WO1998058111A1 - Non-woven fabric laminate - Google Patents

Non-woven fabric laminate Download PDF

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Publication number
WO1998058111A1
WO1998058111A1 PCT/GB1998/001671 GB9801671W WO9858111A1 WO 1998058111 A1 WO1998058111 A1 WO 1998058111A1 GB 9801671 W GB9801671 W GB 9801671W WO 9858111 A1 WO9858111 A1 WO 9858111A1
Authority
WO
WIPO (PCT)
Prior art keywords
laminate
fabric
fibres
fabrics
vinyl monomer
Prior art date
Application number
PCT/GB1998/001671
Other languages
English (en)
French (fr)
Inventor
Giovanni Gentilcore
Ian Michael Lancaster
Original Assignee
Scimat Limited
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Scimat Limited filed Critical Scimat Limited
Priority to CA002294599A priority Critical patent/CA2294599A1/en
Priority to EP98925860A priority patent/EP0991804A1/en
Priority to JP50394299A priority patent/JP2002504874A/ja
Publication of WO1998058111A1 publication Critical patent/WO1998058111A1/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered 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
    • B32B5/22Layered 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
    • B32B5/24Layered 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 one layer being a fibrous or filamentary layer
    • B32B5/26Layered 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 one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered 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
    • B32B5/22Layered 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
    • B32B5/24Layered 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 one layer being a fibrous or filamentary layer
    • B32B5/28Layered 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 one layer being a fibrous or filamentary layer impregnated with or embedded in a plastic substance
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/08Impregnating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered 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
    • B32B5/02Layered 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 structural features of a fibrous or filamentary layer
    • B32B5/022Non-woven fabric
    • DTEXTILES; PAPER
    • D04BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04HMAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H13/00Other non-woven fabrics
    • DTEXTILES; PAPER
    • D04BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04HMAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H5/00Non woven fabrics formed of mixtures of relatively short fibres and yarns or like filamentary material of substantial length
    • D04H5/04Non woven fabrics formed of mixtures of relatively short fibres and yarns or like filamentary material of substantial length strengthened or consolidated by applying or incorporating chemical or thermo-activatable bonding agents in solid or liquid form
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409Separators, membranes or diaphragms characterised by the material
    • H01M50/411Organic material
    • H01M50/414Synthetic resins, e.g. thermoplastics or thermosetting resins
    • H01M50/417Polyolefins
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409Separators, membranes or diaphragms characterised by the material
    • H01M50/44Fibrous material
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/409Separators, membranes or diaphragms characterised by the material
    • H01M50/449Separators, membranes or diaphragms characterised by the material having a layered structure
    • H01M50/457Separators, membranes or diaphragms characterised by the material having a layered structure comprising three or more layers
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/489Separators, membranes, diaphragms or spacing elements inside the cells, characterised by their physical properties, e.g. swelling degree, hydrophilicity or shut down properties
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/40Separators; Membranes; Diaphragms; Spacing elements inside cells
    • H01M50/489Separators, membranes, diaphragms or spacing elements inside the cells, characterised by their physical properties, e.g. swelling degree, hydrophilicity or shut down properties
    • H01M50/494Tensile strength
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02Composition of the impregnated, bonded or embedded layer
    • B32B2260/021Fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02Synthetic macromolecular fibres
    • B32B2262/0253Polyolefin fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/718Weight, e.g. weight per square meter
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/73Hydrophobic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2309/00Parameters for the laminating or treatment process; Apparatus details
    • B32B2309/08Dimensions, e.g. volume
    • B32B2309/10Dimensions, e.g. volume linear, e.g. length, distance, width
    • B32B2309/105Thickness
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2310/00Treatment by energy or chemical effects
    • B32B2310/08Treatment by energy or chemical effects by wave energy or particle radiation
    • B32B2310/0806Treatment by energy or chemical effects by wave energy or particle radiation using electromagnetic radiation
    • B32B2310/0831Treatment by energy or chemical effects by wave energy or particle radiation using electromagnetic radiation using UV radiation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2457/00Electrical equipment
    • B32B2457/10Batteries
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00Secondary cells; Manufacture thereof
    • H01M10/34Gastight accumulators
    • H01M10/345Gastight metal hydride accumulators
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries

