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CA1229296A - Linear polyethylene shrink film and process for making same - Google Patents

Linear polyethylene shrink film and process for making same

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Publication number
CA1229296A
CA1229296A CA000443913A CA443913A CA1229296A CA 1229296 A CA1229296 A CA 1229296A CA 000443913 A CA000443913 A CA 000443913A CA 443913 A CA443913 A CA 443913A CA 1229296 A CA1229296 A CA 1229296A
Authority
CA
Canada
Prior art keywords
film
layer
vinyl acetate
shrink
density polyethylene
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
CA000443913A
Other languages
French (fr)
Inventor
Walter B. Mueller
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.)
Cryovac LLC
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 CA1229296A publication Critical patent/CA1229296A/en
Expired legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • 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
    • B29C61/00Shaping by liberation of internal stresses; Making preforms having internal stresses; Apparatus therefor
    • B29C61/06Making preforms having internal stresses, e.g. plastic memory
    • B29C61/0608Making preforms having internal stresses, e.g. plastic memory characterised by the configuration or structure of the preforms
    • B29C61/0616Making preforms having internal stresses, e.g. plastic memory characterised by the configuration or structure of the preforms layered or partially layered preforms, e.g. preforms with layers of adhesive or sealing compositions
    • 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
    • B32B27/30Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
    • B32B27/306Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers comprising vinyl acetate or vinyl alcohol (co)polymers
    • 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
    • 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
    • B29K2023/00Use of polyalkenes or derivatives thereof as moulding material
    • 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
    • B29K2023/00Use of polyalkenes or derivatives thereof as moulding material
    • B29K2023/04Polymers of ethylene
    • B29K2023/08Copolymers of ethylene
    • B29K2023/083EVA, i.e. ethylene vinyl acetate copolymer
    • 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
    • B29L2007/00Flat articles, e.g. films or sheets
    • B29L2007/008Wide strips, e.g. films, webs
    • 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
    • B32B2307/70Other properties
    • B32B2307/732Dimensional properties
    • B32B2307/734Dimensional stability
    • B32B2307/736Shrinkable
    • 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
    • B32B2323/00Polyalkenes
    • B32B2323/04Polyethylene
    • B32B2323/046LDPE, i.e. low density polyethylene
    • 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

Landscapes

  • Laminated Bodies (AREA)
  • Shaping By String And By Release Of Stress In Plastics And The Like (AREA)
  • Manufacture Of Macromolecular Shaped Articles (AREA)

Abstract

ABSTRACT OF THE INVENTION
A multi-layered thermoplastic film having improved physical characteristics is formulated through utilization of a linear low density polyethylene or linear medium density polyethylene resin as a core layer con-stituent. The film has demonstrated improved physical characteristics when compared to a presently known polyvinyl/chloride film. An improved process for manufacturing the film is also disclosed. Utilization of the process results is a film having a lower degree of orientation and improved elongation.

Description

~%~

This application is related to prior cop ending Canadian application Serial No. ~19,695 filed on January 18, 19~3.
FIELD OF TIRE INVENTION
This invention relates to heat shrinkable, thermoplastic pack-aging films. In particular, the present invention is directed to shrink films utilizing linear low density polyethylene or linear medium density polyethylene resins as a constituent of a core layer in a multi-layer film.
BACKGROUND OF THE INVENTION
The present invention is directed to new and useful heat shrink able film formulations. One distinguishing feature of a shrink film is the film's ability) upon exposure to a certain temperature, to shrink or if restrained from shrinking, to generate shrink tension within the film.

