JPH09314763A - Laminate - Google Patents
LaminateInfo
- Publication number
- JPH09314763A JPH09314763A JP16110196A JP16110196A JPH09314763A JP H09314763 A JPH09314763 A JP H09314763A JP 16110196 A JP16110196 A JP 16110196A JP 16110196 A JP16110196 A JP 16110196A JP H09314763 A JPH09314763 A JP H09314763A
- Authority
- JP
- Japan
- Prior art keywords
- layer
- thermoplastic elastomer
- laminate
- gas barrier
- elastic modulus
- 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.)
- Pending
Links
- 230000004888 barrier function Effects 0.000 claims abstract description 21
- 229920002725 thermoplastic elastomer Polymers 0.000 claims abstract description 18
- 229920005549 butyl rubber Polymers 0.000 claims abstract description 11
- 229920000459 Nitrile rubber Polymers 0.000 claims abstract description 10
- 239000000463 material Substances 0.000 claims abstract description 9
- 229920000219 Ethylene vinyl alcohol Polymers 0.000 claims abstract description 7
- 238000010030 laminating Methods 0.000 claims description 4
- 238000004073 vulcanization Methods 0.000 abstract description 4
- 239000004715 ethylene vinyl alcohol Substances 0.000 abstract 1
- RZXDTJIXPSCHCI-UHFFFAOYSA-N hexa-1,5-diene-2,5-diol Chemical compound OC(=C)CCC(O)=C RZXDTJIXPSCHCI-UHFFFAOYSA-N 0.000 abstract 1
- 239000010410 layer Substances 0.000 description 38
- 239000007789 gas Substances 0.000 description 21
- 239000000047 product Substances 0.000 description 9
- 150000001875 compounds Chemical class 0.000 description 8
- 229920001971 elastomer Polymers 0.000 description 5
- -1 polypropylene Polymers 0.000 description 5
- 239000005060 rubber Substances 0.000 description 5
- 229920002397 thermoplastic olefin Polymers 0.000 description 5
- 239000004743 Polypropylene Substances 0.000 description 4
- XLOMVQKBTHCTTD-UHFFFAOYSA-N Zinc monoxide Chemical compound [Zn]=O XLOMVQKBTHCTTD-UHFFFAOYSA-N 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 4
- 229920001155 polypropylene Polymers 0.000 description 4
- 239000012790 adhesive layer Substances 0.000 description 3
- 239000012530 fluid Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 229920002647 polyamide Polymers 0.000 description 3
- 229920005989 resin Polymers 0.000 description 3
- 239000011347 resin Substances 0.000 description 3
- 235000021355 Stearic acid Nutrition 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 2
- 150000001336 alkenes Chemical class 0.000 description 2
- 239000006229 carbon black Substances 0.000 description 2
- 229920001577 copolymer Polymers 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- FPYJFEHAWHCUMM-UHFFFAOYSA-N maleic anhydride Chemical compound O=C1OC(=O)C=C1 FPYJFEHAWHCUMM-UHFFFAOYSA-N 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 description 2
- OQCDKBAXFALNLD-UHFFFAOYSA-N octadecanoic acid Natural products CCCCCCCC(C)CCCCCCCCC(O)=O OQCDKBAXFALNLD-UHFFFAOYSA-N 0.000 description 2
- JRZJOMJEPLMPRA-UHFFFAOYSA-N olefin Natural products CCCCCCCC=C JRZJOMJEPLMPRA-UHFFFAOYSA-N 0.000 description 2
- 239000008117 stearic acid Substances 0.000 description 2
- 229910052717 sulfur Inorganic materials 0.000 description 2
- 239000011593 sulfur Substances 0.000 description 2
- 229920003051 synthetic elastomer Polymers 0.000 description 2
- 239000005061 synthetic rubber Substances 0.000 description 2
- 229920006345 thermoplastic polyamide Polymers 0.000 description 2
- 239000011787 zinc oxide Substances 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 1
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 1
- VGGSQFUCUMXWEO-UHFFFAOYSA-N Ethene Chemical compound C=C VGGSQFUCUMXWEO-UHFFFAOYSA-N 0.000 description 1
- 239000005977 Ethylene Substances 0.000 description 1
- 229920000181 Ethylene propylene rubber Polymers 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- 230000003712 anti-aging effect Effects 0.000 description 1
