CA3130079A1 - Battery containment system - Google Patents
Battery containment systemInfo
- Publication number
- CA3130079A1 CA3130079A1 CA3130079A CA3130079A CA3130079A1 CA 3130079 A1 CA3130079 A1 CA 3130079A1 CA 3130079 A CA3130079 A CA 3130079A CA 3130079 A CA3130079 A CA 3130079A CA 3130079 A1 CA3130079 A1 CA 3130079A1
- Authority
- CA
- Canada
- Prior art keywords
- tray
- containment system
- cover
- shield
- battery containment
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
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- 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
- H01M10/60—Heating or cooling; Temperature control
- H01M10/63—Control systems
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/204—Racks, modules or packs for multiple batteries or multiple cells
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/204—Racks, modules or packs for multiple batteries or multiple cells
- H01M50/207—Racks, modules or packs for multiple batteries or multiple cells characterised by their shape
- H01M50/209—Racks, modules or packs for multiple batteries or multiple cells characterised by their shape adapted for prismatic or rectangular cells
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/218—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by the material
- H01M50/22—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by the material of the casings or racks
- H01M50/227—Organic material
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/218—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by the material
- H01M50/22—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by the material of the casings or racks
- H01M50/229—Composite material consisting of a mixture of organic and inorganic materials
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/218—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by the material
- H01M50/22—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by the material of the casings or racks
- H01M50/231—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by the material of the casings or racks having a layered structure
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/233—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by physical properties of casings or racks, e.g. dimensions
- H01M50/24—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by physical properties of casings or racks, e.g. dimensions adapted for protecting batteries from their environment, e.g. from corrosion
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/233—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by physical properties of casings or racks, e.g. dimensions
- H01M50/242—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by physical properties of casings or racks, e.g. dimensions adapted for protecting batteries against vibrations, collision impact or swelling
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/249—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders specially adapted for aircraft or vehicles, e.g. cars or trains
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/262—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders with fastening means, e.g. locks
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/262—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders with fastening means, e.g. locks
- H01M50/264—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders with fastening means, e.g. locks for cells or batteries, e.g. straps, tie rods or peripheral frames
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/271—Lids or covers for the racks or secondary casings
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/271—Lids or covers for the racks or secondary casings
- H01M50/273—Lids or covers for the racks or secondary casings characterised by the material
- H01M50/278—Organic material
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/271—Lids or covers for the racks or secondary casings
- H01M50/273—Lids or covers for the racks or secondary casings characterised by the material
- H01M50/282—Lids or covers for the racks or secondary casings characterised by the material having a layered structure
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/289—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by spacing elements or positioning means within frames, racks or packs
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M2220/00—Batteries for particular applications
- H01M2220/20—Batteries in motive systems, e.g. vehicle, ship, plane
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- 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
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Manufacturing & Machinery (AREA)
- Composite Materials (AREA)
- Inorganic Chemistry (AREA)
- Materials Engineering (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
Description
RELATED APPLICATIONS
[0001] This application claims priority benefit of US Provisional Application Serial Number 63/047,951 filed July 3, 2020; the contents of which are hereby incorporated by reference.
FIELD OF THE INVENTION
BACKGROUND OF THE INVENTION
Composite materials are materials made from two or more constituent materials with significantly different physical or chemical properties, that when combined, produce a material with characteristics different from the individual components. The individual components remain separate and distinct within the finished structure. A composite material may be preferred for reasons that include materials which are stronger, lighter, or less expensive when compared to traditional materials of steel or aluminum. Still another advantage over metals is reduced corrosion, leading to longer operational life and reduced maintenance costs.
Date Recue/Date Received 2021-09-07
Date Recue/Date Received 2021-09-07
SUMMARY OF THE INVENTION
cover is includes having a cover body portion and a first flange extending from the cover body portion, the cover body portion configured to overlie the cavity within the tray and the walls of the tray, the first flange of said cover configured to extend beyond the walls of the tray. A shield having a shield body portion and a second flange extending from the shield body portion, the shield body portion is configured to underlie the bottom of the tray, the second flange of the shield is configured to extend beyond the bottom of the tray and configured to engage the first flange of the cover.
BRIEF DESCRIPTION OF THE DRAWINGS
Date Recue/Date Received 2021-09-07
with reference lines detailing angle a;
Date Recue/Date Received 2021-09-07
FIG. 16 is a cross sectional view of a cover and a shield of a battery containment system according to embodiments of the present invention;
Date Recue/Date Received 2021-09-07
and
DESCRIPTION OF THE INVENTION
energy absorber to protect the battery from forces during potential impacts with other vehicles or Date Recue/Date Received 2021-09-07 objects. Additionally, because of the position and size of a battery case on vehicles, the batteries are susceptible to impalement from road or collision debris. Therefore, according to embodiments, the inventive battery containment system includes a shield that is designed to resist such impalements in order to protect the batteries. Furthermore, because vehicle batteries are prone to extreme fire in the event of an impact or impalement, embodiments of the present inventive containment system provide a sealed battery environment to keep fluid and moisture out during normal operation and to limit oxygen in the event of a battery fire.
Hence, the following specification is intended to illustrate some particular embodiments of the invention, and not to exhaustively specify all permutations, combinations, and variations thereof.
Date Recue/Date Received 2021-09-07
It is appreciated that the relative placement of an inventive system 10 on a vehicle largely dictates the need for additional impact resistance. By way of example, a system 10 surrounded by a vehicle chassis has reduced or no need for energy absorption components, while in contrast, placement under a vehicle side door has a considerable need to inhibit impact induced intrusion into the contained volume of a system 10.
