Abstract:
A multiple layer structure comprising a skin layer composed of a polypropylene copolymer with styrene ethylene-butene styrene block copolymer within a range of 0-20% by weight skin layer, and, a radio frequency (“RF”) susceptible layer adhered to the skin layer. The RF layer has a first component of a propylene based polymer, a second component of a nonpropylene polyolefin, a third component of a radio frequency susceptible polymer, and a fourth component of a polymeric compatibilizing agent wherein the radio frequency susceptible polymer is selected from the group consisting of ethylene acrylic acid copolymers, ethylene methacrylic acid copolymers, polyimides, polyurethanes, polyesters, and polyureas.

Description:
CONTINUATION INFORMATION 
     This application is a continuation of application Ser. No. 08/153,602, filed Nov. 16, 1993, U.S. Pat. No. 5,998,019, which is incorporated by reference and made a part thereof. 
    
    
     TECHNICAL FIELD 
     The present invention relates generally to materials for making medical grade products and more specifically to a thin film product which may be used to manufacture articles such as plastic containers and medical tubing. 
     BACKGROUND OF THE INVENTION 
     In the medical field, where beneficial agents are collected, processed and stored in containers, transported, and ultimately delivered through tubes by infusion to patients to achieve therapeutic effects, materials which are used to fabricate the containers must have a unique combination of properties. For example, in order to visually inspect solutions for particulate contaminants, the container must be optically transparent. To infuse a solution from a container by collapsing the container walls, without introducing air into the container, the material which forms the walls must be sufficiently flexible. The material must be functional over a wide range of temperatures. The material must function at low temperatures by maintaining its flexibility and toughness because some solutions, for example, certain premixed drug solutions are stored and transported in containers at temperatures such as −25 to −30° C. to minimize the drug degradation. The material must also be functional at high temperatures to withstand the heat of sterilization; a process which most medical packages and nutritional products are subjected to prior to shipment. The sterilization process usually includes exposing the container to steam at temperatures typically 121° C. and at elevated pressures. Thus, the material needs to withstand the temperature and pressures without significant distortions (“heat distortion resistance”). 
     For ease of manufacture into useful articles, it is desirable that the material be sealable using radio frequency (“RF”) generally at about 27.12 MHz. Therefore, the material should possess sufficient dielectric loss properties to convert the RF energy to thermal energy. 
     A further requirement is to minimize the environmental impact upon the disposal of the article fabricated from the material after its intended use. For those articles that are disposed of in landfills, it is desirable to use as little material as possible and avoid the incorporation of low molecular weight leachable components to construct the article. Thus, the material should be light weight and have good mechanical strength. Further benefits are realized by using a material which may be recycled by thermoplastically reprocessing the post-consumer article into other useful articles. 
     For those containers which are disposed of through incineration, it is necessary to use a material which helps to eliminate the dangers of biological hazards, and to minimize or eliminate entirely the formation of inorganic acids which are environmentally harmful, irritating, and corrosive, or other products which are harmful, irritating, or otherwise objectionable upon incineration. 
     It is also desirable that the material be free from or have a low content of low molecular weight additives such as plasticizers, stabilizers and the like which could be released into the medications or biological fluids or tissues thereby causing danger to patients using such devices or are contaminating such substances being stored or processed in such devices. For containers which hold solutions for transfusion, such contamination could make its way into the transfusion pathway and into the patient possibly causing injury to the patient. 
     Traditional flexible polyvinyl chloride materials meets a number of, and in some cases, most of the above-mentioned requirements. Polyvinyl chloride (“PVC”) also offers the distinct advantage of being one of the most cost effective materials for constructing devices which meet the above requirements. However, PVC may generate objectionable amounts of hydrogen chloride (or hydrochloric acid when contacted with water) upon incineration, causing corrosion of the incinerator. PVC sometimes contains plasticizers which may leach into drugs or biological fluids or tissues that come in contact with PVC formulations. Thus, many materials have been devised to replace PVC. However, most alternate materials are too expensive to implement and still do not meet all of the above requirements. 
