WO2003072350A1 - Film material - Google Patents
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- WO2003072350A1 WO2003072350A1 PCT/JP2003/002072 JP0302072W WO03072350A1 WO 2003072350 A1 WO2003072350 A1 WO 2003072350A1 JP 0302072 W JP0302072 W JP 0302072W WO 03072350 A1 WO03072350 A1 WO 03072350A1
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- Prior art keywords
- copolymer
- yarns
- film material
- yarn
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/08—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer the fibres or filaments of a layer being of different substances, e.g. conjugate fibres, mixture of different fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
Definitions
- the present invention relates to a membrane material, and more specifically, can be suitably used as a material for a hull of a soft flying ship used for earth observation, meteorological observation, radio wave relay, and the like, which is retained in the stratosphere. It is related to membrane materials. Background art
- Japanese Patent Application Laid-Open No. 2001-239605 discloses a sheet formed by laminating a woven fabric and a film.
- the fineness of the yarn constituting the woven fabric is 10 to 250 dte X, the strength is 10 cN / dtex or more, the elastic modulus is 350 cN / dtex or more, and the fabric weight is 10 to 200. g / m 2 , and that the finolem is a film made of an ethylene-vinylinoleanol copolymer having a thickness of 10 to 40 ⁇ m.
- JP-A-2001-2777391 discloses that, in a sheet formed by laminating a woven fabric and a film, the yarn constituting the woven fabric comprises a melt anisotropic aromatic polyester as a core component.
- Polyphenylene Sulfur It is disclosed that it is a core-sheath type composite fiber having an iod as a sheath component.
- Japanese Patent Application Laid-Open Publication No. 2001-3344594 discloses that in a sheet in which a woven fabric and a film are laminated, the yarn constituting the woven fabric is formed of polybenzoxazole and / or polybenzoxane. It is composed of a fiber mainly composed of thiazole, the fineness of the yarn is 10 to 300 d t'ex, and the strength is
- the elastic modulus is not less than 200 cNZ dtex and the elastic modulus is not less than 700 cN / dtex.
- the above-mentioned known membrane material was unsuitable as an airship membrane material used in the stratosphere in the following points. That is, the outermost film of the film material does not have sufficient light resistance, so that deterioration due to light occurs, and the film cannot be used for a long period of time.
- the base fabric of the film material is a woven fabric, its constituent yarns are bent.
- An object of the present invention is to solve the above-mentioned problems of the prior art and to provide a light-weight, high-strength film material having excellent light resistance.
- the present inventor has conducted intensive studies to achieve the above object, and as a result, has used a laminate of a group of sheet-like yarns in which yarns are arranged in the negative direction as a base fabric of the film material.
- a resin layer with excellent gas barrier properties and a light-resistant resin layer that can be used in an atmosphere of minus 80 ° C to 80 ° C while maximizing the strength, on the surface of the laminate It was determined that a desired film material could be obtained.
- a base fabric, a gas barrier layer and a light-resistant resin layer are provided, and the base fabric is composed of a plurality of sheet-like yarn groups in which the yarns are arranged in the negative direction, and
- the film material is characterized in that the sheet-like yarn groups are laminated so that the arrangement direction of the yarns is different from each other, and the intersections of the yarns are bonded and integrated with an adhesive.
- a plurality of sheet-like yarn groups in which the yarns are arranged in the minus direction are laminated as a base fabric of the membrane material so that the arrangement direction of the yarns in each sheet-like yarn group is different from each other. Use the laminated body.
- the yarn it is preferable to use a fiber yarn having a tensile strength of 14 lcN / dtex or more, which is called a so-called high-strength fiber, so that the obtained membrane material has as high a strength as possible. .
- high-strength fiber examples include para-aramid fibers such as polyparaphenylene-terephthalate-noreamide fibers, copolymer fibers of para-aramid and meta-aramid, or aromatic ethers, for example, 3,4- Para-based aramide fibers copolymerized with diaminodivinyl ether, as well as polypropylene raphenylene benzobisoxazole fibers, polyimide fibers, wholly aromatic polyester fibers, polyarylate fibers, and polyetherimids. Fiber, polyetheretherketone fiber, or a mixed fiber thereof.
- para-aramid fibers such as polyparaphenylene-terephthalate-noreamide fibers, copolymer fibers of para-aramid and meta-aramid, or aromatic ethers, for example, 3,4- Para-based aramide fibers copolymerized with diaminodivinyl ether, as well as polypropylene raphenylene benzobisoxazole
- polyparafene nitrene terephthalamide fibers (Dupont, Kepler, Teijin Twaron, Twaron) and para-aramid fibers copolymerized with 3,4 diamino diphenyl ether (Teijin shares) Company "Technola”), or polyparaphenylene benzobisoxazole fiber (manufactured by Toyobo Co., Ltd., "Xylon”) has excellent heat resistance and is particularly preferably exemplified.
