Classifications

• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B32—LAYERED PRODUCTS
  • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
  • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
  • B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
  • B32B5/32—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed at least two layers being foamed and next to each other
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
  • B29C55/00—Shaping by stretching, e.g. drawing through a die; Apparatus therefor
  • B29C55/02—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets
  • B29C55/10—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets multiaxial
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
  • B01D—SEPARATION
  • B01D67/00—Processes specially adapted for manufacturing semi-permeable membranes for separation processes or apparatus
  • B01D67/0002—Organic membrane manufacture
  • B01D67/0023—Organic membrane manufacture by inducing porosity into non porous precursor membranes
  • B01D67/0025—Organic membrane manufacture by inducing porosity into non porous precursor membranes by mechanical treatment, e.g. pore-stretching
  • B01D67/0027—Organic membrane manufacture by inducing porosity into non porous precursor membranes by mechanical treatment, e.g. pore-stretching by stretching
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
  • B29C39/00—Shaping by casting, i.e. introducing the moulding material into a mould or between confining surfaces without significant moulding pressure; Apparatus therefor
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
  • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
  • B29C48/03—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
  • B29C48/07—Flat, e.g. panels
  • B29C48/08—Flat, e.g. panels flexible, e.g. films
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
  • B29C55/00—Shaping by stretching, e.g. drawing through a die; Apparatus therefor
  • B29C55/005—Shaping by stretching, e.g. drawing through a die; Apparatus therefor characterised by the choice of materials
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
  • B29C55/00—Shaping by stretching, e.g. drawing through a die; Apparatus therefor
  • B29C55/02—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets
  • B29C55/10—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets multiaxial
  • B29C55/12—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets multiaxial biaxial
  • B29C55/14—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets multiaxial biaxial successively
  • B29C55/143—Shaping by stretching, e.g. drawing through a die; Apparatus therefor of plates or sheets multiaxial biaxial successively firstly parallel to the direction of feed and then transversely thereto
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B32—LAYERED PRODUCTS
  • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
  • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
  • B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
• • C—CHEMISTRY; METALLURGY
  • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
  • C08F—MACROMOLECULAR COMPOUNDS OBTAINED BY REACTIONS ONLY INVOLVING CARBON-TO-CARBON UNSATURATED BONDS
  • C08F110/00—Homopolymers of unsaturated aliphatic hydrocarbons having only one carbon-to-carbon double bond
  • C08F110/04—Monomers containing three or four carbon atoms
  • C08F110/06—Propene
• • C—CHEMISTRY; METALLURGY
  • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
  • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
  • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
  • C08J5/18—Manufacture of films or sheets
• • C—CHEMISTRY; METALLURGY
  • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
  • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
  • C08J9/00—Working-up of macromolecular substances to porous or cellular articles or materials; After-treatment thereof
  • C08J9/0061—Working-up of macromolecular substances to porous or cellular articles or materials; After-treatment thereof characterized by the use of several polymeric components
• • C—CHEMISTRY; METALLURGY
  • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
  • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
  • C08J9/00—Working-up of macromolecular substances to porous or cellular articles or materials; After-treatment thereof
  • C08J9/22—After-treatment of expandable particles; Forming foamed products
  • C08J9/228—Forming foamed products
• • D—TEXTILES; PAPER
  • D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
  • D01D—MECHANICAL METHODS OR APPARATUS IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS
  • D01D5/00—Formation of filaments, threads, or the like
  • D01D5/12—Stretch-spinning methods
• • 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
  • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
  • H01M50/409—Separators, membranes or diaphragms characterised by the material
  • H01M50/411—Organic material
  • H01M50/414—Synthetic resins, e.g. thermoplastics or thermosetting resins
• • 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
  • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
  • H01M50/409—Separators, membranes or diaphragms characterised by the material
  • H01M50/449—Separators, membranes or diaphragms characterised by the material having a layered structure
  • H01M50/457—Separators, membranes or diaphragms characterised by the material having a layered structure comprising three or more layers
• • 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
  • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
  • H01M50/489—Separators, membranes, diaphragms or spacing elements inside the cells, characterised by their physical properties, e.g. swelling degree, hydrophilicity or shut down properties
  • H01M50/491—Porosity
• • 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
  • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
  • H01M50/489—Separators, membranes, diaphragms or spacing elements inside the cells, characterised by their physical properties, e.g. swelling degree, hydrophilicity or shut down properties
  • H01M50/494—Tensile strength
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
  • B01D—SEPARATION
  • B01D2323/00—Details relating to membrane preparation
  • B01D2323/08—Specific temperatures applied
  • B01D2323/082—Cooling
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
  • B01D—SEPARATION
  • B01D2323/00—Details relating to membrane preparation
  • B01D2323/14—Ageing features
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
  • B01D—SEPARATION
  • B01D2325/00—Details relating to properties of membranes
  • B01D2325/02—Details relating to pores or porosity of the membranes
  • B01D2325/021—Pore shapes
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
  • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
  • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
  • B29K2105/04—Condition, form or state of moulded material or of the material to be shaped cellular or porous
• • 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
  • H01M50/40—Separators; Membranes; Diaphragms; Spacing elements inside cells
  • H01M50/489—Separators, membranes, diaphragms or spacing elements inside the cells, characterised by their physical properties, e.g. swelling degree, hydrophilicity or shut down properties
• • 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
• • 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
  • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
  • Y10T428/00—Stock material or miscellaneous articles
  • Y10T428/249921—Web or sheet containing structurally defined element or component
  • Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
• • 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
  • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
  • Y10T428/00—Stock material or miscellaneous articles
  • Y10T428/249921—Web or sheet containing structurally defined element or component
  • Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
  • Y10T428/249955—Void-containing component partially impregnated with adjacent component
  • Y10T428/249958—Void-containing component is synthetic resin or natural rubbers
• • 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
  • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
  • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
  • Y10T428/00—Stock material or miscellaneous articles
  • Y10T428/249921—Web or sheet containing structurally defined element or component
  • Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
  • Y10T428/249975—Void shape specified [e.g., crushed, flat, round, etc.]