     There have been many attempts to develop a film material to replace PVC, but most attempts have been unsuccessful for one reason or another. For example, in U.S. Pat. No. 4,966,795 which discloses multilayer film compositions capable of withstanding the steam sterilization, cannot be welded by radio frequency dielectric heating thus cannot be assembled by this rapid, low costs, reliable and practical process. European Application No. EP 0 310 143 A1 discloses multilayer films that meet most of the requirements, and can be RF welded. However, components of the disclosed film are cross-linked by radiation and, therefore, cannot be recycled by the standard thermoplastic processing methods. In addition, due to the irradiation step, appreciable amounts of acetic acid is liberated and trapped in the material. Upon steam sterilization, the acetic acid migrates into the packaging contents as a contaminant and by altering the pH of the contents acts as a potential chemical reactant to the contents or as a catalyst to the degradation of the contents. 
     The main objective of the present invention is the creation of thermoplastic materials which are, overall, superior to those materials, of which we are aware, which have been heretofore known to the art or have been commercially used or marketed. The properties of such materials includes flexibility, extensibility, and strain recoverability, not just at room temperatures, but through a wide range of ambient and refrigerated temperatures. The material should be sufficiently optically transparent for visual inspection, and steam sterilizable at temperatures up to 121° C. The material should be capable of being subjected to significant strains without exhibiting strain whitening, which can indicate a physical and a cosmetic defect. A further objective is that the material be capable of assembly by the RF methods. Another objective is that the material be substantially free of low molecular weight leachable additives, and be capable of safe disposal by incineration without the generation of significant amounts of corrosive inorganic acids. Another objective is that the material be recyclable by standard thermoplastic processing methods after use. It is also desirable that the material incorporate reground scrap material recovered during the manufacturing process to save material costs and reduce manufacturing waste. Finally, the material should serve as a cost effective alternative to various PVC formulations currently being used for medical devices. 
     When more than one polymer is blended to form an alloying composition, it is difficult to achieve all of the above objectives simultaneously. For example, in most instances alloy composition may scatter light; thus, they fail to meet the optical clarity objective. The light scattering intensity (measured by haze) depends on the domain size of components in the micrometer (μ) range, and the proximity of the refractive indices of the components. As a general rule, the selection of components that can be satisfactorily processed into very small domain sizes, and yet with a minimum of refractive index mismatches, is a difficult task. 
     The present invention is provided to solve these and other problems. 
     SUMMARY OF THE INVENTION 
     In accordance with the present invention certain multiple layer polymer based structures are disclosed. The films may be fabricated into medical grade articles such as containers for storing medical solutions or blood products, blood bags, and related items, or other products constructed from multi-layered structures. 
     It is an object of the present invention to prepare a multi-layered film having the following physical properties: (1) a mechanical modulus less than 40,000 psi and more preferably less than 25,000 psi when measured in accordance with ASTM D-882, (2) a greater than or equal to 70%, and more preferably greater than or equal to 75%, recovery in length after an initial deformation of 20%, (3) and optical haze of less than 30%, and more preferably less than 15%, when measured for a composition 9 mils thick and in accordance to ASTM D-1003, (4) the loss tangent measured at 1 Hz at processing temperatures is greater than 1.0, and more preferably greater than 2.0, (5) the content of elemental halogens is less than 0.1%, and more preferably less than 0.0 1%, (6) the low molecular weight water soluble fraction is less than 0.1%, and more preferably less than 0.005%, (7) the maximum dielectric loss between 1 and 60 MHz and between the temperature range of 25-250° C. is greater than or equal to 0.05 and more preferably greater than or equal to 0.1, (8) autoclave resistance measured by sample creep at 121° C. under 27 psi loading is less than or equal to 60% and more preferably less than or equal to 20%, and (9) there is no strain whitening after being strained at moderate speeds of about 20 inches (50 cm) per minute at about 100% elongation and the presence of strain whitening is noted or the lack thereof. 