Y22LB/kd - 1 -I' I
The manufacture of shrink films, as is well known in the hut, may be generally accomplished by extrusion of the resinous neutrals which have been heated to their flow or melting point frown an extrusion die in tubular or planar (sheet) form. After a posy extrusion quenching to cool, the extradite is then reheated to its orientation temperature range. The orientation temperature range for a given film will voyeur with the different resinous polymers and blends thereof which comprise the film. However, the orientation temperature range may generally be stated to be above room temperature and below the melting point of the film.
the orientation temperature range for a given film is readily determine able by those of ordinary skill in the art without undue experimentation.
The terms "oriented" or "orientation" are used herein to desk crime the process and resultant product characteristics obtained by stretching and immediately cooling a resinous polymeric material which has been heated to its orientation temperature range so as to revise the molecular configuration of the material by physical alignment of the molecules to improve mechanical properties of the film such as , for example, shrink tension and orientation release stress. Both of these properties may be measured in accordance with ASTM D 283~-69 (reproved 1975). When the stretching force is applied in one direction uniaxial orientation results. ennui the stretching force is applied in two direct lions biaxial orientation results. orientation is also herein used interchangeably with "heat shrinkability" with these terms designating a material which has been stretched and set by cooling at its stretched dimensions. An oriented (i.e., heat shrinkable) material will tend to return to its original unstretched dimensions when heated to an appear-private temperature below its melting temperature range.
Returning to the basic process for manufacturing the film as discussed above, it can be seen that the film once extruded and initially quenched to cool is then reheated to its orientation temperature range and oriented. The stretching to orient may be accomplished in many ways such as, for example, by "blown bubble" techniques or "tinter framing".
These terms are well known to those in the art and refer to orientation steps whereby the material is stretched in the cross or transverse direct lion (TO) and/or in the longitudinal or machine direction (MD). After being stretched, the film is rapidly cooled to quench and thus set or lock-in the oriented molecular configuration.
~22LB2/kd After locking-in the oriented molecular configuration the film may then be stored in rolls and utilized to tightly package a variety of items. In this regard, the product to be packaged is first enclosed in the heat shrinkable material by heat sealing the shrink film to itself where necessary. Thereafter, the enclosed product is subjected to elevated temperatures by, for example, passing the product through a hot air or hot water tunnel. This causes the film to shrink around the product to produce a tight wrapping that closely conforms to the contour of the product.
The above general outline for manufacturing films is not meant to be all inclusive since -this process is well known to those in the art. For example, see U. S. Patent Nos. 4,274,900;
4,229,241; 4,194,039; 4,188r443; 4,048,42~; 3,821,182 and 3,022,543.
Many variations on the above discussed general processing theme are available to those in the art depending upon the end use for which the film is to be put and the characteristics desired to be instilled in the film. For example, the molecular of the film may be cross-linked during processing to improve the films abuse resistance and other characteristics. Cross-linking and methods for cross-linking are well known in the art. Cross-linking may be accomplished by irradiating the film or, alternatively, may be accomplished chemically through the utilization of peroxides.
Radiation dosages are referred to herein in terms of the radiation units "fad", with one million fads or a mergarad being designated as "MY". The degree of molecular cross linking is expressed in terms of the radiation dosage that induces the cross-linking. "Radiation" as used herein generally means ionizing ~2~2~ ~53~-540 radiation such as X-rays, gamma rays, and electrons which directly induce molecular cross-linking. (However, when used in conjunction with cross-linking agents dispersed within a material, both heat and light can be considered forms of radiant energy which induce cross-linking.) Electrons are the preferred form of radiant energy and are preferably produced by commercially available accelerators in the range of 0.5 to 2.0 me.
Another possible processing variation is the application of a fine mist of silicone spray -to the interior of the freshly extruded material to improve the further process ability of the material. A method for accomplishing such internal application is disclosed in cop ending Canadian Application Serial No. 403,969 filed in the Canadian Patent Office on Ma 28, 1982. Alternatively an anti-fog agent can be internally applied. Anti-fog agents have also been found to be of beneficial use in improving process ability.
In an addition to those materials disclosed in my cop ending application serial no. 403,969, anti-fog materials have demonstrated the ability to eliminate internal tape welding of an extended tube.
The polyolefin family and, in particular, the polyethyl-one family of shrink films provides a wide range of physical and performance characteristics such as shrink force (the amount of force that a film exerts per unit area of its cross-section during shrinkage), the degree of free shrink (the reduction in linear dimension in a specified direction that a material undergoes when subjected -to elevated temperatures while unrestrained), tensile strength (the highest force that can be applied to a unit area of film before it begins to tear apart), sealability, shrink tempera lure curve (the relationship of shrink to temperature), tear I