The filler material 202 is any of glass fibers, carbon fibers, natural fibers, hollow or solid glass microspheres, or a combination thereof. The fibers may be oriented or non-oriented. In some inventive embodiments in which SMC forms the high gloss surface, a resin package sold by Continental Structural Plastics, Inc. under the tradenames TCAO. Exemplary formulations of which are detailed in U.S. 7,700,670;
W02017/184761; and U.S. 7,524,547B2. It is appreciated that the surface sheets 176 or 178 routinely includes additives to retain dimensionality. Such additives routinely including glass fiber; carbon fiber; inorganic particulate fillers such as calcium carbonate, talc, and carbon black;
glass microspheres; carbon nanotubes; graphene; low profile additives;
moisture scavengers; and combinations thereof. Typical thicknesses of the high gloss surface sheet in the present invention range from 0.5 to 5 millimeters (mm) without regard to edges.
The walls extend from one side of the bottom 22 of the tray 20. The walls and the bottom 22 define a cavity 28 within the tray 10. The first and second energy absorption components 30, 30' are attached to the bottom 22 of the tray 20 external to the cavity 28. That is, a first of the energy absorption components 30 is attached to the bottom 22 of the tray 20 external to the first side wall Date Recue/Date Received 2021-09-07 24 while the second energy absorption component 30' is attached to the bottom 22 of the tray 20 external to the second side wall 24'. It is appreciated that the tray 20 is readily formed of traditional SMC or an open areas core sandwich structure as detailed in co-owned application publication W02020/117717A1. It is further appreciated that in the formation of a tray 20 or cover 40 in some inventive embodiments that there is no need for a high gloss surface and instead is provided with a skin to enhance a property such as impact resistance, or fire retardency.
An open area core, such as that depicted at 174 is formed of a lightweight material that defines a plurality of pores 186 so as to reduce the overall density of the open area core 174. An open area core according to the present invention is formed from a variety of materials that include Date Recue/Date Received 2021-09-07 cellulosics such as corrugated fiberboard, paper board, paper stock;
thermoplastics such as poly(methyl methacrylate) (PMMA), acrylonitrile butadiene styrene (ABS), polyamides, polylactides, polybenzimidazoles, polycarbonates, polyether sulfones, polyethylene, polypropylene, polystyrene, polyvinyl chloride, and block copolymers of any one of the aforementioned where at least one of the aforementioned makes up the majority by weight of the copolymer and regardless of the tacticity of the polymer or copolymer;
thermosets such as polyesters, polyureas, polyurethanes, polyurea/polyurethanes, epoxies, vinyl esters; metal such as aluminum, magnesiumõ and alloys of any one of the aforementioned where at least one of the aforementioned metals constitutes the majority by weight of the alloy; a foam formed from polyurethane, polyethylene, ethylene vinyl acetate, polypropylene, polystyrene, polyvinyl chloride, oraerogels, regardless of whether the foam is open-celled or closed-celled.
Alternatively, metals or polymers are plasma treated to modify surface energies to facilitate adhesion thereto.
In certain inventive embodiments, the ratio of the thickness of a wall 188 to the maximal linear extent between faces 177 and 177' is between 0.01-10:1. A wall thickness ranges from 0.1 mm to 100 mm in such inventive embodiments.
Date Recue/Date Received 2021-09-07
According to some inventive embodiments, a fire retardant or intumescent layer 191 is attached to the exposed surface 193 of the first surface 176.
Date Recue/Date Received 2021-09-07
The shield 80 includes a shield body portion 82 and a second flange 86 that extends from the shield body portion 82. As shown in FIG. 1, the shield body portion 82 of the shield 80 may include a plurality of walls 84 from which the flange 85 extends such that the flange and the shield body portion 82 are in separate planes. According to embodiments, the second flange 86 of the shield 80 extends from the shield body portion 82 such that the shield 80 is a substantially planar component. The shield body portion 82 of the cover is configured to underlie the bottom 22 of the tray 20. The second flange 86 of the shield 80, which extends from the shield body portion 82, is configured to extend beyond the bottom 22 of the tray 20. Additionally, the second flange 86 of the shield 80 is configured to engage the first flange 96 of the cover 40.
Date Recue/Date Received 2021-09-07
That is, according to embodiments, the tray 20, the energy absorption components 30, 30', the cover 40, the shield 80, or a combination thereof are coated in a fire resistant, or a fire-retardant material. A fire-resistant material is one that is designed to resist burning and withstand heat and provide insulation to the substrate, while a fire-retardant material is designed to burn slowly and reduce the rate of flame spread. Intumescent fire-resistant materials work by expanding their volume from 15 to 30 times and generating an ash-like char layer that erodes as fire exposure continues. Expansion then occurs again with the number of times the process repeats itself dependent upon the thickness of the coating. For example, such fire resistant or fire retardant materials for packing in voids 34 or coating any of the tray 20, the energy absorption components 30, 30', the cover 40, and the shield 80 include any of the following:
silicone, casein or vinyl resins, aluminum trihydrate or antimony oxide, ammonium polyphosphate, pentaerythritol, melamine derivatives, boric acid (H3B03) and borax (Na2B407.10}120), disodium octaborate tetrahydrate (Na2B8013.4H20), dicyandiamide-formaldehyde-phosphoric acid, melamine-dicyandiamide-formaldehyde-phosphoric acid, poly(n-vinylpyrolidone), colloidal silica, magnesium hydroxide (MDH), monoammonium phosphate (MAP), aluminum hydroxide (ATH), carbonates and hydrogen carbonates, potassium carbonate, Na2W04, Na2Sn03, Na2Mo04, ammonium polyphosphate, pentaerythritol, melamine, expandable graphite, or combinations thereof. Phenolic resins operative herein illustratively includes epoxy phenolic resins, and phenol formaldehyde resins that impart corrosion resistance and a mar resistance surface relative to the underlying substrate of the system 10. EMI-RFI shielding coatings operative herein illustratively include nickel coated glass mat; carbon fiber matting; copper or nickel paint;
various metal foils, such as aluminum, nickel, iron, copper, and alloys thereof; and or combinations thereof with the proviso that the EMI-RFI shielding is grounded so as to function as a Faraday cage. It is further Date Recue/Date Received 2021-09-07 appreciated that coatings 35 in the form of sheets are readily applied as an underlying sheet below an inventive system 10 or are included as filler in the materials that are used to form the tray 20, the cover 40, and the shield 80.