- a sheet-like yarn group in which yarns are arranged in one direction is a sheet-like material in which the fiber yarns are arranged in a minus direction and fixed with an adhesive resin sheet or a film or the like.
- the base fabric is formed by laminating a plurality of sheets so that the arrangement direction of the yarns is different from each other.
- the arrangement direction of the yarns in each sheet-like yarn group may be different from each other, and is not particularly limited, but when the number of laminations is two, the yarns may be arranged in any direction of the base fabric.
- the base fabric is preferable to the arrangement direction of the yarn 9 0 ° different, the intersection of the yarns constituting the sheet-like yarn group is bonded and integrated with an adhesive It is necessary.
- the yarns are arranged linearly without adopting a bent structure as in a woven fabric, so that the inherent strength of the yarns can be sufficiently exhibited.
- the gas barrier layer a film or film of polyvinylidene chloride, ethylene-vinyl alcohol copolymer, polyacrylonitrile, polyethylene naphthalate, polyketone, phenoxy resin, or the like can be used.
- ethylene-vinyl alcohol-based copolymer (“Kebare”, “EVAL”), which has a particularly excellent gas shielding performance, in order to confine gas with small molecules such as helium.
- one layer of the gas barrier may be subjected to aluminum vapor deposition for the purpose of further improving gas barrier properties and weather resistance.
- the method for forming the gas barrier layer As the method for forming the gas barrier layer, a conventionally known method can be arbitrarily adopted. Specifically, a method of melt-coating or wet-coating the resin, a method of laminating a film made of the resin, and the like are exemplified.
- membrane materials used for airships and the like need to have extremely high weather resistance because they are used in the stratosphere. That is, in the stratosphere, the sun is constantly exposed to sunlight during the daytime and the outside temperature reaches nearly 80 ° C, while at night the temperature drops and drops to minus 80 ° C. Therefore, the film material of the present invention can withstand such severe conditions for a long period of time, so that the base fabric and one layer of the gas barrier can be used even in an atmosphere of minus 80 ° C to 80 ° C. It is preferably covered with a light-resistant resin layer.
- Examples of light-resistant resins that can be used in an atmosphere of minus 80 ° C to 80 ° C include fluorine-based resins, such as polytetrafluoroethylene, polyvinylidene fluoride, and polyvinylfluoride.
- Tetrafluoroethylene-perfluoroalkyl vinyl ether copolymer Tetrafluoroethylene-perfluoroalkyl vinyl ether copolymer, tetrafluoroethylene-ethylene copolymer, tetrafluoroethylene-hexafluorolobe pyrene copolymer, vinylidene phenolic copolymer Propylene copolymer, vinylidenefluoride dotetratetranoleole-ethylene-hexafluoropropylene copolymer, polycyclo-triphenylene-olethrene ethylene, ethylene-chloro-trifluoroethylene copolymer, etc. are preferred. Is exemplified.
- Examples of other light-resistant resins that can be used in an atmosphere of minus 80 to 80 ° C. include polyethylene polymerized using a meta-mouth catalyst.
- the light-resistant resin layer may cover either one side or both sides of the film material, but the surface exposed to sunlight and in contact with outside air must be coated.
- a conventionally known method can be arbitrarily adopted. Specific examples include a method of performing wet coating using an emulsion solution of the above resin, and a method of laminating a film made of the above resin.
- a yarn composed of the fibers shown in Table 1 and having a fineness of 450 dtex is wound around a yarn support member through a rotating arm, and the yarn is arranged with a density of 20 yarns Z 2.54 cm.
- the fibers also shown in Table 1 A yarn with a fineness of 44 dtex, consisting of fibers, is pulled out from the creel stand, and 20 yarns are arranged from the top and bottom with an arrangement density of 2.54 cm so that the arrangement directions of the yarns are 90 ° different from each other. After stacking them together, they were led to the holding jaws.
- the yarn group was immersed in a tank containing an acrylic ester resin emulsion adhesive to impregnate and adhere the adhesive. It was dried by bringing it into contact with a cylinder heated to C and wound up on a winding roll to obtain a base fabric on which a group of sheet-like yarns was laminated. Table 1 shows the strength utilization rate of the obtained base cloth.
- An ethylene copolymer film (manufactured by Asahi Glass: "Aflex”) was bonded to obtain a film material.