4536-5~0 initiation and resistance (the force at which a film will begin to tear and continue to tear), optics (gloss, haze and transpire-envy of material), and dimensional stability (the ability of the film to retain its original dimensions under different types of storage conditions). Film characteristics play an important role in the selection of a particular film and they differ for each type of packaging application and for each package. Consideration must be given to the product size, weight, shape, rigidity, number of product components, other packaging materials which may be used along with the film, and the type of packaging equipment available.
In view of the many above discussed physical character-is tics which are associated with polyethylene films and in further view of the numerous applications with which these films have already been associated and those to which they may be applied in the future, it is readily discernible that the need for ever improving any or all of the above described physical characteristics of -these films is great and, naturally, ongoing.
OBJECTS OF THE INVENTION
Accordingly, it is a general object of the invention to provide a heat shrinkable polyolefin film that will be an improvement over those films already utilized in the prior art.
It is another object of the present invention to provide a polyolefin film having improved ball burst properties.
Yet a further object of the present invention is to provide a polyolefin film having high elongation.
In another object of the present invention is to provide an improved polyolefin shrink film having improved optical quell-ties.

eye 4536-5~0 A still further object of the invention is to provide a polyolefin shrink film having a wide shrink temperature range.
Another object of the present invention is to provide an improved polyolefin shrink film having improved sealability.
Furthermore, yet another object of the present invention is to provide a polyolefin shrink film having improved resistance to tear propagation.
An even further object of the invention is to provide a polyolefin shrink film having an improved machinability.
Yet another object of the present invention is to provide an improved polyethylene shrink film which utilizes either a linear low density or a linear medium density polyethylene as a constituent of a core layer.
Still another object of -the present invention is to provide an improved process for manufacturing the film.
These and other objects are achieved by the polyolefin shrink film which is disclosed herein.
DEFINITIONS
Unless specifically set forth and defined or limited, the terms "polymer" or "polymer resin" as used herein generally include homopolymers, copolymers, terpolymers, block, graft polymers, random, and alternating polymers.
Polyolefin or olefin polymer or polymers as used herein includes not only polymers of unsaturated aliphatic hydrocarbons of the general formula CnH2n but also copolymers of olefins with other monomers such as ethylene with vinyl acetate.

~536-540 The term "melt flow" as used herein or "melt flow index"
is the amount, in grams, of a thermoplastic resin which can be forced through a given orifice under a specified pressure and them-portray within ten minutes as described in ASTM D 1238.
The term "core" or "core layer" as used herein means a layer in a multi-layer film which is enclosed on both sides by additional layers.
The term "skin" or "skin layer" as used herein means an outer (i.e., surface) layer of a multi-layer film.
The term "low density polyethylene" (LOPE) as used herein refers to homopolymers of ethylene having a density of from 0.910 to 0.925.
The term "linear low density polyethylene" (LLDPE) as used herein refers to a copolymer of ethylene and 8% or less of butane, octane or Helene having a density of from 0.910 to 0.925 and in which the molecules comprise long chains with few or no branches or cross-linked structures.
The term "linear medium density polyethylene" (LMDPE~
as used herein refers to a copolymer of ethylene and less than 8%
butane, octane or Helene having a density of from 0.926 to 0.940 and in which the molecules comprise long chains with few or no branches or cross-linked structures.
The term "ethylene vinyl acetate copolymer" (EVA) as used herein refers to a copolymer formed from ethylene and vinyl acetate monomers wherein the ethylene derived units are present in major amounts and the vinyl acetate derived units are present in minor amounts. Preferred ethyl vinyl acetate copolymers are those having from 2 - 12% vinyl acetate derived units.