     The multiple layer structure of the present invention comprises a skin layer preferably composed of a polypropylene copolymers with styrene and hydrocarbon block copolymers. More preferably a propylene copolymer with ethylene-butene styrene (“SEBS”) within a range of 0-20% by weight of the skin layer. The structure further includes a radio frequency (“RF”) susceptible layer adhered to the skin layer. The RF layer is composed of a first component of a polypropylene polymer, a second component of a non-propylene polyolefin (one that does not contain propylene repeating units), a third component of a radio frequency susceptible polymer, and a fourth component of a polymeric compatibilizing agent. In alternate embodiments, additional layers such as core, scrap, and barrier layers are added to the skin and RF layers to confer additional or enhanced functionality of the resultant film structure. 
     The RF layer is the subject of the concurrently filed U.S. Pat. No. 5,849,843 which is incorporated herein by reference. The multi-layered film structure of the present invention offers additional features that the compositions of the RF layer alone do not provide. The additional features of the multi-layer film include an exterior surface gloss and reduced tackiness to the outside surface of the film structure. Additionally, the multilayered film structure has improved vapor barrier properties, greater strength and optical clarity, and is cleaner or has reduced tendency to migrate into the contents of the container. 
     The core layer, which is interposed between the skin layer and the RF layer consists of three components. Preferably, the first component is polypropylene which constitutes about 40% of the core layer, the second component is an ultra low density polyethylene (“ULDPE”) which constitutes about 50% by weight of the core layer, and the third component is styrene-hydrocarbon block copolymer and more preferably an SEBS block copolymer which constitutes about 10% by weight of the core layer. The entire core layer should be 4.0 mils thick. 
     It is also desirable, for economic reasons among others, to incorporate reground scrap material recovered during the processing of the film material back into the composition of a film structure. This can lead to using significant amount of scrap material as a weight percent of the entire layer structure, thereby substantially decreasing the costs of the film product. The reground scrap may be incorporated into the above-described structure either as an additional discrete layer located somewhere between the skin layer and the RF layer or may be blended into the core layer as an additional component. In either case, significant resources are saved by reprocessing the scrap material. 
     To increase gas barrier properties of the structure, it is desirable to incorporate a barrier layer between the skin layer and the RF layer. The barrier layer may be attached to surrounding layers using adhesive tie layers. The barrier layer may be selected from ethylene vinyl alcohols such as that sold under the name Evalca (Evalca Co.), highly glass or crystalline polyamide such as Sclar PA® (Dupont Chemical Co.), high nitrile content acrylonitrile copolymers such as those sold under the tradename Barex® sold by British Petroleum. 
     Films having the aforesaid structure and compositions have been found to be flexible, optically clear, non-strain whitening, and steam and radiation sterilizable. Additionally, the films are compatible with medical applications because the components which constitute the film have a minimal extractability to the fluids and contents that the composition come in contact with. Further, the films are environmentally sound in that they do not generate harmful degradants upon incineration. Finally, the films provide a cost effective alternative to PVC. 
     Additional features and advantages of the present invention are described in, and will be apparent from, the drawing and the detailed description of the presently preferred embodiments. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     FIG. 1 shows a cross-sectional view of a two layered film structure of the present invention; 
     FIG. 2 shows a cross-sectional view of a three layered film structure of the present invention including a core layer added to the film of FIG. 1; 
     FIG. 3 shows a cross-sectional view of the film of FIG. 1 with a solution contact layer; 
     FIG. 4 shows a cross-sectional view of a four layered structure of the present invention having a discrete layer of scrap material between the skin and the core layers; 
     FIG. 5 shows a cross-sectional view of a film structure using reground scrap as a discrete layer between the core and the RF layers; 
     FIG. 6 shows a cross-sectional view of a film structure using reground scrap as a discrete layer which splits the core layer into two core layers; 
     FIG. 7 shows a cross-sectional view of a film structure of the present invention having seven layers including a barrier layer between the core and the RF layers and two tie layers; 
     FIG. 8 shows the same structure of FIG. 6 except the barrier layer is disposed between the core layer and the skin layers; 
     FIG. 9 shows a cross-sectional view of a film structure having a barrier layer dividing the core layers; and, 
     FIG. 10 shows a container constructed from one of the film structures of the present invention. 
    
