin film battery typically comprises a substrate that supports a stack of thin films that can include one or more of a current collector, cathode, anode and electrolyte, the thin films typically having a thickness of less than 100 microns. The thin films can be formed on the substrate by conventional fabrication processes, such as for example, physical or chemical vapor deposition (PVD or CVD), oxidation, nitridation, electron beam evaporation, and electroplating processes.
- A lithium ion, thin film battery typically includes a cathode of a lithium-based material such as LiCoOx, and in these batteries, increasing the thickness of this cathode film increases the energy density of the battery. The thicker cathode film provides greater charge retention and faster charging and discharging rates. For example, specific energy levels of at least 250 Whr/L can be achieved using a cathode film having a thickness of 5 microns or higher, as for example is taught in commonly assigned U.S. patent application Ser. No. 11/007,362 entitled “THIN FILM BATTERY AND METHOD OF MANUFACTURE” which is incorporated by reference herein, and in its entirety. The cathode film can be deposited as an amorphous or microcrystalline film in a single pass deposition process, and thereafter, crystallized by heating the film; or deposited in a sequence of thin films to form a thicker cathode comprising a stack of films.
- However, conventional sputtering processes have several limitations, which include relatively slow cathode film deposition rates that make it economically difficult to manufacture thick cathode films. For example, conventional radio frequency magnetron sputtering processes often result in deposition rates of around 0.2 microns per hour. Increasing the sputter deposition rates can result in plasma arcing which affects the quality of deposited films. These processes also require an impedance matching network to match the impedance of magnetron and power supply to increase plasma stability and efficiency. However, it is also often difficult to identify the correct impedance matching parameters.
- Thus it is desirable to have a process for depositing relatively thick cathode films in a short time to provide a battery having relatively higher energy density or specific energy. There is also a need for depositing such cathode films with decreased electrical contact resistances while still maintaining good deposition rates. There is further a need for depositing lithium cobalt oxide without arcing or impedance matching problems.
- A method of depositing lithium metal oxide on a battery substrate in a sputtering chamber comprising (i) a substrate support, (ii) first and second sputtering targets each comprising a sputtering surface of lithium metal oxide and having a backside surface, and (iii) a first electrode about the backside surface of the first sputtering target and a second electrode about the backside surface of the second sputtering target. In the method, one or more substrates is placed on the substrate support, and sputtering gas is provided at a pressure in the sputtering chamber. The sputtering gas is energized by applying an alternating voltage of AC power to the first and second electrodes so that each electrode is alternately either an anode or a cathode, the alternating voltage being applied at a frequency of between about 10 and about 100 kHz. A time varying magnetic field is applied about each of the sputtering surfaces of the first and second targets.
- In one version, the deposition method uses first and second sputtering targets that each comprise lithium metal oxide comprising lithium cobalt oxide, lithium nickel oxide, lithium manganese oxide, lithium iron oxide, lithium cobalt nickel oxide, or a mixtures of transition metals. For example, the first and second sputtering targets can each consist essentially of lithium cobalt oxide.
- In another version, the method further comprises applying a time varying magnetic field comprising a rotational frequency of between about 0.005 and about 0.1 Hz. In still other versions, each magnetron comprises a first magnet having a first magnetic flux or first magnetic field orientation, and a second magnet having a second magnetic flux or second magnetic field orientation.
- These features, aspects and advantages of the present invention will become better understood with regard to the following description, appended claims, and accompanying drawings, which illustrate examples of the invention. However, it is to be understood that each of the features can be used in the invention in general, not merely in the context of the particular drawings, and the invention includes any combination of these features, where:
-
FIG. 1A is a sectional side view of an embodiment of a thin film battery comprising a battery cell on a substrate; -
FIG. 1B is a sectional side view of another embodiment of a battery comprising a first battery cell on a first surface of a substrate and a second battery cell on a second surface; -
FIG. 2 is a top plan view of a thin film battery showing a plurality of battery cells on a single surface of the substrate; -
FIG. 3A is a top plan schematic view of an embodiment of a twin magnetron deposition chamber; -
FIG. 3B is a sectional side schematic view of the twin magnetron deposition chamber ofFIG. 3A ; -
FIGS. 4A and 4B are plots of the X-ray diffraction pattern of a deposited lithium cobalt oxide film before and after annealing, respectively; and -
FIG. 5 is a plot of the energy capacity versus current for an embodiment of a thin film battery. - An embodiment of a
thin film battery 20 comprising asingle battery cell 22 enclosed on one side by thesubstrate 24, is illustrated inFIG. 1A . Thebattery 20 can also have single ormultiple battery cells 22 a,b on opposing surfaces of asubstrate 24, as illustrated for example inFIG. 1B . A further embodiment of abattery 20 comprising a plurality ofbattery cells 22 a-c on aplanar surface 26 of asubstrate 24 is illustrated inFIG. 2 . - Referring back to
FIG. 1A , thebattery cell 22 comprises a plurality ofbattery component films 30. Thebattery component films 30 are typically formed on anadhesion layer 32 but can also be formed directly on thesubstrate 24. The battery component films 30 cooperate to form a battery capable of receiving, storing, and discharging electrical energy. Thefilms 30 can be employed in a number of different arrangements, shapes, and sizes. Thebattery component films 30 includes at least a pair of electrode films on either side of anelectrolyte film 40. The electrode films can include one or more of a cathodecurrent collector film 34, acathode film 38 ananode film 42, and an anodecurrent collector film 44, which are all inter-replaceable. For example, thebattery 20 can include (i) a pair of cathode and anode films or a pair of current collector films, (ii) both the anode/cathode films and the current collector films, or (iii) various combinations of these films, for example, a cathode film and an anode and anode current collector film but not a cathode current collector film, and so on. The exemplary versions of thebattery 20 illustrated herein are provided to demonstrate features of the battery and to illustrate their processes of fabrication; however, it should be understood that these exemplary battery structures should not be used to limit the scope of the invention, and alternative battery structures as would be apparent to those of ordinary skill in the art are within the scope of the present invention. - Referring to
FIG. 1B , thebattery 20 can include afirst battery cell 22 a on a firstplanar surface 26 of thesubstrate 24, and asecond battery cell 22 b on a secondplanar surface 27 of thesame substrate 24. Eachbattery cell 22 a,b comprises a plurality ofbattery component films 30 a,b that include one ormore adhesion films 32 a,b; first or cathodecurrent collector films 34 a,b;cathode films 38 a,b;electrolyte films 40 a,b;anode films 42 a,b; and second or anodecurrent collector films 44 a,b. This version of thebattery 20 with twoopposing cells 22 a,b can be formed using the same processes used to form thebattery 20 with the single cell 22 (FIG. 1A ), by flipping over thesubstrate 24 to form thebattery film components 30 b of thesecond battery cell 22 b, during or after processing of thefirst battery cell 30 a. Alternatively, thebattery film components 30 b of thesecond battery cell 22 b can be formed simultaneously with thebattery film components 30 a ofcell 22 a, using chambers having multiple process zones, an exemplary version of which is described in copending U.S. patent application Ser. No. 11/681,754, filed Mar. 2, 2007, which is incorporated herein by reference and in it's entirety. - The
battery component films 30 are formed on abattery substrate 24 to fabricate abattery 20 in several fabrication steps, which can be performed separately or as a combination of steps. In a first step, asuitable substrate 24 is selected, thesubstrate 24 being a dielectric having sufficient mechanical strength to supportbattery component films 30, and typically having a surface suitable for the deposition of thin films.Suitable substrates 24 can be made from, for example, ceramics such as aluminum oxide or silicon dioxide; metals such as titanium and stainless steel; semiconductors such as silicon; or even polymers. One desirable substrate comprises a crystalline sheet formed by cleaving the planes of a cleavable crystalline structure. The cleavable crystalline structure splits along definite planes to create flat surfaces, and can include (i) basal cleavage crystals having cleavage planes parallel to the base of a crystal or to the plane of the lateral axes; (ii) cubic cleavage crystals having cleavage planes parallel to the faces of a cube, (iii) diagonal cleavage crystals which has cleavage planes parallel to a diagonal plane; (iv) lateral cleavage crystals which have cleavage planes parallel to the lateral planes; (v) octahedral, dodecahedral, or rhombohedral cleavage crystals in which cleavage occurs parallel to the faces of an octahedron, dodecahedron, or rhombohedron (respectively); and (vi) prismatic cleavage crystals in which cleavage occurs parallel to a vertical prism. The crystalline cleaving structure can be, for example, mica or graphite. Mica can be split into thin crystal sheets having thicknesses of less than about 100 microns or even less than about 25 microns, as described in a U.S. Pat. No. 6,632,563 “THIN FILM BATTERY AND METHOD OF MANUFACTURE”, filed on Sep. 9, 2000, which is incorporated by reference herein and in its entirety. In one version, an array ofsubstrates 24 that each comprise a mica sheet is used in the fabrication process. Each mica sheet can be a rectangle which is sized, for example, having dimensions from about 10 mm to about 200 mm. - The