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~536-5~0 The term "gauge" as used herein refers to -the dimension-at thickness of a film. 100 gauge is equal to 1 mix which is equal to 0.001 inch.
The term "racking ratio" as used herein refers to the ratio of expansion, (i.e. stretching) during orientation, of a film. For example, a racking ratio of four (4) or four (4) to one (1) would mean that the film had been stretched -to four times its original, unstretched, dimension during orientation.

-6b-
2~3~

Swallower OF THE lo lo It has been discovered that a Flexible, heat shrinkable thermos plastic packaging film having a desirable combination of physical char-acteristics such as syrinx tension, optical characteristics, curability, sealability, shrink temperature range, and tear resistance has breed achieved by the multi-layer flexible, thermoplastic packaging film of the present invention. This rnulti-layer film has a "core" layer that come proses a linear low density or linear medium density polyethylene resin.
A preferred three layer embodiment comprises, in addition to the above identified "core" layer, two skin Ayers each comprising an ethylene vinyl acetate copolymer. Preferably, the multi-layer film is irradiated.
It is also preferable to orient the film so that it is heat shrinkable in at least one direction.
The multi-layer film may be combined with other polymeric materials for specific applications. For instance, relatively thin layers may be added on either or both sides of the basic preferred three Mayer structure to improve seal strength or to lower gas and moisture permeability.
The invention also includes an improved process for manufacturing the film. One important aspect of the improved process is the utilize-lion of racking ratios id the ridge of 2.5 - I to 1 in the transverse direction and 2.5 to 4.2 in the longitudinal direction.

BRIEF DESCRIPTION OF THE DRAYING
Figure I is a cross sectional view of a preferred three layered embodiment of the present invention.
Figure If is a schematic representation of a preferred process for manufacturing the film of the present invention.

DESCRIPTION OF THE PREFERRED EMBODIMENTS
Referring to Figure 1, which is a cross sectional view of a three layered preferred embodiment of the present invention, it is seen that this embodiment comprises core layer 2 and skin layers I and 3. A
thickness ratio of the three layers of 1/2/1 is demonstrated in Figure I.
However the thickness of each skin layer may range between JO - 30% of the total film thickness thus, the thickness of the core layer may range ibid between 40 - 80% of the total film thickness. A preferred core layer 2 constituent comprises a linear low density polyethylene polymer. However, a linear medium density polyethylene polymer may be substituted as a core layer constituent without substantial alteration of the characteristics of the final film product.
LLDPE is herein utilized as an abbreviation for linear low density polyethylene as defined above. LMDPE is herein utilized as an abbreviation for linear medium density polyethylene as defined above.
My experimentation has revealed that an especially preferred core layer formulation consists essentially of a linear low density polyethylene. This material may be obtained from the Dow Chemical Company under the trademark Dow X2045.
Returning to Figure 1 and, in particular, to skin layers 1 and 3, my experimentation has also determined that a particularly preferred skin layer formulation consists essentially of an ethylene vinyl acetate copolymer. This material may be obtained from Dupont under the trademark Elvax 3128. Elvax 3128 is a copolymer of ethylene and vinyl acetate having from 8.4 - 9.4% of vinyl acetate having a Melt Flow of 2.0 -I 0.2. Alternatively, the material may be obtained from El Paso (formerly Reaction) under the -trademark PUCKS. PUCKS is a copolymer of ethylene and vinyl acetate having from 3.3 to 4.1% of vinyl acetate having a Melt Index of 2.0 + 0.5 and a density of 0.9232 - 0.9250.
Throughout this specification and claims all percentages are "by weight" percentages.
Throughout the specification and claims all references to density are in gm/cc at 23C.