- Table 1 also shows the performance of the obtained film material.
- the strength utilization rate is defined as the theoretical strength, where the tensile strength of the base fabric assuming that the tensile strength of the yarn constituting the obtained base fabric has developed 100% is defined as the theoretical strength. It was expressed as the ratio (%) of the measured tensile strength. If this value is 95% or more, it can be said that it is lightweight and has high strength.
- the light resistance was measured in accordance with JIS 1415, by measuring the tensile strength after the film material was exposed for 2000 hours, and expressed as a ratio (%) of the tensile strength to the tensile strength before the exposure. If this value is 90% or more, it can be said that the film has good light fastness.
- the light-resistant resin can be used in an atmosphere of minus 80 ° C to 80 ° C depends on whether the resin is used in a minus 80 ° C atmosphere and in a 80 ° C atmosphere, respectively. After exposure for 24 hours, the strength was measured immediately after being taken out of the atmosphere and evaluated by the retention from the original strength. If the retention rate is 80% or more, it can be determined that it can be used.
- Example 3 After exposure for 24 hours, the strength was measured immediately after being taken out of the atmosphere and evaluated by the retention from the original strength. If the retention rate is 80% or more, it can be determined that it can be used.
- Example 1 in place of the tetrafluoroethylene-ethylene copolymer film, a polyethylene film having a thickness of 60 ⁇ , which was polymerized using a metallocene catalyst (“Umerit” manufactured by Ube Industries, Ltd.) ) was performed in the same manner as in Example 1 except that) was used.
- a metallocene catalyst (“Umerit” manufactured by Ube Industries, Ltd.)
- Table 1 also shows the performance of the obtained film material.
- Example 2 in place of the tetrafluoroethylene-ethylene copolymer film, a polyethylene film having a thickness of 60 ⁇ and polymerized using a metallocene catalyst (“Umerit J” manufactured by Ube Industries) The procedure was performed in the same manner as in Example 2 except for using.
- a metallocene catalyst (“Umerit J” manufactured by Ube Industries)
- Table 1 also shows the performance of the obtained film material. '' Comparative Examples 1-2
- Example 1 was carried out in the same manner as in Example 1 except that a tetrachloroethylene-ethylene copolymer film was replaced by a 30 ⁇ m-thick polychlorinated vinyl film or a polyurethane film. Table 1 also shows the performance of the obtained film material.
- Example 2 was carried out in the same manner as in Example 2 except that a polychlorinated vinyl film or a polyurethane film having a thickness of 30 ⁇ m was used instead of the tetrafluoroethylene-ethylene copolymer film.
- Table 1 shows the performance of the obtained film material.
- a yarn having a fineness of 450 dteX composed of the fibers shown in Table 1 was arranged in the course, and a base fabric made of a plain weave having a weave density of 20 yarns / 2.54 cm was obtained.
- Table 1 shows the strength utilization rate of the obtained base cloth.
- Table 1 also shows the performance of the obtained film material.
- the film material of the present invention has excellent light resistance, is lightweight and has high strength, and is therefore suitable as a material for the hull of a soft airship used for earth observation, weather observation, radio wave relay, and the like. Can be used.
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Abstract
Description
明 細 書 膜材 技術分野 Description Membrane materials Technical field
本発明は、 膜材に関するものであり、 さらに詳しくは、 成層圏に 滞留させて、 地球観測、 気象観測、 電波中継等に利用される軟式飛 行船の船体の材料などに好適に使用することができる膜材に関する ものである。 背景技術 The present invention relates to a membrane material, and more specifically, can be suitably used as a material for a hull of a soft flying ship used for earth observation, meteorological observation, radio wave relay, and the like, which is retained in the stratosphere. It is related to membrane materials. Background art
近年、 パーソナルコンピューターや携帯電話の普及が急速に進み、 これに伴うネッ トワークの整備の必要性が高まっている。 また、 ォ ゾンホール、 地球温暖化、 海洋汚染等の地球環境問題がクローズ アップされており、 それらを監視するためのシステム構築の必要性 も高まってきている。 In recent years, the spread of personal computers and mobile phones has been rapidly progressing, and the necessity of network maintenance has increased accordingly. In addition, global environmental issues such as ozone holes, global warming and marine pollution have been highlighted, and the need to build a system to monitor them is increasing.
このような状況の中、 成層圏に通信機器、 観測センサー等を搭载 した飛行船を滞空させ、 地球環境の観測、 気象観測、 電話中継等に 利用しょうとす'る研究が進められている。 Under such circumstances, research is being conducted to make airships equipped with communication devices, observation sensors, and the like in the stratosphere afloat and use them for observation of the global environment, meteorological observation, telephone relay, and the like.