Definitions

  • This invention relates to a laminate formed from non-woven fabrics and to a method of treating a non-woven fabric laminate.
  • the laminate can be used as a separator in an electrochemical device.
  • Non-woven fabrics can be made by processes which include (a) melt blowing, (b) spinning, and (c) wet or dry laying.
  • the fibres of fabrics made by spinning and wet or dry laying require bonding to one another for the fabric to have integrity, so that it has the mechanical properties required for satisfactory performance.
  • the fibres are bonded to one another by the application of heat and pressure.
  • polyethylene is incorporated into the fabric, either as fibres consisting essentially of polyethylene or as bicomponent fibres consisting of a polypropylene core and a polyethylene sheath.
  • the polyethylene in the fabric can provide the necessary bonds as a result of heating the fabric to a temperature that is greater than the softening point of the polyethylene.
  • Non-woven fabrics can be used to form an electrode separator in an electrochemical device.
  • Examples of such devices include nickel-cadmium and nickel-metal hydride cells.
  • the separator should be inert towards materials with which it comes into contact in the cell including in particular the alkaline electrolyte and the electrode materials. It should also have physical characteristics which enable it to withstand the treatment encountered during assembly of the device and during use. For example, it should be able to withstand the stresses encountered during spiral winding of the cell components. It should also be capable of resisting the growth of dendrites between the electrodes during recharging .
  • a fabric that is made from spun fibres which are then bonded together has the disadvantage that the bonds reduce the effective surface area of the fabric that is available to ion transfer by effectively blocking the pores of the fabric.
  • the uneven current distribution that results from this uneven pore distribution can give rise to dendrite formation during recharging of a secondary cell, ultimately leading to a short circuit in the cell.
  • a melt-blown fabric has the further advantage of small fibres size (which is generally less than about 5 ⁇ m, and often as low as 1 ⁇ m or less) so that the fabric can provide a separator with good barrier properties.
  • small fibres size which is generally less than about 5 ⁇ m, and often as low as 1 ⁇ m or less
  • the fine size of the fibres of the fabric means that the fabric is only able to withstand the application of small stresses and small degrees of strain. A large stress or high strain can result in fracture of the fabric.
  • Non-woven fabrics formed by wet or dry laying of fibres can have satisfactory mechanical properties.
  • the fibre size can tend to be undesirably large, often greater than 15 ⁇ m.
  • a further disadvantage which arises from the use of bicomponent fibres is their high cost.
  • the present invention provides a laminate of melt-blown and spun fibre fabrics, the fibres of which have been treated by graft copolymerisation of a vinyl monomer such as acrylic acid.
  • the invention provides a laminate formed from first and second non-woven fabrics which each comprise fibres of a hydrophobic polymeric material, the first fabric being formed from spun fibres and the second fabric being a melt-blown fabric, the fibres of the fabrics having undergone a copolymerisation reaction with a vinyl monomer which is capable of reacting with an acid or a base to form a salt directly or indirectly, the reaction involving exposure of the laminate to ultraviolet radiation while impregnated with a solution of the vinyl monomer resulting in grafting of- the vinyl monomer to the surfaces of the fibres.
  • the laminate of the invention has the advantage that it is able to tolerate stresses imposed when it is being manipulated, for example prior to and during assembly of an electrochemical device in which the laminate is incorporated as an electrode separator.
  • the structure of the laminate remains stable under moderate loads and does not exhibit the tendency to open as in the case of fabrics formed from spun fibres.
  • the laminate structure has a reduced tendency to fracture when placed under load compared with melt-blown fabrics.
  • a further advantage of the laminate of the invention is that it can exhibit the good barrier properties which can be obtained from melt-blown non-woven fabrics when it is used as an electrode separator in an electrochemical device. This arises from the small effective pore size that is presented by the laminate.
  • the effective size of the pores defined by the fibres of the fabrics can be measured using a Coulter porometer.
