CA1125229A - Irradiated laminate film having heat sealing characteristics - Google Patents

Irradiated laminate film having heat sealing characteristics

Info

Publication number
CA1125229A
CA1125229A CA337,225A CA337225A CA1125229A CA 1125229 A CA1125229 A CA 1125229A CA 337225 A CA337225 A CA 337225A CA 1125229 A CA1125229 A CA 1125229A
Authority
CA
Canada
Prior art keywords
layer
irradiation
enhancer
layer structure
heat
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA337,225A
Other languages
French (fr)
Inventor
Alfred P. Engelmann
William G. Baird, Jr.
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
WR Grace and Co Conn
Original Assignee
WR Grace and Co
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 WR Grace and Co filed Critical WR Grace and Co
Application granted granted Critical
Publication of CA1125229A publication Critical patent/CA1125229A/en
Expired legal-status Critical Current

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
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03Extrusion 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
    • B29C48/07Flat, e.g. panels
    • B29C48/08Flat, e.g. panels flexible, e.g. films
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03Extrusion 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
    • B29C48/09Articles with cross-sections having partially or fully enclosed cavities, e.g. pipes or channels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03Extrusion 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
    • B29C48/09Articles with cross-sections having partially or fully enclosed cavities, e.g. pipes or channels
    • B29C48/10Articles with cross-sections having partially or fully enclosed cavities, e.g. pipes or channels flexible, e.g. blown foils
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/14Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the particular extruding conditions, e.g. in a modified atmosphere or by using vibration
    • B29C48/147Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the particular extruding conditions, e.g. in a modified atmosphere or by using vibration after the die nozzle
    • B29C48/1472Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the particular extruding conditions, e.g. in a modified atmosphere or by using vibration after the die nozzle at the die nozzle exit zone
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/16Articles comprising two or more components, e.g. co-extruded layers
    • B29C48/18Articles comprising two or more components, e.g. co-extruded layers the components being layers
    • B29C48/21Articles comprising two or more components, e.g. co-extruded layers the components being layers the layers being joined at their surfaces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/30Extrusion nozzles or dies
    • B29C48/32Extrusion nozzles or dies with annular openings, e.g. for forming tubular articles
    • B29C48/335Multiple annular extrusion nozzles in coaxial arrangement, e.g. for making multi-layered tubular articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/88Thermal treatment of the stream of extruded material, e.g. cooling
    • B29C48/91Heating, e.g. for cross linking
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/25Component parts, details or accessories; Auxiliary operations
    • B29C48/88Thermal treatment of the stream of extruded material, e.g. cooling
    • B29C48/919Thermal treatment of the stream of extruded material, e.g. cooling using a bath, e.g. extruding into an open bath to coagulate or cool the material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C71/00After-treatment of articles without altering their shape; Apparatus therefor
    • B29C71/04After-treatment of articles without altering their shape; Apparatus therefor by wave energy or particle radiation, e.g. for curing or vulcanising preformed articles
    • 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
    • B32B27/18Layered products comprising a layer of synthetic resin characterised by the use of special additives
    • B32B27/26Layered products comprising a layer of synthetic resin characterised by the use of special additives using curing agents
    • 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
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/15Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with at least one layer being manufactured and immediately laminated before reaching its stable state, e.g. in which a layer is extruded and laminated while in semi-molten state
    • B32B37/153Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with at least one layer being manufactured and immediately laminated before reaching its stable state, e.g. in which a layer is extruded and laminated while in semi-molten state at least one layer is extruded and immediately laminated while in semi-molten state
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2791/00Shaping characteristics in general
    • B29C2791/004Shaping under special conditions
    • B29C2791/007Using fluid under pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/001Combinations of extrusion moulding with other shaping operations
    • B29C48/0018Combinations of extrusion moulding with other shaping operations combined with shaping by orienting, stretching or shrinking, e.g. film blowing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/001Combinations of extrusion moulding with other shaping operations
    • B29C48/0019Combinations of extrusion moulding with other shaping operations combined with shaping by flattening, folding or bending
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/24Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2995/00Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037Other properties
    • B29K2995/0049Heat shrinkable
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2009/00Layered products
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2023/00Tubular articles
    • B29L2023/001Tubular films, sleeves
    • 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
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/72Cured, e.g. vulcanised, cross-linked
    • 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
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/31Heat sealable
    • 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
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/514Oriented
    • B32B2307/518Oriented bi-axially
    • 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
    • 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
    • B32B2309/12Pressure
    • 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
    • B32B2439/00Containers; Receptacles

Abstract

IRRADIATED LAMINATE FILM HAVING
HEAT SEALING CHARACTERISTICS

Abstract A coextruded irradiated film has a crosslinked layer and a heat sealable layer. The crosslinked layer is crosslinked by irradiation at a dosage level sufficiently low that the heat sealing properties of the heat sealable layer are not adversely affected. The crosslinked layer is crosslinked to a desirable level due to the presence of irradiation crosslinking enhancers which are incorporated within the crosslinked layer so as to promote crosslinking at a low dosage level.