Definitions

• the invention is directed to a biaxially oriented microporous membrane and the method of its manufacture.
• Microporous membranes are known, can be made by various processes, and the process by which the membrane is made has a material impact upon the membrane's physical attributes. See, Resting, R. , Synthetic Polymeric Membranes, A structural perspective, Second Edition, John Wiley & Sons, New York, NY, (1985) .
• Three commercially viable processes for making microporous membranes include: the dry-stretch process (also known as the CELGARD process) , the wet process, and the particle stretch process.
• the dry-stretch process refers to a process where pore formation results from stretching the nonporous precursor. See, Resting, Ibid, pages 290-297, incorporated herein by reference.
• the dry-stretch process is different from the wet process and particle stretch process.
• the wet process also know as the phase inversion process, or the extraction process or the TIPS process (to name a few)
• the polymeric raw material is mixed with a processing oil (sometimes referred to as a plasticizer)
• a processing oil sometimes referred to as a plasticizer
• pores are then formed when the processing oil is removed (these films may be stretched before or after the removal of the oil) . See, Resting, Ibid, pages 237-286, incorporated herein by reference.
• the polymeric raw material is mixed with particulate, this mixture is extruded, and pores are formed during stretching when the interface between the polymer and the particulate fractures due to the stretching forces. See, U.S. Patent Nos . 6,057,061 and 6,080,507, incorporated herein by reference.
• each membrane arising from these processes are physically different and the process by which each is made distinguishes one membrane from the other.
• Dry-stretch membranes have slit shaped pores due to the inability to stretch the precursor in the transverse machine direction.
• Wet process membranes have rounder pores due to the ability to stretch the precursor in the transverse machine direction.
• Particle stretched membranes are filled with particulate needed for pore formation. Accordingly, each membrane may be distinguished from the other by its method of manufacture .
• membranes made by the dry-stretch process have met with excellent commercial success, there is a need to improve their physical attributes, so that they may be used in wider spectrum of applications .
• Some areas of improvement include pore shapes other than slits and increase transverse direction tensile strength.
• U.S. Patent No. 6,602,593 is directed to a microporous membrane, made by a dry-stretch process, where the resulting membrane has a ratio of transverse direction tensile strength to machine direction tensile strength of 0.12 to 1.2.
• the TD/MD tensile ratio is obtained by a blow-u ⁇ ratio of at least 1.5 as the precursor is extruded.
• a microporous membrane is made by a dry-stretch process and has substantially round shaped pores and a ratio of machine direction tensile strength to transverse direction tensile strength in the range of 0.5 to 5.0.
• the method of making the foregoing microporous membrane includes the steps of: extruding a polymer into a nonporous precursor, and biaxially stretching the nonporous precursor, the biaxial stretching including a machine direction stretching and a transverse direction stretching, the transverse direction including a simultaneous controlled machine direction relax.
• Figure 1 is a photograph of one embodiment of the instant invention (single ply membrane) .
• Figure 2 is a photograph of another embodiment of the instant invention (multi-ply membrane, plies laminated together then stretched) .
• Figure 3 is a photograph of another embodiment of the instant invention (multi-ply membrane, plies coextruded then stretched) .
• Figure 4 is a photograph of a prior art dry-stretched membrane (single ply membrane) .