  • the effective pore size of the laminate is less than about 30 ⁇ m, more preferably less than about 20 ⁇ m, for example less than about 15 ⁇ m.
  • a small pore size has the advantage of enhancing the ability of the laminate to resist penetration of electrode materials, for example as dendrites .
  • the laminate of the invention can be subjected to a calendering step during its manufacture. Amongst other advantages, this can have the result of reducing the effective pore size of the laminate.
  • a small pore size also enhances the ability of the laminate to absorb and retain electrolyte once the fibres have been treated to render them hydrophilic.
  • a high electrolyte absorption has the advantage of reducing the internal resistance of an electrochemical device in which the laminate is incorporated as an electrode separator, and of extending the cycle life of the device.
  • Yet another advantage of the laminate of the present invention arises from the fine structure presented by the melt-blown fabric when the laminate is used as an electrode separator.
  • the laminate is able to combine the good physical properties discussed above with an ability to absorb contaminants. These contaminants, including ammonia and metal ions, can be found in electrochemical devices following the production and use of certain electrode materials, for example nickel hydroxide and metal hydride electrodes. Absorption of contaminants in the device has the advantage of inhibiting self-discharge reactions.
  • the shelf-life of a device with a laminate of the present invention as its separator can therefore be enhanced compared with devices with previously known separators.
  • it is at least about 0.15 meq.g "1 , preferably at least about 0.25 meq.g “1 , more preferably at least about 0.3 meq.g -1 , for example at least about 0.35 meq.g "1 .
  • the laminate of the present invention also has the advantage of reduced cost compared with products based on bicomponent fibres such' as bicomponent polyethylene and polypropylene fibres .
  • the fibres of the first fabric can be bonded to one another prior to formation of the laminate, for example by localised welds between the fabrics .
  • the first fabric might then be a spun bonded fabric.
  • the fibres of the first fabric can be substantially unbonded to one another in which the fabric is formed without a step of bond formation by the application of heat and pressure.
  • bonds between the first and second fabrics of the laminate there are bonds between the first and second fabrics of the laminate.
  • the bonds might be formed by localised application of heat and pressure.
  • the heat and pressure can be applied by passing the laminate between heated rollers with appropriately profiled surfaces.
  • Such treatment can lead to the formation of localised welds between the fabrics. They will also tend to form bonds between the fibres of the first fabric (which might already be bonded to one another prior to lamination) .
  • the proportion of the area of the laminate in which the bonds are formed is less than about 20%, more preferably less than about 15%, especially less than about 10%, for example about
  • the mean thickness of the fibres of the first fabric (which might be measured as a mean diameter, especially when the fibres have a circular cross-section) from which the non-woven fabric is formed is not more than about 30 ⁇ m, more preferably not more than about 20 ⁇ m.
  • the thickness of the fibres of the first fabric will often be at least about 5 ⁇ m, for example at least about 10 ⁇ m.
  • the mean thickness of the fibres of the second fabric (which might be measured as a mean diameter, especially when the fibres have a circular cross-section) from which the non-woven fabric is formed is not more than about 8 ⁇ m, more preferably not more than about 5 ⁇ m.
  • the thickness of the fibres of the second fabric will generally be at least about 0.5 ⁇ m.
  • the ratio of the weight of the fibres of the second fabric to the weight of the fibres of the entire laminate is at least about 0.1, more preferably at least about 0.2, especially at least about 0.4, for example at least about 0.5.
  • the laminate of the invention can include one or more fabrics in addition to the first and second fabrics.
  • the laminate of the invention can include the first and second fabrics as discussed above, together with a third fabric and possibly a fourth fabric.
  • the third fabric can be formed from spun fibres.
  • the third fabric can have the same construction as the first fabric.
  • Spun fibres of a third fabric can be bonded to one another prior to formation of the laminate, that is as a spun bonded fabric.