Description

~L~L~S~ 3 Backyround Of ~he Invention The present invention relates generally to the art of crosslinked films and more particularly to the art of coextruded ~ilms having improved heat seal properties while simultaneously having the benefit of radiation induced crosslinking.
The use of heat shrinkable thermoplastic film in many packaging applications is well known. Usually a product is enclosed within a film, sealed and heated to shrink the film snugly about the product.
One of the most useful and satisfactory thermoplastic materials for packaging film is polyethylene. In the prior art, there are a number of methods to convert polyethylene into suitable heat shrinkable packaging films. One such method is disclosed in U. S. Patent No. 2,85~,517 to W.
C. Ranier et al. Another method is disclosed in U. S. Patent No. 3,022,543 to W. G. Baird, Jr. et al. In the Baird, Jr. et al process, polyethylene is continuously extruded in the fonn of a tube, drawn, lrradiated with electrons to crosslink the polyethylene molecules, heated and stretched again by applying internal pressure to the tubing. The resulting film from this proccess has highly desirable heat shrink properties.
It is generally known in the art that polymers and copolymers of olefins, particularly polyethylene, become thermosets if a sufficient radiation dosage is applied to the olefin object. For this reason it has been customary to fonm articles prior to an irradiation step in order to avoid the undesirable forming properties brought about by the transition from a thermoplastic to a thermosetting material. Also accompanying the transition from a thermoplastic to a thermosetting article is the progressively lessening ability of an olefin polymer article to heat seal to ltself or to some other object as the radiation dosage is increased. For this reason ;t has generally been recognized in the film art that highly irradiated polyethylene films do not possess
-2-.

' .
.

25,Z~3 the ability to form reliable high strength heat seals. The prior art has thus had to either rely upon a low radiation dosage in order to preserve heat sealing properties or to utili~e a second layer or lamination which possesses desirable heat sealing properties and which is applied to the irradiated layer at some time after the process of irradiating.
Summary Of The Invention It is thus an object of this invention to provide a novel ~ilm laminate which possesses the desirable characteristics associated with crosslinking brought about by irradiation while at the same time possessing heat sealing characteristics similar to those of non-irradiated articles.
The invention provides a process for producing a multi-layer irradiated structure having heat seal characteristics comprising the steps of:
providing a multi-layer structure having a crosslinkable layer including an irradiation enhancer and a heat sealable layer;
irradiating said multi-layer structure at a radiation dosage sufficient to crosslink said crosslinkable layer but insufficient to adversely affect the heat sealing characteristics of said heat sealable layer.
The invention also provides a coextruded multi-layer polymeric structure having a crosslinked layer including an irradiation crosslinking enhancer and a heat sealable layer.

:```

~ _3_ :
:
;

Brief Descriptlon Of The Drawings The single figure of drawing schematically illustrates a process for producing the coextruded laminate film of this invention.
Detailed Uescr7ption In accordance with this invention it has been found that it is possible to produce a coextruded laminate film structure which is crosslinked by irradiation while retaining the desirable hea'c sealing characteristics associated with non crosslinked structures within an outer layer of the laminate. This desirable combination of properties is brought about by incorporating into one of the layers of the laminate an irradiation crosslinking enhancer so as to greatly improve the crosslinking efficiency of the radiation utilized in the step of irradiating. The irradiation enhancer sufficiently lowers the necessary dosage level to a point at which the heat sealable layer is not adversely affected in its heat sealing characteristics by the incident radiation.
As used within this disclosure the term "polymer" is used with its normal meaning to include homopolymers, copolymers, terpolymers, etc. The term "crosslinking" is utilized to mean the union of polymer molecules by a mechanism involving primary chemical bonds to have the effect of binding a polymer into a single network so that functionally several molecules become bound together into a single molecule. As applied to polymers of mono-olefins particularly polymers and copolymers of ethylene, crosslinking is detectable by an increase in the remaining residue when the sample is contacted with toluene under reflux condition for about two days. This is generally referred to as the gel content.
Thus, crosslinking is detected by an increase in the gel content of the crosslinked sample as compared to a non or lesser crosslinked sample.