- 125000000484 butyl group Chemical group [H]C([*])([H])C([H])([H])C([H])([H])C([H])([H])[H] 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000007334 copolymerization reaction Methods 0.000 description 1
- 229910001873 dinitrogen Inorganic materials 0.000 description 1
- MIMDHDXOBDPUQW-UHFFFAOYSA-N dioctyl decanedioate Chemical compound CCCCCCCCOC(=O)CCCCCCCCC(=O)OCCCCCCCC MIMDHDXOBDPUQW-UHFFFAOYSA-N 0.000 description 1
- 229910001882 dioxygen Inorganic materials 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000005038 ethylene vinyl acetate Substances 0.000 description 1
- 239000012466 permeate Substances 0.000 description 1
- 239000003348 petrochemical agent Substances 0.000 description 1
- 239000004014 plasticizer Substances 0.000 description 1
- 229920001200 poly(ethylene-vinyl acetate) Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- QQONPFPTGQHPMA-UHFFFAOYSA-N propylene Natural products CC=C QQONPFPTGQHPMA-UHFFFAOYSA-N 0.000 description 1
- 125000004805 propylene group Chemical group [H]C([H])([H])C([H])([*:1])C([H])([H])[*:2] 0.000 description 1
- 229920003031 santoprene Polymers 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
Landscapes
- Laminated Bodies (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】本発明は、積層体に関する。
更に詳しくは、ガスバリア性および低温伸長耐久性にす
ぐれた積層体に関する。The present invention relates to a laminate.
More specifically, it relates to a laminate having excellent gas barrier properties and low temperature extension durability.
【0002】[0002]
【従来の技術】ダイアフラム、ブラダ等は、気体などの
流体圧力を伝達するアキュムレータ等に用いられてお
り、流体を透過させることなく、流体の圧力に応じて変
形するような性質が求められているので、水素ガス、酸
素ガス、窒素ガス等に対してガスバリア性を有するばか
りではなく、その用途に応じて低温伸長耐久性にもすぐ
れていることが要求されている。2. Description of the Related Art Diaphragms, bladders and the like are used in accumulators and the like for transmitting the pressure of fluid such as gas, and are required to have the property of deforming according to the pressure of fluid without allowing the fluid to permeate. Therefore, it is required not only to have gas barrier properties against hydrogen gas, oxygen gas, nitrogen gas, etc., but also to have excellent low temperature extension durability depending on the application.
【0003】ガスバリア性と低温伸長耐久性とを両立さ
せるためには、それぞれの妥協点で利用する必要があ
り、ガスバリア性を重視した場合には低温伸長耐久性が
大きく劣ってしまうため、ガスバリア性樹脂の選択が必
要となる。例えば、ガスバリア性樹脂として周知のエチ
レン-ビニルアルコール共重合体(エチレン-酢酸ビニル
共重合体けん化物)を用いる場合には、弾性率が高く、
伸長作動時には亀裂や破損を生ずるため、可塑剤を添加
して弾性率を低下せしめて使用した例はあるものの、ガ
スバリア性および低温伸長耐久性を高レベルでバランス
させることは一般には困難であるとされている。In order to achieve both the gas barrier property and the low temperature elongation durability, it is necessary to use them at their respective compromise points. When the gas barrier property is emphasized, the low temperature elongation durability is greatly deteriorated. Selection of resin is required. For example, when a well-known ethylene-vinyl alcohol copolymer (saponified ethylene-vinyl acetate copolymer) is used as a gas barrier resin, the elastic modulus is high,
Since cracks and damages occur during extension operation, although there are examples where a plasticizer was added to reduce the elastic modulus, it is generally difficult to balance gas barrier properties and low temperature extension durability at a high level. Has been done.
【0004】[0004]
【発明が解決しようとする課題】本発明の目的は、エチ
レン-ビニルアルコール共重合体をガスバリア層とする
積層体であって、低温伸長耐久性にもすぐれているもの
を提供することにある。SUMMARY OF THE INVENTION An object of the present invention is to provide a laminate having an ethylene-vinyl alcohol copolymer as a gas barrier layer, which has excellent low temperature elongation durability.
【0005】[0005]
【課題を解決するための手段】かかる本発明の目的は、
引張弾性率3×1010〜7×1010ダイン/cm2(-40℃)のエチ
レン-ビニルアルコール共重合体よりなるガスバリア層
の両面に、引張弾性率7×109〜3×1010ダイン/cm2(-40
℃)の接合材料層および引張弾性率3×109〜7×109ダイ
ン/cm2(-40℃)の熱可塑性エラストマー層を順次積層し
た積層体によって達成される。この積層体の熱可塑性エ
ラストマー層上には更にブチルゴムまたはニトリルゴム
を加硫接着させることができる。SUMMARY OF THE INVENTION The object of the present invention is as follows.