  • the fibres of a third fabric will be bonded to one another by localised application of heat and pressure by which bonds between the fabrics of the laminate are formed.
  • the first fabric and a third fabric formed from spun fibres can be arranged on opposite faces of the second fabric.
  • the ion exchange capacity of the laminate is measured in meq.g "1 according to the test routine referred to below, to provide a measure of the extent of the graft copolymerisation reaction between of the material of the fibres and the vinyl monomer.
  • the ion exchange capacity is at least about 0.25, -more preferably at least about 0.4, especially at least about 0.6.
  • the ion exchange capacity is not more than about 2.0, more preferably not more than about 1.6, especially not more than about 1.4, for example not more than about 1.2.
  • the gel fraction of the material of the laminate is measured according to ASTM D2765-84, providing a measure of the extent of crosslinking of the material of the fibres.
  • the gel fraction is at least about 10%, more preferably at least about 20%, especially at least about 30%.
  • the thickness of the laminate measured using test method DIN 53105 which involves lowering a 2.0 kg weight onto a sample of the laminate of area 2.0 cm 2 at a speed of 2.0 mm.s "1 , is greater than about 80 ⁇ m, more preferably greater than about 100 ⁇ m; preferably, the thickness is less than about 400 ⁇ m, more preferably less than about 250 ⁇ m.
  • the method by which the laminate is made may include a calendering step to reduce its thickness to a value within the range referred to above, the reduction being by at least about 5%, preferably at least about 15%, more preferably at least about 25%, and less than about 60%, preferably less than about 45%, more preferably less than about 40%.
  • Calendering can have the advantage of reducing the effective size of the pores in the fabric, giving rise to the advantages discussed above.
  • the calendering step may take place before or after the material of the laminate is reacted with the graft-polymerisation solution. Calendering the laminate before the graft-polymerisation reaction has been found to give rise to increased rates of the reaction. Calendering the laminate after the graft-polymerisation reaction has been found to give rise to enhanced electrolyte absorption.
  • a laminate that has been calendered after the graft reaction can have an improved ability to absorb impurities, especially ammonia, which might be present in the electrolyte system.
  • the vinyl monomer which is graft-polymerised with the material of the fibre surface can be capable of reacting with an acid or a base directly to form a salt, or indirectly to form a salt after appropriate work up, perhaps involving for example hydrolysis or sulphonation .
  • Preferred vinyl monomers include ethylenically unsaturated carboxylic acids and esters thereof such as acrylic acid, methacrylic acid, methyl acrylate, and methylmethacrylate .
  • Other vinyl monomers which might be used include acrylamide, vinylpyridine, vinyl- pyrrolidone and styrene-sulphonic acid.
  • the material of the surface of at least some of the fibres for example at least about 40% by weight, preferably at least about 60%, more preferably at least about 80%, comprises polypropylene.
  • at least 40% by weight of the material of the fibres of the first fabric or the second fabric or both is polypropylene, more preferably at least about 60%, especially at least about 80%.
  • the material of at least some of the fibres from which the first or second fabric (or each of the fabrics) is formed is substantially homogeneous throughout the thickness of the fibres. It can be preferred for many applications for the material of substantially all of the fibres to be substantially homogeneous throughout their thickness, so that those fibres are formed only from polypropylene or another suitable material (with appropriate additives where necessary) .
  • the invention provides a method of treating a laminate formed from first and second non-woven fabrics which each comprise polymeric fibres, in which the first fabric is formed from spun fibres and the second fabric is a melt-blown fabric, the method comprising: (a) impregnating the laminate with a solution of a vinyl monomer which is capable of reacting with an acid or a base to form a salt directly or indirectly, the solvent being one which does not evaporate significantly in the subsequent step of exposing the fabric to radiation, and