.

:

.,~ . . ,. . ~

z~

As used within this disclosure9 the term "irradiation crosslinking enhancer" is a chemical composition which when blended with a polymer in the melt form produces a material which crosslinks to a greater extent from a given radiation dosage than does the same polymer without the irradiation crosslinking enhancer additive. Thus an additive which when blended with a polymer to produce an irradiated crosslinked product having a higher gel content than the same polymer at the same radiation dosage level without the additive is an irradiation crosslinking enhancer.
In its broadest aspects the lami-nate of this invention comprises a core layer and a heat sealable layer which have both been through an irradiation step to crosslink the core layer to a high degree due to the presence therein of an irradiation crosslinking enhancer. The term "core" as used herein with reference to the core layer of the laminate of this invention is used to identify as an essential 1ayer the layer which is crosslinkable, rather than to l;mit the core layer to a central or innermost layer. The laminate may comprise, however, additional layers such as additional heat sealing layers, or a layer to inhibit the passage of gaseous or liquid substances such as oxygen or moisture.
The core layer of the laminate of this invention i5 a polymer which is crosslinkable by irradiation and which may be enhanced in its crosslinking ability when blended with an irradiation crosslinking enhancer in accordance with this invention. Crosslinking using irradiation can be accomplished by various methods. Thus there can be used electrons, x-rays, and radiation of actinic origin such as ultraviolet light having a wave length above about 2,000 angstroms and below about 2,700 angstroms.
Preferably, however, electrons of at least 105 electron volts energy are applied. The irradiation source can be a Van der Graaff type electron accelerator having an operat;onal voltage of 2 megavolts at a power , , ~` ~L ~5'~

output of about 5 to 10 kilowatts. Preferably, however, the source of electrons is an electron accelerator powered by an insulated core transformer having an accelerating voltage from about 300 to 3,000 kilovolts.
The absorbed radiation within the core layer is stated by the term "RAD". The RAD is defined as an energy dosage level of 100 ergs per gram imparted by the ionizing radiation to the irradiated material at the point of interest. The core material utilized in this inYention, i.e., the polymer blended with the irradiation enhancer, is a material which will when blended with an enhancer undergo sufficient crosslinkage to increase the gel content thereof at a dosage level within the range of about 0.1 to about 5 megarads (MR).
The polymeric material with which is blended an irradiation enhancer to form the core layer of the laminate of this invention may be selected from a broad class of materials, i.e., those materials which crosslink when subjected to irradiation. While polymers of ethylene including copolymers thereof constitute the preferred material utilized within this invention, the invention may generally be carried out with polymers of other mono-olefins particularly the l-alkenes and copolymers thereof. Particularly the invention may be carried out with polymers of propylene, butylene, pentene and hexene. The invention may additionally -be carried out on vinyl chloride polymers and copolymers. The invention ~ -is particularly applicable to copolymers of ethylene and vinyl esters, e.g., vinyl acetate~ The invention is applicable to any of the polymers of ethylene such as high and low density ethylene polymers produced by ` 25 both high pressure and low pressure processes as well as mixtures and - blends thereof. 5 Many irradiation crosslinking enhancers are known to the art.
; Any such enhancer may be utilized within the core layer of the laminateof this invention. While not meant to be limiting, the fullowing is a .
, .

^ " ~L~L~5'~ 3 general listing of suitable classes of irradiation enhancers;
dialkyl maleates and fumarates in which the alkyl group contains 4 or more (usually 4 to 20) carbon atoms;
vinyl esters of fatty acids in which the fatty acid contains 3 or more (usually 3 to 20) carbon atoms;
vinyl alkyl ethers in which the alkyl group con-tains 18 or more (usually 18 to 30~ carbon atoms;
alkyl acrylates in which the alkyl group contains 1 or more (usually from 1 to 20) carbon atoms; and alkyl methacrylates in which the alkyl group contains
3 or more (usually from 3 to 20) carbon atoms.
Particularly preferred irradiation crosslinking enhancers for use with this invention are allyl methacrylate, allyl acrylate and diallyl maleate. The irradiation crosslinking enhancer can be incorporated into the core layer by several conventional techniques, e.g., mixing the materials from the powder form, blending the enhancer into the polymer in the molten state or by diffusing the irradiation crosslinking enhancer in the gaseous or liquid form into the solid polymer. It is preferred, however, to first mix the irradiation crosslinking enhancer in the powder form prior to melt blending the precursor of the core layer prior to melt extrusion. The irradiation enhancer in the solid polymer will not cause any crosslinking until the layer has been acted upon by a source of radiation as discussed above. The irradiation enhancer is normally employed in a small amount from about 0.~05 to about 10 weight percent of the overall composition of the core layer, but in any event in an amount sufficient to ;ncrease the gel content of the core layer~ -The heat sealable layer of the laminate film of this invention which is coextruded simultaneously with the extrusion of the core layer is of any material conventionally used for its heat sealing capability.
Such materials generally heat seal to themselves at a temperature within the range of about 70 to about 150~ C under a pressure from about 5 :, , .
' :- .

