WO1984001327A1 - Coextruded elastomeric films - Google Patents

Coextruded elastomeric films Download PDF

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Publication number
WO1984001327A1
WO1984001327A1 PCT/US1983/001360 US8301360W WO8401327A1 WO 1984001327 A1 WO1984001327 A1 WO 1984001327A1 US 8301360 W US8301360 W US 8301360W WO 8401327 A1 WO8401327 A1 WO 8401327A1
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Prior art keywords
vinyl acetate
composite
copolymer
ethylene
film structure
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Application number
PCT/US1983/001360
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French (fr)
Inventor
Luccio Robert Cosmo Di
Original Assignee
Du Pont
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Publication of WO1984001327A1 publication Critical patent/WO1984001327A1/en

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    • 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
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/32Layered products comprising a layer of synthetic resin comprising polyolefins
    • B32B27/322Layered products comprising a layer of synthetic resin comprising polyolefins comprising halogenated polyolefins, e.g. PTFE
    • 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
    • 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
    • B32B2307/40Properties of the layers or laminate having particular optical properties
    • B32B2307/412Transparent
    • 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
    • B32B2307/51Elastic
    • 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
    • B32B2553/00Packaging equipment or accessories not otherwise provided for

Definitions

  • This invention relates to a process for producing transparent elastomeric polymer films particularly suitable for wrapping heat-sensitive articles, to the transparent elastomeric films themselves, and to articles wrapped in such films.
  • Transparent films are commonly used for packaging various consumer items, which thus can be examined by the prospective purchaser without opening the package.
  • the most common are heat-shrinkable films, but those cannot be used for packaging heat-sensitive products, especially certain food articles.
  • non-elastomeric stretch-films such, for example, as poly(vinylidene chloride). Those films, however, lack sufficient elastic recovery for forming an esthetically pleasing, snug overwrap.
  • EVA copolymers especially those containing about 30-50 weight % of vinyl acetate comonomer, form a transparent elastomeric film, which can be used in packaging applications.
  • EVA copolymers In order to improve the film's formability, for example, creep resistance, the film is normally exposed to high energy radiation, which induces crosslinking.
  • EVA copolymer films having a vinyl acetate content in excess of 30% have satisfactory mechanical properties, they also have high surface tackiness, which causes difficulties both in production windup and in machine packaging applications.
  • various approaches to solving this high tackiness problem have been proposed. For example, the copending application Serial No.
  • Mahr et al. proposes alcoholysis or hydrolysis of surface vinyl acetate groups, preferably followed by attachment to the surface of finely divided mineral particulates.
  • a transparent, elastomeric, composite film structure having nontacky surface properties comprising a core layer of an EVA copolymer containing about 30-50 weight percent of vinyl acetate and two outer layers, coextruded with said core layer, of a polymeric material selected from the class consisting of homopolyethylene and copolymers of ethylene with up to 10% by weight of the copolymer of a C 3 -C 8 ⁇ -olefin or vinyl acetate, said outer layer polymeric material having a density of at most 0.94 g/cm , said two outer layers providing about 0.5-10% of the total thickness of said composite film structure, which structure following coextrusion is exposed to high energy radiation of which it absorbs about 4-16 megarads.
  • This invention also includes a process which comprises coextruding a composite film structure having the above composition and irradiating the coextruded structure with high energy radiation to improve its elastic recovery and reduce stress whitening after stretching and relaxing.
  • FIG. 1 illustrates schematically the process of the present invention.
  • Fig. 2 is a cross-sectional view of a three-layer combining adapter and a die mounted together as an assembly.