  • the ultraviolet radiation initiated polymerisation reaction can be completed surprisingly quickly, for example by exposing the impregnated laminate to radiation for as little as 15 seconds, even as little as 5 or 10 seconds, and it has been found that the fabrics of the laminate after reaction contain a significant amount of grafted monomer, which can be sufficient for the fabrics to be rendered wettable by aqueous solutions such as might be found in certain electrochemical devices.
  • the exposure of the impregnated laminate to oxygen is restricted during the irradiation, for example, by carrying out the ultraviolet irradiation step in an inert atmosphere such as an atmosphere of argon or nitrogen, or by sealing the impregnated laminate between sheets of material which are impervious to oxygen, but are transparent to ultraviolet radiation of appropriate wavelength for initiating the copolymerisation reaction.
  • an inert atmosphere such as an atmosphere of argon or nitrogen
  • the impregnation solution includes an initiator for the polymerisation reaction.
  • the initiator initiates the reaction by abstracting an atomic species from one of the reacting materials, for example by abstracting a hydrogen atom from polypropylene of the fabric fibres to create a polymeric radical. Following such abstraction, the polymeric radical, in contact with the monomer in solution, can initiate the formation of a grafted branch.
  • the activated polymer can react either with another polymer molecule so that the material of the fabric becomes cross- linked, or with the vinyl monomer in a co-polymerisation reaction.
  • An example of a suitable initiator is benzo- phenone .
  • the mole ratio of the vinyl monomer to the initiator is preferably at least about 50, more preferably at least about 100, especially at least about 175; the ratio is preferably less than about 1500, more preferably less than about 1000, especially less than about 500, more especially less than about 350; for example the ratio may be about 200.
  • the impregnation solution may include a component by which homopolymerisation of the vinyl monomer is inhibited.
  • suitable inhibitors include iron (II) and copper (II) salts which are soluble in the reaction medium, a preferred material for aqueous media being iron (II) sulphate.
  • the impregnation solution may include additional components to optimise reaction conditions such as surfactants to ensure that the solution fully impregnates the laminate, an appropriate mixture of solvents to ensure homogeneity of the solution, and so on.
  • a benefit of the present invention is that physical properties of the treated laminate (in particular, its tensile strength or its ability to be wetted by aqueous solutions or both) can be stable on prolonged exposure to an alkaline solution.
  • a laminate with stable physical properties is particularly appropriate for use as a separator in electrochemical devices in which the electrolyte comprises an alkaline solution.
  • a test to determine stability on exposure to alkaline solution involves storing a sample of a laminate to a solution containing 30% by weight of potassium hydroxide at 71°C for 21 days, and then comparing the selected property of the exposed laminate to that of a fabric that has not been exposed to the alkaline solution.
  • the invention provides an electrochemical device, comprising an anode, a cathode, a quantity of an electrolyte, and an electrode separator of the type discussed above.
  • the cathode in the device comprises nickel (II) hydroxide.
  • An example of material which can form the anode in such a device includes cadmium.
  • the anode may be a metal hydride electrode.
  • Other types of electrochemical device in which the separator of the invention finds application include secondary cells such as lead-acid cells.
  • a sample of a non-woven fabric weighing about 0.5 g is converted into the acid (H + ) form by immersion in 1.0 M hydrochloric acid at 60°C for 2 hours.
  • the sample is washed in distilled water until the washing water shows a pH in the range of about 6 to 7.
  • the sample is then dried to constant weight at 70°C.
  • the dried sample is placed in a 100 ml polyethylene bottle to which is added accurately 10 ml of approximately 0.1 M potassium hydroxide. Additional distilled water can be added to immerse the sample fully. A further 10 ml of potassium hydroxide is added to a second polyethylene bottle, together with the same amount of distilled water as that added to the bottle containing the sample. Both bottles are stored at 60°C for at least two hours.
  • each bottle After being allowed to cool, the contents of each bottle are transferred to glass conical flasks, and the amount of potassium hydroxide in each is determined by titration with standardised 0.1 M hydrochloric acid, using a phenolphthalein indicator .