そして、 飛行船の船体に使われる膜材として、 例えば、 特開 2 0 0 1 - 2 3 9 6 0 5号公報には、 織物とフィルムとが積層されてな るシートが開示されており、 該織物を構成する糸の繊度が 1 0〜 2 5 0 d t e X、 強度が 1 0 c N / d t e x以上、 弾性率が 3 5 0 c N / d t e x以上で、 織物の目付が 1 0〜 2 0 0 g / m 2であること、 また、 フイノレムが厚さ 1 0〜4 0 μ mのエチレン一ビニノレアノレコー ル系共重合体からなるフィルムであることも記載されている。 As a membrane material used for the hull of an airship, for example, Japanese Patent Application Laid-Open No. 2001-239605 discloses a sheet formed by laminating a woven fabric and a film. The fineness of the yarn constituting the woven fabric is 10 to 250 dte X, the strength is 10 cN / dtex or more, the elastic modulus is 350 cN / dtex or more, and the fabric weight is 10 to 200. g / m 2 , and that the finolem is a film made of an ethylene-vinylinoleanol copolymer having a thickness of 10 to 40 μm.
また、 特開 2 0 0 1 — 2 7 7 3 9 1号公報には、 織物とフィルム とが積層されてなるシートにおいて、 該織物を構成する糸が、 溶融 異方性芳香族ポリエステルを芯成分と し、 ポリフエ二レンサルファ ィ ドを鞘成分とする芯鞘型複合繊維であることが開示されている。 さらに、 特開 2 0 0 1 — 3 3 4 5 9 4号公報には、 織物とフィル ムとが積層されてなるシートにおいて、 該織物を構成する糸がポリ ベンズォキサゾールおよび/またはポリベンズチアゾールを主成分 とする繊維からなり、 該糸の繊度が 1 0〜 3 0 0 d t'e x、 強度がAlso, JP-A-2001-2777391 discloses that, in a sheet formed by laminating a woven fabric and a film, the yarn constituting the woven fabric comprises a melt anisotropic aromatic polyester as a core component. And Polyphenylene Sulfur It is disclosed that it is a core-sheath type composite fiber having an iod as a sheath component. Further, Japanese Patent Application Laid-Open Publication No. 2001-3344594 discloses that in a sheet in which a woven fabric and a film are laminated, the yarn constituting the woven fabric is formed of polybenzoxazole and / or polybenzoxane. It is composed of a fiber mainly composed of thiazole, the fineness of the yarn is 10 to 300 d t'ex, and the strength is
2 0 c NZ d t e x以上、 弾性率が 7 0 0 c N/ d t e x以上であ ることが開示されている。 It is disclosed that the elastic modulus is not less than 200 cNZ dtex and the elastic modulus is not less than 700 cN / dtex.
しかしながら、 上記公知の膜材は、 次のような点で成層圏にて使 用される飛行船用の膜材としては不適当であった。 即ち、 膜材の最 外層のフィルムが充分な耐光性を有していないので光による劣化が 起こり、 長期間使用できない上、 膜材の基布が織物であるので、 そ の構成糸条が屈曲されており、 該糸条が本来持っている強力を完全 に発現させることができないという問題があった。 発明の開示 However, the above-mentioned known membrane material was unsuitable as an airship membrane material used in the stratosphere in the following points. That is, the outermost film of the film material does not have sufficient light resistance, so that deterioration due to light occurs, and the film cannot be used for a long period of time. In addition, since the base fabric of the film material is a woven fabric, its constituent yarns are bent. However, there has been a problem that the inherent strength of the yarn cannot be fully exhibited. Disclosure of the invention
本発明の目的は、 上記従来技術の有する問題点を解消し、 耐光性 に優れ、 且つ軽量で高い強力を有する膜材を提供することにある。 An object of the present invention is to solve the above-mentioned problems of the prior art and to provide a light-weight, high-strength film material having excellent light resistance.
、本発明者は上記目的を達成するために鋭意検討した結果、 膜材の 基布と して、 糸条がー方向に配列されたシート状糸条群の積層体を 使用し、 糸条の強力を最大限に発現させると共に、 ガスパリヤー性 に優れた樹脂層と、 マイナス 8 0 °Cから 8 0 °Cの雰囲気下で使用可 能な耐光性樹脂層とを積層体の表面に形成させるとき、 所望の膜材 が得られることを究明した。 The present inventor has conducted intensive studies to achieve the above object, and as a result, has used a laminate of a group of sheet-like yarns in which yarns are arranged in the negative direction as a base fabric of the film material. When forming a resin layer with excellent gas barrier properties and a light-resistant resin layer that can be used in an atmosphere of minus 80 ° C to 80 ° C while maximizing the strength, on the surface of the laminate It was determined that a desired film material could be obtained.