  • An elastomeric material is a material which, when stretched to twice its original length and released, returns with force to substantially its original length.
  • EVA copolymers suitable in the process of the present invention are available from several sources including E. I. du Pont de Nemours and Company.
  • the preferred EVA copolymer contains about 40 weight percent of vinyl acetate. As the proportion of this comonomer in the copolymer increases, the elastomeric properties of the copolymer improve, but its tackiness also increases. Above about 50% of vinyl acetate, the tackiness of the copolymer may be impractically high. Below about 30% of vinyl acetate, the elastomeric properties of the copolymer tend to be unsatisfactory.
  • At least one outer polymer layer is thin, about 1% of the total composite film structure or less, it is advantageous to add to the EVA copolymer prior to coextrusion about 1-3% by weight of a long chain aliphatic amide or bisamide to improve the composite's slip properties and reduce blocking.
  • Various commercially available products can be used, including stearamide, oleamide, erucamide, palmitamide, ethylenebis(oleamide), and ethylenebis(erucamide).
  • the compositions of the outer layers of the composite film structure can be the same or different. In practice, they will be made of the same polymeric material since no particular advantage will normally be gained by using different materials for this purpose. However, it may sometimes be practical to have different outer layers, either based on different polymers or compounded with different components, e.g., pigments of different colors, or having different thicknesses. All such alternatives are contemplated by the present invention.
  • a suitable ethylene homopolymer is a branched material obtained by a free radical-initiated polymerization at a high pressure.
  • a copolymer of ethylene with vinyl acetate is made by the same technique.
  • Suitable copolymers of ethylene with ⁇ -olefins may be made either by a free radical-initiated polymerization or by polymerization in the presence of a coordination catalyst, a so-called Ziegler type catalyst. These latter type copolymers are essentially linear. They are often sold as so-called linear low density polyethylene (LLDPE) , which strictly speaking is an incorrect designation.
  • LLDPE linear low density polyethylene
  • the linear copolymers are preferred to either the branched homopolymer or branched copolymers because branched polymers have a tendency to assume spatial orientation and to crystallize, thus reducing the polymer film's ability to retract after stretching.
  • the ⁇ -olefin comonomer can be, for example, prooene, 1-butene, isobutene, 1-hexene, 1-octene, and 2-methylhexene.
  • Ethylene copolymers with small amounts of vinyl acetate also are commercially available. They do not suffer from the shortcoming of high viscosity associated with copolymers having high vinyl acetate content and have physical properties which are entirely satisfactory for this purpose.
  • the composite film structures of the present invention are made by coextrusion, which is possible with a special three-layer combining adapter made by Cloeren Co. , Orange, Texas.
  • This adapter is described in U.S. Patent 4,152,387 to Peter Cloeren, which is incorporated herein by reference.
  • Thermoplastic materials flowing out of extruders at different velocities are separately introduced into the adapter containing back pressure cavities and flow restriction channels, and the several layers exiting the flow restriction channels converge into a melt composite. These separate streams are at the same flow velocity and thus form uniform composite layers.
  • the combining adapter is used in conjunction with extruders supplying the thermoplastic materials to be laminated. Since the outer ethylene polymer layers are very thin as compared with the core layer, it is advisable to use a low throughput delivery means such as a pump, preferably a gear pump, in the ethylene polymer feed line.
  • extruder A supplies to combining adapter C the core EVA copolymer, while extruder B supplies through gear pump G the outer layer ethylene polymer.
  • the three streams leaving adapter C enter die D, wherein they are formed into a three-layer composite melt having the desired thickness.
  • the composite melt is solidified on chill roll R1, then wound up on roll R2 and slit as required.
  • Fig. 2 shows a cross-section of the combining adapter C and die D of Fig. 1.
  • the flow from extruder B enters channels e and f of the adapter, while the flow from extruder A enters channel d of the adapter.