    
     DETAILED DESCRIPTION 
     While this invention is susceptible of embodiments in many different forms, and will herein be described in detail, preferred embodiments of the invention are disclosed with the understanding that the present disclosure is to be considered as exemplifications of the principles of the invention and are not intended to limit the broad aspects of the invention to the embodiments illustrated. 
     According to the present invention, multiple layered film structures are provided which meet the requirements set forth above. 
     FIG. 1 shows a two layered film structure  10  having a skin layer  12  and a radio frequency (“RF”) susceptible layer  14 . The skin layer  12  confers heat distortion resistance and abrasion resistance and is preferably a polypropylene and more preferably a polypropylene copolymer blended with styrene and hydrocarbon block copolymers. More preferably, the skin layer  12  is a polypropylene copolymer blended with SEBS block copolymer within a range of 0-20% by weight. The skin layer  12  should have a thickness within the range of 0.2-3.0 mils thick. 
     The RF susceptible layer  14  of the present invention should have a dielectric loss of greater than 0.05 at frequencies within the range of 1-60 MHz within a temperature range of ambient to 250° C. The RF layer  14  preferably has four components. The RF layer  14  confers RF sealability, flexibility, heat distortion resistance, and compatibility to the film structure  10 . The first component of the RF layer  14  is chosen from polypropylene copolymers and preferably the propylene alpha-olefin random copolymers (“PPE”). The PPE&#39;s possess the required rigidity and the resistance to yielding at the autoclave temperatures of about 121° C. However, by themselves, the PPE&#39;s are too rigid to meet the flexibility requirements. When combined by alloying with certain low modulus polymers, good flexibility can be achieved. 
     These low modulus copolymers can include ethylene based copolymers such as ethylene-co-vinyl acetate (“EVA”), ethylene co-alpha olefins, or the so-called ultra low density (typically less than 0.90 Kg/L) polyethylenes (“ULDPE”). These ULDPE include those commercially available products sold under the trademarks TAFMER® (Mitsui Petrochemical Co.) under the product designation A485, Exact® (Exxon Chemical Company) under the product designations 4023-4024, and Insite® technology polymers (Dow Chemical Co.). In addition, poly butene-1 (“PB”), such as those sold by Shell Chemical Company under product designations PB-8010, PB-8310; thermoplastic elastomers based on SEBS block copolymers, (Shell Chemical Company), poly isobutene (“PIB”) under the product designations Vistanex L-80, L-100, L-120, L-140 (Exxon Chemical Company), ethylene alkyl acrylate, the methyl acrylate copolymers (“EMA”) such as those under the product designation EMAC 2707, and DS-1130 (Chevron), and n-butyl acrylates (“ENBA”) (Quantum Chemical) were found to be acceptable copolymers. Ethylene copolymers such as the acrylic and methacrylic acid copolymers and their partially neutralized salts and ionomers, such as PRIMACOR® (Dow Chemical Company) and SURYLN® (E.I. DuPont de Nemours &amp; Company) were also acceptable. Typically, ethylene based copolymers have melting point temperatures of less than about 110° C. are not suited for autoclaving at 121° C. applications. Furthermore, only a limited range of proportions of each component allows the simultaneous fulfillment of the flexibility and autoclavability requirements. 
     Preferably the first component is chosen from the group of polypropylene homo and random copolymers with alpha olefins which constitutes approximately 30-60%, more preferably 35-45%, and most preferably 45%, by weight of the film. For example, random copolymers of propylene and ethylene where the ethylene content is in an amount within the range of 0-6%, and more preferably within the range of 2-6%, of the weight of the propylene is preferred as the first component. 
     The second component of the RF layer  14  confers flexibility and low temperature ductility to the RF layer  14  and is chosen from the group consisting of polyolefins that do not have propylene repeating units (“non propylene based polyolefins”) including ethylene copolymers including ULDPE, polybutene, butene ethylene copolymers, ethylene vinyl acetate, copolymers with vinyl acetate contents between approximately 18-50%, ethylene methyl acrylate copolymers with methyl acrylate contents being between approximately 20-40%, ethylene n-butyl acrylate copolymers with n-butyl acrylate content of between 20-40%, ethylene acrylic acid copolymers with the acrylic acid content of greater than approximately 15%. An example of these products are sold under such product designations as Tafmer A-4085 (Mitsui), EMAC DS-1130 (Chevron), Exact 4023, 4024 and 4028 (Exxon). Preferably, the second component is either ULDPE sold by Mitsui Petrochemical Company under the designation TAFMER A-4085, or polybutene-1, PB8010 and PB8310 (Shell Chemical Co.), and should constitute approximately 25-50%, more preferably 35-45%, and most preferably 45%, by weight of the film. 
     The first and second components of the RF layer  14  may be replaced by a single component selected from a high melting temperature and flexible olefins such as those polypropylenes sold by the Rexene Company under the product designation FPO. The melting point temperature of this component should be greater than 130° C. and the modulus less than 20,000 psi. This component should constitute between 30-60% by weight of the RF layer. 