r ;;25~

to abDut 50 lbs. per square inches (35 KPa to 350 KPa). Such materials then have a peel strength above 1 lb. per inch of width (17.9 kg/m) as measured by ASTM D-903. Such ~aterials preferably have a peel strength above about 10 lbs per inch of width (179 kg/m).
Materials which can be utilized for the heat sealable layer of the laminate of this invention include both high and low density polyethylene, polypropylene and other polymers of l-mono-olefins. Particularly effective heat sealable substances include unsaturated ester polymers 5uch as ethylene/unsaturated ester copolySmers, e.g. ethylene/vinyl acetate, ethylene/vinyl propianate, ethylene/ethyl methacrylate, ethylene/ethyl methacrylate, ethylene/ethyl acrylate, ethylene/isobutyl acrylate, and the like; unsaturated carboxylic acid copolymers~ e.g., ethylene/unsaturated carboxylic acid copolymers, e.g., ethylene/acrylic acid, ethylene/methacrylic acid, ethylene/maleic acid, ethylene/fumaric acid9 ethylene/itaconic acid, and the like. The carboxylic acid groups of the acid copolymers may be either partly or wholly-neutralized to form what is commonly referred to as an ionomer. Particularly preferred heat sealable materials .~
are copolymers of ethylene and vinyl acetate containing from about 5 to about 40 weight percent of vinyl acetate. This listing, however, is not meant to be exhaustive but merely exemplary of the materials which might be utilized as a heat sealable layer within the laminate of this invention.
These materials generally tend to diminish in their heat sealing ability upon exposure to irradiation sufficient to crosslink an otherwise non irradiation enhanced layer. By utilizing a core layer having an irradiation enhancer, however, the heat sealable layer is not exposed to sufficient radiation dosage to significantiy deleteriously affect the heat sealing quality of the heat sealable layer.
' .

, -~L~2 5'~ 3 The laminate film of this invention after being coextruded by conventional techniques is irradiated to a dosage level su~ficient to enhance the mechanical and chemiGal properties of the core layer film without deleteriously affecting the heat seal qualities of the heat sealable layer. Preferably irradiation is carried out to a dosage level of about 0.1 to about 4 MR. This dosage level is sufficient to assure crosslinking within the core layer without adversely affecting the heat sealing characteristics of the heat sealable layer. One of the primary reasons for carrying out a crosslinking reaction is to enhance the ability of the core layer to undergo an orientation process so as to provide a heat shrinkable film. It is not necessary to the concept of this invention that an orientation process be carried out, however, since the irradiation crosslinking process enhances other desirable characteristics of the laminate film other than the ability to undergo orientation. It is preferred, however that the laminate film produced by this invention be oriented by conventional techniques so as to provide a film having heat shrink characteristics. It is especially preferred that such heat shrink characteristics exist at a temperature at or below the boiling point of water, i.e., lOO~C. For purposes of this invention a laminate is biaxially oriented, if it exhibits a free shrinkage at 96C of at least 10~ in both the longitudinal and transverse directions.
The laminate of this invention is preferably produced by coextrusion of the materials in a tubular form as is generally described in U. S. Patent 3,874,967 to H. G. Sch;rmer commonly assigned herewith.
The process of producing a laminate film of this invention is generally illustrated in the single figure of drawing. As is illustrated therein, two extruders, 2 and 3, are utilized for supplying coextrusion die 4 with var;ous layers utilized for the laminate of this invention. Thus extruder 2 may be supplied with the core layer polymer including the irrad;ation enhancer and extruder 3 may be suppl;ed w;th the heat 9 :
.

.