Sheet molding compound (SMC) or sheet molding composite is a ready to mold fiber-reinforced polyester material primarily used in compression molding. SMC is a reinforced composite material that is manufactured by dispersing long strands (20-60 mm) of chopped glass fibers in a matrix of polyester resin. It is appreciated that fibers with long range order are also operative herein and include woven mats, continuous fibers, or sheet forms.
Thermoplastic materials operative herein amenable to functioning as a fiber matrix illustratively include: poly(methyl methacrylate) (PMMA), acrylonitrile butadiene styrene (ABS), polyamides, polylactides, polybenzimidazoles, polycarbonates, polyether sulfones, polyethylene, polypropylene, polystyrene, polyvinyl chloride, or block copolymers of any one of the aforementioned constituting the majority by monomer number. Reinforcing fibers and fillers operative herein illustratively include carbon fibers, glass fibers, aramid fibers, cellulosic fibers, or a combination thereof. In some inventive embodiments, the chopped fiber is glass fiber, alone or in combination with other types of fiber or reinforcing fillers. According to embodiments, the cover 40 is formed of glass fiber reinforced SMC. As noted above, a coating 35 is readily applied to a cover 40 in some inventive embodiments.
According to embodiments, the material forming the cover 40 includes an EMI-RFI shielding filler which illustratively include nickel coated glass mat; carbon fiber matting;
copper or nickel paint;
Date Recue/Date Received 2021-09-07 various metal foils, such as aluminum, nickel, iron, copper, and alloys thereof; and or combinations thereof with the proviso that the cover 40 is grounded so as to function as a Faraday cage.
According to certain inventive embodiments, the shield 80 is formed of reinforced sheet molding compound (SMC), a phenolic-SMC, epoxy, acrylonitrile butadiene styrene (ABS), polycarbonate, random-oriented fiber reinforced thermoplastic resin (FRTP), steel, or aluminum.
Sheet molding compound (SMC) or sheet molding composite is a ready to mold fiber-reinforced polyester material primarily used in compression molding. SMC is a reinforced composite material that is manufactured by dispersing long strands (20-60 mm) of chopped glass fibers in a matrix of polyester resin. It is appreciated that fibers with long range order are also operative herein and include woven mats, continuous fibers, or sheet forms.
Thermoplastic materials operative herein amenable to functioning as a fiber matrix illustratively include: poly(methyl methacrylate) (PMMA), acrylonitrile butadiene styrene (ABS), polyamides, polylactides, polybenzimidazoles, polycarbonates, polyether sulfones, polyethylene, polypropylene, polystyrene, polyvinyl chloride, or block copolymers of any one of the aforementioned constituting the majority by monomer number. Reinforcing fibers and fillers operative herein illustratively include carbon fibers, glass fibers, aramid fibers, cellulosic fibers, or a combination thereof. In some inventive embodiments, the chopped fiber is glass fiber, alone or in combination with other types of fiber or reinforcing fillers. According to embodiments, the shield 80 is formed of aramid fiber reinforced SMC, which is particularly well suited for resisting impalement by crash or road debris. As noted above, a coating 35 is readily applied to a shield 80 in some inventive embodiments. According to embodiments, the material forming the shield 80 includes an EMI-RFI shielding filler which illustratively include nickel coated glass mat; carbon fiber matting; copper or nickel paint; various Date Recue/Date Received 2021-09-07 metal foils, such as aluminum, nickel, iron, copper, and alloys thereof; and or combinations thereof with the proviso that the shield 80 is grounded so as to function as a Faraday cage.
According to certain inventive embodiments, the tray 20 further includes internal divider walls 29, which divide the cavity 28 into sections of sub-cavities. The internal divider walls 29 extend from the bottom 22 of the tray 20 between the first side wall 24 and the second side wall 24'. It will be appreciated that the internal divider walls 29 could alternatively or additionally span between the first end wall 26 and the second end wall 26'. The internal divider walls 29 provide additional structural rigidity to the battery containment system 10 and provide support to batteries 50 positioned within the tray 20 to limit shifting of the batteries 50 within the tray 20. According to embodiments, the tray 20 also includes a through hole 27 defined in at least one of the walls 24, 24', 26, 26'. The through hole 27 allows a wire or cable 52 to be passed therethrough, such as a high voltage wire 52 for connecting the batteries 50 contained within the battery containment system 10 to the other systems of the hybrid or electric vehicle systems. In FIG. 1, the through hole 27 is defined in the first end wall 26; however it will be understood that a through hole 27 may be provided in any of the plurality of walls 24, 24', 26, 26', the cover 40, or the bottom 22 of the tray 20 based on design requirements and routing of a high voltage wire 52 for connecting the batteries 50 to other systems of the hybrid or electric vehicle.
Date Recue/Date Received 2021-09-07
According to certain inventive embodiments, the energy absorption components 30, 30' are formed of a carbon fiber reinforced thermoplastic known as SEREEBO(R)', having composition including Carbon fibers "Tenax" (registered trademark) STS40-24KS (average fiber diameter: 7 µm, single yarn number: 24,000) manufactured by Teijin., Ltd., which had been cut to an average fiber length of 20 mm were used as carbon fibers. Nylon-6 resin A1030 manufactured by Unichika, Ltd. was used. In accordance with the method described in U.S. Pat.