• Figure 5 is a photograph of a prior art dry-stretched membrane (multi-ply membrane, plies laminated then stretched) .
• a microporous membrane is made by a dry-stretch process and has substantially round shaped pores and a ratio of machine direction tensile strength to transverse direction tensile strength in the range of 0.5 to 4.0.
• a microporous membrane is a thin, pliable, polymeric sheet, foil, or film having a plurality of pores therethrough.
• Such membranes by be used in a wide variety of applications, including, but not limited to, mass transfer membranes, pressure regulators, filtration membranes, medical devices, separators for electrochemical storage devices, membranes for use in fuel cells, and the like.
• the instant membrane is made by the dry-stretch process (also known as the CELGARD process) .
• the dry-stretch process also known as the CELGARD process.
• s refers to a process where pore formation results from stretching the nonporous precursor. See, Resting, R., Synthetic Polymeric Membranes, A structural perspective, Second Edition, John Wiley Sc Sons, New York, NY, (1985), pages 290-297, incorporated herein by reference.
• the dry-stretch process is distinguished from the wet process and particle stretch process, as discussed above.
• the instant membrane may be distinguished from prior dry- stretched membranes in at least two ways: 1) substantially round shape pores, and 2) a ratio of machine direction tensile strength to transverse direction tensile strength in the range of 0.5 to 4.0.
• the pores are characterized as substantially round shaped. See, Figures 1-3. This pore shape is contrasted with the slit shaped pores of the prior art dry- stretched membranes. See Figures 4-5 and Resting, Ibid.
• the pore shape of the instant membrane may be characterized by an aspect ratio, the ratio of the length to the width of the pore. In one embodiment of the instant membrane, the aspect ratio ranges from 0.75 to 1.25. This is contrasted with the aspect ratio of the prior dry-stretched membranes which are greater than 5.0. See Table below. Regarding the ratio of machine direction tensile strength to transverse direction tensile strength, in one embodiment, this ratio is between 0.5 to 5.0. This ratio is contrasted with the corresponding ratio of the prior art membranes which is greater than 10.0. See Table below.
• the instant membrane may be further characterized as follows: an average pore size in the range of 0.03 to 0.30 microns ( ⁇ ) ; a porosity in the range of 20-80%; and/or a transverse direction tensile strength of greater than 250 Kg/cm 2 .
• ⁇ microns
• the polymers used in the instant membrane may be characterized as thermoplastic polymers. These polymers may be further characterized as semi-crystalline polymers.
• semi-crystalline polymer may be a polymer having a crystallinity in the range of 20 to 80%.
• Such polymers may be selected from the following group: polyolefins, fluorocarbons, polyamides, polyesters, polyacetals (or polyoxymethylenes) , polysulfides , polyvinyl alcohols, co-polymers thereof, and combinations thereof.
• Polyolefins may include polyethylenes (LDPE, LLDPE, HDPE, UHMWPE) , polypropylene, polybutene, polymethylpentene, co-polymers thereof, and blends thereof.
• Fluorocarbons may include polytetrafluoroethylene (PTFE) , polychlorotrifluoroethylene (PCTFE) , fluorinated ethylene propylene (FEP) , ethylene chlortrifluoroethylene (ECTFE) , ethylene tetrafluoroethylene (ETFE) , polyvinylidene fluoride (PVDF) , polyvinylfluoride (PVF) , prefluoroalkoxy (PFA) resin, co-polymers thereof, and blends thereof.
• Polyamides may include, but are not limited to: polyamide 6, polyamide 6/6, Nylon 10/10, polyphthalamide (PPA), co-polymers thereof, and blends thereof .