~~ ~L~L~5'~ 3 sealable layer of material. The extruders supply coextrusion die 4 so as to produce a tubular film 6. The die is positioned to extrude the tube downwardly into a cooling bath 8 of water or other inert liquid maintained at a temperature of between -18~C and ~21C. The cooled and flattened tubing of tape 16 is fed through feed rolls 18 into an irradiation vault 20 which houses and encloses a source of electrons 22. Following irradiation, the tape is fed by feed rolls 20 to a hot bath 30 in racking tank 46 which contains water or other liquid inert to the polymer layers. This liquid is maintained at a temperature sufficient to heat the tape to a desirable orientation temperature for the inner core layer. This temperature will vary somewhat depending upon the composition of the core layer. Orientation techniques are well known in the art, however, and a desirable orientation temperature is readily ascertainable for a particular polymer film material. For example, crosslinked low density polyethylene orients well at a temperature of about 88 to 102C.
The preferred temperature, however, is about 96C. Air or other gasses are introduced into the heated tape to form a bubble 38 between the ; surface of the hot bath and the upper deflate rolls 34. The amount of inflation is preferably sufficient to provide a stretch of from about 3 ~-to 1 to about 8 to 1 ;n each direction.
While the above description refers primarily to a coextruded laminate having only the two layers, it is readily apparent that other materials may be coextruded along wlth the two essential layers. The most read;ly extrudable layer would be an additional heat sealable layer identica~l in composition to the primary heat sealable layer in order to "": : : :
` provide a three layer laminate wh;ch sandw;ches the core layer. Other ~ . .
materials, however, such as layers to inhibit oxygen permeat;on, may be .
included along with the core and heat sealable layer or layers.
:
~ 30 .

. ~.

~z~z~

Having generally set forth the invention above, the following specific examples are given as a further exemplification of the laminate of this invention.
EXAMPLE I
Several samples were produced utilizing a core layer having incorporated therein an irradiation crosslinking enhancer in accordance with this invention. Structures comprising three concentric layers were coextruded from a 4 inch die utilizing an equal weight blend of high and low density polyethylenes within each layer. The central layer of the structures, however, contained a small percentage of diallyl maleate as an irradiation enhancer. All samples were oriented by the bubble technique at a temperature of approx;mately 250 F to provide a stretch of about 5 to 1 in both the machine and transverse directions. The samples were immediately chilled after orientation. Each of the samples had a thickness of about 1 mil (25 micrometers) after the orientation step. The properties of each sample as well as an identification of each sample is contained in the following table.

` 20 ;

:

:

-Z~
L~
~n o o 0 o~ o o~
~ o 1~ t~ a~ r~
> r~
n~ o ?~ L o N ~ ,_ C ~
~1) ~ 0 ~ C~J N
Q) ~ O C;~ oD CO 0 .,_ L~
cn o C O
_, L~
C o '~ ~. O O~
ul ~ O ~ N r-- ~
D_ ~5 ~ N ~> N
.
C ~ o O C O U~ N
O O 0;~ N
N r-- N

c a~ O
O O CO r~ ~
c ~ o o co u~ d-C o ~S O O ~ N

I_ __ ' 1~1 `~CD c_ ~ C~ ~
QJ :
3 :~: O O O

C_ .C~ : ' Ln t _ O
,, s .
t_ ~ ~ ~ ,_ N
; `'. :
?`
~ : ~

E
U~ C

-~L~ 2 EXAMPLE II
Two samples were produced utilizing a core layer having incorporated therein an irradiation crosslinking enhancer in accordance with this invention. The two structures were produced of the same material in substantially the same way as ~he samples in Example 1. Samples 3 and 4 were produced of polyethylene blends similar to the blends utilized in samples 1 and 2 but did not contain an irradiation crosslinking enhancer and were produced as a single layer having a thickness comparable to that of samples 1 and 2. All samples had a total thickness of about 0.75 mils (about 19 micrometers~. The coèxtruded structures had layers of equal thickness.
The gel content of each sample was determined by refluxing samples in toluene for 21 hours in order to insure complete solution of all soluble portions. This data is tabulated in Table Il along with an identification of the samples, the dosage and an indication as to whether the gel content was determined from the outer heat sealable layer or core layer. It should be noted that the outer layers of the samples having no irradiation crossl;nking enhancer had no gel while the core layer which contained the enhancer had gel percentages higher than sample no. 3 which contained no irradiation crosslinking enhancer.
Samples 1 through 4 were tested for seal strengths utilizing ASTM standard F88-68 for both lap seals and trim seals at various electric current levels within the heating element. The lap seals were formed using a nickel-chromium heating ribbon covered with a sheet of polytetrafluoroethylene.
The heating ribbon was operated in impulse fashion using a 2 second heating and 2 second cooling cycle. The trim seals were formed using a heating wire of the same alloy heated continuously with a six second interval between trim~seals. The data are tabulated in Tables 3 and 4 along with some retabulation of identifying data from Table 2. It is seen that the seal strength of the highly irradiated samples 3 and 4 is significantly less at comparable amperage than the lesser irradiated samples containin9 a Fore~layer n th an irradiùtion crosslinking enhancer.
;