substrate 24 of mica or other materials, can optionally be annealed to temperatures sufficiently high to clean the deposition surface, such as the cleavage plane surface, by burning-off contaminants and impurities, such as organic materials, water, dust, and other materials formed or deposited on the 26, 27 of theplanar surfaces substrate 24; or even heated to temperatures high enough to remove any water of crystallization present within the substrate. The annealing temperatures can be from about 150 to about 600° C., even at least about 400° C., or even at least about 540° C. The annealing process can be conducted in an oxygen-containing gas, such as oxygen or air, or other gas environments, for about 10 to about 120 minutes, for example, about 60 minutes. The cleaning process can also be conducted in an oxygen plasma containing cleaning step. Suitable annealing and other cleaning processes are described, for example, in U.S. patent application Ser. No. 11/681,754 which is incorporated by reference herein and in its entirety. - After the substrate cleaning and annealing step, a plurality of
battery component films 30 are deposited on the 26, 27 of thesurfaces substrate 24 to formbattery cells 22 that can generate or store electrical charge. Thecomponent films 30 are typically formed using a PVD sputter deposition process, under controlled process conditions and in one or more sputtering chambers. - In one exemplary fabrication method, one or more
battery component films 30 are deposited onto thebattery substrate 24 using asputtering chamber 100, as shown, for example, inFIGS. 3A and 3B . Thechamber 100 comprises acircular sidewall 108, achamber ceiling 110 and alower wall 112 which surrounds and encloses aprocess zone 114. Thechamber sidewall 108 can be electrically isolated from thechamber ceiling 110 and thelower wall 112 and can even be electrically grounded. The chamber walls are typically composed of stainless steel, steel or aluminum. In one version, the sputteringchamber 100 is separated from a loading chamber by aslit valve 115 for passage and transport ofsubstrates 24 into and out of thechamber 100. Theslit valve 115 can lead to adry box 117 for loading thesubstrates 24.Substrates 24 are placed onto a substrate holding fixture which is then carried into the sputtering chamber by a conveyer, the substrate holding fixture is electrically isolated from the chamber walls. - One or more substrate supports 104, or 104 a,b, are positioned about the peripheral edge of the
chamber 100 for receivingsubstrates 24. The substrate supports 104 or 104 a,b are oriented to face inward and towards a radiallyinward region 116 of thechamber 100. In one version, the substrate supports 104 can be moved during sputter processing, thereby allowing thesubstrates 24 to be rotated about the periphery of thesputtering chamber 100 or even around a circumference that encloses the plurality ofsputtering targets 102 a-d. Rotation of thesubstrates 24 during processing increases the deposition uniformity. In a further version, thesubstrate support 104 is electrically isolated from thechamber sidewall 108 and sputtering targets 102. The substrate supports 104 can be biased at a negative voltage relative to the plasma, or even relative to the time averaged potential of the cathodes. The negativelybiased substrate support 104 serves to attract the positively charged ions and sputtered material from theplasma zone 114. In one version the substrate supports 104 are biased by a biasing power supply. The biasing power supply provides a pulsed DC voltage bias of from about −5 to about −200 V or even about −40 V between the substrate supports 104 and the radiallyinward region 116 of thechamber 100. The pulsed biasing voltage has a duty cycle of from about 10% to about 90%, or even about 30%. Thesubstrate support 104 can also include a heater and heating control circuitry to maintain thesubstrate 24 at an appropriate processing temperature. In one version thesubstrate 24 is maintained at a temperature of from about 50 to about 200° C. during processing. - A plurality of
sputtering targets 102 are mounted in the radiallyinward region 116 of thechamber 100. The sputtering targets 102 can comprise lithium metal oxide, such as for example, lithium cobalt oxide, lithium nickel oxide, lithium manganese oxide, lithium iron oxide, or even lithium oxides comprising mixtures of transition metals such as for example, lithium cobalt nickel oxide. The sputtered target material deposits onto a plurality ofbattery substrates 24 in the chamber. Thetargets 102 comprise an even number of targets such as for example two, four, six or even ten or more targets. In one version, the number oftargets 102 and the size of thechamber 100 is scaleable to accommodate a larger batch ofsubstrates 24 for processing. The sputtering targets 102 can be rectangular or cylindrical. The cylindrically shaped targets are mounted to cylindrically shaped magnetrons 106. These magnetrons 106 can be configured to self-rotate during the deposition process, exposing fresh sputtering surface and reducing localized heating of the attachedtargets 102, thereby increasing the target lifespan, in on-time plasma hours, by from 15% to 70%. - One or more magnetrons 106 are provided in the radially
inward region 116 of thechamber 100. The magnetrons 106 are capable of generating a time varying magnetic field at a particular location in thechamber 100. Each magnetron 106 comprises a set of rotatable magnets or electromagnets. The magnetron 106 can be a single structure or a set of structures. In one version, the magnetron 106 includes a firstrotatable magnet assembly 146 a which is rotated behind a backside surface of afirst sputtering target 102 a, and a secondrotatable magnet assembly 146 b which is rotated behind the backside surface of asecond sputtering target 102 b. - The rotatable magnet assembly comprises a magnet that is capable of being rotated about a central axis. In the version shown in
FIG. 3B afirst magnet 148 having a first magnetic flux or magnetic field orientation, and one or moreperipheral magnets 150 having a second magnetic flux or magnetic field orientation are mounted to asupport plate 152. Thesupport plate 152 is rotated by anaxle 154 that is powered by a motor (not shown). In one version, the ratio of the first magnetic flux to the second magnetic flux is at least about 1:2, for example, from about 1:3 to about 1:8, or even about 1:5. This allows the magnetic field from theperipheral magnets 150 to extend deeper into thechamber 100. For example, the second magnetic field orientation can be generated by positioning theperipheral magnets 150 so that their polarity direction is opposite to the polarity direction of thecentral magnets 150. In one embodiment, the first and secondrotatable magnet assemblies 146 a,b are rotated at a rotational frequency of between about 0.005 and about 0.1 Hz, whereby a time varying magnetic field is provided about the surface of the first andsecond targets 102. - The magnetron 106 can also be connected to an
AC power source 118 that provides an alternating voltage to excite the sputtering gas within thechamber 100. When the chamber comprisestwin magnetrons 106 a,b, thepower source 118 serves to bias thetwin magnetrons 106 a,b relative to each other. For example, when thefirst magnetron 106 a is on a negative potential relative to thesecond magnetron 106 b, thefirst magnetron 106 a acts as the sputtering cathode, while thesecond magnetron 106 b acts as an anode. In the present example, the magnetrons 106 are powered with an AC voltage that is between 200V and 1200V and has a power of between 1 kW and 20 kW. During processing the momentary cathode generates secondary electrons which are accelerated towards the anode and neutralize positive surface charges having been built up in insulating areas during the negative half cycle. The magnetrons 106 can be mounted to thechamber ceiling 110 orlower wall 112. Typically, a sputtering target is attached to each magnetron 106. The magnetron 106 transmits the voltage to the attachedsputtering target 102, and the sputtering gas between the ACbiased targets 102 is excited. In one version, thechamber 100 comprises twin magnetrons which are each connected to atarget 102. - In one embodiment,
twin magnetrons 106 a,b are operated by a voltage or current maintained at a mid-frequency level, which is a frequency of from about 10 to about 100 kHz. It has been found that the mid-frequency sputtering process desirably reduces or eliminates co-excitation modes that would otherwise occur between the twin magnetrons 106. Absence of the co-excitation mode results in reduced arcing of the sputtering targets 102, thereby increasing the lifespan of thetargets 102, and also improving the quality of the deposited films. Arcing is often initiated by electrical breakdown of the insulating layer on the magnetron cathode. However, application of a mid-frequency power from a mid-frequencyAC power source 118 to a twin-magnetron arrangement, reduces charging up of the insulating layer and resultant plasma process instabilities. Fortargets 102 comprising lithium cobalt oxide, sputtered films can be produced in this manner without arcing over almost the entire lifetime of thetarget 102. Thus higher power levels can be applied to the sputtering targets 102. As a result, the deposition process is more continuous and results in high quality films and higher deposition throughput. For example, the mid-frequency dual magnetron process provides a deposition rate of from about 0.2 to about 4 microns/hour. - The