No. 8,946,342, there was manufactured a molding material precursor of the carbon fibers and the Nylon-6 resin, in which the carbon fibers had been randomly oriented in two-dimensions. The obtained molding material precursor was heated at 2.0 MPa for 5 minutes with a pressing device heated to 260 degree C. to obtain a CFRTP material.
Date Recue/Date Received 2021-09-07
4B, 4C, and 4D), an open semi-circle (FIG. 4F), and open semi oval (FIG. 4G), an open triangle (FIG. 4K), an open semi square (FIG. 4M), and open semi rectangle (FIG. 4R), and a sine wave (FIG. 40). As shown in FIGS. 4H, 41, 4J, 12A, and 12B the first and second energy absorption components 30, 30' are extruded or roll formed elongated forms with a continuous cross section. In some inventive embodiments, the continuous forms 30, 30' have internal partitions 170, 170' and in still other inventive embodiments, one or more of the compaiiments formed therein is filled with an energy absorbing foam to enhance the impact protection of the battery compartment against collision induced intrusions. Foams operative herein for beam filling illustratively include polyvinylchloride; polyurethanes; and those detailed in Canadian Pat. No.
860,386; and U.S. Pat.
No. 4,158,087.
measured from a first end to a second end, however the length L is not shown in all of the figures for clarity. FIGS.
5A-5R show end view of each of the first and second energy absorption components 30, 30' show in FIGS. 4A-4R, respectively. As shown in FIG. 5A the first and second energy absorption Date Recue/Date Received 2021-09-07 components 30, 30' have a width W and a height H. As with the length L, it will be understood that the width W and height H have not been shown in all of the figures for clarity. According to certain inventive embodiments, the length L of each energy absorption component 30, 30' is 5 to 5000 mm, the width W is 5 to 100 mm, and the height H is 5 to 100 mm. The length, L, width W, and height H of each energy absorption component 30, 30' generally corresponds to the overall length of the tray 20, height of the side walls 24, 24', and the width of a lip of the bottom 22 that extends beyond the walls 24, 24', 26, 26' of the tray 20 onto which the energy absorption components 30, 30' are attached.
and 6B, which are detailed views of FIGS. 4A and 4B. Wall angle a is shown in FIGS. 7B-7C
and 15. Notably, the component shown in FIG. 7A is the same as the component shown in FIG. 4B.
It will be understood that these dimensions are applicable to the various shapes of the first and second energy absorption components 30, 30' shown throughout FIGS. 4A-4R, but are not labeled in each figure for clarity. For example, as best shown in the exemplary shapes of FIGS. 4B, 4C, and 4D, the length 1 of each repeated shape and the distance d between each repeated shape can be increased or decreased to vary the strength characteristics of the first and second energy absorption components 30, 30'. According to certain inventive embodiments, the distance d between the repeated shapes is 0 to 300 mm. According to certain inventive embodiments, the length of each Date Recue/Date Received 2021-09-07 repeated shape is 20 to 300 mm. According to certain inventive embodiments, the pitch is 45 to 120 degrees. According to certain inventive embodiments, the thickness Ti is 0.25 to 5 mm and the thickness T2 is 0.25 to 10 mm in the case of steel. In the case of a carbon fiber composite material, thickness Ti is preferably 7 to 13 mm, and thickness T2 is preferably 14 to 24 mm.
According to certain inventive embodiments, the thickness T2 is two times the thickness to Ti.
According to certain inventive embodiments, the wall angle a or tilt inward toward the voids 34 of the upward extensions of the repeated shapes is 0 to 25 degrees. For example, in FIG. 7A the wall angle a is 0 degrees, in FIG. 7B the wall angle a is 5 degrees, and in FIG. 7C the wall angle a is 12.5 degrees.
According to certain inventive embodiments, an adhesive 67 is applied between the cross member 66 (or other members of the frame 60) and the second side of the tray 20. Batteries 50 are shown positioned on opposite sides of the internal divider wall 29 within the tray 20. According to certain inventive embodiments, the batteries 50 sit in direct contact with the bottom 22 of the tray 20. In further inventive embodiments, an intermediate layer of material, for example foam or another suitable Date Recue/Date Received 2021-09-07 shock absorbing material, is positioned between the batteries 50 and the tray 20, along the bottom 22 or the walls 24, 24', 26, 26' of the tray 20. As shown in FIG. 8, embodiments of the inventive battery containment system 10 include a temperature regulation system 70 that can be positioned around or near the batteries. The temperature regulation system 70 may include a water or coolant circulation system or a phase change material. As shown, the temperature regulation system 70 is posited in a downward protrusion formed in the bottom 22 of the tray 20, such that the batteries 50 are positioned on top of the temperature regulation system 70. According to certain inventive embodiments, the batteries 50 are held in a secured position by a bracket 54 that is secured to the tray 20 by a fastener 56. As shown in FIG. 8, the cover 40 is positioned above the batteries 50 and the shield 80 is positioned under the bottom 22 of the tray 20.
Date Recue/Date Received 2021-09-07 9, the shield 80 includes walls 84 that extend from the body portion 82 of the shield 80 and from which the second flange 86 extends. The first flange 96 and the second flange 86 engage one another in an abutting relationship and are joined together by a joiner clip 100. According to embodiments, a cushioning or shock absorbing material 44 such as foam is provided between the cover 40 and the batteries 50.