~536 540 In summary, my experimentation has determined that a particularly preferred embodiment of the present invention comprises a core layer consisting essentially linear low density polyethylene and skin layers consisting essentially of an ethylene vinyl acetate copolymer of an ethylene vinyl acetate copolymer.
Although the above-discussed three layer formulations are generally preferred over structures having more than three layers as a result of the economics of manufacture, I have also produced various five layer formulations which are also sails-factory from a physical characteristics point of view. However the cost of manufacturing a five layer film is greater than that of a three layer film.
Those skilled in the art will readily recognize that all of the above disclosed, by weight, percentages are subject to slight variation. Additionally, these percentages may vary slightly as a result of the inclusion or application of additives such as the silicon mist and anti-fog agents discussed above or agents such as slip and anti-block events. A preferred anti-block agent is silica which is available from Johns Manville under the trademark White Mist. Preferred slip agents are Erucamide (available from Hummock Chemical under the trademark Kemamide E), and Strummed (available from the Hummock Chemical Company under the trademark Kemamide S) and, N, No Dioleoylethylenediamine (available from Glyco Chemical under the trademark Acrawax C).
A preferred Silicon spray is a liquid polyorganosiloxane manufac-lured by General Electric under -the trademark General Electric SF18 polydimethylsiloxane.
The general ranges for application of these additives ~2~2~;
4536-5~0 are as follows:
(l) Silica - 250 - 3000 PAM
12) Acrawax C: 200 - 4000 PAM
(3) Erucamide 200 - 5000 PAM
(4) Strummed: 200 - 5000 PAM
(5) Silicon Spray: .5 mgft2 _ and up.

When utilized within the specification and claims of the instant application the term "consisting essentially of" is not meant to exclude slight percentage variations or additives lo and agents of this sort.
Additional polyolefin layers and/or minor amounts of additives of the types described above may be added to the 3-layer structure of the present invention as described but care must be taken not to adversely alter -the desirable shrink tensions, shrink properties, optics and other characteristics or the multi-layer film of the present invention.
In the preferred process for making the multi-layer linear low or linear medium density polyethylene shrink film of the present invention the basic steps are blending the polymers for the various layers, coextruding the layers to form a multi-layer film, and then stretching the film to biaxially orient.
These steps and additional desirable steps will be explained in detail in the paragraphs which follow.

-pa-329~;

he process begins by blending the raw neutrals (i.e. polyp metric resins) in the proportions and ranges desired as discussed above.
the resins are usually purchased from a supplier in pellet form and can be blended in any one of a number of commercially available blenders as is well known in the art. During the blending process any additives and/or agents which are desired to be utilized are also incorporated.
The blended resins and applicable additives and/or agents are toed fed into the hoppers of extrudes which feed the coextrusion die.
For the three-layer film at least Tory extrudes need to be employed if each layer is to have a different composition. two extrudes are fed the materials desirable for the inner and outer skin layers and the other extrude is fed the linear low or linear medium density polyethylene material which is desired for utilization in the core layer. Additional extrudes may be employed, if desired. Preferably the materials are coextruded as a tube having a diameter. The final diameter of the coed-trued film will be dependent on the original diameter of the extruded tube and the subsequently applied racking ratio. the coextruded tube is relatively thick and is referred to as the "tape". Circular or tubular coextrusion dies are well known in the art and can be purchased from a number of manufactures. In addition to tubular coextrusion, slot dies could be used to coextrude the material in planar form. Well known single or multi-layer extrusion coating processes could also be employed if desired.
An additional process step which may be utilized is to irradi-ate the tape or unexpanded tubing or sheet by bombarding it with high-energy electrons from an accelator to cross-link the materials of the tape. Cross-linking greatly increases the structural strength of the film or the force at which the material can be stretched before tearing apart when the film materials are predominately ethylene such as polyp ethylene or etheylene-vinyl acetate. Irradiation also improves the optical properties of the film and changes the properties of the film at higher temperatures. If an irradiation step is employed a preferred irradiation dosage level is in the range of 0.5~ to ]2.0MR. MY is an abbreviation for megarads. A megarad is 1 x 10 fads with a fad being the quantity of ionizing irradiation that results in the absorption of loo ergs of energy per gram of irradiated material regardless of the ~L~]01kd I I
4536-5~0 source of the radiation. In some instances, it may be desirable to stretch the multi-layer film first and then irradiate it, or, if sequential coating is employed one layer or a group of layers could be irradiated and then another layer or layers could be added before the final step of stretching and orienting.
As stated above, an additional optional process step is the application of a fine silicon spray to the interior of the newly extruded tape. The details of this process step are disclosed in Canadian Application Serial Number 403,969 filed on May 28, 1982.
Following coextrusion, quenching to cool, and if desired irradiation, the extruded tape is reheated and is continuously inflated by internal elf pressure into a bubble thereby trays-forming the narrow tape with thick walls into a wide film with thin walls of the desired film thickness. This process is sometimes referred to as the "trapped bubble technique" of orientation or as "racking". After stretching, the bubble is then deflated and the film is wound onto semi-finished rolls called "mill rolls".
The racking process orients the film, by stretching it transversely and, to some extent, longitudinally to rearrange the molecules and thus impart shrink capabilities to the film and modify the film's physical characteristics. Additional longitudinal or machine direction stretching may be accomplished by revolving the deflate rollers which aid in the collapsing of the "blown bubble" at a speed greater than that of the rolls which serve to transport the reheated "tape" to the racking or blown bubble area.
All of these methods of orientation are well known in the art.
It has now been found that utilization of racking ratios ~22~