chamber 100 also has a plurality of cathodes 120, as shown for example inFIGS. 3A and 3B . Each cathode 120 is formed by binding atarget 102 to a magnetron 106, which provides an unbalanced magnetic field about the surface of thetarget 102 and results in a more continuous bombardment of the target during sputtering. - The
chamber 100 can further include a plurality ofion sources 122 that are capable of supplying ionized gas for in-situ active cleaning and activation of thesubstrates 24. In the embodiment shown inFIG. 3A , theion sources 122 are located adjacent to thetargets 102. For example, theion sources 122 can be located within a radiallyinward region 116 of thechamber 100, or even between thetargets 102. During the cleaning process, a cleaning gas is provided to thechamber 100 such as for example, argon and oxygen. A voltage is supplied between the radially inward region of thechamber 116 and the substrate supports 104, such that the cleaning gas ions are drawn towards and bombard the surface of thesubstrate 24. Typical ion-source cleaning processes are erosive to, and can decrease the lifespan of, thesputtering target 102. In one embodiment, a fixture (not shown) covering half of the surface of atarget 102 can be rotated to first and second orientations within thechamber 100. In the first orientation, the exposed part of thetargets 102 face thesubstrates 24 for film deposition and in the second orientation, the exposed part of thetargets 102 faces the center for in-situ active substrate cleaning, thereby decreasing target contamination. - The
chamber 100 is connected to agas supply 123,gas distributor 126 andgas exhaust 130, which supply and control the pressure and concentration of process gas within thechamber 100. The process gas mixture is controlled by first evacuating thechamber 100 and then introducing controlled amounts of process gas into thechamber 100. In one version thechamber 100 is evacuated to a pressure of less than about 5×10−5 Torr or even less than about 2×10−5 Torr prior to introduction of the sputtering gas. Sputtering process gas is introduced into the chamber and maintained at a pressure of from about 1.1 to about 15 mTorr. In one version the sputtering gas comprises argon and oxygen. The argon provides stable plasma and oxygen can prevent oxygen loss in the targets or the deposited films during the process. The sputtering argon gas is maintained in thechamber 100 at a pressure of from about 1 to about 10 mTorr. The sputtering oxygen gas is maintained in thechamber 100 at a pressure of from about 0.1 to about 5 mTorr. - The twin magnetrons are connected to a
power source 118, such as for example, anAC power supply 134. TheAC power supply 134 and provides an alternating voltage having a wave form that is approximately sinusoidal and that has a frequency in the mid-frequency range of between about 10 and about 100 kHz, or even about 40 kHz. During processing, thepower supply 134 energizes the process gas by applying a voltage bias across the first andsecond magnetrons 106 a,b at a frequency of from about 10 to about 100 kHz, or even from about 20 to about 80 kHz. The voltage bias can also be applied at a power level of at least about 1 kW, or even at a power level of from about 3 kW to about 20 kW. In one exemplary process, thepower supply 134 supplies a power density to the surface of thetargets 102 that is at least 0.1 W/cm2 or even between about 0.1 W/cm2 and about 20 W/cm2. - The
chamber 100 is controlled by acontroller 119 that comprises program code having instruction sets to operate components of thechamber 100 to processsubstrates 24 in thechamber 100. For example, thecontroller 119 can comprise a substrate positioning instruction set to operate a substrate transport mechanism to position asubstrate 24 in thechamber 100; a gas flow control instruction set to operate theflow control valves 125 to set a flow of gas to thechamber 100; a gas pressure control instruction set to operate theexhaust 130 to maintain a pressure in thechamber 100; power supply control instruction sets such as a gas energizer control instruction set to operate theelectrode power supply 134 to set a gas energizing power level and a DC power supply control instruction set to operate aDC power supply 121 to provide a DC voltage bias to thesubstrate support 104; a temperature control instruction set to control temperatures in thechamber 100; and a process monitoring instruction set to monitor the process in thechamber 100, for example by monitoring temperatures or pressure via one ormore sensors 137 that are within the chamber. - The mid-frequency twin magnetron sputtering process is particularly efficient at deposition of lithium cobalt oxide films and can provide deposition rates of between 0.2 and 4 microns per hour. The sputtering rate is sensitive to adjustments in power, processing gas pressure and DC bias voltage. In one exemplary process, two or four LiCoO2 targets are installed in the chamber. The substrate is placed in the chamber which is pumped down to below 5×10−5 Torr. A
suitable substrate 24 comprises a 35 mm×62 mm sheet of mica. Process gas, such as for example, argon and oxygen, are introduced into thechamber 100 to serve as the sputtering gas. The sputtering gas comprising argon is maintained in thechamber 100 at a pressure from about 1 to about 10 mTorr and in one version about 2 mTorr, and oxygen is maintained at the pressure of from 0.1 to 5 mTorr and in one version about 0.75 m Torr. Sputtering is performed by applying an 0.1 to 20 W/cm2 power density to eachtarget 102 and a pulsed DC voltage bias of between −5 and −100 V or even about −40 V between the substrate supports 104 and the radiallyinward region 116 of thechamber 100. The duty cycle is between 10% and 90%, even at 30%. Thesubstrate 24 is maintained at a temperature of from about 50 to about 200° C. during processing. In one version the voltage bias is applied for a sufficient time to deposit a lithium cobalt oxide film having a thickness of from about 0.25 to about 0.75 of the total thickness of a stack of films formed on thesubstrate 24. - The deposition rates obtained from the mid-frequency twin magnetron process were found to be higher than the deposition rates obtained by conventional sputtering processes, as illustrated by the following examples:
- Four LiCoO2 targets were installed in the chamber 100 a mica substrate was placed in the chamber onto a
substrate support 104 in thechamber 100. Thechamber 100 was pumped down to 2×10−5 Torr prior to introduction of the sputtering gas. Sputtering gas comprising argon and oxygen were introduced into thechamber 100. The argon gas was maintained in thechamber 100 at a pressure of about 8.2 mTorr and the oxygen gas was maintained in thechamber 100 at a pressure of about 0.75 mTorr. Sputtering was performed by applying an oscillating voltage bias between the targets, the oscillation having a frequency of about 40 kHz. The power applied to each pair of targets was about 3 kW, and with a density of about 3.5 W/cm2. A pulsed DC voltage bias of about −40 V was applied between thesubstrate support 104 and the radiallyinward region 116 of thechamber 100 with a duty cycle of about 30%. Thesubstrate 24 was maintained at a temperature of about 120° C. during processing. The as-deposited lithium cobalt oxide film had a thickness of 3.5 microns after 5 hours deposition. The deposition rate was found to be about 0.7 microns per hour. The volume deposition rate per kilowatt hour was about 0.050 cm3/kW·hr. - For comparison, a conventional RF sputtering process and deposition rate for lithium cobalt oxide film with a single magnetron chamber are presented.
- A single LiCoO2 target was installed in the chamber and a substrate was placed onto a substrate support in the chamber. The chamber was pumped down to 1×10−5 Torr prior to introducing the sputtering gas. A process gas comprising argon and oxygen were introduced into the chamber. The argon gas was maintained in the chamber at a pressure of about 8.2 mTorr and the oxygen gas was maintained in the chamber at a pressure of about 0.75 mTorr. Sputtering was performed by applying an oscillating voltage bias to the target, with a frequency of about 13.5 MHz. A power density of 1.8 W/cm2 was thereby applied to the target. The
substrate 24 was maintained at a temperature of about 120° C. during processing. The as-deposited lithium cobalt oxide film had a thickness of 2 microns after 5 hours deposition. The deposition rate of the conventional RF system was found to be about 0.4 microns/hr. The volume deposition rate per kilowatt hour was about 0.016 cm3/kW·hr. In addition, the RF deposition process was limited in the amount of power that could be applied to the target because the system was prone to arcing at higher power densities. - As supported in the examples above, the volume deposition rate per kilowatt hour of the dual-magnetron mid-frequency process was found to be 3.1 times higher than the volume deposition rate per kilowatt hour of the RF process.
- The deposited film can be annealed to reduce or even eliminate point defects in the crystal lattice by heating the
substrate 24 to a temperature that is sufficient for annealing for example, to a temperature of from about 200 to about 500° C. Thesubstrate 24 can be annealed in-situ by direct heating from a temperature controlledsubstrate support 104 or by radiation heating from an infrared radiation source (not shown). In another embodiment, thesubstrate 24 is removed and annealed in a separate chamber or even outside the chamber environment. - Unexpectedly and surprisingly, LiCoOx films deposited using a mid-frequency, dual magnetron process were found to anneal sufficiently well at a temperature of only about 400° C., as compared to a previous anneal temperature of about 540° C. for the conventionally deposited film. It is believed that this reduction in the temperature of annealing is because the as-deposited film contains fewer lattice defects. The reduction in lattice defects may be caused by a higher plasma density during the mid-frequency twin-magnetron deposition process, which may break down the sputtered material into smaller pieces.
- A LiCoOx film fabricated according to the present method and without an additional annealing step comprises LiCoO2 which is crystalline with a strong (012) preferred orientation and with a smaller amount of (003) oriented grains.