FIG. 16 shows a cross sectional view of a cover 40 and a shield 80 of the present invention joined together by a joiner clip 100. In FIG. 16, the tray 20 of the inventive battery containment system 10 is not shown for clarity. As shown, joiner clip 100 having a C-shaped cross section joins the cover 40 and the shield 80 together. The cover 40, the shield 80, and the joiner clip 16 are configured to be assembled around the tray 20 in such a way as to form a high strength, light weight containment system 10 that provides impalement resistance, impact resistance, fire resistance, and fluid penetration prevention to contents contained within the construct 10, which according to embodiments is a plurality of batteries 50.
Date Recue/Date Received 2021-09-07
silicone, casein or vinyl resins, aluminum trihydrate or antimony oxide, ammonium polyphosphate, pentaerythritol, melamine derivatives, boric acid (H3B03) and borax (Na2B407.10}120), disodium octaborate tetrahydrate (Na2B8013.41120), dicyandiamide-formaldehyde-phosphoric acid, melamine-dicyandiamide-formaldehyde-phosphoric acid, poly(n-vinylpyrolidone), colloidal silica, magnesium hydroxide (MDH), monoammonium phosphate Date Recue/Date Received 2021-09-07 (MAP), aluminum hydroxide (ATH), carbonates and hydrogen carbonates, potassium carbonate, Na2W04, Na2Sn03, Na2Mo04, ammonium polyphosphate, pentaerythritol, melamine, expandable graphite, or combinations thereof. Phenolic resins operative herein illustratively includes epoxy phenolic resins, and phenol formaldehyde resins that impart corrosion resistance and a mar resistance surface relative to the underlying substrate of the construct 10.
Similarly, according to embodiments, the second flange 86 surrounds the perimeter of the shield 80. According to embodiments, such as those shown in FIGS. 17A, 17B, 19A, and 19B, the flanges 96, 86 are each continuous in that they entirely cover the perimeter of the cover 40 and shield 80, respectively. According to other embodiments, such as those shown in FIGS.
18A, 18B, and 19C, the flanges 96, 86 are each made up of separate and discrete flange portions that non-continuously surround the cover 40 and shield 80, respectively. According to embodiments, in which the flanges 96, 86 are continuous and entirely surround the cover 40 and shield 80, the joiner clip 100 is either a single continuous joiner clip, as shown in FIG. 19A, that also entirely surrounds the cover 40 and shield 80, or the joiner clip 100 is a plurality of separate and discrete joiner clips, as shown in FIG. 19B, positioned at separate locations along the first flange 96 and the second flange 86 to non-continuously surround the cover 40 and the shield 80. According to embodiments, in which the flanges 96, 86 are each made up of separate and discrete flange portions that non-continuously surround the respective cover 40 and shield 80, the joiner clip 100 is a plurality of separate and discrete joiner clips positioned at separate locations along the first flange 96 and the second flange 86 to non-continuously surround the cover 40 and shield 80, as shown in FIG.
19C.
According to embodiments, one or both of the jaws 134, 134' are straight or feature a curve such that the free ends 136, 136' of each of the jaws 134, 134' are flared away from one another, such as shown in FIGS. 20A and 20C-5D and 20B, respectively. The flared free ends 136, 136' facilitate easy application of the joiner clip 100 onto the flanges 96, 86. That is, to apply the joiner clip 100, the flanges 96, 86 are positioned between the free ends 136, 136' of the joiner clip and the joiner clip 100 is pushed or pounded onto the flanges 96, 86, thereby eliminating the need for a special tool for separating the jaws 134, 134'. The flared free ends 136, 136' also reduce wear on the composite material of the flanges 96, 86 by ensuring that the free ends 136, 136' do not rub on the flanges 96, 86.
According to embodiments, the free ends 136, 136' of each of the jaws 134, 134' are biased toward one another. Thus, when the joiner clip 100 is engaged with the flanges 96, 86, such that the flanges 96, 86 are positioned between the jaws 134, 134' of the joiner clip 100, the joiner clip applies a compressive force to the first flange 96 and the second flange 86 to join the cover 40 and the shield 80 together. According to embodiments, the joiner clip is formed of a metal, such as spring steel, a thermoplastic, or an elastomeric material. Embodiments in which the joiner clip is formed of an elastomeric material provide the additional benefit of sealing the cover 40 and shield 80 while also joining them together. According to embodiments, the joiner clip 100 also includes at least on barb positioned on an inner surface of at least one of the jaws 134, 134'. The barb or barbs 138 are configured to dig into the composite material of the flanges 96, 86 or may engage with a groove 140 formed in the flanges to prevent the joiner clip 100 from falling off of or being easily removed from the flanges 96, 86.
Date Recue/Date Received 2021-09-07
According to embodiments, the containment construct 10 also includes a barrier material 128 positioned between the first flange 96 and the second flange 86. According to embodiments, the barrier material 128 acts as a seal and/or a connector between the first cover 40 and the shield 80 to limit movement or slippage between the cover 40 and the shield 80.
According to embodiments, the barrier material 128 is any of an adhesive, a gasket, or a connector. In some embodiments, such as that shown in FIG. 16, at least one of the first flange 96 and second flange 86 define a channel 130 that is configured to receive and retain the barrier material 128. The channel 130 may be a continuous channel or may be a plurality of discrete channels spaced along the length of the flanges 96, 86 at spaced apart positions. According to embodiments in which at least one of the flanges 96, 86 includes a channel, the barrier material 128 is placed in the channel 130 before the flanges 96, 86 are brought into contact with one another.