• Polyesters may include polyester terephthalate (PET) , polybutylene terephthalate (PBT) , poly- 1-4- cyclohexylenedimethylene terephthalate (PCT) , polyethylene naphthalate (PEN) , and liquid crystal polymers (LCP) .
• Polysulfides include, but are not limited to, polyphenylsulfide, polyethylene sulfide, co-polymers thereof, and blends thereof.
• Polyvinyl alcohols include, but are not limited to, ethylene- vinyl alcohol, co-polymers thereof, and blends thereof.
• the instant membrane may include other ingredients, as is well known.
• those ingredients may include: fillers (inert particulates used to reduce the cost of the membrane, but otherwise having no significant impact on the manufacture of the membrane or its physical properties), anti-static agents, anti- blocking agents, anti-oxidants, lubricants (to facilitate manufacture), and the like.
• Various materials may be added to the polymers to modify or enhance the properties of the membrane.
• Such materials include, but are not limited to: (1) polyolefins or polyolefin oligomers with a melting temperature less than 130° C;
• Mineral fillers include, but are not limited to: calcium carbonate, zinc oxide, diatomaceous earth, talc, kaolin, synthetic silica, mica, clay, boron nitride, silicon dioxide, titanium dioxide, barium sulfate, aluminum hydroxide, magnesium hydroxide and the like, and blends thereof;
• Elastomers include, but are not limited to: ethylene-propylene (EPR), ethylene-propylene-diene (EPDM) , styrene- butadiene (SBR) , styrene isoprene (SIR) , ethylidene norbornene (ENB) , epoxy, and polyurethane and blends thereof;
• Wetting agents include, but
• beta-nucleated polypropylene is a substance that causes the creation of beta crystals in polypropylene.
• the instant membrane may be a single ply or multi-ply membrane.
• the instant membrane may be one ply of the multi-ply membrane or the instant membrane may be all of the plies of the multi-ply membrane. If the instant membrane is less than all of the plies of the multiply membrane, the multi-ply membrane may be made via a lamination process. If the instant membrane is all plies of the multi-ply membrane, the multi-ply membrane may be made via an extrusion process. Further, multi-ply membranes may be made of plies of the same materials or of differing materials .
• the instant membrane is made by a dry-stretch process where the precursor membrane is biaxially stretched (i.e., not only stretched in the machine direction, but also in the transverse machine direction) .
• the process for making the foregoing membrane includes the steps of extruding a nonporous precursor, and then biaxially stretching the nonporous precursor.
• the nonporous precursor may be annealed prior to stretching.
• the biaxial stretching includes a machine direction stretch and a transverse direction with a simultaneous controlled machine direction relax.
• the machine direction stretch and the transverse direction stretch may be simultaneous or sequential.
• the machine direction stretch is followed by the transverse direction stretch with the simultaneous machine direction relax. This process is discussed in greater detail below.
• Extrusion is generally conventional (conventional refers to conventional for a dry-stretch process) .
• the extruder may have a slot die (for flat precursor) or an annular die (for parison precursor) .
• an inflated parison technique may be employed (e.g., a blow up ratio (BUR)) .
• BUR blow up ratio
• the birefringence of the nonporous precursor does not have to be as high as in the conventional dry-stretch process.
• the birefringence of the precursor would be > 0.0130; while with the instant process, the birefringence of the PP precursor could be as low as 0.0100.
• a membrane with a > 35% porosity from a polyethylene resin the birefringence of the precursor would be > 0.0280; while with the instant process, the birefringence of the PE precursor could be as low as 0.0240.
