Gas-barrier multilayer structure and process for producing the same
A multi-layer structure, gas barrier technology, applied in chemical instruments and methods, lamination, rigid containers, etc., can solve the problems of not specifying the specific properties of the multi-layer structure, and not recording the specific conditions of stretching.
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preparation example Construction
[0044] Next, a method for producing the gas barrier multilayer structure of the present invention will be described. First, a multilayer laminate comprising at least one layer 1 , at least one layer 2 and optionally layer 3 is prepared by known methods.
[0045] The multilayer laminate is then stretched and thermoformed under specific conditions to increase the crystallinity and orientation of layer 1, thereby improving gas barrier properties. "Stretch thermoforming" as used herein includes stretching of a film or sheet, stretch blow molding of a parison, etc., and deep draw forming of a film or sheet. Stretch thermoforming is generally performed at a temperature equal to or higher than the glass transition point of the resin material. Since the glass transition point varies with the type of resin and the degree of moisture absorption, thermoformability at a temperature equal to or higher than the glass transition point of the composite resin material varies greatly depending...
Embodiment
[0069] The present invention will be described in more detail below with reference to the following Examples and Comparative Examples. However, these examples are only for illustrating the present invention, and are not intended to limit the present invention. In the following Examples and Comparative Examples, various properties were measured and evaluated by the following methods.
[0070] (1) Melting point, glass transition point and Heat of Temperature-Rise Crystallization
[0071] The measurement was performed using a heat flow differential scanning calorimeter "DSC-50" from Shimadzu Corporation under the following conditions:
[0072] Standard: α-alumina
[0073] Sample: 10 mg
[0074] Heating rate: 10°C / min
[0075] Measuring temperature range: 25-300°C
[0076] Atmosphere: 30ml / min nitrogen
[0077] (2) Haze
[0078] Measured according to ASTM D-1003 using "COH-300A" color haze measuring device from Nippon Denshoku Industries Co., Ltd.
[0079] (3) Oxygen perme...
reference example 1
[0089] Composite resin C1 was formed at 260° C. to a thickness of 180 μm using a small-sized film forming machine (“LaboPlastomil” from Toyo Seiki Seisaku-Sho, Ltd.; screw diameter: 20 mmΦ; T-die width: 200 mm) single-layer unstretched film. The resulting unstretched film was subjected to simultaneous biaxial stretching using a tentering biaxially stretching machine available from Toyo Seiki Seisaku-Sho, Ltd. under the following conditions: a stretching temperature of 100° C., The preheating time is 30 seconds, the line speed in each direction is 60% / second, and the stretching ratio is 3×3 times. The maximum tensile stress during stretching was 0.7 MPa per unit cross-sectional area, and the haze of the obtained film (thickness: 20 µm) was 0.5%. The oxygen permeability at 23°C and 60% relative humidity (RH) is 0.05 ml·mm / square meter·day·atmospheric pressure, the heat of crystallization measured by DSC is 9 joules / gram, and the degree of orientation is 19.
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