  • Vanes V streamline the polymer flow in all three channels in the adapter. The vanes move in response to changes in the volumetric flow rates within the channels. This permits changes in layer thickness over a wide range while maintaining layer uniformity.
  • the combining adapter C is made of 4140 stainless steel which can withstand pressures as high as 10,000 psi (690 MPa) at 600oF (316oC).
  • the three-layer melt exits the adapter through channel i and enters channel k of the die block and thence continues to channel 1 of a flexible lip extrusion die, which has a gap typically set at about 10 mils (0.25 mm) and is drawn down to 2 mils (0.05 mm) or less.
  • extruder A used in this work was a Killion 1 1/2-in. (3.8 cm) model KL-500 single screw extruder having a length to diameter ratio of 24:1.
  • the barrel was made of
  • Extruder B used for the outer layer ethylene polymer, was a Killion 1-in. (2.5 cm) model KTS-100 single screw extruder having a length to diameter ratio of 24:1. The screws in both extruders were of the type used for polyethylene. The extruders were purchased from Killion Co. in Pompano Beach, Florida. Gear pump G, installed downstream of extruder B, was purchased from Zenith Products, Newton, Massachusetts. With this pump, flow rates of molten ethylene polymer lower than 0.454 kg/hr were possible. Die D was an 18-in. (45.7 cm) "Ultraflex" H75 model obtained from Extrusion Dies, Inc., Chippewa, Wisconsin. The composite film exiting the die was passed over a chill roll and wound up without stretching on a low tension winder.
  • the core EVA copolymer was "Vynathene" 901-25, manufactured by U.S. Industrial Chemicals, Inc., New York, New York, a copolymer of 60% ethylene and 40% vinyl acetate. It had a density of 0.962 g/cm and a melt index of 7.5 g/10 min determined according to ASTM D1238.
  • the outer layer ethylene polymer was a commercial, branched, high pressure homopolymer which had a density of 0.917 g/cm and a melt index of 15 g/10 min.
  • the extruder feed temperature was 270oF (132oC), and the body temperature was 355oF (180oC).
  • the molten extruded composite was cooled in contact with a chill roll maintained at 40°C.
  • the extruders operated as follows:
  • Extruder A 10-50 rpm, output 4.5-10 kg/hr.
  • Extruder B 5-22 rpm, output from the gear pump 0.15-1.135 kg/hr.
  • each layer in the final composite structure depends on the polymer output from the appropriate extruder. If, for example, extruder A delivers EVA copolymer at a rate of 9.8 kg/hr, and extruder B delivers ethylene polymer at a rate of 0.2 kg/hr, the composite will have a core constituting 98% of the composite's thickness and two outer layers each accounting for 1% of the thickness. Extruder A was operated at pressures within the range of 1200-1900 psi (8.3-13.1 MPa).
  • Extruder B was operated at pressures within the range of 1200-3100 psi (8.3-21.4 MPa) Gear pump G pressures: upstream 1000-3000 psi (6.9-20 MPa), downstream 800-2800 psi (5.5-19.3 MPa).
  • the upstream pressure was always at least equal to the downstream pressure.
  • Irradiation of the composite film was accomplished using a General Electric 2MV electron beam scanner Model 11 AD6.
  • a composite film having a cross-section of 1% polyethylene/93% EVA copolymer/1% polyethylene was made and examined microscopically. It had uniform layers with good adhesion. All irradiated films were clear, free of haze, and resistant to stress whitening. Good slip and blocking properties were observed. The recovery of these samples after stretching was 85-92%.
  • EXAMPLE 4 Whitening after stretching was determined for composite film structures having an EVA copolymer core and polyethylene outer layers having the indicated thicknesses (as percentages of the total thickness). Those film structures were irradiated at four radiation levels, stretched to varying lengths, and released. Whitening, if any, was observed visually. The following results were obtained:
  • composite films having outer layers of a total thickness of either 2% or 6% can be stretched by 120% without whitening.
  • the total thickness is 10%, they can be stretched by 100% without whitening and by 120% with moderate whitening.
  • the total thickness is 20%, the films show whitening even at 100% stretching.
  • these film structures are suitable for wrapping various articles, especially consumer goods which can be visually inspected without opening the package, and particularly heat-sensitive articles which otherwise might be damaged by heat-shrinking operations, especially food articles, various biologically active preparations, and similar goods.