Tensile modulus of elasticity of 3 × 10 10 to 7 × 10 10 dynes / cm 2 (-40 ℃) made of ethylene-vinyl alcohol copolymer on both sides, tensile modulus of elasticity of 7 × 10 9 to 3 × 10 10 dynes / Cm 2 (-40
Is achieved by bonding the material layers and tensile elastic modulus 3 × 10 9 ~7 × 10 9 dynes / cm 2 thermoplastic elastomer layer sequentially stacked laminate (-40 ° C.) in ° C.). Butyl rubber or nitrile rubber can be further vulcanized and adhered onto the thermoplastic elastomer layer of this laminate.
【0006】[0006]
【発明の実施の形態】ガスバリア層に用いられるエチレ
ン-ビニルアルコール共重合体としては、エチレンの共
重合割合が高くなると、ガスバリア性、引張弾性率が共
に高くなる性質があり、その共重合割合が40モル%以上
になると、フィルム換算10cc・10μ/m2・24hr・atm(70
℃)以下というガスバリア性を満足させることができ、
引張弾性率(-40℃)も3×1010ダイン/cm2以上となる。
このような引張弾性率はガスバリア性との関係から規定
されるものであり、ただしその値が7×1010ダイン/cm2
以上になると、変形に耐えられなくなる。かかる共重合
体よりなるガスバリア層は、一般に約20〜200μm、好ま
しくは約50〜100μmの厚さで形成される。BEST MODE FOR CARRYING OUT THE INVENTION The ethylene-vinyl alcohol copolymer used in the gas barrier layer has the property that when the copolymerization ratio of ethylene is high, both the gas barrier property and the tensile elastic modulus are high. At 40 mol% or more, film equivalent 10cc / 10μ / m 2 / 24hr ・ atm (70
It is possible to satisfy the gas barrier property of (° C) or less,
The tensile modulus (-40 ° C) is also 3 × 10 10 dynes / cm 2 or more.
Such a tensile elastic modulus is specified in relation to the gas barrier property, provided that the value is 7 × 10 10 dynes / cm 2
If it becomes above, it will not be able to endure deformation. The gas barrier layer made of such a copolymer is generally formed to a thickness of about 20 to 200 μm, preferably about 50 to 100 μm.
【0007】ガスバリア層の両面には、柔軟層としての
熱可塑性エラストマー層を接合させるための接合材料層
が、一般に約10〜200μm、好ましくは約20〜100μmの厚
さで設けられる。かかる接合材料としては、無水マレイ
ン酸変性ポリプロピレンなどが用いられ、この材料層は
ガスバリア層と柔軟層との間の接合効果を図るばかりで
はなく、これら両者の中間の引張弾性率を保持せしめる
ことにより、低温伸長耐久性の向上をも図っている。A bonding material layer for bonding a thermoplastic elastomer layer as a flexible layer is generally provided on both surfaces of the gas barrier layer in a thickness of about 10 to 200 μm, preferably about 20 to 100 μm. As such a bonding material, a maleic anhydride modified polypropylene or the like is used, and this material layer not only has a bonding effect between the gas barrier layer and the flexible layer, but also holds a tensile elastic modulus between these two. Also, the low temperature extension durability is improved.
【0008】熱可塑性エラストマーとしては、好ましく
はオレフィン系熱可塑性エラストマーが用いられる。オ
レフィン系熱可塑性エラストマーとしては、エチレン-
プロピレンゴムとポリプロピレンとのブレンド体、高粘
度エチレン-プロピレンゴムとポリプロピレンとのブレ
ンド体、結晶性を有するエチレン-プロピレン共重合体
とポリエチレンとのブレンド体などであって、引張弾性
率が3×109〜7×109ダイン/cm2のものが用いられる。
オレフィン系熱可塑性エラストマー以外にはポリアミド
系熱可塑性エラストマーなども用いられ、これらの熱可
塑性エラストマー層上には、好ましくは更に低弾性率の
ブチルゴムまたはニトリルゴムが加硫接着されるので、
それの下層としてこのような引張弾性率を有するものが
選択されて用いられ、これ以上の引張弾性率のものを用
いると、低温伸長耐久性が低下するようになる。かかる
熱可塑性エラストマー層は、一般に約100〜1000μm、好
ましくは約300〜500μmの厚さで形成される。As the thermoplastic elastomer, an olefinic thermoplastic elastomer is preferably used. As the olefinic thermoplastic elastomer, ethylene-
Blends of propylene rubber and polypropylene, blends of high-viscosity ethylene-propylene rubber and polypropylene, blends of crystalline ethylene-propylene copolymer and polyethylene, etc., having a tensile modulus of 3 × 10 Those having a size of 9 to 7 × 10 9 dynes / cm 2 are used.
