WO1995005940A1 - Multi-layered composite - Google Patents

Multi-layered composite Download PDF

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Publication number
WO1995005940A1
WO1995005940A1 PCT/GB1994/001609 GB9401609W WO9505940A1 WO 1995005940 A1 WO1995005940 A1 WO 1995005940A1 GB 9401609 W GB9401609 W GB 9401609W WO 9505940 A1 WO9505940 A1 WO 9505940A1
Authority
WO
WIPO (PCT)
Prior art keywords
layer
composite
composite according
base layer
tie
Prior art date
Application number
PCT/GB1994/001609
Other languages
French (fr)
Inventor
Grant William Duguid
Michael Bert Gill
Original Assignee
Bxl Plastics 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 Bxl Plastics Limited filed Critical Bxl Plastics Limited
Priority to AU72332/94A priority Critical patent/AU7233294A/en
Priority to JP7507395A priority patent/JPH08502701A/en
Priority to EP94921728A priority patent/EP0665784A1/en
Publication of WO1995005940A1 publication Critical patent/WO1995005940A1/en

Links

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
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/06Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B27/08Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • 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
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/32Layered products comprising a layer of synthetic resin comprising polyolefins
    • 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
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/12Interconnection of layers using interposed adhesives or interposed materials with bonding properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K15/00Arrangement in connection with fuel supply of combustion engines or other fuel consuming energy converters, e.g. fuel cells; Mounting or construction of fuel tanks
    • B60K15/03Fuel tanks
    • B60K15/03177Fuel tanks made of non-metallic material, e.g. plastics, or of a combination of non-metallic and metallic material
    • 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
    • B32B2307/20Properties of the layers or laminate having particular electrical or magnetic properties, e.g. piezoelectric
    • B32B2307/202Conductive
    • 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
    • B32B2309/02Temperature

Abstract

This invention relates to a multi-layer composite comprising one or more sequences comprising a base layer/tie-layer/EVOH/tie-layer/base layer, said composite having on at least one of its outer surfaces a conductive material either impregnated thereon or applied as a film on said outer surface. The base layer is preferably a polyolefin such as polyethylene. These composites are useful as vapour containment layers for fuel tanks.