of from 2.5 to 4.2 in the transverse direction and 2,5 - 4.2 in the longitudinal direction result in films having lower degrees of orientation along with improved physical characteristics such as, for example, improved elongation as measured in accordance with ASTM 882.
To further disclose and clarify the scope of my invent lion to those skilled in the art the following examples are presented.

-ha-I
E~.~IPLE 1 A three layered structure having an approximate layer thickness ratio of l/2/l was extruded by supplying four extrudes. Extrudes number 2 and 3 which supplied the die orifice for the core layer were provided with 100% linear low density polyethylene (Dow X2045 (0.920 density, Melt index lo Extrudes No. l and 4 each supplied a die orifice for a skin layer and both were supplied with 100% ethylene vinyl acetate copolymer having 3.3 - 4.1h vinyl acetate. IPE204-CS95 (0~9232 -0.9250 density, Melt Index 2.0 0.5)].
The temperature of extrude Dumber 1 was set in the temperature range of from DOW. Extrude No. 2 was maintained at a temperature range of from 425-485F. Extrude No. 3 was maintained at a temperature range of from 425-495F and Extrude No. 4 was maintained at a tempera-lure from 350-375F. The circular die was maintained at a temperature range of 400~F.
The tape was extruded at 53 feet per minute.
After extrusion of the layers through the 6 inch circular die orifice the tubular extradite which had a tape thickness of approximately 9 mill and a tubular width of approximately 5 5/8 inches was quenched to cool by passing through a cold water bath. Upon extrusion of the tape a wine silicon mist was applied to the interior of the extruded tube at the rate of 6 my. ft. . The tape was wound up. Thereafter, the tube was passed through a irradiation unit at approximately 68 feet per minute to accomplish an irradiation level of 6 MR. The irradiated tubular extra-date was then reheated to orient by passing though a heating zone or oven. Thereafter the film was cooled by water quenching to lock-in the oriented molecular structure. final film thickness was approximately 75 gauge.

EXPEL II
The compositions utilized were the same as in example I.
All of the process parameters were the same as example one with the exception that the tape was extruded at 68 feet per minute and was 6 mix in thickness. The tape was transversely racked at 3.6 to 1 and longitudinally racked at 3.14 to ]. final film thickness was I gauge.

