SOLID STATE FIBER-BASED BATTERY SYSTEM AND METHOD OF FORMING SAME
20180123165 ยท 2018-05-03
Inventors
Cpc classification
Y02P70/50
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B64C3/26
PERFORMING OPERATIONS; TRANSPORTING
Y02T50/60
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
Y02T10/70
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
Y02E60/10
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
H01M50/213
ELECTRICITY
H01M2220/20
ELECTRICITY
Y02T50/40
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
H01M10/0525
ELECTRICITY
International classification
H01M10/0525
ELECTRICITY
H01M10/054
ELECTRICITY
B64C3/26
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A solid state battery system and methods of forming a solid state battery system. The solid state battery system has a plurality of fiber battery cells formed into a pattern. Each fiber battery cell has a fiber inner core which may be a carbon-graphite, carbon-nanotube, boron-nanotube or boron-nitride-nanotube fiber and serves as the anode. In addition, the fiber battery cell has an electrolyte layer formed over the fiber inner core and an outer conductive layer (the cathode) formed over the electrolyte layer. A first terminal is electrically coupled to the fiber inner core of each of the plurality of fiber battery cells. A second terminal is electrically coupled to the outer conductive layer of each of the plurality of fiber battery cells. The solid state battery system may be incorporated into a composite part for a vehicle, such as an aircraft.
Claims
1. A solid state battery system, comprising: a plurality of fiber battery cells formed into a pattern, each fiber battery cell comprising: a fiber inner core; an electrolyte layer formed over the fiber inner core; and an outer conductive layer formed over the electrolyte layer; a first terminal electrically coupled to the fiber inner core of each of the plurality of fiber battery cells; and a second terminal electrically coupled to the outer conductive layer of each of the plurality of fiber battery cells.
2. The solid state battery system of claim 1, wherein the fiber inner core is formed from a carbon-graphite fiber or a carbon-nanotube fiber.
3. The solid state battery system of claim 1, wherein the fiber inner core is formed from boron-nanotube fiber or a boron-nitride-nanotube fiber.
4. The solid state battery system of claim 1, wherein the electrolyte layer is formed from a solid electrolyte.
5. The solid state battery system of claim 4, wherein the solid electrolyte is a glassy material.
6. The solid state battery system of claim 5, wherein the glassy material is a lithium ion conducting material.
7. The solid state battery system of claim 4, wherein the solid electrolyte is a crystalline material.
8. The solid state battery system of claim 7, wherein the crystalline material is beta-Alumina.
9. The solid state battery system of claim 1, wherein the outer conductive layer comprises a magnesium intercalation compound.
10. The solid state battery system of claim 1, wherein the outer conductive layer comprises a lithium intercalation compound.
11. The solid state battery system of claim 1, wherein the outer conductive layer comprises a Group 1 or 2 metal compound.
12. The solid state battery system of claim 1, wherein the plurality of fiber battery cells are formed into a planar configuration having at least one row of fiber battery cells.
13. The solid state battery system of claim 1, wherein the plurality of fiber battery cells are formed into a mesh or weave pattern.
14. The solid state battery system of claim 1, wherein the pattern is a part of a composite part for a vehicle.
15. The solid state battery system of claim 1, wherein the pattern is a part of a wing skin for an aircraft.
16. The solid state battery system of claim 1, wherein the pattern is a part of a spar for an aircraft.
17. A method of forming a solid state battery, comprising the steps of: forming an electrolyte layer over a fiber core; forming an outer conductive layer over the electrolyte layer to form a fiber battery cell; forming a plurality of fiber battery cells into a pattern; electrically coupling a first terminal to the fiber core of each of the fiber battery cells; and electrically coupling a second terminal to the outer conductive layer of each of the fiber battery cells.
18. The method of claim 17, further comprising the step of applying an electrical and/or magnetic field to the electrolyte layer during a curing period after the formation thereof.
19. A method of forming a solid state battery, comprising the steps of: forming an electrolyte layer over a fiber core to form a partial fiber battery cell; forming a plurality of partial fiber battery cells into a pattern; electrically coupling a first terminal to the fiber core of each of the fiber battery cells; and forming an outer conductive layer over the electrolyte layer of each of the partial fiber battery cells.
20. The method of claim 19, further comprising the step of applying an electrical and/or magnetic field to the electrolyte layer during a curing period after the formation thereof.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0011] The following detailed description, given by way of example and not intended to limit the present disclosure solely thereto, will best be understood in conjunction with the accompanying drawings in which:
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DETAILED DESCRIPTION
[0016] In the present disclosure, like reference numbers refer to like elements throughout the drawings, which illustrate various exemplary embodiments of the present disclosure.
[0017] Carbon-graphite fibers, carbon-nanotube fibers, boron-nanotube fibers, and boron-nitride-nanotube fibers and structures formed therefrom have a high stiffness, high tensile strength, low weight, high chemical resistance, high temperature tolerance and low thermal expansion. This makes composite structures formed from carbon-graphite fibers, carbon-nanotube fibers, boron-nanotube fibers, and boron-nitride-nanotube fibers popular for use in aerospace, civil engineering, military, and motorsport applications.
[0018] The present disclosure describes a solid state battery system formed from a plurality of fiber battery cells having a coaxial structure including an inner fiber core that acts as the battery anode, a solid electrolyte layer formed over the inner carbon core, and an outer conductive layer that is formed over the solid electrolyte layer and acts as the battery cathode. By forming a composite fiber structure, at least in part, from a plurality of such fiber battery cells (e.g., in parallel or in a woven pattern), the resultant structure will have all the benefits recited above of a composite structure (since the core of each fiber battery cell is a carbon or boron fiber) and will also act as an energy storage device (battery). This is quite different from a structure formed in layers, with a conventional battery inserted in an inner layer thereof, because the solid state battery system of the present disclosure contributes to the structural integrity of the resultant structure, instead of adding weight and reducing the structural integrity thereof as would occur when a conventional battery is incorporated into an inner layer of a layered structure. It is particularly important to ensure that the structural integrity of the part is maintained when the resultant structure is a composite part for an aircraft, e.g., a wing skin or spar. In addition, the coaxial structure of each fiber battery cell provides a significantly higher surface area than a planar structure, and a structural part including a battery formed from coaxial fiber battery cells will have a much higher energy storage capability than a structural part including an integral internal planar battery.
[0019] Referring now to
[0020] Referring now to
[0021] Referring now to
[0022] Referring now to
[0023] Although the present disclosure has been particularly shown and described with reference to the preferred embodiments and various aspects thereof, it will be appreciated by those of ordinary skill in the art that various changes and modifications may be made without departing from the spirit and scope of the disclosure. It is intended that the appended claims be interpreted as including the embodiments described herein, the alternatives mentioned above, and all equivalents thereto.