According to embodiments, in which both flanges 96, 86 define a channel 130 therein, the barrier material 128 is placed in the channel 130 of for example the first flange 96 and then the second flange 86 is brought into contact with the first flange 96 and the barrier material. In such embodiments, the barrier material 128 can be used as a position locator for ensuring that the first flange 96 and second flange 86 are properly positioned relative to one another. Additionally, once assembled, the barrier material 128 ensures that the cover 40 and the shield 80 remain properly positioned relative to one another during use, by preventing slippage, which in turn reduces wear on the parts. It will also be understood that when the barrier material 128 is a gasket, the barrier material may act to seal the cover 40 and shield 80 in water tight engagement and act to locate and retains the cover 40 and shield 80 relative to one another.
According to embodiments, the ramp 156 extends the entire length of the first end 148 of the shield body portion 142, that is the ramp 156 extends from the first end 148 of said shield body portion 142 from the first side 152 to the second side 154 of said shield body portion 142.
According to embodiments, the puncture resistant shield 80 is configured to be attached to a battery containment system 10 such that first ramp 156 is positioned towards a front of the vehicle.
According to embodiments, first ramp 156 is configured to be angled upwards towards said battery containment system 10 when said puncture resistant shield 80 is attached to the battery containment system 10. Such positioning and orientation of the first ramp 156 of the shield 80 allows the ramp 156 to further protect batteries 50 contained in the containment system 10 by deflecting road and crash debris that the vehicle may encounter when traveling in a forward direction.
According to embodiments, the shield 80 additionally includes at least one additional ramp extending from at least one of the second end 150, the first side 152, and the second side 154 of the shield body portion 142.
According to embodiments, the puncture resistant shield 80 is configured to be attached to the battery containment system 10 using an adhesive 160 applied between the first surface 144 of the shield body portion 142 and a lower surface 22 of the of the tray 20.
According to embodiments, the puncture resistant shield 80 is configured to be attached to the battery containment system 10 by a plurality of fasteners 162, 162' that extend through said shield body portion 142 through a plurality of through holes formed in said shield body portion 142. According to embodiments, such through holes may be formed in the material of the shield body portion 142 Date Recue/Date Received 2021-09-07 when the SMC material is laid up or may be formed subsequently by a drilling or stamping process.
The plurality of fasteners 162 for example may include screws or bolts that are inserted through the shield body portion 142 such that the threaded end is secured within the battery containment system 10. Alternatively, the plurality of fasteners 162' for example may include bolts that have their heads embedded in the battery containment system and their threads exposed downward for insertion through the holes formed in the shield body portion 142. In such an instance, nuts 166 or other suitable securing devices are installed onto the threaded portions of the embedded bolts 162' to secure the shield 80 to the battery containment system 10.
Examples
These battery containment systems 10 were subjected to impact testing using a quasi-static load by a 10 inch (25 cm) diameter rigid column located at the center of the system and traveling perpendicular into a predominate longitudinal or lateral edge of the battery containment system 10 as shown in the schematic in FIG. 11.
impacts at an impact angle of 90 degrees. As shown in Table 1, different repeating shapes are tested as well as different Date Recue/Date Received 2021-09-07 thicknesses Ti and T2 and pitches p. The mass of each component and the deformation results of the impact testing are reported in Table 1.
Table 1 Analysis Shape / Ti mm T2 mm Mass kg pitch mm Deformation File Reference mm FIG.
EA-1 FIG. 4A 0.73 1.46 1.33 104.5 11.9 EA-2 FIG. 4B 0.93 1.33 207.8 18.3 EA-3 FIG. 4C 1.01 - 1.33 323.3 28.4 EA-4 FIG. 4D 1.11 1.33 577.3 49.6 EA-5 FIG. 4E 0.71 1.41 1.33 90 8.1 EA-7 FIG. 4F 0.89 1.33 180 16.3 EA-12 FIG. 4G 1.08 - 1.32 360 44 EA-9 FIG. 4H 0.22 - 1.33 >70 EA-10 FIG. 41 0.26 - 1.33 - >70 EA-11 FIG. 4J 0.23 - 1.33 >70 EA-2 FIG. 4B 0.930 - 1.33 207.8 18.3 EA-9-2 FIG. 4H 0.620 - 3.77 18.4 EA-10-2 FIG. 41 0.690 - 3.55 - 18.4 EA-11-2 FIG. 4J 0.790 - 4.68 - 18.2
In a second example, battery containment systems 10 including energy absorption components 30, 30' formed of steel (SPFC590) having an open hexagon repeating shape are tested to compare the effects of varying the wall angle a. In this example, the containment systems are subjected to 250 J impacts at an impact angles of 90 and 75 degrees. As shown in Table 2, in this example the thicknesses Ti and T2, pitch p, and mass are generally unchanged.
The deformation results of the impact testing are reported in Table 2.
Date Recue/Date Received 2021-09-07 Table 2 Analysis Shape / ti mm Mass kg pitch Deformation wall Impact file Reference mm mm angle angle FIG.
EA-2 FIG. 7A 0.93 1.33 207.8 18.3 0 90 (FIG. 4B) EA-13 FIG. 7B 0.93 1.33 207.8 19.5 5 90 EA-14 FIG. 7C 0.92 1.33 207.8 19.7 12.5 90 EA-2- FIG. 7A 0.93 1.33 207.8 19.8 0 75 obli (FIG. 4B) EA-13- FIG. 7B 0.93 1.33 207.8 19.4 obli EA-14- FIG. 7C 0.92 1.33 207.8 19.9 12.5 75 obli 100931 In a third example, battery containment systems 10 including energy absorption components 30, 30' formed of steel (SPFC590), aluminum (A5052), and CFRTP
(Teijin-SEREEBOO) having various geometries are tested for comparison. In this example, the containment systems are subjected to 250 J impacts at an impact angle of 90 degrees. Table 3 reports the details of the different geometries tested and resulting impact deformations for each material.
Date Recue/Date Received 2021-09-07 Table 3 Analysis Shape/ Material ti t2 Mass pitch Deformation file Reference mm mm kg mm mm FIG.