• Annealing may be carried out, in one embodiment, at temperatures between T m -80°C and T m -10°C (where T m is the melt temperature of the polymer); and in another embodiment, at temperatures between T m -50°C and T m -15°C.
• T m is the melt temperature of the polymer
• T m -15°C the melt temperature of the polymer
• Machine direction stretch may be conducted as a cold stretch or a hot stretch or both, and as a single step or multiple steps.
• cold stretching may be carried out at ⁇ T m -50°C, and in another embodiment, at ⁇ T n ,- 8O 0 C.
• hot stretching may be carried out at ⁇ T m -10°C.
• total machine direction stretching may be in the range of 50-500%, and in another embodiment, in the range of 100-300%.
• the precursor may shrink in the transverse direction (conventional) .
• Transverse direction stretching includes a simultaneous controlled machine direction relax.
• the precursor is stretched in the transverse direction the precursor is simultaneously allowed to contract (i.e., relax), in a controlled manner, in the machine direction.
• the transverse direction stretching may be conducted as a cold step, or a hot step, or a combination of both.
• total transverse direction stretching may be in the range of 100- 1200%, and in another embodiment, in the range of 200-900%.
• the controlled machine direction relax may range from 5-80%, and in another embodiment, in the range of 15-65%.
• transverse stretching may be carried out in multiple steps.
• the precursor may or may not be allowed to shrink in the machine direction.
• the first transverse direction step may include a transverse stretch with the controlled machine relax, followed by simultaneous transverse and machine direction stretching, and followed by transverse direction relax and no machine direction stretch or relax.
• the precursor, after machine direction and transverse direction stretching may be subjected to a heat setting, as is well known.
• a heat setting as is well known.
• test values reported herein, thickness, porosity, tensile strength, and aspect ratio were determined as follows: thickness-ASTM-D374 using the Emveco Microgage 210-A micrometer; porosity-ASTM D-2873; tensile strength-ASTM D-882 using an Instron Model 4201; and aspect ratio-measurements taken from the SEM micrographs .
• Example 1 Polypropylene (PP) resin is extruded using a 2.5 inch extruder.
• the extruder melt temperature is 221°C.
• Polymer melt is fed to a circular die.
• the die temperature is set at 22O 0 C, polymer melt is cooled by blowing air.
• Extruded precursor has a thickness of 27 ⁇ and a birefringence of 0.0120.
• the extruded film was then annealed at 15O 0 C for 2 minutes.
• the annealed film is then cold stretched to 20% at room temperature, and then hot stretched to 228% and relaxed to 32% at 14O 0 C.
• the machine direction (MD) stretched film has a thickness of 16.4 micron ( ⁇ ) , and porosity of 25%.
• the MD stretched film is then transverse direction (TD) stretched 300% at 140 0 C with MD relax of 50%.
• the finished film has a thickness of 14.1 microns, and porosity of 37%.
• TD tensile strength of finished film is 550 Kg/cm 2 . See Figure 1.
• Example 2 Polypropylene (PP) resin is extruded using a 2.5 inch extruder.
• the extruder melt temperature is 220 0 C.
• Polymer melt is fed to a circular die.
• the die temperature is set at 200 0 C, polymer melt is cooled by blowing air.
• Extruded precursor has a thickness of 9.5 ⁇ and a birefringence of 0.0160.
• HDPE resin is extruded using a 2.5 inch extruder.
• the extruder melt temperature is 210 0 C.
• Polymer melt is fed to a circular die. Die temperature is set at 205 0 C, polymer melt is cooled by air.
• Extruded precursor has a thickness of 9.5 ⁇ and a birefringence of 0.0330.
• Lamination roll temperature is 15O 0 C.
• Laminated tri-layer film is then annealed at 125°C for 2 minutes. The annealed film is then cold stretched to 20% at room temperature, and then hot stretched to 160% and relaxed to 35% at 113 0 C.