     To impart RF dielectric loss to the RF layer  14 , certain known high dielectric loss ingredients are included as the third component of the film structure  10 . For example, EVA and EMA of sufficiently high co-monomer contents exhibit significant loss properties at 27 MHz to allow the compositions to be sealed by the dielectric process. Polyamides as a class of material, and ethylene vinyl alcohol (“EVOH”) copolymers (typically produced by hydrolysing EVA copolymers), both possess high dielectric loss properties at suitable temperatures. Other active materials include PVC, vinylidine chlorides, and fluorides, copolymer of bis-phenol-A and epichlorohydrines known as PHENOXYS® (Union Carbide). However, significant contents of these chlorine and fluorine containing polymers would make them environmentally unsound as incineration of such a material would generate inorganic acids. Therefore, the third component of the RF layer  14  is preferably chosen from the class of polyamides. 
     Preferably, the polyamides of the present invention will be chosen from aliphatic polyamides resulting from the condensation reaction of di-amines having a carbon number within a range of 2-13, aliphatic polyamides resulting from a condensation reaction of di-acids having a carbon number within a range of 2-13, polyamides resulting from the condensation reaction of dimer fatty acids, and amide containing copolymers (random, block or graft). 
     Polyamides such as nylons are widely used in film material because they offer abrasion resistance to the film. However, rarely are the nylons found in the layer which contacts medical solutions as they typically contaminate the solution by leaching out into the solution. However, it has been found by the applicants of the present invention that various dimer fatty acid polyamides sold by, for example, Henkel Corporation under the product designations MACRO-MELT and VERSAMID do not lead to such contamination and thus are the most preferred third component of the RF layer  14 . The third component should constitute approximately 3-40%, more preferably between 7-13%, and most preferably 10%, by weight of the RF layer  14 . 
     The radio frequency susceptible polymers can also be selected from two groups of polymers. The first group consists of ethylene copolymers having 50-85% ethylene content with comonomers selected from the group consisting of acrylic acid, methacrylic acid, ester derivatives of acrylic acid with alcohols having 1-10 carbons, ester derivatives of methacrylic acid with alcohols having 1-10 carbons, vinyl acetate, and vinyl alcohol. The RF susceptible polymer may also be selected from a second group consisting of copolymers containing segments of polyurethane, polyester, polyurea, polyimide, polysulfones, and polyamides. These functionalities may constitute between 5-100% of the RF susceptible polymer. The RF susceptible polymer should constitute by weight within the range of 5-50% of the composition. Preferably, the RF component is copolymers of ethylene methyl acrylate with methyl acrylate within the range of 15-25% by weight of the polymer. 
     The fourth component of the RF layer  14  confers compatibility between the polar and nonpolar components of the RF layer  14 . The fourth component was chosen from styrene-hydrocarbon block copolymers and preferably SEBS block copolymers that are modified by maleic anhydride, epoxy, or carboxylate functionalities. Most preferably the fourth component is an SEBS block copolymer that is maleic anhydride functionalized. Such a product is sold by Shell Chemical Company under product designation KRATON RP-6509. The fourth component should constitute approximately 5-40%, more preferably 7-13%, and most preferably 10% by weight of the RF layer  14 . 
     It may also be desirable to include a fifth component to the RF layer  14  of an SEBS block copolymer, not modified by the above functional groups, such as the one sold by the Shell Chemical Company under the product designation KRATON G-1652. This component should constitute between 5-40% by weight of the RF Layer, more preferably between 7-13%, and most preferably 10%. 
     Preferably the RF susceptible layer will have a thickness within the range of 1-9 mils are more preferably 5.0 mils-8.0 mils, and most preferably 5.0 mils. The skin layer will have a thickness within the range of 0.2-3.0 mils and most preferably 0.5 mils. 
     FIG. 2 shows another embodiment of the present invention having a core layer  16  interposed between the skin layer  12  and the RF layer  14 . The core layer  16  confers heat distortion resistance, and flexibility to the film structure  10  and compatibility among the components of the film structure  10 . Preferably, the core layer will have a thickness within the range of 0.5-10 mils and more preferably 1-4 mils. The core layer  16  includes three components. The first component is a polyolefin and preferably a polypropylene in an amount that constitutes in a range of 20-60% by weight of the core layer  16 , more preferably 35-50%, and most preferably 45% of the core layer  16 . 
     The second component of the core layer  16  is chosen from a group consisting of compounds that confer flexibility to the core layer  16  including ULDPE, polybutene copolymers. Preferably, the second component of the core layer is ULDPE or polybutene-1 in an amount by weight of 40%-60%, more preferably 40-50%, and most preferably 40%. 
     The third component of the core layer  16  is chosen from a group of compounds that confer compatibility among the components of the core layer  16  and includes styrene-hydrocarbon block copolymers and most preferably SEBS block copolymers. The third component is in an amount preferably within a range of 5-40% by weight of the core layer  16 , more preferably 7-15%, and most preferably 15%. 
     It is also possible to add as a fourth component of the core layer  16 , reground trim scrap material recovered during the manufacturing of containers. The scrap material is dispersed throughout the core layer  16 . Scrap may be added in an amount preferably between approximately 0-50% by weight of the core layer  16 , and more preferably within the range of 10-30% and most preferably within the range of 3-12%. 