FIG. 4A shows a typical x-ray twotheta diffraction pattern 138 of the as-deposited LiCoO2 film. Thelarge peak 140, located at a scattering angle of about 39°, and thesmaller peak 142, located at a scattering angle of about 19°, show that the film is highly crystalline and with a (012) and (003) preferred orientation. The substrate was slightly tilted when taking x-ray diffraction in order to suppress the diffraction peaks from an underlying mica substrate to better reveal the crystalline properties of the LiCoO2 film. It is believed that the crystalline material was deposited due to a combination of plasma heating, oxygen activation and plasma enhanced nucleation and growth processes. The as deposited crystalline material was a good cathode material. - Optionally, the film formed on the substrate may be annealed at 150 to 600° C. to further improve the quality of the cathode film. An x-ray diffraction pattern 136 of crystalline LiCoO2 film after annealing at 400° C. for 10 hours is shown in
FIG. 4B . Thelarger intensity peak 148, located at a scattering angle of about 37.5° shows a strong (101) preferred orientation and thesmaller intensity peak 150, located at a scattering angle of about 40° shows a small amount of (012) oriented grains. The annealing step was found to increase the battery capacity by 10 to 20%, increase the charge and discharge current by more than 50%, and improve the resistance to moisture. It is believed that these attributes arise from the elimination of point defects and the reduction of electrical contact resistances in the cathode material. - In one version, the area of the battery is 2.9 cm2. The mica substrate is 20 microns thick, and overall thickness of the battery is around 50 microns. The battery is sealed with Surlyn (epoxy) for temporary protection against the oxidizing environment.
FIG. 5 shows the discharge curves of four test batteries, each comprising a LiCoOx film deposited by the method described above (with 400° C. annealing). The curves indicate that the higher the discharge current, the lower the capacity, which is consistent with previous data obtained from LiCoOx film batteries formed using an RF deposition process. This Surlyn sealed battery has an energy density of around 62.4 wh/l. - While a particular sequence of process steps is described to illustrate an embodiment of the process, it should be understood that other sequences of process steps can also be used as would be apparent to one of ordinary skill in the art.
- The above methods or other deposition methods can be used to deposit one or more of the
component films 30, which in one embodiment include anadhesion film 32. Theadhesion film 32 is deposited on theplanar surface 26 of thesubstrate 24 to improve adhesion of overlying battery component films 30 (FIG. 1A ). Theadhesion film 32 can comprise a metal or metal compound, such as for example, aluminum, cobalt, titanium, other metals, or their alloys or compounds thereof; or a ceramic oxide such as, for example, lithium cobalt oxide. Exemplary process conditions for deposition of atitanium adhesion film 32 comprise: argon maintained at a pressure of 2 mTorr; DC (direct current) sputtering plasma at a power level of 1 kW, a deposition time of 30 seconds, a titanium target size of 5×20 inches, and a target-to-substrate distance of 10 cm. In the version shown inFIG. 1B , after deposition of afirst adhesion film 32 a on the firstplanar surface 26 of thesubstrate 24, thesubstrate 24 is flipped over and asecond adhesion film 32 b is deposited on the secondplanar surface 27 which forms the other side of the substrate. Theadhesion film 32 can be deposited on thesubstrate 24 not only to cover the area under the subsequently depositedbattery cells 22 a-c and theirbattery component films 30 but also thearea 36 extending beyond thebattery component films 30, as described in aforementioned U.S. patent application Ser. No. 11/681,754. Theadhesion film 32 is typically deposited in a thickness of from about 100 to about 1500 angstroms. - A cathode
current collector film 34 is formed on theadhesion film 32 to collect the electrons during charge and discharge process. The cathodecurrent collector film 34 typically comprises a conductor such as, for example, aluminum, platinum, silver or gold or even the same metal as theadhesion film 32 in a thickness that is sufficient to provide the desired electrical conductivity. The firstcurrent collector film 34 typically has a thickness that is from about 0.05 microns to about 2 microns. The cathodecurrent collector film 34 a-c can be formed as a pattern of features 68 a-c, as illustrated inFIG. 2 , that each comprise a spaced apart discontinuous region that covers a small region of theadhesion film 32. The features 68 a-c are over the covered regions 71 a-c of theadhesion film 32, and adjacent to the features 68 a-c are exposed regions 70 a-c of theadhesion film 32. To deposit the patternedfilm 34 a-c, a patterned mechanical mask is placed on top of thesubstrate 24, and a firstcurrent collector film 34 of platinum is deposited by DC magnetron sputtering to form the features 68 a-c between the patterned mask regions. Exemplary process conditions for argon sputter deposition of a platinum cathodecurrent collector film 34 a-c comprise a gas pressure of 5 mTorr to form a DC plasma at a power level of 40 Watts for 10 minutes. - After forming the features 68 a-c on the
adhesion film 32, the adhesion film with its covered regions 71 a-c below the patterned features 68 a-c and exposed surface regions 70 a-d, is then exposed to an oxygen-containing environment and heated to temperatures of from about 200° C. to about 600° C., for example, about 400° C., for about an hour, to oxidize the exposed regions 70 a-d of titanium that surround the deposited platinum features but not the titanium regions covered and protected by the platinum features. The resultant structure, advantageously, includes not only the non-exposed covered regions 71 a-c ofadhesion film 32 below the features 68 a-c of thecurrent collector film 38, but also oxygen-exposed or oxidized regions 70 a-d which form non-conducting regions that electrically separate the plurality ofbattery cells 22 a-c formed on thesame substrate 24. - A
cathode film 38 comprising an electroactive material is then formed over thecurrent collector film 34. In one version, thecathode film 38 is composed of lithium metal oxide, such as for example, lithium cobalt oxide, lithium nickel oxide, lithium manganese oxide, lithium iron oxide, or even lithium oxides comprising mixtures of transition metals such as for example, lithium cobalt nickel oxide. Other types ofcathode films 38 that may be used comprise amorphous vanadium pentoxide, crystalline V2O5 or TiS2. In one example, thecathode film 38 comprises crystalline lithium cobalt oxide, which in one version, has the stoichiometric formula of LiCoO2. Thecathode film 38 can be fabricated in a single continuous deposition step or using a multiple sequential deposition and stress reducing annealing step that is performed at a temperature of between about 150 and 600° C. Typically, thecathode film 38 or cathode film stack has a thickness of at least about 5 microns, or even at least about 10 microns. In one exemplary embodiment, thecathode film 38 is deposited using a twin-magnetron, mid-frequency sputtering process, as described above. The twin-magnetron mid-frequency process is particularly well suited for deposition of thecathode film 38 because of it's comparatively high sputtering rates for lithium metal oxides. Thecathode film 38 can also be annealed in a defect reducing step to temperatures of from about 150 to about 700° C., for example, by about 400° C., to further improve the quality of thecathode film 38 by reducing the amount of defects. - An
electrolyte film 40 is formed over thecathode film 38. Theelectrolyte film 40 can be, for example, an amorphous lithium phosphorus oxynitride film, also known as a LiPON film. In one embodiment, the LiPON has the stoichiometric form LixPOyNz in an x:y:z ratio of about 2.9:3.3:0.46. In one version, theelectrolyte film 40 has a thickness of from about 0.1 micron to about 5 microns. This thickness is suitably large to provide sufficiently high ionic conductivity and suitably small to reduce ionic pathways to minimize electrical resistance and reduce stress. - An
anode film 42 formed over theelectrolyte film 40. Theanode film 42 can be the same material as thecathode film 38, as already described. A suitable thickness is from about 0.1 micron to about 20 microns. In one version,anode film 42 is made from lithium which is also sufficiently conductive to also serve as the anode current collector film, and in this version theanode film 42 and anodecurrent collector film 44 are the same. In another version, the anodecurrent collector film 44 is formed on theanode film 42, and comprises the same material as the cathodecurrent collector film 34 to provide a conducting surface from which electrons may be dissipated or collected from theanode film 42. For example, in one version, the anodecurrent collector film 44 comprises a non-reactive metal such as silver, gold, platinum, in a thicknesses of from about 0.05 microns to about 5 microns. - After the deposition of all the
battery component films 30, a variety of protective layers or electrically conducting layers can be formed over thebattery component films 30 to provide protection against environmental elements. In one example, the protective layer comprises a plurality of polymer and ceramic layers that are superimposed on each other. In another example, a portion of the cathodecurrent collector film 34 or anodecurrent collector film 44 that extends out from under abattery cell 22 forms a contact portion that is used to connect thebattery cell 22 or thebattery 20 to the external environment. This contact portion is coated with an electrically conducting barrier layer. The layers can protect thebattery cell 22 during pulsed laser cutting of the individual battery cells from an array of cells formed on a larger mica substrate. For example, the electrically conducting barrier layer is formed in a thickness sufficiently large to prevent the pulsed laser beam from penetrating therethrough. - The
thin film battery 20 can also be fabricated to provide a plurality ofbattery cells 22 a-c on asingle substrate 24. Thebattery cells 22 a-c can be arranged horizontally across asingle substrate surface 26 or fabricated on thefront surface 26 and backside surface 27 of abattery substrate 24 to substantially increase the energy density and capacity of thebattery cell 22. Suitable battery configurations, protective layers, and packaging, are described in for example, U.S. patent application Ser. No. 11/090,408, filed on Mar. 25, 2005, entitled “THIN FILM BATTERY WITH PROTECTIVE PACKAGING” by Krasnov et al., which is incorporated by reference herein and in its entirety. - While a particular sequence of process steps and chamber configuration is described to illustrate an embodiment of the process, it should be understood that other sequences of process steps can also be used as would be apparent to one of ordinary skill in the art. For example the order of deposition of the
component films 30 can be interchanged or other films can be deposited on top of or in between films of thebattery 20. Also, other configurations of thechamber 100 are possible for example the chamber can have more pairs of cathodes 120, such as 3, 4, or more. Therefore, the spirit and scope of the appended claims should not be limited to the description of the preferred versions contained herein.