  • the ion exchange capacity, measured in milliequivalents per gram, of the membrane in the dry acid (H + ) form is calculated according to the equation: t 2 - t ⁇
  • t x is the titration value of HC1 from bottle with the sample
  • t 2 is the titration value of HC1 from bottle without the sample
  • W is the weight of the dried membrane in acid (H0 form.
  • a weighed sample of a non-woven fabric laminate is converted into the potassium salt form by immersion in 0.1 M KOH for about 1 hour at 70°C.
  • the sample is washed in distilled water to remove excess KOH. Excess water is removed using a paper towel .
  • An ammonia solution is prepared by mixing 120 ml of distilled water and 5 ml 0.3 M NH 3 . The sample is immersed in the solution and placed in an oven at 40°C for 2 hours. The sample is then allowed to cool.
  • a control reading is obtained from the solution of ammonia in distilled water, without the laminate sample.
  • the fabric was impregnated with a solution of acrylic acid by passing the fabric around rollers located in a chamber with an atmosphere of nitrogen so that the fabric passed through the solution.
  • the solution was formulated as follows (percentages by weight) :
  • the impregnated fabric was maintained in an atmosphere of nitrogen and passed through an irradiation chamber defined by quartz glass walls.
  • Medium pressure mercury vapour lamps were positioned parallel to one another on opposite sides of the chamber outside the quartz glass walls.
  • the lamps had a power output of 120 W.c ⁇ f 1 and were located 16 cm from the fabric.
  • Each lamp provided a parallel ultraviolet light beam with a width of 10 cm.
  • the total exposure time of the fabric to the radiation was about 6 seconds.
  • the fabric was then washed in de-ionised water to remove unreacted components and then dried in an air oven at approximately 70°C.
  • the properties of the treated fabric are set out below, and compared with the corresponding properties of the polypropylene fabric starting material:
  • Electrolyte wicking rate time 60s 600s 60s 600s (30% w/w KOH) (DIN 53924-78) (mm) 0 0 45 80
  • Residual ion exchange capacity (meq.g -1 ) 0 0.28
  • a melt blown non-woven polypropylene fabric with a thickness of 200 ⁇ m, a fibre size of about 3 to 5 ⁇ m, and a basis weight of 46 g.m -2 was impregnated with an acrylic acid solution and irradiated as described above in Comparative Example 1.
  • the properties of the treated fabric are set out below, and compared with the corresponding properties of the polypropylene fabric starting material:
  • Electrolyte wicking rate time 60s 600s 60s 600s (30% w/w KOH) (DIN 53924-78) (mm) 0 0 39 132
  • Residual ion exchange capacity (meq.g -1 ) 0 0.48
  • a laminate was formed from a melt blown polypropylene fabric and a fabric formed from spun fibres.
  • the melt blown fabric had a basis weight of 14 g.m -2 and a fibre size of about 3 to 5 ⁇ m.
  • the spun fibre fabric had a basis weight of 36 g.m "2 and a fibre size of about 15 to 20 ⁇ m.
  • the laminate was created by the localised application of heat and pressure to form localised welds between the fibres of the fabrics.
  • the laminate had a thickness of 294 ⁇ m. It was densified by passage through a set of smooth rollers which were heated to a temperature of 125°C. Its thickness following densification was 170 ⁇ m.
  • the laminate was impregnated with an acrylic acid solution and irradiated as described above in Example 1.
  • Electrolyte wicking rate 60s 600s 60s 600s (30% w/w KOH) (DIN 53924-78) (mm) 0 0 50 110
  • Residual ion exchange capacity (meq.g -1 ) 0 0.4
  • a laminate was formed ⁇ from a melt blown polypropylene fabric, and two fabrics formed from spun fibres arranged on opposite surfaces of the melt blown fabric.
  • the melt blown fabric had a basis weight of 12 g.m -2 and a fibre size of about 3 to 5 ⁇ m.
  • the spun fibre fabric had a basis weight of 19 g.m "2 and a fibre size of about 15 to 20 ⁇ m.
  • the laminate was created by the localised application of heat and pressure to form localised welds between the fibres of the fabrics.
  • the laminate had a thickness of 229 ⁇ m.
  • the laminate was impregnated with an acrylic acid solution and irradiated as described above in Example 1.
  • the laminate was passed through smooth rollers heated to 97°C to reduce its thickness further, to 151 ⁇ m.
  • Residual ion exchange capacity (meq.g -1 ) 0.37
  • the spun fibre fabric of Comparative Example 1 can withstand large deformation at high strain rates. However, the pore structure is disrupted as a result.
  • the pore structure of the laminated structure of Example 2 is maintained at high deformation and at high strain rates.