EA-1-2 FIG. 4A Steel (SPFC590) 0.33 0.66 0.60 104.5 18.2 EA-2 FIG. 4B Steel (SPFC590) 0.93 -1.33 207.8 18.3 EA-11-2 FIG. 4J Steel (SPFC590) 0.79 - 4.68 - 18.2 EA-1-Al FIG. 4A Aluminum(A5052) 0.82 1.64 0.52 104.5 18.6 EA-2-Al FIG. 4B Aluminum (A5052) 1.90 - 0.94 207.8 18.7 EA-9-Al FIG. 4H Aluminum(A5052) 0.95 - 2.00 - 18.8 EA-1-Se FIG. 4A CFRTP(Teijin- 1.40 2.80 0.45 104.5 17.9 SEREEBOO) EA-2-Se FIG. 4B CFRTP(Teijin- 3.00 - 0.75 207.8 18.7 SEREEBOO) [0094] In a fourth example, like the third example, battery containment systems 10 including energy absorption components 30, 30' formed of steel (SPFC590), aluminum (A5052), and CFRTP (Teijin-SEREEBOO) having various geometries are tested for comparison.
In this example, the containment systems are subjected to 250 J impacts at an impact angle of 90 degrees.
Table 4 reports the details of the different geometries tested and resulting impact deformations for each material.
Date Recue/Date Received 2021-09-07 Table 4 Analysis Shape / Material Ply Percent ti Mass pitch Deformation file Reference of mm kg mm mm FIG. O'ply EA-2 FIG. 4B Steel - - 0.93 1.33 207.8 18.3 (SPFC590) EA-11-2 FIG. 4J Steel - - 0.79 4.68 - 18.2 (SPFC590) EA-2-Al FIG. 4B aluminum - - 1.90 0.94 207.8 18.7 (A5052) EA-9-Al FIG. 4H aluminum - - 0.95 2.00 - 18.8 (A5052) EA-2-Se FIG. 4B CFRTP - - 3.00 0.75 207.8 18.7 (Teijin-SEREEBO(R)) EA-2- FIG. 4B CFRP(DSM, [0/45/- 50 1.92 0.51 207.8 17.7 CFRP PA410) 45]s EA-9- FIG. 4H CFRP(DSM, [0/90]s 25 0.80 0.90 - 17.6 CFRP PA410) EA-2- FIG. 4B GFRP(DSM, [0/45/- 50 2.72 0.85 207.8 17.9 GFRP PA410) 45]s EA-9- FIG. 4H GFRP(DSM, [0/90]s 25 1.12 1.49 - 18.5 GFRP PA410) [0095] In a fifth example, battery containment systems 10 including energy absorption components 30, 30' formed of CFRP (DSM, PA410) having a repeating open hexagon shape and an extruded rectangular shape of various geometries are tested for comparison of ply. In this example, the containment systems are subjected to 250 J impacts at an impact angle of 90 degrees.
The results of these tests are shown in Table 5.
Date Recue/Date Received 2021-09-07 Table 5 Analysis Shape / Material Ply Percent ti Mass pitch Deformation file Reference of O'ply mm kg mm mm FIG.
EA-2- FIG. 4B CFRP 0 100 5.000 1.33 207.8 33.6 EA-2- FIG. 4B CFRP [0/90]s 50 5.000 1.33 207.8 5.7 EA-2- FIG. 4B CFRP [0/45/- 50 5.000 1.33 207.8 5.1 CFRP-3 45]s EA-2- FIG. 4B CFRP [0/45/- 75 5.000 1.33 207.8 5.6 CFRP-4 45]s EA-2- FIG. 4B CFRP [0/45/- 25 5.000 1.33 207.8 5.2 CFRP-5 45]s EA-2- FIG. 4B CFRP [45/- 0 5.000 1.33 207.8 6.4 CFRP-6 45]s EA-9- FIG. 4H CFRP 0 100 1.180 1.33 - >70 EA-9- FIG. 4H CFRP [0/90]s 50 1.180 1.33 - 15.8 EA-9- FIG. 4H CFRP [0/45/- 50 1.180 1.33 - 19.7 CFRP-3 45]s EA-9- FIG. 4H CFRP [0/90]s 75 1.180 1.33 - 22.6 EA-9- FIG. 4H CFRP [0/90]s 25 1.180 1.33 - 9.9 EA-9- FIG. 4H CFRP 90 0 1.180 1.33 - >70 [0096] Patent documents and publications mentioned in the specification are indicative of the levels of those skilled in the art to which the invention pertains. These documents and publications are incorporated herein by reference to the same extent as if each individual document or publication was specifically and individually incorporated herein by reference.
[0097] The foregoing description is illustrative of particular embodiments of the invention but is not meant to be a limitation upon the practice thereof. The following claims, including all equivalents thereof, are intended to define the scope of the invention.
Date Recue/Date Received 2021-09-07
Claims (20)
a unitary battery tray having a bottom and a plurality of walls including a first side wall, a second side wall, a first end wall, and a second end wall, the plurality of walls extending from the bottom of said tray and defining a cavity within said tray;
a cover having a cover body portion and a first flange extending from the cover body portion, the cover body portion configured to overlie the cavity within said tray and the plurality of walls of said tray, the first flange of said cover configured to extend beyond the plurality of walls of said tray; and a shield having a shield body portion and a second flange extending from the shield body portion, the shield body portion configured to underlie the bottom of said tray, the second flange of said shield configured to extend beyond the bottom of said tray and configured to engage the first flange of said cover.