Claims (17)
1. A method of depositing lithium metal oxide on a battery substrate, in a sputtering chamber comprising (i) a substrate support, (ii) first and second sputtering targets each comprising a sputtering surface of lithium metal oxide and having a backside surface, and (iii) a first electrode about the backside surface of the first sputtering target and a second electrode about the backside surface of the second sputtering target, the method comprising:
(a) placing one or more substrates on the substrate support in the sputtering chamber;
(b) maintaining a sputtering gas at a pressure in the sputtering chamber;
(c) energizing the sputtering gas by applying an alternating voltage of AC power to the first and second electrodes so that each electrode is alternately either an anode or a cathode, the alternating voltage being applied at a frequency of between about 10 and about 100 kHz; and
(d) applying a time varying magnetic field about each of the sputtering surfaces of the first and second targets.
2. A method according to claim 1 wherein the time varying magnetic field comprises a rotational frequency.
3. A method according to claim 2 wherein the rotational frequency is between about 0.005 and about 0.1 Hz.
4. A method according to claim 1 comprising providing a magnetron behind each sputtering target, the magnetron comprising first and second magnets that have different magnetic fluxes or magnetic field orientations.
5. A method according to claim 1 wherein the sputtering chamber comprises a cathode formed by binding a sputtering target to a magnetron, and wherein (d) comprises rotating the magnetron.
6. A method according to claim 5 comprising mounting a cylindrically shaped target to a cylindrically shaped magnetron.
7. A method according to claim 1 wherein the sputtering chamber comprises a cathode formed by binding a sputtering target to a magnetron comprising a rotatable magnet assembly, and wherein (d) comprises rotating the magnet assembly.
8. A method according to claim 1 comprising applying the alternating voltage at at least one of (i) a frequency of from about 20 to about 80 kHz, and (ii) a power level of from about 3 kW to about 10 kW.
9. A method according to claim 1 wherein the substrate support is electrically isolated from a sputtering chamber wall and from the first and second sputtering targets and wherein (a) comprises applying to the substrate support, a biasing voltage that is at least one of (i) a pulsed voltage, (ii) from about −20V to about −200V, and (iii) has a duty cycle from 10% to 90%.
10. A method according to claim 1 wherein the lithium metal oxide comprises lithium cobalt oxide, lithium nickel oxide, lithium manganese oxide, lithium iron oxide, lithium cobalt nickel oxide, or a mixtures of transition metals.
11. A method according to claim 1 wherein the lithium metal oxide consists essentially of lithium cobalt oxide.
12. A method of depositing lithium cobalt oxide on a battery substrate in a sputtering chamber comprising (i) a substrate support, (ii) first and second sputtering targets each comprising a sputtering surface of lithium cobalt oxide and having a backside surface, and (iii) a first electrode about the backside surface of the first sputtering target and a second electrode about the backside surface of the second sputtering target, the method comprising:
(a) placing one or more substrates on the substrate support in the sputtering chamber;
(b) maintaining a sputtering gas at a pressure in the sputtering chamber;
(c) energizing the sputtering gas by applying an alternating voltage of AC power to the first and second electrodes so that each electrode is alternately either an anode or a cathode, the alternating voltage being applied at a frequency of between about 10 and about 100 kHz; and
(d) applying a time varying magnetic field about each of the sputtering surfaces of the first and second targets, the time varying magnetic field comprising a rotational frequency of between about 0.005 and about 0.1 Hz.
13. A method according to claim 12 comprising providing a magnetron behind each sputtering target, the magnetron comprising first and second magnets that have different magnetic fluxes or magnetic field orientations.
14. A method according to claim 12 wherein the sputtering chamber comprises a cathode formed by binding a sputtering target to a magnetron, and wherein (d) comprises rotating the magnetron.
15. A method according to claim 12 wherein the sputtering chamber comprises a cathode formed by binding a sputtering target to a magnetron comprising a rotatable magnet assembly, and wherein (d) comprises rotating the magnet assembly.
16. A method according to claim 12 comprising applying the alternating voltage at at least one of a frequency of from about 20 to about 80 kHz and a power level of from about 3 kW to about 10 kW.
17. A method of depositing lithium cobalt oxide on a battery substrate in a sputtering chamber comprising (i) a substrate support, (ii) first and second sputtering targets that each have a sputtering surface consisting essentially of lithium cobalt oxide, and (iii) a first electrode about the first sputtering target and a second electrode about the second sputtering target, the method comprising:
(a) placing one or more substrates on the substrate support in the sputtering chamber;
(b) maintaining a sputtering gas at a pressure in the sputtering chamber;
(c) energizing the sputtering gas by applying an alternating voltage of AC power to the first and second electrodes so that each electrode is alternately either an anode or a cathode, the alternating voltage being applied at a frequency of between about 10 and about 100 kHz;
(d) providing a magnetron about each of the first and second sputtering targets, each magnetron comprising a first magnet having a first magnetic flux or first magnetic field orientation, and one or more peripheral magnets having a second magnetic flux or second magnetic field orientation; and
(e) applying a time varying magnetic field about each of the sputtering surfaces of the first and second targets, the time varying magnetic field comprising a rotational frequency of between about 0.005 and about 0.1 Hz.