     FIG. 3 shows the film or sheet structure of FIG. 1 including a solution contact layer  17  adhered to a side of the RF layer opposite the skin layer  12 . The solution contact layer  17  includes three components that may be chosen from the same first three components and the same weight percentage ranges of the core layer  16  set forth above. Preferably, the solution contact layer  17  has a thickness within the range of 0.2-1.0 mils and most preferably 1.0 mils. 
     FIG. 4 shows another embodiment of the multiple layer film structure having the skin layer  12 , core layer  16 , and RF layer  14  as described above with an additional discrete layer of scrap  20  between the skin layer  12  and the core layer  16 . FIG. 5 shows the discrete scrap layer  20  between the core layer  16  and the RF layer  20 . FIG. 6 shows the scrap layer  20  dividing the core layer  16  into first and second core layers  16   a  and  16   b . Preferably, the layer of regrind should have a thickness within the range of 0.5-5.0 mils and most preferably 1.0 mils. 
     FIG. 7 shows another embodiment of the present invention having seven layers including the skin  12 , core  16 , and RF layers  14  discussed above, with a barrier layer  26  interposed between the core  16  and RF layers  14  and adhered thereto with tie layers  28  attached to opposite sides of the barrier layer  26 . FIG. 8 shows the barrier layer  26  between the core layer  16  and the skin layer  12 . FIG. 9 shows the barrier layer  26  dividing the core layer  14  into two core layers  14   a  and  14   b . The barrier layer  26  increases the gas barrier properties of the film structure  10 . The barrier layer  26  is selected from the group consisting ethylene vinyl alcohols such as that sold under the name Evalca (Evalca Co.), highly glassy or crystalline polyamide such as Sclar PA® (Dupont Chemical Co.), high nitrile content acrylonitrile copolymers such as Barex® sold by British Petroleum. Preferably, the barrier layer  26  is ethylene vinyl alcohol, and has a thickness within the range of 0.3-1.5 mils and most preferably 1.0 mils. 
     The tie layers  28  may be selected from modified ethylene and propylene copolymers such as those sold under the product designations Prexar (Quantum Chemical Co.) and Bynel (Dupont) and should have a thickness within the range of 0.2-1.0 mils and most preferably 0.5 mil. 
     The above layers may be processed by coextrusion, coextrusion coating, or other acceptable process. It should be understood; however, that the method of manufacturing the film structure is not a part of the present invention, and thus the scope of this invention should not be limited to this extent. 
     These materials may be used to manufacture I.V. therapy bags such as the one shown in FIG.  10  and generally designated as  30 . 
     Films having various combinations of the above components and weight percentages as set forth in the examples below were tested using the following methods. 
     (1) AUTOCLAVABILITY: 
     Autoclave resistance is measured by sample creep, or the increase in the sample length, at 121° C. under 27 psi loading for one hour. The autoclave resistance must be less than or equal to 60%. 
     (2) LOW AND AMBIENT TEMPERATURE DUCTILITY: 
     (A) Low Temperature Ductility 
     In an instrumented impact tester fitted with a low temperature environmental chamber cooled with liquid nitrogen, film samples about 7 by 7 inches (18 cm by 18 cm) are mounted onto circular sample holders about 6 inches (15 cm) in diameter. A semi-spherical impact head with stress sensors is driven at high velocities (typically about 3 m/sec) into the preconditioned film loading it at the center. The stress-displacement curves are plotted, and the energy of impact is calculated by integration. The temperature at which the impact energy rises dramatically, and when the fractured specimen changes from brittle to ductile, high strain morphology is taken as a measure of the low temperature performance of the film (“L.Temp”). 
     (B) Mechanical Modulus and Recovery 
     The autoclaved film sample with a known geometry is mounted on a servohydraulically driven mechanical tester having cross heads to elongate the sample. At 10 inches (25 cm) per minute crosshead speed, the sample is elongated to about 20% elongation. At this point, the cross-heads travel and then reverse to travel in a direction opposite that originally used to stretch the sample. The stress strain behavior is recorded on a digital recorder. The elastic modulus (“E(Kpsi)”) is taken from the initial slope on the stress-strain curve, and the recovery taken from the excess sample dimension as a percentage of sample elongation. 
     (3) RF PROCESSIBILITY: 
     Connected to a Callahan 27.12 MHz, 2 KW Radio Frequency generator, is a rectangular brass die of about 0.25 (6.3 mm) by 4 inches (10 cm) opposing to a flat brass electrode, also connected to the generator. Upon closing the die with two sheets of the candidate material in between with solution sides facing each other, RF power of different amplitudes and durations are applied. When the RF cycle is over, the die is opened and the resultant seal examined by manually pulling apart the two sheets. The strength of the seal (versus the film strength) and the mode of failure (peel, tear, or cohesive failures) are used to rate the RF responsiveness of the material. 
     Alternatively, the candidate film is first sputter coated with gold or palladium to a thickness of 100 angstroms to render the surface conductive, cut into a circular geometry and mounted between the parallel electrodes in a dielectric capacitance measuring cell. Using a Hewlett Packard 4092 automatic RF bridge, the dielectric constant and the dielectric losses are measured at different frequencies up to 10 MHz and temperatures up to 150° C. The dielectric loss allows the calculation of heat generation under an RF field. From calculations or correlations with RF seal experiments the minimum dielectric loss for performance is obtained. 
     If the RF seal performance is obtained from the Callahan sealer, the following ranking scale is adopted: 
     