In addition to the olefin-based thermoplastic elastomer, a polyamide-based thermoplastic elastomer or the like is also used, and on these thermoplastic elastomer layers, butyl rubber or nitrile rubber having a lower elastic modulus is preferably vulcanized and adhered.
A layer having such a tensile elastic modulus is selected and used as a lower layer therefor, and if a layer having a tensile elastic modulus higher than that is used, the low temperature elongation durability is lowered. Such a thermoplastic elastomer layer is generally formed with a thickness of about 100 to 1000 μm, preferably about 300 to 500 μm.
【0009】最外層としてブチルゴムまたはニトリルゴ
ムが加硫接着される場合には、熱可塑性エラストマーと
の接合性のよいゴム配合物、例えば次のようなゴム配合
物が用いられる。 (ブチルゴム配合物) ブチルゴム(日本合成ゴム製品ブチル365) 100重量部 酸化亜鉛 10 〃 ステアリン酸 1 〃 FEFカーボンブラック 60 〃 イオウ 2 〃 加硫促進剤 2 〃 (ニトリルゴム配合物) ニトリルゴム(日本合成ゴム製品JSR240S) 100重量部 酸化亜鉛 5 〃 ステアリン酸 1 〃 HAFカーボンブラック 65 〃 ジオクチルセバケート 20 〃 老化防止剤(RD) 2 〃 〃 (810NA) 3 〃 〃 (NBC) 2 〃 加硫促進剤(CZ) 2 〃 〃 (TT) 2 〃 イオウ 0.5 〃When butyl rubber or nitrile rubber is vulcanized and bonded as the outermost layer, a rubber compound having a good bondability with the thermoplastic elastomer, for example, the following rubber compound is used. (Butyl rubber compound) Butyl rubber (Nippon synthetic rubber product Butyl 365) 100 parts by weight Zinc oxide 10 〃 Stearic acid 1 〃 FEF carbon black 60 〃 Sulfur 2 〃 Vulcanization accelerator 2 〃 (Nitrile rubber compound) Nitrile rubber (Nippon Synthetic rubber) Rubber product JSR240S) 100 parts by weight Zinc oxide 5 〃 Stearic acid 1 〃 HAF carbon black 65 〃 Dioctyl sebacate 20 〃 Anti-aging agent (RD) 2 〃 〃 (810NA) 3 〃 〃 (NBC) 2 〃 Vulcanization accelerator ( CZ) 2 〃 〃 (TT) 2 〃 sulfur 0.5 〃
【0010】ガスバリア層、接合材料層および熱可塑性
エラストマー層の積層は、これら各層の単層フィルムを
貼り合わせ、ラミネートする方法によっても行うことが
できるが、これら各層成分がいずれも熱可塑性であるの
で共押出法によって行われることが好ましい。これらの
積層体上に更にブチルゴムまたはニトリルゴムを加硫接
着させる場合には、これらゴム配合物の未加硫シートを
積層体上に接合させた上で、加熱加圧条件下での加硫接
着が行われる。The gas barrier layer, the bonding material layer, and the thermoplastic elastomer layer can be laminated by a method of laminating and laminating the monolayer films of these layers. However, since each of these layer components is thermoplastic. Preference is given to coextrusion. When further vulcanizing and adhering butyl rubber or nitrile rubber onto these laminates, an unvulcanized sheet of these rubber compounds is bonded onto the laminate, and then vulcanization and adhesion under heat and pressure conditions. Is done.