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| US14/089,019 US20140166471A1 (en) | 2007-09-04 | 2013-11-25 | Depositing lithium metal oxide on a battery substrate |
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| US11/849,959 US8628645B2 (en) | 2007-09-04 | 2007-09-04 | Manufacturing method for thin film battery |
| US14/089,019 US20140166471A1 (en) | 2007-09-04 | 2013-11-25 | Depositing lithium metal oxide on a battery substrate |
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| US14/089,019 Abandoned US20140166471A1 (en) | 2007-09-04 | 2013-11-25 | Depositing lithium metal oxide on a battery substrate |
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Cited By (6)
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|---|---|---|---|---|
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| US9356320B2 (en) | 2012-10-15 | 2016-05-31 | Front Edge Technology Inc. | Lithium battery having low leakage anode |
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| US10008739B2 (en) | 2015-02-23 | 2018-06-26 | Front Edge Technology, Inc. | Solid-state lithium battery with electrolyte |
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Families Citing this family (37)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8679674B2 (en) * | 2005-03-25 | 2014-03-25 | Front Edge Technology, Inc. | Battery with protective packaging |
| US7846579B2 (en) | 2005-03-25 | 2010-12-07 | Victor Krasnov | Thin film battery with protective packaging |
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| US8870974B2 (en) * | 2008-02-18 | 2014-10-28 | Front Edge Technology, Inc. | Thin film battery fabrication using laser shaping |
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| US20090136839A1 (en) * | 2007-11-28 | 2009-05-28 | Front Edge Technology, Inc. | Thin film battery comprising stacked battery cells and method |
| US8502494B2 (en) * | 2009-08-28 | 2013-08-06 | Front Edge Technology, Inc. | Battery charging apparatus and method |
| JP2011108603A (en) * | 2009-11-20 | 2011-06-02 | Ulvac Japan Ltd | Thin film lithium secondary battery, and forming method of thin film lithium secondary battery |
| US20150125622A1 (en) * | 2010-04-01 | 2015-05-07 | The Trustees of Columbia University in HIe City of | Systems and methods for high and ultra-high vacuum physical vapor deposition with in-situ magnetic field |
| JP2013537690A (en) * | 2010-08-04 | 2013-10-03 | フロント エッジ テクノロジー,インコーポレイテッド | Rechargeable battery with current limiter |
| EP2565291A1 (en) * | 2011-08-31 | 2013-03-06 | Hauzer Techno Coating BV | Vaccum coating apparatus and method for depositing nanocomposite coatings |
| JP5301021B2 (en) * | 2011-09-06 | 2013-09-25 | 出光興産株式会社 | Sputtering target |
| US8865340B2 (en) | 2011-10-20 | 2014-10-21 | Front Edge Technology Inc. | Thin film battery packaging formed by localized heating |
| FR2983356B1 (en) * | 2011-11-24 | 2014-01-24 | Commissariat Energie Atomique | METHOD FOR MANUFACTURING AN ALL-SOLID BATTERY |
| US9887429B2 (en) | 2011-12-21 | 2018-02-06 | Front Edge Technology Inc. | Laminated lithium battery |
| US8864954B2 (en) * | 2011-12-23 | 2014-10-21 | Front Edge Technology Inc. | Sputtering lithium-containing material with multiple targets |
| US9257695B2 (en) | 2012-03-29 | 2016-02-09 | Front Edge Technology, Inc. | Localized heat treatment of battery component films |
| KR20150038445A (en) * | 2012-07-26 | 2015-04-08 | 어플라이드 머티어리얼스, 인코포레이티드 | Electrochemical device fabrication process with low temperature anneal |
| US8753724B2 (en) | 2012-09-26 | 2014-06-17 | Front Edge Technology Inc. | Plasma deposition on a partially formed battery through a mesh screen |
| KR20150073192A (en) * | 2012-10-15 | 2015-06-30 | 사임베트 코퍼레이션 | Thin film batteries comprising a glass or ceramic substrate |
| GB201400276D0 (en) * | 2014-01-08 | 2014-02-26 | Ilika Technologies Ltd | Vapour deposition method for fabricating lithium-containing thin film layered structures |
| GB201400274D0 (en) | 2014-01-08 | 2014-02-26 | Ilika Technologies Ltd | Vapour deposition method for preparing amorphous lithium-containing compounds |
| TW201529873A (en) * | 2014-01-24 | 2015-08-01 | Applied Materials Inc | Deposition of solid state electrolyte on electrode layers in electrochemical devices |
| WO2015197594A2 (en) | 2014-06-23 | 2015-12-30 | Schott Ag | Electric storage system containing a discrete disc-shaped element, discrete disc-shaped element and method for producing and using the same |
| US9455437B2 (en) * | 2014-10-08 | 2016-09-27 | Intermolecular, Inc. | Solid-state batteries utilizing template layers for electrode formation and methods for forming the same |
| WO2016087311A2 (en) | 2014-12-01 | 2016-06-09 | Schott Ag | Electrical storage system comprising a sheet-type discrete element, discrete sheet-type element, method for the production thereof and use thereof |
| US10290838B2 (en) * | 2015-09-08 | 2019-05-14 | Stmicroelectronics (Tours) Sas | Methods for encapsulating flexible thin-film micro-batteries to protect against environmental intrusion |
| CN109643784B (en) | 2016-06-15 | 2022-09-06 | 爱利卡技术有限公司 | Lithium borosilicate glass as electrolyte and electrode protection layer |
| GB201814039D0 (en) | 2018-08-29 | 2018-10-10 | Ilika Tech Ltd | Method |
| US12506137B2 (en) | 2019-09-23 | 2025-12-23 | International Business Machines Corporation | High capacity compact lithium thin film battery |
| GB2588932B (en) | 2019-11-15 | 2022-08-24 | Dyson Technology Ltd | Method and apparatus for sputter deposition of target material to a substrate |
| GB2588935B (en) | 2019-11-15 | 2022-09-07 | Dyson Technology Ltd | Method and apparatus for sputter deposition of target material to a substrate |
| GB2588947B (en) | 2019-11-15 | 2024-02-21 | Dyson Technology Ltd | A method of manufacturing solid state battery cathodes for use in batteries |
| GB2588944B (en) * | 2019-11-15 | 2022-08-17 | Dyson Technology Ltd | Method of forming crystalline layer, method of forming a battery half cell |
| GB2588939B (en) | 2019-11-15 | 2022-12-28 | Dyson Technology Ltd | Sputter deposition apparatus and method |
| GB2588940B (en) | 2019-11-15 | 2022-06-22 | Dyson Technology Ltd | Sputter deposition |
| RU2765222C1 (en) * | 2020-12-30 | 2022-01-26 | Тхе Баттериес Сп. з о.о. | METHOD FOR FORMING A LiCoO2 FILM AND APPARATUS FOR IMPLEMENTATION THEREOF |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5522976A (en) * | 1991-09-03 | 1996-06-04 | Societe Nationale Elf Aquitaine | Target component for cathode sputtering |
| US5833815A (en) * | 1996-04-24 | 1998-11-10 | Anelva Corporation | Sputter deposition system |
| US6039850A (en) * | 1995-12-05 | 2000-03-21 | Minnesota Mining And Manufacturing Company | Sputtering of lithium |
| US6338777B1 (en) * | 1998-10-23 | 2002-01-15 | International Business Machines Corporation | Method and apparatus for sputtering thin films |
Family Cites Families (124)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3375135A (en) | 1965-06-04 | 1968-03-26 | Melpar Inc | Galvanic cell with thin metal electrode and method of making same |
| US3414685A (en) | 1965-09-23 | 1968-12-03 | Dahlberg Electronics | In-the-ear hearing aid |
| US3530007A (en) | 1967-12-19 | 1970-09-22 | Us Air Force | Solar cell including aceanthraquinoxaline photosensitive material |
| US3844841A (en) | 1972-12-29 | 1974-10-29 | Energy Res Corp | Modular battery construction |
| US3969142A (en) | 1975-03-10 | 1976-07-13 | Wilson Greatbatch Ltd. | Lithium iodine battery |
| US3993508A (en) | 1975-06-20 | 1976-11-23 | Polaroid Corporation | Method for manufacturing flat batteries |
| FR2347785A1 (en) | 1976-04-09 | 1977-11-04 | Catalyst Research Corp | THERMAL BATTERY WITH DEPOLARIZER |
| US4309494A (en) | 1979-05-15 | 1982-01-05 | Stockel Richard F | Electrochemical cell having battery separator of ethylene-vinyl alcohol copolymer |
| IL59925A (en) | 1980-04-25 | 1983-09-30 | Yeda Res & Dev | Storage of electrical energy with a tin-tin-sulfide sulfur/sulfide system |
| US4459328A (en) | 1981-12-21 | 1984-07-10 | Gte Products Corporation | Articles coated with wear-resistant titanium compounds |
| JPS5930709A (en) | 1982-08-13 | 1984-02-18 | Toa Nenryo Kogyo Kk | Method for synthesizing carbon film and carbon granule in vapor phase |
| JPS59147469A (en) | 1983-02-14 | 1984-08-23 | Hitachi Ltd | Amorphous silicon solar cell |