       
         
               
               
               
               
               
             
           
               
                   
                   
               
               
                   
                 RF Power 
                 RF Time 
                 Seal Strength 
                 Rating 
               
               
                   
                   
               
             
             
               
                   
                 80% 
                 10 
                 No 
                 0 
               
               
                   
                 80% 
                 10 
                 Peelable 
                 1 
               
               
                   
                 80% 
                 05 
                 Peelable 
                 2 
               
               
                   
                 60% 
                 03 
                 Strong 
                 3 
               
               
                   
                 50% 
                 03 
                 Strong 
                 4 
               
               
                   
                 30% 
                 03 
                 Strong 
                 5 
               
               
                   
                   
               
             
          
         
       
     
     (4) OPTICAL CLARITY: 
     Post autoclaved film samples are first cut into about 2 by 2 inches (5 by 5 cms) squares, mounted on a Hunter Colorimeter and their internal haze measured according to ASTM D-1003. Typically, internal haze level of less than 30% is required, preferably less than 20% for these thicknesses (“Haze %”). 
     (5) STRAIN WHITENING: 
     The autoclaved film is strained at moderate speeds of about 20 inches (50 cm) per minute to about 100% elongation (twice the original length) and the presence of strain whitening (indicated by 1) or lack thereof (indicated by 0) is noted (“S.Whitening”). 
     (6) ENVIRONMENTAL COMPATIBILITY: 
     The environmental compatibility comprises three important properties: (a) the material is free of low molecular weight plasticizers which could leach into landfills upon disposal, (2) the material can be thermoplastically recycled into useful items upon fulfilling the primary purpose of medical delivery, and (3) when disposed of by energy reclaim by incineration, no significant inorganic acids are released to harm the environment. (“Envir.”). The composition will also contain less than 0.1% halogens by weight. In order to facilitate recycling by melt processing, the resultant composition should have a loss tangent greater than 1.0 at 1 Hz measured at processing temperatures. 
     (7) SOLUTION COMPATIBILITY: 
     By solution compatibility we mean that a solution contained within the film is not contaminated by components which constitute the composition. (“S.Comp.”) The low molecular weight water soluble fraction of the composition will be less than 0.1%. 
     The following combinations were tested using the above test for the films set forth below. 
     
       
         
               
               
               
               
               
               
               
               
               
               
               
             
               
               
               
               
               
               
               
               
               
               
               
               
             
           
               
                   
               
               
                   
                   
                   
                 Mod- 
                 Strain 
                   
                   
                   
                 Dielec- 
                 Low 
                   
               
               
                 Reference 
                 Layer 
                   
                 ulus 
                 Recovery 
                 % 
                 Environ- 
                   
                 tric 
                 Tem- 
                 S. 
               
               
                 Number 
                 Type 
                 Layer Composition 
                 (psi) 
                 E (kpsi) 
                 Haze 
                 mental 
                 Autoclav. 
                 Loss 
                 perature 
                 Comp. 
               
               
                   
               
             
             
               
                   
               
             
          
           
               
                 FIG. 1 
                 Skin 
                 0.5 mil - 
                 100% Amoco PP Copolymer 8410 
                 25 
                 75 
                 10 
                 Yes 
                 Yes 
                 3 
                 −35° C. 
                 Yes 
               
               
                   
                 RF 
                 8.0 mils - 
                 40% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 10% Shell Kraton ™ RP-6509 
               
               
                   
                   
                   
                 10% Henkel Macromelt ™ 6301 
               
               
                 FIG. 2 
                 Skin 
                 0.5 mil - 
                 100% Amoco PP Copolymer 8410 
                 25 
                 75 
                 12 
                 Yes 
                 Yes 
                 4 
                 −40° C. 
                 Yes 
               
               
                   
                 Core 
                 4.0 mils - 
                 45% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 15% Shell Kraton ™ G1657 
               
               
                   
                 RF 
                 5.0 mils - 
                 40% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 10% Shell Kraton ™ RP-6509 
               
               
                   
                   
                   
                 10% Henkel Macromelt ™ 6301 
               
               
                 FIG. 3 
                 Skin 
                 0.5 mil - 
                 100% Amoco PP Copolymer 8410 
                 25 
                 70 
                 15 
                 Yes 
                 Yes 
                 2 
                 −35° C. 
                 Yes 
               
               
                   
                 RF 
                 8.0 mils - 
                 40% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 10% Shell Kraton ™ EP-6509 
               
               
                   
                   
                   
                 10% Henkel Macromelt ™ 6301 
               
               
                   
                 Solution 
                 1.0 mils - 
                 45% Solvay Fortiline ™ PP 
               
               
                   
                 Contact 
                   
                 Copolymer 4208 
               
               
                   
                 Skin 
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 15% Shell Kraton ™ G1657 
               
               
                 FIG. 4 
                 Skin 
                 0.5 mil - 
                 100% Amoco PP Copolymer 8410 
                 25 
                 75 
                 16 
                 Yes 
                 Yes 
                 4 
                 −35° C. 
                 Yes 
               
               
                   
                 Regrind 
                 1.0 mil - 
                 100% Regrind 
               
               
                   
                 Core 
                 3.0 mils - 
                 45% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 15% Shell Kraton ™ G1657 
               
               
                   
                 RF 
                 5.0 mils - 
                 40% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 10% Shell Kraton ™ RP6509 
               
               
                   