Abstract

A transparent, elastomeric, composite film structure having a core ethylene/vinyl acetate copolymer and outer layers of a low density ethylene homopolymer or copolymer with a small amount of another alpha-olefin or vinyl acetate is made by coextrusion of the polymers in a three-layer combining adapter and quenching on a chill roll (not shown). This film structure is useful as a wrapping material, especially for heat-sensitive articles.

Description

TITLE COEXTRUDED ELASTOMERIC FILMS This is a continuation-in-part of my application Serial No. 424,448, filed September 27, 1982.
BACKGROUND OF THE INVENTION This invention relates to a process for producing transparent elastomeric polymer films particularly suitable for wrapping heat-sensitive articles, to the transparent elastomeric films themselves, and to articles wrapped in such films.
Transparent films are commonly used for packaging various consumer items, which thus can be examined by the prospective purchaser without opening the package. The most common are heat-shrinkable films, but those cannot be used for packaging heat-sensitive products, especially certain food articles. There are also used non-elastomeric stretch-films, such, for example, as poly(vinylidene chloride). Those films, however, lack sufficient elastic recovery for forming an esthetically pleasing, snug overwrap.
Certain ethylene/vinyl acetate copolymers (sometimes hereafter abbreviated to EVA copolymers), especially those containing about 30-50 weight % of vinyl acetate comonomer, form a transparent elastomeric film, which can be used in packaging applications. In order to improve the film's formability, for example, creep resistance, the film is normally exposed to high energy radiation, which induces crosslinking. But even though such irradiated EVA copolymer films having a vinyl acetate content in excess of 30% have satisfactory mechanical properties, they also have high surface tackiness, which causes difficulties both in production windup and in machine packaging applications. Various approaches to solving this high tackiness problem have been proposed. For example, the copending application Serial No. 259,422 of Mahr et al. filed May 1, 1981, proposes alcoholysis or hydrolysis of surface vinyl acetate groups, preferably followed by attachment to the surface of finely divided mineral particulates. Another copending application of Mahr et al., Serial No. 278,435, filed June 25, 1981, teaches treating the EVA film surface with a coupling agent and then attaching particulate material to the surface.
However, still other methods of improving the properties and reducing the surface tackiness of elastomeric EVA films are sought. SUMMARY OF THE INVENTION
According to the present invention, there is now provided a transparent, elastomeric, composite film structure having nontacky surface properties, said film structure comprising a core layer of an EVA copolymer containing about 30-50 weight percent of vinyl acetate and two outer layers, coextruded with said core layer, of a polymeric material selected from the class consisting of homopolyethylene and copolymers of ethylene with up to 10% by weight of the copolymer of a C3-C8 α-olefin or vinyl acetate, said outer layer polymeric material having a density of at most 0.94 g/cm , said two outer layers providing about 0.5-10% of the total thickness of said composite film structure, which structure following coextrusion is exposed to high energy radiation of which it absorbs about 4-16 megarads.
This invention also includes a process which comprises coextruding a composite film structure having the above composition and irradiating the coextruded structure with high energy radiation to improve its elastic recovery and reduce stress whitening after stretching and relaxing.
Brief Description of the Drawings Fig. 1 illustrates schematically the process of the present invention.
Fig. 2 is a cross-sectional view of a three-layer combining adapter and a die mounted together as an assembly.
Detailed Description of the Invention Definition: An elastomeric material is a material which, when stretched to twice its original length and released, returns with force to substantially its original length.
EVA copolymers suitable in the process of the present invention are available from several sources including E. I. du Pont de Nemours and Company. The preferred EVA copolymer contains about 40 weight percent of vinyl acetate. As the proportion of this comonomer in the copolymer increases, the elastomeric properties of the copolymer improve, but its tackiness also increases. Above about 50% of vinyl acetate, the tackiness of the copolymer may be impractically high. Below about 30% of vinyl acetate, the elastomeric properties of the copolymer tend to be unsatisfactory.