即ち、 本発明によれば、 基布、 ガスバリ ヤ一層及ぴ耐光性樹脂層か らなり、 該基布が、 糸条がー方向に配列された複数のシート状糸条 群から構成され、 且つ各シート状糸条群が糸条の配列方向を互いに 異にする様に積層されていると共に、 各糸条の交点が接着剤にて接 着一体化されていることを特徴とする膜材が提供される。 ― That is, according to the present invention, a base fabric, a gas barrier layer and a light-resistant resin layer are provided, and the base fabric is composed of a plurality of sheet-like yarn groups in which the yarns are arranged in the negative direction, and The film material is characterized in that the sheet-like yarn groups are laminated so that the arrangement direction of the yarns is different from each other, and the intersections of the yarns are bonded and integrated with an adhesive. Provided. ―
3 発明を実施するための最良の形態 3 BEST MODE FOR CARRYING OUT THE INVENTION
本発明においては、 膜材の基布と して、 糸条がー方向に配列され た複数のシート状糸条群を、 各シート状糸条群の糸条の配列方向が 互いに異なる様に積層した積層体を使用する。 In the present invention, a plurality of sheet-like yarn groups in which the yarns are arranged in the minus direction are laminated as a base fabric of the membrane material so that the arrangement direction of the yarns in each sheet-like yarn group is different from each other. Use the laminated body.
ここで、 糸条としては、 得られる膜材ができるだけ高い強力を有 する様、 いわゆる高強力繊維と呼ばれる、 1 4 . l c N / d t e x 以上の引張強度を有する繊維糸条を使用することが好ましい。 Here, as the yarn, it is preferable to use a fiber yarn having a tensile strength of 14 lcN / dtex or more, which is called a so-called high-strength fiber, so that the obtained membrane material has as high a strength as possible. .
上記高強力繊維の具体例としては、 ポリパラフエ-レンテレフタ ノレアミ ド繊維などのパラ系ァラミ ド繊維、 パラ系ァラミ ドとメタ系 ァラミ ドとの共重合体繊維、 または芳香族エーテル、 例えば 3 , 4 ージァミノジブヱニルエーテルを共重合したパラ系ァラミ ド繊維、 さらにポリ ノくラフェニレンべンゾビスォキサゾール繊維、 ポリイミ ド繊維、 全芳香族ポリ エステル繊維、 ポリアリ レート繊維、 ポリ エーテルイ ミ ド繊維、 ポリエーテルエーテルケトン繊維、 又はこれ らの混合繊維などが例示される。 Specific examples of the above-mentioned high-strength fiber include para-aramid fibers such as polyparaphenylene-terephthalate-noreamide fibers, copolymer fibers of para-aramid and meta-aramid, or aromatic ethers, for example, 3,4- Para-based aramide fibers copolymerized with diaminodivinyl ether, as well as polypropylene raphenylene benzobisoxazole fibers, polyimide fibers, wholly aromatic polyester fibers, polyarylate fibers, and polyetherimids. Fiber, polyetheretherketone fiber, or a mixed fiber thereof.
この う ち、 ポリ パラフエ二レンテレフタルアミ ド繊維 (デュポン 社製、 「ケプラー」 、 帝人トワロン社製、 「トワロン」 ) や 3, 4 ージァミノ ジフエニルエーテルを共重合したパラ系ァラミ ド繊維 (帝人株式会社製、 「テクノーラ」 ) 、 或いはポリパラフ 二レン ベンゾビスォキサゾール繊維 (東洋紡績株式会社製、 「ザイ ロ ン」 ) などは、 耐熱性に優れており、 特に好ましく例示される。 Of these, polyparafene nitrene terephthalamide fibers (Dupont, Kepler, Teijin Twaron, Twaron) and para-aramid fibers copolymerized with 3,4 diamino diphenyl ether (Teijin shares) Company "Technola"), or polyparaphenylene benzobisoxazole fiber (manufactured by Toyobo Co., Ltd., "Xylon") has excellent heat resistance and is particularly preferably exemplified.