                   
                   
                 10% Henkel Macromelt ™ 6301 
               
               
                 FIG. 5 
                 Skin 
                 0.5 mil - 
                 100% Amoco PP Copolymer 8410 
                 25 
                 75 
                 16 
                 Yes 
                 Yes 
                 4 
                  35° C. 
                 Yes 
               
               
                   
                 Core 
                 3.0 mils - 
                 45% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 15% Shell Kraton ™ G1657 
               
               
                   
                 Regrind 
                 1.0 mil - 
                 100% Regrind 
               
               
                   
                 RF 
                 5.0 mils - 
                 40% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 10% Shell Kraton ™ RP6509 
               
               
                 FIG. 6 
                 Skin 
                 0.5 mil - 
                 100% Amoco PP Copolymer 8410 
                 25 
                 75 
                 16 
                 Yes 
                 Yes 
                 4 
                 −35° C. 
                 Yes 
               
               
                   
                 Core 
                 1.5 mils - 
                 45% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 15% Shell Kraton ™ G1657 
               
               
                   
                 Regrind 
                 1.0 mil - 
                 100% Regrind 
               
               
                   
                 Core 
                 1.5 mils - 
                 45% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 15% Shell Kraton ™ 1657 
               
               
                   
                 RF 
                 5.0 mils - 
                 45% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 15% Shell Kraton ™ RP6509 
               
               
                   
                   
                   
                 10% Henkel Macromelt ™ 6301 
               
               
                 FIG. 7 
                 Skin 
                 0.5 mil - 
                 100% Amoco PP Copolymer 8410 
                 30 
                 20 
                 20 
                 Yes 
                 Yes 
                 4 
                 −20° C. 
                 Yes 
               
               
                   
                 Core 
                 2.0 mils - 
                 45% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 15% Shell Kraton ™ G1657 
               
               
                   
                 Tie 
                 0.5 mil - 
                 100% Bynel 
               
               
                   
                 Barrier 
                 1.0 mil - 
                 100% EVOH 
               
               
                   
                 Tie 
                 0.5 mil - 
                 100% Bynel 
               
               
                   
                 RF 
                 5.0 mils - 
                 40% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 10% Shell Kraton ™ RP6509 
               
               
                   
                   
                   
                 10% Henkel Macromelt ™ 6301 
               
               
                 FIG. 8 
                 Skin 
                 0.5 mil - 
                 100% Amoco PP Copolymer 8410 
                 30 
                 70 
                 20 
                 Yes 
                 Yes 
                 3 
                 20° C. 
                 Yes 
               
               
                   
                 Tie 
                 0.5 mil - 
                 100% Bynel 
               
               
                   
                 Barrier 
                 1.0 mil - 
                 100% EVOH 
               
               
                   
                 Tie 
                 0.5 mil - 
                 100% Bynel 
               
               
                   
                 Core 
                 2.0 mils - 
                 45% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 15% Shell Kraton ™ G1657 
               
               
                   
                 RF 
                 5.0 mils - 
                 40% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 10% Shell Kraton ™ RP6509 
               
               
                   
                   
                   
                 10% Henkel Macromelt ™ 6301 
               
               
                 FIG. 9 
                 Skin 
                 0.5 mil - 
                 100% Amoco PP Copolymer 8410 
                 30 
                 70 
                 20 
                 Yes 
                 Yes 
                 3 
                 −20° C. 
                 Yes 
               
               
                   
                 Core 
                 1.0 mils - 
                 45% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 15% Shell Kraton ™ G1657 
               
               
                   
                 Tie 
                 0.5 mil - 
                 100% Bynel 
               
               
                   
                 Barrier 
                 1.0 mil - 
                 100% EVOH 
               
               
                   
                 Tie 
                 0.5 mil - 
                 100% Bynel 
               
               
                   
                 Core 
                 1.0 mils - 
                 45% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 15% Shell Kraton ™ G1657 
               
               
                   
                 RF 
                 5.0 mils - 
                 40% Solvay Fortiline ™ PP 
               
               
                   
                   
                   
                 Copolymer 4208 
               
               
                   
                   
                   
                 40% Mitsui Tafmer ™ ULDPE 
               
               
                   
                   
                   
                 10% Shell Kraton ™ RP6509 
               
               
                   
                   
                   
                 10% Henkel Macromelt ™ 6301 
               
               
                   
               
             
          
         
       
     
     It will be understood that the invention may be embodied in other specific forms without departing from the spirit or central characteristics thereof. The present examples and embodiments, therefore, are to be considered in all respects as illustrative and not restrictive, and the invention is not to be limited to the details given herein. 
     While the specific embodiments have been illustrated and described, numerous modifications come to mind without significantly departing from the spirit of the invention and the scope of protection is only limited by the scope of the accompanying claims.