~22LB12/kd ~2~9~6 E~PLE. III
A three layered structure having an approximate layer thickness of 114/1 was extruded by supplying 4 extrudes. ~xtruders number 2 and 3 which supplied the die orifice for the core layer were provided with 100%
linear low density polyethylene DOW X2045 (0.920 density, welt Index I ExLruders number 1 and 4 each supplied a die orifice for a skin layer and both were supplied with 100% ethylene vinyl acetate copolymer having from 8.4 - 9.4% vinyl acetate and a melt flow of 2 Q.2.
The temperature of extrude number 1 was set in the temperature range of from 350-375F. Extrude number 2 was set in the temperature range of from 425-475F. Extrude number 3 was set in the temperature range of 425-495F. Extrude number 4 was set in the temperature range of 350-375. The circular die was set at a temperature of 400F.
After extrusion of the layers through the 6 inch circular die orifice the tubular extradite which had a tape thickness of approximately 9 mill and a tubular width of 5 I inches was quenched to cool by pass-in through a cold bath at approximately 48 feet per minute. Upon extra-soon of the tape a fine silicon mist was applied to the interior of the extruded tube at the rate of 9 my. ft. .
The tube was next passed through an irradiation unit at approx-irately 48 feet per minute and irradiated to a level of 6 The irradiated tube was then reheated to orient by passing though a heating zone or oven. After being heated the tubular extradite was transversely stretched "racked" approximately 3.7 to 1 and longitu-finally stretched approximately 4.2 to 1. Thereafter the film was cooled by water quenching to look-in the orientation. Final film gauge was 75 gauge.
The data obtained upon testing of these materials is located in Table I below.

Y22LBl3/kd lo ill ;2%9Z~$

TABLE I
Example I II III

Bayer Ratio 1 lt2/1 1/2j1 1/4/1 Tensile Strength x ]00 (PSI) ED 138.6 ]22.5 129.4 TO ]56.6 ]60.1 ~53.0 jig Elongation (%) HO 202 ]94 ]89 Hades x ]000 (PSI) HO 25.7 23.5 22.6 TO 4 25.8 24.0 21.1 Tear Propagation (gyms.) If, HO 9.25 4.31 7.00 TO 5 4.31 2.81 8.38 Tear Resistance (lobs.) MD 0.64 0.51 0.76 TO 0.69 0.44 0.86 Ball Burst a 73F
0.50 In. Dia. Sphere Ho. (cm - kg) 15.1 ]0.3 20.6 Shrink Properties at ~85F 6 Free Shrink (%) MD , 20 19 22 Shrink tension (PSI) At 245F 6 Free Shrink I

TO 7 So 68 63 Shrink 'tension (PSI) MD 294 ~85 328 Optics Haze (%) 0.9 1.2 0.7 Gloss (45) 95 94 94 Total Transmission 92.6 92.6 92.8 Y22~B14/kd Footnote to Table I 1 2 Z9 2 9 6 ASTM D 882 ;

8ASTM D ]003 All of the above tabulated Table I data are averages obtained by procedures in accordance with the designated ASTM standard.
it should be understood that the detailed description and specific examples which indicate the presently preferred embodiments of the invention are given by way of illustration only since various changes and modifications within the spirit and scope of the invention will become apparent to those of ordinary skill in the art upon review of the above detailed description and examples.
In view of the above:

Y14LC15/kq - I

Claims (13)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A multi-layer polyolefin film comprising a core layer and two skin layers wherein said core layer comprises a linear low density polyethylene and said skin layers comprise an ethylene vinyl acetate copolymer.
2. A multi-layer polyolefin film comprising a core layer and two skin layers wherein said core layer comprises a linear medium density polyethylene and said skin layers comprise an ethylene vinyl acetate copolymer.
3. The multi-layer film of claims 1 or 2, wherein said ethylene vinyl acetate copolymer comprises from 2 - 12% vinyl acetate.
4. The multi-layer film of claims 1 or 2, wherein said ethylene vinyl acetate copolymer comprises from 3.3 - 4.1% vinyl acetate.
5. The multi-layer film of claims 1 or 2, wherein.said ethylene vinyl acetate copolymer comprises 8.4 - 9.4% vinyl acetate.
6. The multi-layer film of claim 1, wherein said film consists of said core and said skin layers.
7. The multi-layer film of claim 2, wherein said film consists of said core and said skin layers.
8. The multi-layer film of claims 1 or 2, wherein said film has been irradiated with from 0.5 to 12.0 MR.
9. The multi-layer film of claims 6 or 7, wherein said ethylene vinyl acetate copolymer comprises from 2 - 12% vinyl acetate.
10. The multi-layer film of claims 6 or 7, wherein said ethylene vinyl acetate copolymer comprises from 3.3 - 4.1% vinyl acetate.
11. The multi-layer film of claims 6 or 7, wherein said ethylene vinyl acetate copolymer comprises from 8.4 - 9.4% vinyl acetate.
12. The multi-layer film of claims 6 or 7, wherein said film has been irradiated with from 0.5 to 12.0 MR.
13. The multi-layer film of claims 6 or 7, wherein said film has been irradiated with 6.0 MR.
CA000443913A 1983-02-18 1983-12-21 Linear polyethylene shrink film and process for making same Expired CA1229296A (en)

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US467,723 1983-02-18

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BE (1) BE898897A (en)
BR (1) BR8305895A (en)
CA (1) CA1229296A (en)
DE (1) DE3332781A1 (en)
DK (1) DK465483A (en)
FI (1) FI833234A (en)
FR (1) FR2541181A1 (en)
GB (2) GB8324003D0 (en)
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Publication number Priority date Publication date Assignee Title
US4617241A (en) * 1984-01-23 1986-10-14 W. R. Grace & Co., Cryovac Div. Linear polyethylene stretch/shrink films
US4820557A (en) * 1987-09-17 1989-04-11 W. R. Grace & Co.-Conn. Thermoplastic packaging film of low I10 /I2
US5250332A (en) * 1988-10-18 1993-10-05 Rxs Schrumpftechnik Garnituren Gmbh Heat-shrinkable envelope having low-tearing susceptibility
EP0423549B1 (en) * 1989-10-20 1994-12-21 RXS Schrumpftechnik-Garnituren GmbH Heat-shrinkable covering with improved edge bear resistance
ATE208708T1 (en) * 1994-10-19 2001-11-15 Cryovac Inc HEAT SHRINKABLE MULTI-LAYER FILMS
EP0707954B1 (en) * 1994-10-19 2001-11-14 Cryovac, Inc. Multilayer heat-shrinkable films
JP3530154B2 (en) * 2001-07-17 2004-05-24 住友電工ファインポリマー株式会社 Polyethylene heat shrink tubing
FR2887801B1 (en) * 2005-07-01 2007-09-07 Bollore Sa FILM WITH SEVERAL LAYERS
JP5997591B2 (en) * 2012-11-19 2016-09-28 旭化成株式会社 Low temperature shrinkable overlap packaging film
WO2022271762A1 (en) * 2021-06-24 2022-12-29 Cryovac, Llc Linear tear multi-layer film

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GB8324003D0 (en) 1983-10-12
BR8305895A (en) 1984-09-18
AU565301B2 (en) 1987-09-10
AU1877683A (en) 1984-08-23
FI833234A (en) 1984-08-19
NZ205515A (en) 1986-08-08
SE8304779D0 (en) 1983-09-06
SE8304779L (en) 1984-08-19
FR2541181A1 (en) 1984-08-24
IT1169587B (en) 1987-06-03
GB2135239A (en) 1984-08-30
FI833234A0 (en) 1983-09-09
DK465483D0 (en) 1983-10-10
DK465483A (en) 1984-08-19
ZA837450B (en) 1985-05-29
NL8303516A (en) 1984-09-17
GB8325032D0 (en) 1983-10-19
DE3332781A1 (en) 1984-08-23
JPS59158254A (en) 1984-09-07
IT8323349A0 (en) 1983-10-18
JPH0450902B2 (en) 1992-08-17
BE898897A (en) 1984-05-30

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