• the MD stretched film has a thickness of 25.4 micron, and porosity of 39%.
• the MD stretched film is then TD stretched 400% at 115°C with MD relax of 30%.
• the finished film has a thickness of 19.4 microns and porosity of 63%.
• TD tensile strength of finished film is 350 Kg/cm 2 . See Figure 2.
• Example 3 PP resin and HDPE resin are extruded using a co- extrusion die to form a PP/PE/PP tri-layer film.
• Extruder melt temperature for PP is 243 0 C
• extruder melt temperature for PE is 214 0 C.
• Polymer melt is then fed to a co-extrusion die which is set at 198 0 C.
• Polymer melt is cooled by blowing air.
• the extruded film has a thickness of 35.6 microns.
• the extruded precursor is then annealed at 125°C for 2 minutes. The annealed film is then cold stretched to 45% at room temperature and hot stretched to 247% and relaxed to 42% at 113 0 C.
• the MD stretched film has a thickness of 21.5 microns and porosity of 29%.
• the MD stretched film is then TD stretched 450% at 115°C with 50% MD relax.
• the finished film has a thickness of 16.3 microns and porosity of 59%.
• TD tensile strength of finished film is 570 Kg/cm 2 .
• Example 4 PP resin and HDPE resin are co-extruded and MD stretched the same way as in example 3. The MD stretched film is then TD stretched 800% at 115 0 C with 65% MD relax. The finished film has a thickness of 17.2 microns and porosity of 49%. TD tensile strength of finished film is 730 Kg/cm 2 . See Figure 3.
• Example 5. PP resin and PB resin are extruded using a co- extrusion die. Extruder melt temperature for PP is 230 0 C, and extruder melt for PB is 206 0 C. Polymer melt is then fed to a co-extrusion die which is set at 210 0 C. Polymer melt is then cooled by blowing air.
• the extruded film has a thickness of 36.0 microns.
• the extruded precursor is then annealed at 105 0 C for 2 minutes.
• the annealed film is then cold stretched to 20%, and then hot stretched at 105 0 C to 155% and then relaxed to 35%.
• the MD stretched film is then TD stretched 140% at 110 0 C with 20% MD relax.
• the finished film has a thickness of 14.8 microns and porosity of 42%.
• TD tensile strength of finished film is 286 Kg/cm 2 .
• Example 6 PP resin and PE resin are extruded using a co- extrusion die to form a PP/PE/PP trilayer film.
• Extruder melt temperature for PP is 245 0 C
• extruder melt temperature for PE is 23O 0 C.
• Polymer melt is then fed to a co-extrusion die which is set at 225 0 C.
• Polymer melt is cooled by blowing air.
• the extruded film has a thickness of 27 microns and a birefringence of 0.0120.
• the extruded precursor is then annealed at 115 0 C for 2 minutes.
• the MD stretched film has a thickness of 15 microns and porosity of 16%.
• the MD stretched film is then TD stretched 260% at 13O 0 C with 50% MD relax, followed by a simultaneous MD and TD stretch of 50% and 216% in each direction at 13O 0 C, and finally the film is held fast in the MD (100%) and allowed to relax 57.6% in the TD at a temperature of 13O 0 C.
• the finished film has a thickness of 7.6 microns and porosity of 52%.
• TD tensile strength of finished film is 513 Kg/cm 2 .
• Example 7 PP resin and PE resin are extruded using a co- extrusion die to form a PP/PE/PP trilayer film.
• Extruder melt temperature for PP is 222 0 C
• extruder melt temperature for PE is 225°C.
• Polymer melt is then fed to a co-extrusion die which is set at 215°C.
• Polymer melt is cooled by blowing air.
• the extruded film has a thickness of 40 microns and birefringence of 0.0110.
• the extruded precursor is then annealed at 105 0 C for 2 minutes.
• the MD stretched film has a thickness of 23.8 microns and porosity of 29.6%.
• the MD stretched film is then TD stretched 1034% at HO 0 C with 75% MD relax.
• the finished film has a thickness of 16.8 microns and porosity of 46%.
• TD tensile strength of finished film is 1037 Kg/cm 2 .