| CA1232228A (en) | 1984-03-13 | 1988-02-02 | Tatsuro Miyasato | Coating film and method and apparatus for producing the same |
| US4698256A (en) | 1984-04-02 | 1987-10-06 | American Cyanamid Company | Articles coated with adherent diamondlike carbon films |
| US4619865A (en) | 1984-07-02 | 1986-10-28 | Energy Conversion Devices, Inc. | Multilayer coating and method |
| US4663183A (en) | 1984-09-10 | 1987-05-05 | Energy Conversion Devices, Inc. | Glow discharge method of applying a carbon coating onto a substrate |
| US4877677A (en) | 1985-02-19 | 1989-10-31 | Matsushita Electric Industrial Co., Ltd. | Wear-protected device |
| US4565753A (en) | 1985-04-03 | 1986-01-21 | Gte Government Systems Corporation | Electrochemical cell having wound electrode structures |
| US4725345A (en) | 1985-04-22 | 1988-02-16 | Kabushiki Kaisha Kenwood | Method for forming a hard carbon thin film on article and applications thereof |
| US4714660A (en) | 1985-12-23 | 1987-12-22 | Fansteel Inc. | Hard coatings with multiphase microstructures |
| US4871433A (en) | 1986-04-04 | 1989-10-03 | Materials Research Corporation | Method and apparatus for improving the uniformity ion bombardment in a magnetron sputtering system |
| US4777090A (en) | 1986-11-03 | 1988-10-11 | Ovonic Synthetic Materials Company | Coated article and method of manufacturing the article |
| JP2692816B2 (en) | 1987-11-13 | 1997-12-17 | 株式会社きもと | Thin primary battery |
| JP2610469B2 (en) | 1988-02-26 | 1997-05-14 | 株式会社 半導体エネルギー研究所 | Method for forming carbon or carbon-based coating |
| US4904542A (en) | 1988-10-11 | 1990-02-27 | Midwest Research Technologies, Inc. | Multi-layer wear resistant coatings |
| US5511587A (en) | 1990-09-28 | 1996-04-30 | Citizen Watch Co., Ltd. | Wear-resistant reed for a high-speed loom |
| GB2251119B (en) | 1990-12-20 | 1995-06-07 | Technology Finance Corp | Electrochemical cell |
| US5670252A (en) | 1991-03-11 | 1997-09-23 | Regents Of The University Of California | Boron containing multilayer coatings and method of fabrication |
| US5330853A (en) | 1991-03-16 | 1994-07-19 | Leybold Ag | Multilayer Ti-Al-N coating for tools |
| JPH04295015A (en) * | 1991-03-26 | 1992-10-20 | Showa Electric Wire & Cable Co Ltd | Production of bi-base oxide superconducting thin film |
| JPH07109034B2 (en) | 1991-04-08 | 1995-11-22 | ワイケイケイ株式会社 | Hard multilayer film forming body and method for producing the same |
| US5171413A (en) | 1991-09-16 | 1992-12-15 | Tufts University | Methods for manufacturing solid state ionic devices |
| WO1993008316A1 (en) | 1991-10-14 | 1993-04-29 | Commissariat A L'energie Atomique | Multi-layer material for anti-erosion and anti-abrasion coating |
| US5197889A (en) | 1992-02-03 | 1993-03-30 | Motorola, Inc. | Electrical contact for battery package or similar device |
| US5786582A (en) | 1992-02-27 | 1998-07-28 | Symbol Technologies, Inc. | Optical scanner for reading and decoding one- and two-dimensional symbologies at variable depths of field |
| US5262028A (en) | 1992-06-01 | 1993-11-16 | Sierra Applied Sciences, Inc. | Planar magnetron sputtering magnet assembly |
| US5338625A (en) | 1992-07-29 | 1994-08-16 | Martin Marietta Energy Systems, Inc. | Thin film battery and method for making same |
| DE69319531T2 (en) | 1992-10-12 | 1999-04-15 | Sumitomo Electric Industries, Ltd., Osaka | Ultra thin film laminate |
| US5249554A (en) | 1993-01-08 | 1993-10-05 | Ford Motor Company | Powertrain component with adherent film having a graded composition |
| US5516340A (en) | 1993-03-17 | 1996-05-14 | Wilson Greatbatch Ltd. | Process for making a metal oxide composite cathode material for high energy density batteries |
| US5478456A (en) | 1993-10-01 | 1995-12-26 | Minnesota Mining And Manufacturing Company | Sputtering target |
| US5985485A (en) | 1993-11-19 | 1999-11-16 | Ovshinsky; Stanford R. | Solid state battery having a disordered hydrogenated carbon negative electrode |
| US5512387A (en) | 1993-11-19 | 1996-04-30 | Ovonic Battery Company, Inc. | Thin-film, solid state battery employing an electrically insulating, ion conducting electrolyte material |
| US5490911A (en) | 1993-11-26 | 1996-02-13 | The United States Of America As Represented By The Department Of Energy | Reactive multilayer synthesis of hard ceramic foils and films |
| US5569520A (en) | 1994-01-12 | 1996-10-29 | Martin Marietta Energy Systems, Inc. | Rechargeable lithium battery for use in applications requiring a low to high power output |
| WO1995021467A1 (en) | 1994-02-02 | 1995-08-10 | Valence Technology, Inc. | Equalizing charge rates of individual battery cells |
| US5961672A (en) | 1994-02-16 | 1999-10-05 | Moltech Corporation | Stabilized anode for lithium-polymer batteries |
| GB9405744D0 (en) | 1994-03-23 | 1994-05-11 | Rolls Royce Plc | A multilayer erosion resistant coating and a method for its production |
| US5670272A (en) | 1994-03-31 | 1997-09-23 | Valence Technology, Inc. | Battery packaging for flat cell batteries having a compressing material for the cell stack |
| US5554456A (en) | 1994-06-14 | 1996-09-10 | Ovonic Battery Company, Inc. | Electrochemical hydrogen storage alloys and batteries containing heterogeneous powder particles |
| US5445906A (en) | 1994-08-03 | 1995-08-29 | Martin Marietta Energy Systems, Inc. | Method and system for constructing a rechargeable battery and battery structures formed with the method |
| DE69527236T2 (en) | 1994-09-16 | 2003-03-20 | Sumitomo Electric Industries, Ltd. | Multi-layer film made of ultra-fine particles and hard composite material for tools that contain this film |
| EP0822996B1 (en) * | 1995-04-25 | 2003-07-02 | VON ARDENNE ANLAGENTECHNIK GmbH | Sputtering system using cylindrical rotating magnetron electrically powered using alternating current |
| US5705297A (en) | 1996-03-04 | 1998-01-06 | Bell Communications Research, Inc. | Electrical connection for a polymeric laminate battery structure |
| US5824374A (en) | 1996-07-22 | 1998-10-20 | Optical Coating Laboratory, Inc. | In-situ laser patterning of thin film layers during sequential depositing |
| US6022640A (en) | 1996-09-13 | 2000-02-08 | Matsushita Electric Industrial Co., Ltd. | Solid state rechargeable lithium battery, stacking battery, and charging method of the same |
| US5705293A (en) | 1997-01-09 | 1998-01-06 | Lockheed Martin Energy Research Corporation | Solid state thin film battery having a high temperature lithium alloy anode |
| US5894656A (en) | 1997-04-11 | 1999-04-20 | Valence Technology, Inc. | Methods of fabricating electrochemical cells |
| US5871865A (en) | 1997-05-15 | 1999-02-16 | Valence Technology, Inc. | Methods of fabricating electrochemical cells |
| US6051114A (en) * | 1997-06-23 | 2000-04-18 | Applied Materials, Inc. | Use of pulsed-DC wafer bias for filling vias/trenches with metal in HDP physical vapor deposition |
| US6017654A (en) | 1997-08-04 | 2000-01-25 | Carnegie Mellon University | Cathode materials for lithium-ion secondary cells |
| US6217623B1 (en) | 1997-11-03 | 2001-04-17 | Motorola, Inc. | Method of fabricating an electrochemical device |
| US6402795B1 (en) | 1998-02-18 | 2002-06-11 | Polyplus Battery Company, Inc. | Plating metal negative electrodes under protective coatings |
| US6118248A (en) | 1998-04-02 | 2000-09-12 | The Procter & Gamble Company | Battery having a built-in controller to extend battery service run time |
| US6287711B1 (en) | 1998-07-01 | 2001-09-11 | Front Edge Technology, Inc. | Wear-resistant coating and component |
| KR100305903B1 (en) | 1998-08-21 | 2001-12-17 | 박호군 | Electrical and electronic devices with thin-film batteries connected vertically and integrated and methods for fabricating the same |
| US6197450B1 (en) | 1998-10-22 | 2001-03-06 | Ramot University Authority For Applied Research & Industrial Development Ltd. | Micro electrochemical energy storage cells |
| US6365010B1 (en) * | 1998-11-06 | 2002-04-02 | Scivac | Sputtering apparatus and process for high rate coatings |
| US6940988B1 (en) | 1998-11-25 | 2005-09-06 | Insound Medical, Inc. | Semi-permanent canal hearing device |
| US6379835B1 (en) | 1999-01-12 | 2002-04-30 | Morgan Adhesives Company | Method of making a thin film battery |
| US6280875B1 (en) | 1999-03-24 | 2001-08-28 | Teledyne Technologies Incorporated | Rechargeable battery structure with metal substrate |
| US6148503A (en) | 1999-03-31 | 2000-11-21 | Imra America, Inc. | Process of manufacturing porous separator for electrochemical power supply |