When at least one outer polymer layer is thin, about 1% of the total composite film structure or less, it is advantageous to add to the EVA copolymer prior to coextrusion about 1-3% by weight of a long chain aliphatic amide or bisamide to improve the composite's slip properties and reduce blocking. Various commercially available products can be used, including stearamide, oleamide, erucamide, palmitamide, ethylenebis(oleamide), and ethylenebis(erucamide). The compositions of the outer layers of the composite film structure can be the same or different. In practice, they will be made of the same polymeric material since no particular advantage will normally be gained by using different materials for this purpose. However, it may sometimes be practical to have different outer layers, either based on different polymers or compounded with different components, e.g., pigments of different colors, or having different thicknesses. All such alternatives are contemplated by the present invention.
A suitable ethylene homopolymer is a branched material obtained by a free radical-initiated polymerization at a high pressure. A copolymer of ethylene with vinyl acetate is made by the same technique. Suitable copolymers of ethylene with α-olefins may be made either by a free radical-initiated polymerization or by polymerization in the presence of a coordination catalyst, a so-called Ziegler type catalyst. These latter type copolymers are essentially linear. They are often sold as so-called linear low density polyethylene (LLDPE) , which strictly speaking is an incorrect designation. The linear copolymers are preferred to either the branched homopolymer or branched copolymers because branched polymers have a tendency to assume spatial orientation and to crystallize, thus reducing the polymer film's ability to retract after stretching. The α-olefin comonomer can be, for example, prooene, 1-butene, isobutene, 1-hexene, 1-octene, and 2-methylhexene. Ethylene copolymers with small amounts of vinyl acetate also are commercially available. They do not suffer from the shortcoming of high viscosity associated with copolymers having high vinyl acetate content and have physical properties which are entirely satisfactory for this purpose.
The composite film structures of the present invention are made by coextrusion, which is possible with a special three-layer combining adapter made by Cloeren Co. , Orange, Texas. This adapter is described in U.S. Patent 4,152,387 to Peter Cloeren, which is incorporated herein by reference. Thermoplastic materials flowing out of extruders at different velocities are separately introduced into the adapter containing back pressure cavities and flow restriction channels, and the several layers exiting the flow restriction channels converge into a melt composite. These separate streams are at the same flow velocity and thus form uniform composite layers. The combining adapter is used in conjunction with extruders supplying the thermoplastic materials to be laminated. Since the outer ethylene polymer layers are very thin as compared with the core layer, it is advisable to use a low throughput delivery means such as a pump, preferably a gear pump, in the ethylene polymer feed line.
Referring now to Fig. 1, extruder A supplies to combining adapter C the core EVA copolymer, while extruder B supplies through gear pump G the outer layer ethylene polymer. The three streams leaving adapter C enter die D, wherein they are formed into a three-layer composite melt having the desired thickness. The composite melt is solidified on chill roll R1, then wound up on roll R2 and slit as required.
Fig. 2 shows a cross-section of the combining adapter C and die D of Fig. 1. The flow from extruder B enters channels e and f of the adapter, while the flow from extruder A enters channel d of the adapter. Vanes V streamline the polymer flow in all three channels in the adapter. The vanes move in response to changes in the volumetric flow rates within the channels. This permits changes in layer thickness over a wide range while maintaining layer uniformity. The combining adapter C is made of 4140 stainless steel which can withstand pressures as high as 10,000 psi (690 MPa) at 600ºF (316ºC).
The three-layer melt exits the adapter through channel i and enters channel k of the die block and thence continues to channel 1 of a flexible lip extrusion die, which has a gap typically set at about 10 mils (0.25 mm) and is drawn down to 2 mils (0.05 mm) or less.
Referring again to Fig. 1, extruder A used in this work was a Killion 1 1/2-in. (3.8 cm) model KL-500 single screw extruder having a length to diameter ratio of 24:1. The barrel was made of