【0011】[0011]
【発明の効果】引張弾性率が極めて大きく、従って高ガ
スバリア性の樹脂層上に、順次引張弾性率の小さい接合
材料層および熱可塑性エラストマー層を積層させ、好ま
しくは更にブチルゴム、ニトリルゴムのような低弾性率
の材料を積層させることにより、各層相互間の接合力が
大きくしかも低温伸長耐久性の良好な積層体を得ること
ができる。このような良好な性質を有する積層体は、ダ
イアフラム、ブラダ等として有効に使用される。EFFECT OF THE INVENTION A bonding material layer and a thermoplastic elastomer layer having a small tensile elastic modulus are successively laminated on a resin layer having a very high tensile elastic modulus and therefore a high gas barrier property, and preferably a butyl rubber or a nitrile rubber is further used. By laminating materials having a low elastic modulus, it is possible to obtain a laminate having a large bonding force between the layers and having good low temperature extension durability. The laminate having such good properties is effectively used as a diaphragm, a bladder, or the like.
【0012】[0012]
【実施例】次に、実施例について本発明を説明する。Next, the present invention will be described by way of examples.
【0013】実施例1 共押出法によって、次の各層よりなる積層体を製造し
た。 エチレン-ビニルアルコール共重合体層 100μm (クラレ製品エバール、引張弾性率5×1010ダイン/cm2) 無水マレイン酸変性ポリプロピレン層 50μm (三井石化製品アドマー、引張弾性率2×1010ダイン/cm2) オレフィン系熱可塑性エラストマー層 300μm (AES JAPAN製品サントプレン、引張弾性率5×109ダイン/cm2)Example 1 A laminate having the following layers was produced by a coextrusion method. Ethylene-vinyl alcohol copolymer layer 100 μm (Kuraray product Eval, tensile modulus 5 × 10 10 dynes / cm 2 ) Maleic anhydride modified polypropylene layer 50 μm (Mitsui Petrochemicals Admer, tensile modulus 2 × 10 10 dynes / cm 2 ) Olefinic thermoplastic elastomer layer 300 μm (AES JAPAN product Santoprene, tensile modulus 5 × 10 9 dynes / cm 2 )
【0014】実施例2 実施例1で得られた積層体のオレフィン系熱可塑性エラ
ストマー層上に前記ブチルゴム配合物の加硫接着物層
(厚さ600μm、引張弾性率3×109ダイン/cm2)を更に形
成させた。Example 2 On the olefinic thermoplastic elastomer layer of the laminate obtained in Example 1, a vulcanized adhesive layer of the above butyl rubber compound was formed.
(Thickness 600 μm, tensile modulus 3 × 10 9 dynes / cm 2 ) was further formed.
【0015】実施例3 実施例1で得られた積層体のオレフィン系熱可塑性エラ
ストマー層上に前記ニトリルゴム配合物の加硫接着物層
(厚さ600μm、引張弾性率3.5×109ダイン/cm2)を更に
形成させた。Example 3 On the olefinic thermoplastic elastomer layer of the laminate obtained in Example 1, a vulcanized adhesive layer of the above-mentioned nitrile rubber compound was applied.
(Thickness 600 μm, tensile modulus 3.5 × 10 9 dynes / cm 2 ) was further formed.
【0016】実施例4 実施例1において、オレフィン系熱可塑性エラストマー
の代わりに、ポリアミド系熱可塑性エラストマー(大日
本インキ製品グリラックスA250、引張弾性率7×109ダイ
ン/cm2)の層が同じ厚さ(300μm)で形成された。Example 4 In Example 1, instead of the olefin thermoplastic elastomer, the same layer of polyamide thermoplastic elastomer (Dainippon Ink Products Grelax A250, tensile modulus 7 × 10 9 dynes / cm 2 ) is the same. It was formed with a thickness (300 μm).
【0017】実施例5 実施例4で得られた積層体のポリアミド系熱可塑性エラ
ストマー層上に前記ブチルゴム配合物の加硫接着物層
(厚さ600μm、引張弾性率3×109ダイン/cm2)を更に形
成させた。Example 5 A vulcanized adhesive layer of the above-mentioned butyl rubber compound was formed on the polyamide thermoplastic elastomer layer of the laminate obtained in Example 4.
(Thickness 600 μm, tensile modulus 3 × 10 9 dynes / cm 2 ) was further formed.
【0018】比較例1 実施例4において、他のポリアミド系熱可塑性エラスト
マー(大日本インキ製品グリラックスA100、引張弾性率2
×1010ダイン/cm2)が用いられ、その層が同じ厚さ(300
μm)で形成された。COMPARATIVE EXAMPLE 1 In Example 4, another polyamide-based thermoplastic elastomer (Dainippon Ink Products Grelax A100, tensile modulus 2
× 10 10 dynes / cm 2 ) is used and the layers have the same thickness (300
μm).