Description

MULTI-LAYERED COMPOSITE This invention relates to a novel multi-layered composite comprising a plurality of polymer layers and a layer of a conducting material.
Composites comprising several polymers with or without a conducting layer are well known. In view of the limited ability of virgin polymeric layers to adhere to each other it is customary to introduce intervening tie layers having adhesive properties between the virgin polymers. Such tie layers may comprise grafting of maleic anhydride or acrylate ester polymers on to one surface of a polyolefin film and then applying thereon a further layer of a virgin polymer or a metallic layer in order to produce the desired composite. Such composites have found uses in various industries including the production of protective garments, canning of food products, and barrier films for oxygen, gasoline or other industries where toxic or hazardous emissions have to be .contained. Such composites can also be used to produce a flexible vapour containment liner (hereafter "VCL") for a fuel tank system in order to minimise the risk of accidental ignition and to control emissions from such tanks whether eg they be used in automotive vehicles, aircraft or in oil tankers. However, in the composites used hitherto, the primary problem has been the inability of such composites when used as VCL to contain to the desired degree the emission of fuel vapoursfrom such tanks.
It has now been found that by modifying the nature of and the components in the composites, an improved product can be produced which has all the desirable properties including its ability to be used as a VCL thereby mitigating the problems of prior art composites.
Accordingly, the present invention is a multi-layer composite comprising one or more sequences comprising a base layer/tie- layer/EVOH/tie-layer/base layer, said composite having on at least one of its outer surfaces a conductive material either impregnated thereon or applied as an additioinal layer on said outer surface. By the expression "composite" as used herein and throughout the specification is meant a product prepared either by lamination of several layers and/or by coextrusion of a number of components in order to give the desired product.
In the composite defined above, the expression "EVOH" signifies an ethylene-vinyl alcohol copolymer which may be derived by the hydrolysis of an ethylene-vinyl acetate copolymer.
In the composites of the present invention, the base layer may be that of a polyolefin, ethylene-vinyl acetate or an ionomer. The polyolefin layer, if used, may be suitably a layer of polyethylene, polypropylene or polybutene. Where the polyolefin layer is of polyethylene, it may be of high density polyethylene (hereafter
"HDPE"), of low density polyethylene (hereafter "LDPE"), of linear low density polyethylene (hereafter "LLDPE") or very low density polyethylene (hereafter "VLDPE"). A layer of VLDPE is preferred. If the base layer is that of an ionomer, the ionomer is suitably a salt of (meth)acrylic acid. These are commonly available as the
SURLYN® range of ionomers (ex Du Pont) . Other ionomers which may be used in this invention include the commercially available IOTE ® (ex Exxon) range.
The thickness of each of the base layers in the composite is suitably in the range from 55-70(Λm, preferably from 60-65μm.
The tie-layer in the composite is the adhesive layer which binds the base layers, eg of polyolefin, with the layer of EVOH and/or the film of a conductive material. The tie-layer may be formed by grafting at least one polymerizable ethylenically unsaturated monomer (hereafter "EUM" ) which is suitably an ethylenically unsaturated carboxylic acid, ester or anhydride on to a material which is the same as the base layer to form a graft-- copolymer. This enables the tie layer to key in and blend into the base layer when preparing the composite. ' Thus, if the base layer is of polyethylene, it is preferable for the tie-layer to be a graft copolymer of polyethylene and a polymerizable ethylenically unsaturated monomer. Examples of such polymerizable ethylenically unsatured monomers include maleic acid (hereafter "MA"), maleic anhydride (hereafter "MAH"), acrylic acid (hereafter "AA"), alkyl acrylate esters (hereafter "AAE"), methacrylic acid (hereafter
"MAA"), alkyl methacrylate esters (hereafter "AME"), itaconic acid, citraconic acid, mesaconic acid, 4-methyl cyclohex-4-ene-l,2- dicarboxylic acid anhydride, bicyclo (2.2.2)oct-5-ene-2,3- dicarboxylic acid anhydride, 1,2,3,4,5,8,9,10-octahydronaphthalene- 2,3-dicarboxylic acid anhydride, 2-oxa-l,3-diketospiro(4.4)non-7- ene, bicyclo(2.2.l)hept-5-ene-2,3-dicarboxylic acid anhydride (also known as and sold under the trade name NADIC ANHYDRIDE® by Allied Chemicals Corp and under HIMIC ANHYDRIDE® by Hitachi Chemical Co.), maleopimaric acid, tetrahydrophthalic anhydride, methyl-norborn-5- ene-2, 3-dicarboxylic acid anhydride, norborn-5-ene2,3-dicarboxylic acid anhydride, and other fused ring monomers described in US-A-3 873 643 and US-A-3 882 194. Of these, maleic anhydride, tetrahydrophthalic anhydride and bicyclo(2.2.1)hept-5-ene-2,3- dicarboxylic acid anhydride are preferred. Conjugated unsaturated esters, in addition to the alkyl acrylates and alkyl methacrylates mentioned above, may also suitably be used for cografting. These esters include, eg, dialkyl maleates, dialkyl fumarates, dialkyl itaconates, dialkyl mesaconates, dialkyl citraconates, alkyl crotonates, alkyl tiglates wherein the alkyl group aliphatic, cycloaliphatic, alicyclic or an arlkyl group and suitably has 1-12 carbon atoms. Dibutyl maleate, diethyl fumarate and dimethyl itaconate are particularly preferred. These monomers may be used either alone or in combination with the anhydrides listed above and are suitably applied to at least one side of the base layer. Methods of grafting these monomers on to the base layer are well known in the art. For instance, methods of grafting MAH to the base layer are described eg in US-A-2973344" and US-A-3290415. The grafting may be performed in a solvent by placing the monomer in a solvent followed by irradiation as described in US-A-3290415 with peroxides. Alternatively, the grafting may be carried out, eg in the case of polypropylene, by melt mixing with peroxides. The peroxides that may be used include, eg, t-butyl hydroperoxide, p-menthane hydroperoxide, pinane hydroperoxide and cumene hydroperoxide. Other grafting techniques include extrusion grafting and coating the polyolefin surface with a molten monomer followed by irradiation as described eg in US-A- 3290415. These methods are incorporated herein by reference to these prior publications.