5~

C~

C~

V o o V~

~ ~t . .

._ ~
._ >,~ :
_ ~ ~ ~ ~ ~ ~ ~
'~: b ~ o o ~ ~ .
::

::
, .i` ~ : : `:
~ a! :
Ul 5- C~l ~ U~ o a~ .
~ u~ E

:
.
: ~
a): :
E
, .

`~ :
1 ~, ~ co ~

~7 ~ ~ ~::
Q~ ~ . ~ .
._ V~ N . ~ .C~J . tr _~ _ O ~ N _ ~ : O

~I) ~ r- ~ ~_ _, :
~ _C ~J ~ Q~ ~ aJ 1 +' ~ +~ C~:
m ~ ~ ~ I:n lo . ~ ~ I V7 .'' ~ a) ~ Q~ ~ aJ :
Q~ ~ ~ a ~ ~ ~ ~ I v~
~ : ~

o o C~ O O
.. : :
a~
: ~~ O
~: r .

,,, ~ ~ r ~ ~ .
.-- . r-- r .

:: : :
. E
,~ .
-15- :

. . . - , ~ . :

~5~Zg a~ ~ ~ In, o~ ~ , o ~ ~
,, o ~ ~ ~ ~ ~ ~ ~
a~ C~ ~ a~

D ~ Q
~D ~t ~ 0~
r~ u~ 1_ : 0 ~

`` S I ~ t~ t_ L~ :
~n ~ ~ ~0 ~D ~ ~' ~

aJ s ~ s: ~ ~ Q~ t-cn ~ ~J:
, V~ C C ~ C ~ ~ C : ~ ~
a~ Q) ~
Q L n ~: Q ~ L

~`, V~ : ~: :
æ ~ O
:: : : -:" : : ; : :

Z
. E : ~

:`` ~
'; .

. . . . . . .

5Z'~g It is thus seen that the laminate of this invention and the process by which it is produced provides a multi-layer structure which has all of the desirable attributes of a crosslinked structure without the corresponding deleterious effect on heat sealing characteristics. e , ':

'~

:-; 25 : ~ :
'' ..

Claims (14)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A coextruded multi-layer polymeric structure having a crosslinked layer including an irradiation crosslinking enhancer and a heat sealable layer.
2. The multi-layer structure according to claim 1 wherein said heat sealable layer has heat sealing characteristics substantially similar to a non-irradiated layer of the same material.
3. The multi-layer structure of claim 1 wherein said crosslinked layer is a polymer of a 1-mono-olefin.
4. A multi-layer structure according to claim 3 wherein the irradia-tion enhancer is a material selected from the group consisting of dialkyl maleates, dialkyl fumarates, vinyl esters of fatty acids, vinyl alkyl ethers, alkyl acrylates, and alkyl methacrylates.
5. A multi-layer structure according to claim 4 wherein said irradiation enhancer is selected from the group consisting of allyl methacrylate, allyl acrylate and diallyl maleate.
6. The multi-layer structure according to claim 1, 2 or 3 wherein the heat sealable layer is sealable at a temperature in the range of 70 to 150°C
at a pressure of about 5 to about 50 psi to produce a seal having a peel strength of greater than about 1 lb. per inch of width.
7. The multi-layer structure of claim 1 in the biaxially oriented state.
8. The multi-layer structure of claim 7 with a free shrinkage of at least 10% in both axial and transverse directions at 96°C.
9. A process for producing a multi-layer irradiated structure having heat seal characteristics comprising the steps of:

providing a multi-layer structure having a crosslinkable layer including an irradiation enhancer and a heat sealable layer;
irradiating said multi-layer structure at a radiation dosage sufficient to crosslink said crosslinkable layer but insufficient to adverse-ly affect the heat sealing characteristics of said heat sealable layer.
10. The process according to claim 9 wherein said step of irradiating is carried out so as to provide a dosage level within the range of 0.1 to about 4 MR.
11. The process according to claim 9 wherein said crosslinkable layer is a polymer of a 1-mono-olefin.
12. The process according to claim 9 wherein the irradiation enhancer is selected from the group consisting of dialkyl maleate, dialkyl fumarates, vinyl esters of fatty acids, vinyl alkyl ethers, alkyl acrylates and alkyl methacrylates.
13. The process according to claim 12 wherein said irradiation enhancer is selected from the group consisting of allyl methacrylate, allyl acrylate and diallyl maleate.
14. The process of claim 9, 10 or 11 including the further step of orienting said multi-layer structure.
CA337,225A 1978-12-28 1979-10-09 Irradiated laminate film having heat sealing characteristics Expired CA1125229A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US97385078A 1978-12-28 1978-12-28
US973,850 1978-12-28

Publications (1)

Publication Number Publication Date
CA1125229A true CA1125229A (en) 1982-06-08

Family

ID=25521290

Family Applications (1)

Application Number Title Priority Date Filing Date
CA337,225A Expired CA1125229A (en) 1978-12-28 1979-10-09 Irradiated laminate film having heat sealing characteristics

Country Status (10)

Country Link
JP (1) JPS5595568A (en)
AR (1) AR219850A1 (en)
AU (1) AU5268679A (en)
BR (1) BR7908527A (en)
CA (1) CA1125229A (en)
DE (1) DE2951138A1 (en)
FR (1) FR2445212A1 (en)
GB (1) GB2040804A (en)
NZ (1) NZ192133A (en)
ZA (1) ZA795410B (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4839235A (en) * 1986-06-30 1989-06-13 W. R. Grace & Co. Oxygen barrier film
US4963419A (en) * 1987-05-13 1990-10-16 Viskase Corporation Multilayer film having improved heat sealing characteristics
US5055328A (en) * 1989-06-16 1991-10-08 Viskase Corporation Differentially cross-linked multilayer film
US5106545A (en) * 1987-12-21 1992-04-21 W. R. Grace & Co.-Conn. Oriented polymeric films and process for enhanced orientation of polymeric films
EP0613772A1 (en) * 1993-01-29 1994-09-07 American National Can Company Tough heat shrinkable film structures
US5993922A (en) * 1996-03-29 1999-11-30 Cryovac, Inc. Compositions and methods for selectively crosslinking films and improved film articles resulting therefrom
US6743523B1 (en) 2000-03-16 2004-06-01 Baxter International Inc. Multiple layer film of a new non-PVC material

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2492770B1 (en) * 1980-10-28 1985-11-15 Bean Gerard MULTI-LAYERED FILM FOR CONSTITUTING A HEAT-SHRINKABLE WRAP
US4448792A (en) * 1982-07-26 1984-05-15 W. R. Grace & Co., Cryovac Division Pasteurizable and cook-in shrink bag constructed of a multilayer film
IT1212533B (en) * 1982-10-19 1989-11-30 Montedison Spa FILM FOR PACKAGING AND PROCEDURE FOR ITS PREPARATION.
US4501780A (en) * 1982-12-15 1985-02-26 W. R. Grace & Co., Cryovac Div. Tubular film having sealing layer of propylene ethylene random copolymer
JPS6011342A (en) * 1983-07-01 1985-01-21 Kureha Chem Ind Co Ltd Heat-resistant laminate and manufacture thereof
JPS60154034A (en) * 1984-01-23 1985-08-13 Toa Nenryo Kogyo Kk Stretched polyethylene film
US4740400A (en) * 1986-03-27 1988-04-26 Viskase Corporation Tinted heat-shrinkable multilayer films comprising a vinylidene chloride-vinyl chloride copolymer
DE3681790D1 (en) * 1986-04-15 1991-11-07 Grace W R & Co MULTILAYER PACKAGING FILM.
JPS62273849A (en) * 1986-05-23 1987-11-27 呉羽化学工業株式会社 Heat-shrinkable composite film and manufacture thereof
US4961154A (en) * 1986-06-03 1990-10-02 Scitex Corporation Ltd. Three dimensional modelling apparatus
WO1987007880A1 (en) * 1986-06-19 1987-12-30 Asahi Kasei Kogyo Kabushiki Kaisha Heat shrinkable cylindrical laminated film
US4797235A (en) * 1987-04-16 1989-01-10 W. R. Grace & Co. Process for enhanced orientation of polymeric films
US4957790A (en) * 1987-12-21 1990-09-18 W. R. Grace & Co.-Conn. Oriented polymeric films
US5075156A (en) * 1988-03-15 1991-12-24 Asahi Kasei Kogyo Kabushiki Kaisha Multi-layered crosslinked ethylenic resin film, a process for production thereof and a method of applying said film
NZ237420A (en) * 1990-03-23 1993-11-25 Grace W R & Co Thermoplastic multilayer film having a thermosealing layer of ethylene-methacrylic (or acrylic) acid copolymer or a blend thereof
DE10149371A1 (en) * 2001-10-06 2003-04-24 Dornier Gmbh Lindauer Method and device for processing multilayer plastic films