| JP2000284344A (en) | 1999-03-31 | 2000-10-13 | Olympus Optical Co Ltd | Camera for both silver halide photography and electronic imaging |
| US6242129B1 (en) | 1999-04-02 | 2001-06-05 | Excellatron Solid State, Llc | Thin lithium film battery |
| US6398824B1 (en) | 1999-04-02 | 2002-06-04 | Excellatron Solid State, Llc | Method for manufacturing a thin-film lithium battery by direct deposition of battery components on opposite sides of a current collector |
| US6168884B1 (en) | 1999-04-02 | 2001-01-02 | Lockheed Martin Energy Research Corporation | Battery with an in-situ activation plated lithium anode |
| JP2001044073A (en) | 1999-07-30 | 2001-02-16 | Sony Corp | Thin film capacitor and manufacturing method thereof |
| US6340880B1 (en) | 1999-11-11 | 2002-01-22 | Mitsumi Electric Co., Ltd. | Method of protecting a chargeable electric cell |
| US6387039B1 (en) | 2000-02-04 | 2002-05-14 | Ron L. Moses | Implantable hearing aid |
| US6986965B2 (en) | 2000-03-24 | 2006-01-17 | Cymbet Corporation | Device enclosures and devices with integrated battery |
| US6387563B1 (en) | 2000-03-28 | 2002-05-14 | Johnson Research & Development, Inc. | Method of producing a thin film battery having a protective packaging |
| US6658124B1 (en) | 2000-04-06 | 2003-12-02 | Advanced Bionics Corporation | Rechargeable hearing aid |
| US6402796B1 (en) | 2000-08-07 | 2002-06-11 | Excellatron Solid State, Llc | Method of producing a thin film battery |
| US20020110733A1 (en) | 2000-08-07 | 2002-08-15 | Johnson Lonnie G. | Systems and methods for producing multilayer thin film energy storage devices |
| US7056620B2 (en) | 2000-09-07 | 2006-06-06 | Front Edge Technology, Inc. | Thin film battery and method of manufacture |
| US6632563B1 (en) | 2000-09-07 | 2003-10-14 | Front Edge Technology, Inc. | Thin film battery and method of manufacture |
| KR100890715B1 (en) | 2000-11-01 | 2009-03-27 | 소니 가부시끼 가이샤 | Battery, Method for Manufacturing Battery, Method for Manufacturing Weld and Pedestal |
| US6863699B1 (en) | 2000-11-03 | 2005-03-08 | Front Edge Technology, Inc. | Sputter deposition of lithium phosphorous oxynitride material |
| JP2002164062A (en) | 2000-11-28 | 2002-06-07 | Araco Corp | Separator for fuel cell and its method of manufacture |
| US20020071989A1 (en) | 2000-12-08 | 2002-06-13 | Verma Surrenda K. | Packaging systems and methods for thin film solid state batteries |
| US6558836B1 (en) | 2001-02-08 | 2003-05-06 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Structure of thin-film lithium microbatteries |
| US6498455B2 (en) | 2001-02-22 | 2002-12-24 | Gary Skuro | Wireless battery charging system for existing hearing aids using a dynamic battery and a charging processor unit |
| US20020150823A1 (en) | 2001-04-11 | 2002-10-17 | Breitkopf Richard C. | Atmospheric pressure CVD grown lithium ion-conducting electrolyte |
| US6517968B2 (en) | 2001-06-11 | 2003-02-11 | Excellatron Solid State, Llc | Thin lithium film battery |
| WO2003007556A2 (en) | 2001-07-13 | 2003-01-23 | Nortel Networks Limited | Routing for a communications network |
| KR100641809B1 (en) | 2001-12-28 | 2006-11-02 | 다이니폰 인사츠 가부시키가이샤 | Polyelectrolyte type fuel cell and method for producing the same |
| US20030152829A1 (en) | 2002-02-12 | 2003-08-14 | Ji-Guang Zhang | Thin lithium film battery |
| JP2003249199A (en) | 2002-02-26 | 2003-09-05 | Mitsubishi Materials Corp | Molded body having thin part |
| US6713987B2 (en) | 2002-02-28 | 2004-03-30 | Front Edge Technology, Inc. | Rechargeable battery having permeable anode current collector |
| US6835493B2 (en) | 2002-07-26 | 2004-12-28 | Excellatron Solid State, Llc | Thin film battery |
| JP3789439B2 (en) | 2003-03-03 | 2006-06-21 | Necラミリオンエナジー株式会社 | Film exterior laminated battery pack |
| TW200418220A (en) * | 2003-03-14 | 2004-09-16 | Hon Hai Prec Ind Co Ltd | Method of manufacturing electrode plate of battery |
| CN100392905C (en) | 2003-04-17 | 2008-06-04 | 旭硝子株式会社 | Solid polymer electrolyte membrane, membrane-electrode connector for solid polymer fuel cell, and method for producing solid polymer electrolyte membrane |
| US20050079418A1 (en) | 2003-10-14 | 2005-04-14 | 3M Innovative Properties Company | In-line deposition processes for thin film battery fabrication |
| TWM248123U (en) | 2003-12-02 | 2004-10-21 | Chin Hsen Technology Corp | Improved structure of charging battery circuit |
| TWI244792B (en) | 2004-08-18 | 2005-12-01 | Nan Ya Printed Circuit Board C | Flat panel direct methanol fuel cell and method of making the same |
| TWI243505B (en) | 2004-08-20 | 2005-11-11 | Nan Ya Printed Circuit Board C | Method of manufacturing a flat panel direct methanol fuel cell |
| WO2006063308A2 (en) * | 2004-12-08 | 2006-06-15 | Symmorphix, Inc. | DEPOSITION OF LICoO2 |
| US7959769B2 (en) | 2004-12-08 | 2011-06-14 | Infinite Power Solutions, Inc. | Deposition of LiCoO2 |
| US7471805B2 (en) | 2004-12-20 | 2008-12-30 | Central Coast Patent Agency, Inc. | Hearing aid mechanism |
| CN1307413C (en) | 2005-01-25 | 2007-03-28 | 中国科学院武汉岩土力学研究所 | Method of Femtosecond Laser Cold Cutting of Rock and Soil Porous Media |
| US7846579B2 (en) | 2005-03-25 | 2010-12-07 | Victor Krasnov | Thin film battery with protective packaging |
| WO2006105188A1 (en) | 2005-03-31 | 2006-10-05 | Firefly Energy Inc. | Modular bipolar battery |
| US8162020B2 (en) | 2005-08-24 | 2012-04-24 | Battery Patent Trust | Infra-red thermal imaging of laser welded battery module enclosure components |
| DE102005040542B3 (en) | 2005-08-26 | 2007-04-12 | Siemens Audiologische Technik Gmbh | In-the-ear hearing aid with electronics module |
| JP2009511742A (en) * | 2005-10-13 | 2009-03-19 | ナムローゼ・フェンノートシャップ・ベーカート・ソシエテ・アノニム | Method for depositing a film by sputtering |
| US7620195B2 (en) | 2005-11-09 | 2009-11-17 | Zounds, Inc. | Rechargeable hearing aid |
| KR100913838B1 (en) | 2005-11-30 | 2009-08-26 | 주식회사 엘지화학 | Battery Module of Novel Structure |
| US7862927B2 (en) | 2007-03-02 | 2011-01-04 | Front Edge Technology | Thin film battery and manufacturing method |
| WO2008134053A1 (en) | 2007-04-27 | 2008-11-06 | Front Edge Technology, Inc. | Thin film battery fabrication using laser shaping |
| US7862627B2 (en) | 2007-04-27 | 2011-01-04 | Front Edge Technology, Inc. | Thin film battery substrate cutting and fabrication process |
| US20090010462A1 (en) | 2007-07-02 | 2009-01-08 | Front Edge Technology, Inc. | Compact rechargeable thin film battery system for hearing aid |
| JP5147365B2 (en) | 2007-11-15 | 2013-02-20 | 株式会社日立製作所 | Metal container sealing method |
| JP5354646B2 (en) | 2008-07-31 | 2013-11-27 | Necエナジーデバイス株式会社 | Multilayer secondary battery and manufacturing method thereof |
-
2007
- 2007-09-04 US US11/849,959 patent/US8628645B2/en active Active
-
2013
- 2013-11-25 US US14/089,019 patent/US20140166471A1/en not_active Abandoned
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5522976A (en) * | 1991-09-03 | 1996-06-04 | Societe Nationale Elf Aquitaine | Target component for cathode sputtering |
| US6039850A (en) * | 1995-12-05 | 2000-03-21 | Minnesota Mining And Manufacturing Company | Sputtering of lithium |
| US5833815A (en) * | 1996-04-24 | 1998-11-10 | Anelva Corporation | Sputter deposition system |
| US6338777B1 (en) * | 1998-10-23 | 2002-01-15 | International Business Machines Corporation | Method and apparatus for sputtering thin films |
Cited By (6)
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|---|---|---|---|---|
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| US9905895B2 (en) | 2012-09-25 | 2018-02-27 | Front Edge Technology, Inc. | Pulsed mode apparatus with mismatched battery |
| US9356320B2 (en) | 2012-10-15 | 2016-05-31 | Front Edge Technology Inc. | Lithium battery having low leakage anode |
| US10008739B2 (en) | 2015-02-23 | 2018-06-26 | Front Edge Technology, Inc. | Solid-state lithium battery with electrolyte |
| US10957886B2 (en) | 2018-03-14 | 2021-03-23 | Front Edge Technology, Inc. | Battery having multilayer protective casing |
| GB2597985B (en) * | 2020-08-13 | 2024-07-31 | Dyson Technology Ltd | Method of forming a cathode layer, method of forming a battery half cell |
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| US8628645B2 (en) | 2014-01-14 |
| US20090057136A1 (en) | 2009-03-05 |
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