"Xaloy" 406 (Xaloy, Inc., Princeton, New Jersey) and the screw of flame hardened 4140 stainless steel. The maximum available rotational speed was 115 rpm. Extruder B, used for the outer layer ethylene polymer, was a Killion 1-in. (2.5 cm) model KTS-100 single screw extruder having a length to diameter ratio of 24:1. The screws in both extruders were of the type used for polyethylene. The extruders were purchased from Killion Co. in Pompano Beach, Florida. Gear pump G, installed downstream of extruder B, was purchased from Zenith Products, Newton, Massachusetts. With this pump, flow rates of molten ethylene polymer lower than 0.454 kg/hr were possible. Die D was an 18-in. (45.7 cm) "Ultraflex" H75 model obtained from Extrusion Dies, Inc., Chippewa, Wisconsin. The composite film exiting the die was passed over a chill roll and wound up without stretching on a low tension winder.
The typical operating conditions were as follows:
The core EVA copolymer was "Vynathene" 901-25, manufactured by U.S. Industrial Chemicals, Inc., New York, New York, a copolymer of 60% ethylene and 40% vinyl acetate. It had a density of 0.962 g/cm and a melt index of 7.5 g/10 min determined according to ASTM D1238.
The outer layer ethylene polymer was a commercial, branched, high pressure homopolymer which had a density of 0.917 g/cm and a melt index of 15 g/10 min.
The extruder feed temperature was 270ºF (132ºC), and the body temperature was 355ºF (180ºC). The molten extruded composite was cooled in contact with a chill roll maintained at 40°C. The extruders operated as follows:
Extruder A 10-50 rpm, output 4.5-10 kg/hr. Extruder B 5-22 rpm, output from the gear pump 0.15-1.135 kg/hr.
Gear pump G 2.5-3.0 rpm. The thickness of each layer in the final composite structure depends on the polymer output from the appropriate extruder. If, for example, extruder A delivers EVA copolymer at a rate of 9.8 kg/hr, and extruder B delivers ethylene polymer at a rate of 0.2 kg/hr, the composite will have a core constituting 98% of the composite's thickness and two outer layers each accounting for 1% of the thickness. Extruder A was operated at pressures within the range of 1200-1900 psi (8.3-13.1 MPa). Extruder B was operated at pressures within the range of 1200-3100 psi (8.3-21.4 MPa) Gear pump G pressures: upstream 1000-3000 psi (6.9-20 MPa), downstream 800-2800 psi (5.5-19.3 MPa).
To insure proper feed into the gear pump, the upstream pressure was always at least equal to the downstream pressure.
Irradiation of the composite film was accomplished using a General Electric 2MV electron beam scanner Model 11 AD6.
The following representative examples illustrate this invention. The equipment and conditions were those discussed above. All composite film samples were irradiated to absorb 4, 6, 8, and 12 Mrad of high energy radiation. In Examples 1-3 sample recovery, and/or resistance to whitening were determined after stretching by 120% and relaxing. EXAMPLE 1
A composite film having a cross-section of 1% polyethylene/93% EVA copolymer/1% polyethylene was made and examined microscopically. It had uniform layers with good adhesion. All irradiated films were clear, free of haze, and resistant to stress whitening. Good slip and blocking properties were observed. The recovery of these samples after stretching was 85-92%.
EXAMPLE 2 A composite film having a cross-section of
3% polyethylene/94% EVA copolymer/3% polyethylene was made and examined microscopically. It had uniform layers with good adhesion. All irradiated samples resisted stress whitening. The film had good slip and block properties. The recovery of the samples was 80-88%. EXAMPLE 3
Two film composites having the indicated polyethylene/EVA copolymer/polyethylene thicknesses were prepared and irradiated. Their recoveries after stretching are shown in the table below.
Figure imgf000011_0001
EXAMPLE 4 Whitening after stretching was determined for composite film structures having an EVA copolymer core and polyethylene outer layers having the indicated thicknesses (as percentages of the total thickness). Those film structures were irradiated at four radiation levels, stretched to varying lengths, and released. Whitening, if any, was observed visually. The following results were obtained:
Figure imgf000011_0002
The above data show that composite films having outer layers of a total thickness of either 2% or 6% can be stretched by 120% without whitening. When the total thickness is 10%, they can be stretched by 100% without whitening and by 120% with moderate whitening. When the total thickness is 20%, the films show whitening even at 100% stretching.
Because of good elastomeric properties of the composite film structures of the present invention and of their resistance to stress whitening upon stretching by 100% and relaxing, these film structures are suitable for wrapping various articles, especially consumer goods which can be visually inspected without opening the package, and particularly heat-sensitive articles which otherwise might be damaged by heat-shrinking operations, especially food articles, various biologically active preparations, and similar goods.