Landscapes

• Chemical & Material Sciences (AREA)
• Chemical Kinetics & Catalysis (AREA)
• Engineering & Computer Science (AREA)
• General Chemical & Material Sciences (AREA)
• Electrochemistry (AREA)
• Mechanical Engineering (AREA)
• Polymers & Plastics (AREA)
• Organic Chemistry (AREA)
• Medicinal Chemistry (AREA)
• Health & Medical Sciences (AREA)
• Manufacturing & Machinery (AREA)
• Materials Engineering (AREA)
• Textile Engineering (AREA)
• Manufacture Of Porous Articles, And Recovery And Treatment Of Waste Products (AREA)
• Cell Separators (AREA)
• Separation Using Semi-Permeable Membranes (AREA)
• Shaping By String And By Release Of Stress In Plastics And The Like (AREA)
• Fuel Cell (AREA)
• Laminated Bodies (AREA)

Priority Applications (11)

Applications Claiming Priority (4)

Publications (2)

Family

ID=38428578

Family Applications (1)

Country Status (14)

Cited By (8)

Families Citing this family (67)

Family Cites Families (43)

• 2007
  • 2007-02-13 US US11/674,180 patent/US8795565B2/en active Active
  • 2007-02-14 HU HUE20155006A patent/HUE056772T2/hu unknown
  • 2007-02-14 AU AU2007217288A patent/AU2007217288B2/en not_active Ceased
  • 2007-02-14 KR KR1020127020150A patent/KR20120094152A/ko not_active Ceased
  • 2007-02-14 MX MX2008010744A patent/MX2008010744A/es active IP Right Grant
  • 2007-02-14 CN CN201410242734.0A patent/CN104015348A/zh active Pending
  • 2007-02-14 PL PL20155006T patent/PL3663072T3/pl unknown
  • 2007-02-14 EP EP07756952.3A patent/EP1993811B2/en active Active
  • 2007-02-14 KR KR1020087020453A patent/KR101188570B1/ko active Active
  • 2007-02-14 EP EP15179782.6A patent/EP2974847B1/en active Active
  • 2007-02-14 RU RU2008137597A patent/RU2420400C2/ru active
  • 2007-02-14 HU HUE15179782A patent/HUE050789T2/hu unknown
  • 2007-02-14 CA CA 2637623 patent/CA2637623C/en active Active
  • 2007-02-14 JP JP2008556497A patent/JP5461018B2/ja active Active
  • 2007-02-14 WO PCT/US2007/062095 patent/WO2007098339A2/en not_active Ceased
  • 2007-02-14 BR BRPI0707988-5A patent/BRPI0707988A2/pt not_active IP Right Cessation
  • 2007-02-14 KR KR1020107016837A patent/KR20100101679A/ko not_active Ceased
  • 2007-02-14 PL PL15179782T patent/PL2974847T3/pl unknown
  • 2007-02-14 EP EP20155006.8A patent/EP3663072B1/en active Active
  • 2007-02-26 TW TW96106523A patent/TWI358422B/zh active
• 2012
  • 2012-06-05 JP JP2012127958A patent/JP2012188675A/ja active Pending
• 2014
  • 2014-06-06 US US14/297,688 patent/US10913237B2/en active Active
  • 2014-06-20 US US14/309,931 patent/US11420416B2/en active Active
• 2015
  • 2015-11-09 JP JP2015219123A patent/JP6399993B2/ja active Active
• 2017
  • 2017-06-13 JP JP2017115807A patent/JP6542290B2/ja active Active
• 2021
  • 2021-02-08 US US17/169,572 patent/US12179469B2/en active Active
• 2024
  • 2024-11-19 US US18/952,643 patent/US20250074032A1/en active Pending

Non-Patent Citations (1)

Also Published As

Similar Documents

Legal Events