【0019】比較例2 実施例5において、他のポリアミド系熱可塑性エラスト
マー(グリラックスA100、引張弾性率2×1010ダイン/cm
2)が用いられ、その層が同じ厚さ(300μm)で形成され
た。Comparative Example 2 In Example 5, another polyamide-based thermoplastic elastomer (Greak A100, tensile elastic modulus 2 × 10 10 dynes / cm
2 ) was used and the layers were formed with the same thickness (300 μm).
【0020】以上の各実施例および比較例で得られた積
層体について、次の各項目の測定が行われた。 -40℃条件下での伸長耐久試験:ダンベル状に打ち抜い
た測定サンプルを、-40℃の環境条件下で50%伸長(5Hz)
をくり返し、破断する迄の回数を測定 製品耐久試験後のガスバリア性:製品ダイアフラムを-4
0℃の環境条件下に、0.01Hzの速度で、最上点〜最下点
間を100回上下作動させた後、N2ガスについてのガス透
過係数(単位:cc・10μ/m2・24hr・atm)を70℃で測定With respect to the laminates obtained in each of the above Examples and Comparative Examples, the following items were measured. Elongation durability test under -40 ℃ condition: A measurement sample punched out in a dumbbell shape is extended by 50% under -40 ℃ environment condition (5Hz)
Repeat the measurement and measure the number of times until it breaks. Gas barrier property after product durability test: -4 product diaphragm
After operating up and down 100 times between the highest point and the lowest point at a speed of 0.01 Hz under an environmental condition of 0 ° C, the gas permeation coefficient for N 2 gas (unit: cc · 10 μ / m 2 · 24 hr · atm) measured at 70 ° C
【0021】得られた結果は、次の表に示される。 例 -40℃条件下での伸長耐久試験(回) 製品耐久試験後のガスバリア性 実施例1 >1000 7 〃 2 >1000 〃 〃 3 >1000 〃 〃 4 800 〃 〃 5 800 〃 比較例1 <500 >20 〃 2 <500 〃The results obtained are shown in the following table. Example: Extension durability test under -40 ° C condition (times) Gas barrier property after product durability test Example 1> 1000 7 〃 2> 1000 〃 〃 3> 1000 〃 〃 4 800 〃 〃 5 800 〃 Comparative example 1 <500 > 20 〃 2 <500 〃
Claims (2)
2(-40℃)のエチレン-ビニルアルコール共重合体よりな
るガスバリア層の両面に、引張弾性率7×109〜3×1010
ダイン/cm2(-40℃)の接合材料層および引張弾性率3×1
09〜7×109ダイン/cm2(-40℃)の熱可塑性エラストマー
層を順次積層してなる積層体。1. Tensile modulus 3 × 10 10 to 7 × 10 10 dynes / cm
2 (-40 ℃) ethylene-vinyl alcohol copolymer on both sides of the gas barrier layer, tensile elastic modulus 7 × 10 9 ~ 3 × 10 10
Dyne / cm 2 (-40 ℃) bonding material layer and tensile modulus 3 × 1
A laminate formed by sequentially laminating thermoplastic elastomer layers of 0 9 to 7 × 10 9 dynes / cm 2 (-40 ° C.).
ゴムまたはニトリルゴムを加硫接着してなる請求項1記
載の積層体。2. The laminate according to claim 1, further comprising butyl rubber or nitrile rubber vulcanized and adhered onto the thermoplastic elastomer layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16110196A JPH09314763A (en) | 1996-05-31 | 1996-05-31 | Laminate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16110196A JPH09314763A (en) | 1996-05-31 | 1996-05-31 | Laminate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH09314763A true JPH09314763A (en) | 1997-12-09 |
Family
ID=15728631
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP16110196A Pending JPH09314763A (en) | 1996-05-31 | 1996-05-31 | Laminate |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH09314763A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2004052868A (en) * | 2002-07-18 | 2004-02-19 | Nok Corp | Gasket material and seal structure between two members |
| JP2006315492A (en) * | 2005-05-11 | 2006-11-24 | Yokohama Rubber Co Ltd:The | Thermoplastic elastomer laminated element |
-
1996
- 1996-05-31 JP JP16110196A patent/JPH09314763A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2004052868A (en) * | 2002-07-18 | 2004-02-19 | Nok Corp | Gasket material and seal structure between two members |
| JP2006315492A (en) * | 2005-05-11 | 2006-11-24 | Yokohama Rubber Co Ltd:The | Thermoplastic elastomer laminated element |
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