Claims

I Claim:
1. A transparent, elastomeric composite film structure having nontacky surface properties, said film structure comprising a core layer of an ethylene/vinyl acetate copolymer containing about 30-50 weight percent of vinyl acetate and two outer layers, coextruded with said core layer, of a polymeric material selected from the class consisting of homopolyethylene and copolymers of ethylene with up to 10% by weight of the copolymer of a C3-C8 α-olefin or vinyl acetate, said outer layer polymeric material having a density of at most about 0.94 g/cm , said two outer layers providing about 0.5-10% of the total thickness of said composite film structure, which structure following coextrusion is exposed to high energy radiation of which it absorbs about 4-16 megarads.
2. A composite structure of Claim 1 wherein the two outer layers provide at most about 6% of the total thickness.
3. A composite structure of Claim 1 or 2 wherein the core copolymer contains about 1-3 weight percent of a long chain aliphatic amide or bisamide.
4. A composite structure of Claim 3 wherein the amide or bisamide is selected from the class consisting of stearamide, oleamide, erucamide, palmitamide, ethylenebis(oleamide), and ethylenebis(erucamide).
5. A composite structure of Claim 3 wherein the thickness of at least one outer layer is less than about 1% of the total composite structure thickness.
6. A composite structure of Claim 1 or 2 wherein the core copolymer is a copolymer of about 60 weight percent of ethylene and 40 weight percent of vinyl acetate.
7. A composite structure of Claim 1 or 2 wherein the outer layer polymeric material is a linear copolymer of ethylene with an α-olefin.
8. A process for making a transparent, elastomeric, composite film structure, wherein an ethylene/vinyl acetate copolymer containing about 30-50 weight percent of vinyl acetate is supplied to the central channel of a three layer combining adapter and a polymer selected from the class consisting of homopolyethylene and copolymers of ethylene with another α-olefin or with vinyl acetate, the comonomer being responsible for up to 10% of the copolymer weight, is supplied to the other two channels, the density of the polymer supplied to the other two channels being at most about 0.94 g/cm3 , the temperature of the combining adapter being sufficient to maintain each polymer in molten state, and the molten polymers are extruded through said combining adapter and a die to form a molten composite structure containing a core layer and two outer layers, which is solidified by cooling and recovered, the outer layers providing about 0.5-10% of the total thickness of the composite film structure.
9. A process of Claim 8 wherein the outer layers provide up to about 6% of the total thickness of the composite film structure.
10. A process of Claim 8 or 9 wherein the core ethylene/vinyl acetate copolymer contains about
1-3 weight percent of a long chain aliphatic amide or diamide to improve the composite's slip and block properties.
11. A process of Claim 10 wherein the amide or diamide is selected from the class consisting of stearamide, oleamide, erucamide, palmitamide, ethylenebis(oleamide), and ethylenebis(erucamide).
12. A process of Claim 10 wherein the thickness of at least one outer layer is less than about 1% of the total composite film structure.
13. A process of Claim 8 or 9 wherein the outer layer polymeric material is a linear copolymer of ethylene with an α-olefin.
14. An article wrapped in a composite film structure of Claim 1 or 2.
15. An article of Claim 14 which is heat-sensitive.
PCT/US1983/001360 1982-09-27 1983-09-09 Coextruded elastomeric films WO1984001327A1 (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1991006426A1 (en) * 1989-11-07 1991-05-16 Exxon Chemical Patents Inc. Cling packaging film for wrapping food products

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3595735A (en) * 1968-05-06 1971-07-27 Nat Distillers Chem Corp Blown tubular films
US3817821A (en) * 1972-11-08 1974-06-18 Du Pont Laminar packaging film
US4352849A (en) * 1981-03-26 1982-10-05 W. R. Grace & Co. Coextruded, heat-shrinkable, multi-layer, polyolefin packaging film
US4391362A (en) * 1981-02-17 1983-07-05 Nabisco Brands, Inc. Speed controlled infeed conveyor system

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2925205A1 (en) * 1979-06-22 1981-02-05 Bayer Ag STEAM-STEELABLE, SEALABLE FILMS

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3595735A (en) * 1968-05-06 1971-07-27 Nat Distillers Chem Corp Blown tubular films
US3817821A (en) * 1972-11-08 1974-06-18 Du Pont Laminar packaging film
US4391362A (en) * 1981-02-17 1983-07-05 Nabisco Brands, Inc. Speed controlled infeed conveyor system
US4352849A (en) * 1981-03-26 1982-10-05 W. R. Grace & Co. Coextruded, heat-shrinkable, multi-layer, polyolefin packaging film

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1991006426A1 (en) * 1989-11-07 1991-05-16 Exxon Chemical Patents Inc. Cling packaging film for wrapping food products

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AU556396B2 (en) 1986-10-30
JPS59501620A (en) 1984-09-13
EP0120052A1 (en) 1984-10-03
AU2036583A (en) 1984-04-24
EP0120052A4 (en) 1985-03-08

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