The thickness of the tie-layer is suitably from l-5μm, preferably from 3-7μm. The material used for producing the tie- layer is suitably MAH.
The EVOH used is suitably of a grade which contains from 25-50 mol% of ethylene, preferably from 29-44 mol% and even more preferably from 32-38 mol %. Examples of EVOH grades that may be used include inter alia , the so-called EVAL® LCH 101 or EPJ 102B (both ex Kuraray Industries). The thickness of the EVOH layer is suitably from 7-20μm, preferably from 10-15μm.
The conductive material may be finely powdered carbon or metal which is present in an amount such that the conductivity of the impregnated layer is suitably from 104-105 ohms per unit square.
Powdered carbon is preferred due to its desired surface resistivity properties.
The conductive material may either be impregnated on the base layer or applied as a separate, additional layer on the base layer. Where this is applied as a separate layer, this separate layer is suitably that of a polyethylene or polyurethane containing powdered carbon or other metallic powder impregnated therein.
The co-extrusion, where used, is suitably carried out within an overall average temperature in the range from 210-230°C. , Within this range the base layer is suitably maintained at 190-210 o C, and the EVOH layer at 210-220°C.
Where the composite is prepared by combining more than ortfe sequence of base layer/tie-layer/EVOH/tie-layer/base layer, the adhesive used to combine such sequences is suitably a polyurethane adhesive. Examples of such adhesives that may be used include a polyester/polyurethane adhesive or a polyether/polyurethane adhesive. The adhesive can also be used to bind a layer of the conductive material to a base layer at one end of the composite. The composite preferably has at least two such sequences and the grades of any of the generic components in each sequence may be same or different.
The composites of the present invention and the use thereof as a VCL is illustrated with respect to the following Example: EXAMPLE 1; A specific example of the composite of the present invention is that comprising in sequence the following layers produced initially as 5-layer composites by co-extrusion of a EVOH (EPJ-102B, ex Kuraray) fed to be sandwiched between two layers of VLDPE (STAMYLEX® 09016, ex DSM) each of which VLDPE layers has an inner tie-layer of a copolymer of VLDPE grafted with MAH (ADMER® NF 520E, ex Kuraray) facing each other, using conventional techniques with a co-extruder (BARMAG four-component, 5-layer extruder) maintaining an average temperature of about 220°C. Two such composites having outer VLDPE facings were then laminated together using a two- component polyester/urethane adhesive ADCOTE®102A (which has a diisocyanate catalyst eg MDI or TDI, ex Morton International) to form an 11-layer composite in which the middle layer was the adhesive. This was followed by eventual lamination of one of the outer layers of the 11-layer composite with a carbon filled polyethylene resin grade B701A (ex British Polyethylene Industries Ltd) which forms the conductive layer. Thus, the final extended composite had the following structure:
VLDPE/TL/EVOH/TL/VLDPE/AD/VLDPE/TL/EVOH/TL/VLDPE/AD/CFP wherein VLDPE represents - very low density polyethylene TL represents - the graft copolymer of polyethylene & maleic anhydride used as tie-layer
EVOH represents - ethylene-vinyl alcohol AD represents - the polyester/urethane adhesive CFP represents - the carbon filled polyethylene - The extended composite so formed was cured at 40°C for 48 hours. In such an extended composite the thickness (μ ) of the respective layers was as follows:
65/5/10/5/65/AD/62/5/15/5/63/AD/50 The adhesive layer, AD, was spread on the surface of the appropriate internal polyethylene layer in an amount of about 5g/m2.
The conductive layer of such an extended composite had a conductivity of 1 x IO5 ohms/unit2. The extended composite was subjected successfully to a flex test involving a repeated double folding of the extended composite over 2000 cycles without any change in its appearance or physical characteristics. EXAMPLE 2:
The above process of Example 1 was repeated to produce a second composite except that in this case the EVOH layers were those of EVAL® LCH 101 (ex Kuraray) . This extended composite was also subjected successfully to a flex test involving a repeated double folding thereof over 2000 cycles without any change in its appearance or physical characteristics. EXAMPLE 3: TESTING AS VAPOUR CONTAINMENT LAYERS:
The extended composites from Examples 1 and 2, each of which had already been subjected to 2000 flexing cycles, were then used as a VCL for fuel tanks, the layer containing the conductive material being on the air side and the layer devoid of conducting material being on the fuel side of such a tank, to test its barrier properties. The volatile loss of fuel through the extended composites in each case, which had already been subjected to 2000 flexing cycles, was less than 0.18g/24hrs/m .