Date Recue/Date Received 2021-09-07
Date Recue/Date Received 2021-09-07
Date Recue/Date Received 2021-09-07
Date Recue/Date Received 2021-09-07
Applications Claiming Priority (3)
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| US17/463,840 | 2021-09-01 | ||
| US17/463,840 US12046767B2 (en) | 2020-07-03 | 2021-09-01 | Battery containment system |
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| CA3130079A1 true CA3130079A1 (en) | 2023-03-01 |
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| CA3130079A Pending CA3130079A1 (en) | 2020-07-03 | 2021-09-07 | Battery containment system |
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| US (1) | US12046767B2 (en) |
| CA (1) | CA3130079A1 (en) |
| MX (1) | MX2021010792A (en) |
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| EP4088341A4 (en) * | 2020-01-08 | 2024-09-04 | Teijin Automotive Technologies, Inc. | BATTERY HOLDER DESIGN |
| US11996576B2 (en) * | 2020-07-03 | 2024-05-28 | Teijin Automotive Technologies, Inc. | Impact resistant frame of battery containment system |
| US20240357781A1 (en) * | 2021-04-05 | 2024-10-24 | Magna Exteriors Inc. | Emi shielding for composite battery enclosure |
| US11984611B2 (en) * | 2021-08-17 | 2024-05-14 | Beta Air, Llc | Stack battery pack for electric vertical take-off and landing aircraft |
| DE102021132602A1 (en) * | 2021-12-10 | 2023-06-15 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Sealing system, in particular for a battery housing |
| CN216850175U (en) * | 2022-01-17 | 2022-06-28 | 宁德时代新能源科技股份有限公司 | Battery pack and lower box body of battery pack |
| KR20240119089A (en) * | 2022-03-14 | 2024-08-06 | 비와이디 컴퍼니 리미티드 | Battery trays, battery packs and vehicles |
| US12261315B2 (en) * | 2022-04-21 | 2025-03-25 | Ford Global Technologies, Llc | Battery housing assembly for electric vehicles |
| CN115149187A (en) * | 2022-06-02 | 2022-10-04 | 远景动力技术(江苏)有限公司 | A battery module and electronic device |
| US20230395885A1 (en) * | 2022-06-02 | 2023-12-07 | Aesc Japan Ltd. | Battery module and electronic device |
| KR102940085B1 (en) * | 2022-07-01 | 2026-03-16 | 주식회사 엘지에너지솔루션 | Battery pack |
| US12322823B2 (en) | 2022-09-30 | 2025-06-03 | Ford Global Technologies, Llc | Structurally reinforced enclosure covers for traction battery packs |
| US12132218B2 (en) * | 2022-12-29 | 2024-10-29 | Rivian Ip Holdings, Llc | Structural module |
| US20250038338A1 (en) * | 2023-07-25 | 2025-01-30 | Toyota Motor Engineering & Manufacturing North America, Inc. | Battery pack frame assemblies |
| US12606002B2 (en) * | 2023-09-01 | 2026-04-21 | Ford Global Technologies, Llc | Vehicle battery assembly |
| KR102628969B1 (en) * | 2023-09-27 | 2024-01-24 | 주식회사케이에스엠 | Electric vehicle battery case manufacturing method |
| WO2026044502A1 (en) * | 2024-08-27 | 2026-03-05 | 宁德时代新能源科技股份有限公司 | Battery device, bottom protective plate, and electric apparatus |
| WO2026046610A1 (en) | 2024-08-29 | 2026-03-05 | Sabic Global Technologies B.V. | Fire retardant woven continuous fiber thermoplastic composites and articles |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ATE528807T1 (en) * | 2006-05-11 | 2011-10-15 | Johnson Controls Saft Advanced Power Solutions Llc | MODULAR BATTERY SYSTEM |
| JP5408441B2 (en) * | 2010-01-18 | 2014-02-05 | 三菱自動車工業株式会社 | Battery case for vehicle |
| CN106003850B (en) * | 2016-05-18 | 2018-07-03 | 广东新秀新材料股份有限公司 | Honeycomb sandwich structural part and preparation method thereof |
| CN108630843B (en) * | 2017-03-23 | 2023-10-24 | 宁德时代新能源科技股份有限公司 | Battery pack protection frame and battery pack |
| US10886513B2 (en) * | 2017-05-16 | 2021-01-05 | Shape Corp. | Vehicle battery tray having tub-based integration |
| US10371181B1 (en) * | 2018-04-06 | 2019-08-06 | Ford Global Technologies, Llc | Traction battery enclosure clamping device and securing method |
| FR3062749B1 (en) * | 2018-04-10 | 2023-04-14 | Sogefi Air & Cooling | BATTERY UNIT INTEGRATING HEAT EXCHANGE ZONES |
| US12148903B2 (en) * | 2018-05-24 | 2024-11-19 | Mubea Carbo Tech Gmbh | Battery case |
| CA3120529A1 (en) * | 2018-11-20 | 2020-05-28 | Tpi Composites, Inc. | A composite battery enclosure |
| WO2021123881A1 (en) * | 2019-12-18 | 2021-06-24 | Arcelormittal | Reinforcement frame for a battery pack of an electric or hybrid vehicle, reinforced battery pack and process for assembling said battery pack |
| US11548361B2 (en) * | 2020-02-12 | 2023-01-10 | Ford Global Technologies, Llc | Support structures for vehicle frame mounted battery packs |
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- 2021-09-01 US US17/463,840 patent/US12046767B2/en active Active
- 2021-09-07 CA CA3130079A patent/CA3130079A1/en active Pending
- 2021-09-07 MX MX2021010792A patent/MX2021010792A/en unknown
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| US12046767B2 (en) | 2024-07-23 |
| MX2021010792A (en) | 2023-03-02 |
| US20220006150A1 (en) | 2022-01-06 |
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