また、 糸条が一方向に配列されたシート状糸条群とは、 上記繊維 糸条がー方向に配列された状態で、 接着剤ゃ榭脂シート或いはフィ ルム等により固定されたシート状物を言い、 本発明における基布は、 鎵シート状物が糸条の配列方向を互いに異にする様に複数層積層さ れることにより形成されている。 In addition, a sheet-like yarn group in which yarns are arranged in one direction is a sheet-like material in which the fiber yarns are arranged in a minus direction and fixed with an adhesive resin sheet or a film or the like. In the present invention, the base fabric is formed by laminating a plurality of sheets so that the arrangement direction of the yarns is different from each other.
ここで、 各シート状糸条群における糸条の配列方向は、 互いに異 なっていれば良く、 特に限定されるものではないが、 積層枚数が 2 枚の場合は、 基布の任意の方向にバランス良く強力を発現させると いう観点から、 糸条の配列方向を 9 0 ° 異ならせることが好ましい c 上記基布においては、 シー ト状糸条群を構成する各糸条の交点が 接着剤にて接着一体化されていることが必要である。 このよ うな構 成を採用することにより、 各糸条が織物中のよ うな折れ曲がり構造 を採らずに直線状に配列されるので、 糸条が本来有する強力を充分 に発現させることができる。 Here, the arrangement direction of the yarns in each sheet-like yarn group may be different from each other, and is not particularly limited, but when the number of laminations is two, the yarns may be arranged in any direction of the base fabric. When you express strength in a well-balanced manner From the perspective of, in c the base fabric is preferable to the arrangement direction of the yarn 9 0 ° different, the intersection of the yarns constituting the sheet-like yarn group is bonded and integrated with an adhesive It is necessary. By adopting such a configuration, the yarns are arranged linearly without adopting a bent structure as in a woven fabric, so that the inherent strength of the yarns can be sufficiently exhibited.
本発明においては、 上記基布上にガスパリヤー層を形成させるこ とが必要である。 これは、 飛行船の膜材と して用いられた場合、 そ の内部に注入されるヘリ ゥムガスなどを封じ込めるためである。 In the present invention, it is necessary to form a gas barrier layer on the base cloth. This is because when used as a membrane material for airships, it is to contain the helium gas that is injected into the interior.
ガスパリ ヤー層と しては、 ポリ塩化ビニリデン、 エチレン一ビニ ルアルコール系共重合体、 ポリ アク リ ロニ ト リル、 ポリ エチレンナ フタレー ト、 ポリケ トン、 フエノキシ榭脂などの皮膜、 フィルムを 用いることができるが、 ヘリ ゥムのよ うな分子の小さな気体を封じ 込めるには、 そのガス遮蔽性能が特に優れたエチレン一ビニルアル コール系共重合体 (クラ レ株式会社製、 「ェバール」 ) を用いるの がよい。 また、 上記ガスバリヤ一層には、 さらにガスパリヤー性、 耐候性を向上させる目的で、 アルミ蒸着を施しても良い。 As the gas barrier layer, a film or film of polyvinylidene chloride, ethylene-vinyl alcohol copolymer, polyacrylonitrile, polyethylene naphthalate, polyketone, phenoxy resin, or the like can be used. However, it is better to use ethylene-vinyl alcohol-based copolymer (“Kebare”, “EVAL”), which has a particularly excellent gas shielding performance, in order to confine gas with small molecules such as helium. . Further, one layer of the gas barrier may be subjected to aluminum vapor deposition for the purpose of further improving gas barrier properties and weather resistance.
'上記ガスパリヤー層の形成方法と しては従来公知の方法が任意に 採用できる。 具体的には、 上記樹脂を溶融コーティング或いは湿式 コーティングする方法、 上記樹脂からなるフィルムをラミネートす る方法などが例示される。 As the method for forming the gas barrier layer, a conventionally known method can be arbitrarily adopted. Specifically, a method of melt-coating or wet-coating the resin, a method of laminating a film made of the resin, and the like are exemplified.