Claims

Claims:
1. A multi-layer composite comprising one or more sequences comprising a base layer/tie-layer/EVOH/tie-layer/base layer, said composite having on at least one of its outer surfaces a conductive material either impregnated thereon or applied as an additioinal layer on said outer surface.
2. A composite according to Claim 1 wherein said composite is a product prepared either by lamination of several layers and/or by coextrusion of a number of components.
3. A composite according to any one of the preceding Claims wherein the base layer is that of a polyolefin, ethylene-vinyl acetate or an ionomer
4. A composite according to Claim 3 wherein the polyolefin base layer is a layer of polyethylene, polypropylene or polybutene.
5. A composite according to Claim 3 or 4 wherein the polyolefin base layer is of high density polyethylene, of. low density polyethylene, of linear low density polyethylene or very low density polyethylene.
4. A composite according to Claim 3 wherein the base layer is that of an ionomer which is a salt of (meth)acrylic acid.
5. A composite according to any one of the preceding Claims wherein the thickness of each of the base layers is in the range from 55-70μm.
6. A composite according to any one of the preceding Claims wherein the tie-layer is the adhesive layer which binds the base layers with the layer of EVOH and/or the film of a conductive material.
7. A composite acccording to any one of the preceding Claims- wherein the tie-layer is formed by grafting at least one polymerizable ethylenically unsaturated monomer (hereafter "EUM") on to a material which is the same as the base layer to form a graft- copolymer.
8. A composite according to Claim 7 wherein the base layer is of polyethylene and the tie-layer is a graft copolymer of polyethylene and a polymerizable ethylenically unsaturated monomer.
9. A composite according to any one of the preceding Claims wherein the thickness of the tie-layer is from l-5μm.
10. A composite according to any one of the preceding Claims wherein the EVOH is of a grade which contains from 25-50 mol% of ethylene.
11. A composite according to any one of the preceding Claims whrein the thickness of the EVOH layer is from 7-20μm.
12. A composite according to any one of the preceding Claims wherein the conductive material is finely powdered carbon or metal which is present in an amount such that the conductivity of the impregnated layer is from 10'*-10--' ohms per unit square.
13. A composite according to any one of the preceding Claims wherein the conductive material is either impregnated on the base layer or applied as a separate, additional layer on the base layer.
14. A composite according to any one of the preceding Claims wherein the composite is formed by a co-extrusion process operated within an overall average temperature in the range from 210-230°C and wherein the base layer is maintained at 190-210°C and the EVOH layer at 210-220°C.
15. A composite according to any one of the preceding Claims 1-13 wherein the composite is prepared by combining more than one sequence of base layer/tie-layer/EVOH/tie-layer/base layer and the adhesive used to combine such sequences is a polyurethane adhesive. Examples of such adhesives that may be used include a polyester/polyurethane adhesive or a polyether/polyurethane adhesive. The adhesive can also be used to bind a layer of the conductive material to a base layer at one end of the composite. The composite preferably has at least two such sequences and the grades of any of the generic components in each sequence may be same or different.
16. A composite according any one of the preceding Claims wherein said composite is capable of being subjected to a flex test involving a repeated double folding thereof over 2000 cycles without any change in its appearance or physical characteristics.
17. A vapour containment layer comprising a composite according to any one of the preceding Claims for use in fuel tanks such that in use the layer containing the conductive material is on the air side and the layer devoid of conducting material is on the fuel side of such a tank.
PCT/GB1994/001609 1993-08-25 1994-07-27 Multi-layered composite WO1995005940A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
AU72332/94A AU7233294A (en) 1993-08-25 1994-07-27 Multi-layered composite
JP7507395A JPH08502701A (en) 1993-08-25 1994-07-27 Multi-layer composition
EP94921728A EP0665784A1 (en) 1993-08-25 1994-07-27 Multi-layered composite