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL298844A (en) * 1962-10-04 1900-01-01
GB1287143A (en) * 1969-01-30 1972-08-31 Arthur Charlesby Novel crosslinked polymer

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4839235A (en) * 1986-06-30 1989-06-13 W. R. Grace & Co. Oxygen barrier film
US4963419A (en) * 1987-05-13 1990-10-16 Viskase Corporation Multilayer film having improved heat sealing characteristics
US5106545A (en) * 1987-12-21 1992-04-21 W. R. Grace & Co.-Conn. Oriented polymeric films and process for enhanced orientation of polymeric films
US5055328A (en) * 1989-06-16 1991-10-08 Viskase Corporation Differentially cross-linked multilayer film
EP0613772A1 (en) * 1993-01-29 1994-09-07 American National Can Company Tough heat shrinkable film structures
US6051292A (en) * 1993-01-29 2000-04-18 American National Can Company Heat shrinkable film structures with improved sealability and toughness
EP1018423A1 (en) * 1993-01-29 2000-07-12 American National Can Company Tough heat shrinkable film structures
US5993922A (en) * 1996-03-29 1999-11-30 Cryovac, Inc. Compositions and methods for selectively crosslinking films and improved film articles resulting therefrom
US6743523B1 (en) 2000-03-16 2004-06-01 Baxter International Inc. Multiple layer film of a new non-PVC material

Also Published As

Publication number Publication date
JPS5595568A (en) 1980-07-19
ZA795410B (en) 1980-09-24
GB2040804A (en) 1980-09-03
DE2951138A1 (en) 1980-07-17
FR2445212A1 (en) 1980-07-25
NZ192133A (en) 1981-03-16
AU5268679A (en) 1980-07-03
BR7908527A (en) 1980-10-07
AR219850A1 (en) 1980-09-15

Similar Documents

Publication Publication Date Title
CA1125229A (en) Irradiated laminate film having heat sealing characteristics
AU614005B2 (en) Oriented polymeric films and process for enhanced orientation of polymeric films
JP2654054B2 (en) Thermoplastic multilayer barrier packaging film and bags made therefrom
AU700179B2 (en) Highly oriented multilayer film
CA2013587C (en) High shrink energy/high modulus thermoplastic multi-layer packaging film and bags made therefrom
US4797235A (en) Process for enhanced orientation of polymeric films
US4820557A (en) Thermoplastic packaging film of low I10 /I2
CA2041351C (en) High density polyethylene shrink film
CA1308012C (en) Multilayered polyolefin high shrinkage, low-shrink force shrink film
CA1326992C (en) Heat-shrinkable laminated film
US4636340A (en) Method of producing crosslinked polyethylene stretched film
US5035955A (en) Heat-shrinkable laminated film
US4891173A (en) Process for producing a crosslinked and oriented polyethylene film
JPH02182453A (en) Multi-layer film structural body for packing and bag formed therefrom
EP0679487A1 (en) Multi-layer polyolefin film containing recycle polymer from cross-linked films
GB2297060A (en) Heat-shrinkable polyolefin multilayer film
EP0369705A2 (en) Heat-sealable crosslinked oriented polyethylene film and production thereof
US5332616A (en) Produce packaging film
US5089352A (en) Cross-linked multilayer heat-shrinkable oriented polymeric film
US4699846A (en) Heat-resistant and oil-resistant laminate film and process for preparing the same
US4472485A (en) Stretched composite film
US5106545A (en) Oriented polymeric films and process for enhanced orientation of polymeric films
DE19923839A1 (en) Cardboard box system containing a sealable polyester film
JP2774956B2 (en) Heat shrinkable film
EP0206826A2 (en) Heat shrinkable laminate film and its use

Legal Events

Date Code Title Description
MKEX Expiry