さらに、 飛行船用途などに使用される膜材は、 成層圏で使用され るため、 極めて高い耐候性を有している必要がある。 つま り、 成層 圏では昼間は常に太陽光を浴び、 外気温が 8 0 °C近く に達する一方、 夜になると気温は下がり、 マイナス 8 0 °Cにも低下するからである。 従って、 本発明の膜材は、 このよ うな過酷な条件に長期間耐えう るため、 基布及びガスバ リ ヤ一層がさ らにマイナス 8 0 °Cから 8 0 °cの雰囲気下でも使用可能な耐光性樹脂層で被覆されていること が好ましい。 マイナス 8 0 °Cから 8 0 °Cの雰囲気下で使用可能な耐光性樹脂と しては、 例えばフッ素系の樹脂があり、 ポリテ トラフルォロェチレ ン、 ポリ ビニリデンフルオライ ド、 ポリ ビニルフルオライ ド、 テ ト ラフルォロェチレン一パーフルォロアルキルビニルエーテル共重合 体、 テ トラフルォロエチレン一エチレン共重合体、 テ トラフルォロ エチレン一へキサフルォロブ口ピレン共重合体、 ビニリデンフノレオ ライ ドーへキサフルォロプロピレン共重合体、 ビニリデンフルオラ ィ ドーテトラフノレオ口エチレン一へキサフルォロプロピレン共重合 体、 ポリ ク ロ口 ト リ フノレオ口エチレン、 エチレン一クロロ トリ フノレ ォロエチレン共重合体などが好ましく例示される。 Furthermore, membrane materials used for airships and the like need to have extremely high weather resistance because they are used in the stratosphere. That is, in the stratosphere, the sun is constantly exposed to sunlight during the daytime and the outside temperature reaches nearly 80 ° C, while at night the temperature drops and drops to minus 80 ° C. Therefore, the film material of the present invention can withstand such severe conditions for a long period of time, so that the base fabric and one layer of the gas barrier can be used even in an atmosphere of minus 80 ° C to 80 ° C. It is preferably covered with a light-resistant resin layer. Examples of light-resistant resins that can be used in an atmosphere of minus 80 ° C to 80 ° C include fluorine-based resins, such as polytetrafluoroethylene, polyvinylidene fluoride, and polyvinylfluoride. , Tetrafluoroethylene-perfluoroalkyl vinyl ether copolymer, tetrafluoroethylene-ethylene copolymer, tetrafluoroethylene-hexafluorolobe pyrene copolymer, vinylidene phenolic copolymer Propylene copolymer, vinylidenefluoride dotetratetranoleole-ethylene-hexafluoropropylene copolymer, polycyclo-triphenylene-olethrene ethylene, ethylene-chloro-trifluoroethylene copolymer, etc. are preferred. Is exemplified.
また、 マイナス 8 0 から 8 0 °Cの雰囲気下で使用可能な他の耐 光性樹脂の例として、 メタ口セン触媒を用いて重合されたポリェチ レンなどを挙げることもできる。 Examples of other light-resistant resins that can be used in an atmosphere of minus 80 to 80 ° C. include polyethylene polymerized using a meta-mouth catalyst.
これらの樹脂は単独で使用するか、 或いは複数種のものを組み合 わせ、 多層にして使用してもよい。 また耐光性樹脂層は膜材の片面 あるいは両面の何れを被覆してもよいが、 太陽光が当たり、 外気に 接する面は必ず被覆されている必要がある。 These resins may be used alone or in combination of two or more, and may be used as a multilayer. The light-resistant resin layer may cover either one side or both sides of the film material, but the surface exposed to sunlight and in contact with outside air must be coated.
上記耐光性樹脂層の形成方法としては従来公知の方法が任意に採 用できる。 具体的には、 上記樹脂のェマルジヨ ン溶液を用いて湿式 コーティングする方法、 上記樹脂からなるフィルムをラミネートす る方法などが例示される。 実施例 As a method for forming the light-resistant resin layer, a conventionally known method can be arbitrarily adopted. Specific examples include a method of performing wet coating using an emulsion solution of the above resin, and a method of laminating a film made of the above resin. Example
以下、 実施例により本発明を具体的に説明するが、 本発明はこれらに よって限定されるものではない。 Hereinafter, the present invention will be described specifically with reference to examples, but the present invention is not limited thereto.
実施例 1〜 2 Examples 1-2
表 1 に示す繊維からなる、 繊度 4 4 0 d t e xの糸条を、 回転 アームを通して糸条支持部材に卷きつけることにより、 糸条を 2 0 本 Z 2 . 5 4 c mの密度で配列した糸条群に、 同じく表 1に示す繊 維からなる、 繊度 4 4 0 d t e xの糸条をク リールスタンドから引 き出して、 糸条の配列方向が互いに 9 0 ° 異なる様に 2 0本 Z 2 . 5 4 c mの配列密度で上下から挟むよ うに重ね合わせた後、 押え 口ールに導いた。 A yarn composed of the fibers shown in Table 1 and having a fineness of 450 dtex is wound around a yarn support member through a rotating arm, and the yarn is arranged with a density of 20 yarns Z 2.54 cm. In the group, the fibers also shown in Table 1 A yarn with a fineness of 44 dtex, consisting of fibers, is pulled out from the creel stand, and 20 yarns are arranged from the top and bottom with an arrangement density of 2.54 cm so that the arrangement directions of the yarns are 90 ° different from each other. After stacking them together, they were led to the holding jaws.