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB939317631A GB9317631D0 (en) 1993-08-25 1993-08-25 Multi-layered composite
GB9317631.1 1993-08-25

Publications (1)

Publication Number Publication Date
WO1995005940A1 true WO1995005940A1 (en) 1995-03-02

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ID=10740981

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB1994/001609 WO1995005940A1 (en) 1993-08-25 1994-07-27 Multi-layered composite

Country Status (6)

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EP (1) EP0665784A1 (en)
JP (1) JPH08502701A (en)
AU (1) AU7233294A (en)
CA (1) CA2147763A1 (en)
GB (1) GB9317631D0 (en)
WO (1) WO1995005940A1 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0975909A1 (en) * 1997-04-15 2000-02-02 Nordson Corporation Apparatus for use in applying electrostatically charged coating material
EP1122113A1 (en) * 2000-02-07 2001-08-08 TI Group Automotive Systems Technology Center GmbH Fuel tank having a multilayer structure
US6294269B1 (en) * 1996-06-27 2001-09-25 Elf Atochem, S.A. Coextrusion binder, its use in a multilayer structure and the structure thus obtained
WO2003018699A3 (en) * 2001-08-23 2003-09-04 Dow Global Technologies Inc Fuel tanks
US6664258B1 (en) 1996-08-26 2003-12-16 Pfizer Inc Spirocyclic dopamine receptor subtype ligands
EP1728669A2 (en) 1999-12-22 2006-12-06 Inergy Automotive Systems Research (SA) Fuel tank made of thermoplastic manufactured from an extruded parison
US7360552B2 (en) 2004-04-23 2008-04-22 Dow Global Technologies Inc. Injectable structural adhesive

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4058647A (en) * 1975-02-27 1977-11-15 Mitsubishi Petrochemical Co., Ltd. Process for preparing laminated resin product
EP0365266A2 (en) * 1988-10-17 1990-04-25 Nippon Petrochemicals Company, Limited Multi-layered blow-molded bottle
EP0470606A1 (en) * 1990-08-09 1992-02-12 Ems-Inventa Ag Antistatic fuel line

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4058647A (en) * 1975-02-27 1977-11-15 Mitsubishi Petrochemical Co., Ltd. Process for preparing laminated resin product
EP0365266A2 (en) * 1988-10-17 1990-04-25 Nippon Petrochemicals Company, Limited Multi-layered blow-molded bottle
EP0470606A1 (en) * 1990-08-09 1992-02-12 Ems-Inventa Ag Antistatic fuel line

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6294269B1 (en) * 1996-06-27 2001-09-25 Elf Atochem, S.A. Coextrusion binder, its use in a multilayer structure and the structure thus obtained
US6664258B1 (en) 1996-08-26 2003-12-16 Pfizer Inc Spirocyclic dopamine receptor subtype ligands
EP0975909A1 (en) * 1997-04-15 2000-02-02 Nordson Corporation Apparatus for use in applying electrostatically charged coating material
EP1728669A2 (en) 1999-12-22 2006-12-06 Inergy Automotive Systems Research (SA) Fuel tank made of thermoplastic manufactured from an extruded parison
EP1728669A3 (en) * 1999-12-22 2011-03-16 Inergy Automotive Systems Research (SA) Fuel tank made of thermoplastic manufactured from an extruded parison
EP1122113A1 (en) * 2000-02-07 2001-08-08 TI Group Automotive Systems Technology Center GmbH Fuel tank having a multilayer structure
WO2003018699A3 (en) * 2001-08-23 2003-09-04 Dow Global Technologies Inc Fuel tanks
CN100389979C (en) * 2001-08-23 2008-05-28 陶氏环球技术公司 Fuel tanks
US7360552B2 (en) 2004-04-23 2008-04-22 Dow Global Technologies Inc. Injectable structural adhesive

Also Published As

Publication number Publication date
JPH08502701A (en) 1996-03-26
GB9317631D0 (en) 1993-10-13
EP0665784A1 (en) 1995-08-09
AU7233294A (en) 1995-03-21
CA2147763A1 (en) 1995-03-02

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