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Electrochemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Cell Separators (AREA)
  • Secondary Cells (AREA)
  • Nonwoven Fabrics (AREA)
PCT/GB1998/001671 1997-06-18 1998-06-08 Non-woven fabric laminate WO1998058111A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CA002294599A CA2294599A1 (en) 1997-06-18 1998-06-08 Non-woven fabric laminate
EP98925860A EP0991804A1 (en) 1997-06-18 1998-06-08 Non-woven fabric laminate
JP50394299A JP2002504874A (ja) 1997-06-18 1998-06-08 不織布積層板

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9712692.4A GB9712692D0 (en) 1997-06-18 1997-06-18 Non-woven fabric laminate
GB9712692.4 1997-06-18

Publications (1)

Publication Number Publication Date
WO1998058111A1 true WO1998058111A1 (en) 1998-12-23

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EP (1) EP0991804A1 (ja)
JP (1) JP2002504874A (ja)
CN (1) CN1265166A (ja)
CA (1) CA2294599A1 (ja)
GB (1) GB9712692D0 (ja)
WO (1) WO1998058111A1 (ja)

Cited By (2)

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Publication number Priority date Publication date Assignee Title
WO2000001468A1 (en) * 1998-07-03 2000-01-13 Scimat Limited A gas filter element
EP1286403A2 (de) * 2001-08-23 2003-02-26 Johns Manville Europe GmbH Batterieseparatoren

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CN100347373C (zh) * 2004-12-17 2007-11-07 中国科学院上海应用物理研究所 真丝绸的染色方法
EP2011630A1 (de) * 2007-07-03 2009-01-07 F. Hoffmann-La Roche AG Verfahren zur Herstellung eines Analyseelementes
CN101725044B (zh) * 2009-11-19 2012-09-26 深圳市新纶科技股份有限公司 用于提高织物吸附性的处理方法及其设备
CN107574665A (zh) * 2017-08-29 2018-01-12 苏州市苏真床垫有限公司 一种亲水耐污染的聚丙烯无纺布及其制备方法
CN107574664A (zh) * 2017-08-29 2018-01-12 苏州市苏真床垫有限公司 一种透气阻燃保温聚丙烯无纺布及其制备方法
CN107447512A (zh) * 2017-08-29 2017-12-08 苏州市苏真床垫有限公司 一种适用于燃油过滤芯材的复合聚丙烯无纺布及其制备方法
CN107447513A (zh) * 2017-08-29 2017-12-08 苏州市苏真床垫有限公司 一种壳聚糖‑金属配合物改性的聚丙烯无纺布及其制备方法
CN107583098A (zh) * 2017-08-29 2018-01-16 苏州市苏真床垫有限公司 一种止血聚丙烯无纺布及其制备方法
CN107611323A (zh) * 2017-08-29 2018-01-19 苏州市苏真床垫有限公司 一种纳米二氧化硅改性聚丙烯无纺布的复合锂离子电池隔膜及其制备方法
CN107385905A (zh) * 2017-08-29 2017-11-24 苏州市苏真床垫有限公司 一种抗菌型共辐射接枝磺化聚丙烯无纺布及其制备方法
CN107447514A (zh) * 2017-08-29 2017-12-08 苏州市苏真床垫有限公司 一种阳离子单体接枝聚丙烯无纺布及其制备方法
IT201800005291A1 (it) * 2018-05-11 2019-11-11 Materiale composito stratificato con spalmatura in poliuretano e procedimento per ottenerlo
CN110428982B (zh) * 2019-07-31 2021-03-02 太仓碧奇新材料研发有限公司 一种超级电容器隔膜的制备方法

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WO1993001622A1 (en) * 1991-07-09 1993-01-21 Scimat Limited Polymeric sheet

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000001468A1 (en) * 1998-07-03 2000-01-13 Scimat Limited A gas filter element
EP1286403A2 (de) * 2001-08-23 2003-02-26 Johns Manville Europe GmbH Batterieseparatoren
EP1286403A3 (de) * 2001-08-23 2006-11-22 Johns Manville Europe GmbH Batterieseparatoren

Also Published As

Publication number Publication date
CA2294599A1 (en) 1998-12-23
JP2002504874A (ja) 2002-02-12
CN1265166A (zh) 2000-08-30
EP0991804A1 (en) 2000-04-12
GB9712692D0 (en) 1997-08-20

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