そして、 上記 3層の糸条群を、 押えロールに接触させたまま、 ァ ク リル酸エステル系樹脂エマルジョン接着剤の入った槽に浸漬して 接着剤を含浸付着させた後、 1 3 0 °Cに加熱したシリンダ一に接触 させて乾燥し、 卷取り ロールに卷取って、 シート状糸条群が積層さ れた基布を得た。 得られた基布の強力利用率を表 1に示す。 Then, while keeping the three-layered yarn group in contact with the presser roll, the yarn group was immersed in a tank containing an acrylic ester resin emulsion adhesive to impregnate and adhere the adhesive. It was dried by bringing it into contact with a cylinder heated to C and wound up on a winding roll to obtain a base fabric on which a group of sheet-like yarns was laminated. Table 1 shows the strength utilization rate of the obtained base cloth.
上記基布に、 エチレン一 ビニルアルコール系共重合体フィルム (厚さ 1 2 μ m、 クラレ製 : 「ェバール」 ) を貼り合わせ、 さらに その両面に「厚さ 3 0 ΠΙのテ トラフルォロエチレン一エチレン共 重合体フィルム (旭硝子製 : 「ァフレックス」 ) を貼り合わせて膜 材を得た。 An ethylene-vinyl alcohol copolymer film (12 μm thick, made by Kuraray: “Eval”) is adhered to the above base cloth, and a 30-mm-thick tetrafluoroethylene copolymer film is attached on both sides. An ethylene copolymer film (manufactured by Asahi Glass: "Aflex") was bonded to obtain a film material.
得られた膜材の性能を併せて表 1に示す。 Table 1 also shows the performance of the obtained film material.
表 1において、 強力利用率は、 得られた基布を構成する糸条の引張 強度が 1 0 0 %発現したと仮定した場合の基布の引張強度を理論強 度と し、 該理論強度に対する実測引張強度の比率 (%) で表した。 この値が 9 5 %以上であれば、 軽量で高い強力を有していると言え る。 In Table 1, the strength utilization rate is defined as the theoretical strength, where the tensile strength of the base fabric assuming that the tensile strength of the yarn constituting the obtained base fabric has developed 100% is defined as the theoretical strength. It was expressed as the ratio (%) of the measured tensile strength. If this value is 95% or more, it can be said that it is lightweight and has high strength.
また、 耐光性は、 J I S A 1 4 1 5に準拠し、 膜材を 2 0 0 0時間曝露した後の引張強度を測定し、 曝露前の引張強度に対する 引張強度の比率 (%) で表しだ。 この値が 9 0 %以上であれば、 良 好な耐光性を有していると言える。 In addition, the light resistance was measured in accordance with JIS 1415, by measuring the tensile strength after the film material was exposed for 2000 hours, and expressed as a ratio (%) of the tensile strength to the tensile strength before the exposure. If this value is 90% or more, it can be said that the film has good light fastness.
さらに、 耐光性榭脂がマイナス 8 0 °Cから 8 0 °Cの雰囲気下で使 用可能か否かは、 マイナス 8 0 °C雰囲気下及び 8 0 °C雰囲気下にそ れぞれ樹脂を 2 4時間曝した後、 その雰囲気下から取り出してすぐ に強度を測定し、 もとの強度からの保持率で評価した。 該保持率が 8 0 %以上の場合、 使用可能と判断できる。 実施例 3 Furthermore, whether or not the light-resistant resin can be used in an atmosphere of minus 80 ° C to 80 ° C depends on whether the resin is used in a minus 80 ° C atmosphere and in a 80 ° C atmosphere, respectively. After exposure for 24 hours, the strength was measured immediately after being taken out of the atmosphere and evaluated by the retention from the original strength. If the retention rate is 80% or more, it can be determined that it can be used. Example 3
実施例 1 において、 テ トラフルォロエチレンーェチレン共重合体 フィルムに代えて、 厚さ 6 0 μ πιの、 メタロセン触媒を用いて重合 されたポリエチレンフィルム (宇部興産製「ュメ リ ッ ト」) を使用し た以外は実施例 1 と同様に実施した。 In Example 1, in place of the tetrafluoroethylene-ethylene copolymer film, a polyethylene film having a thickness of 60 μπι, which was polymerized using a metallocene catalyst (“Umerit” manufactured by Ube Industries, Ltd.) ) Was performed in the same manner as in Example 1 except that) was used.
得られた膜材の性能を併せて表 1に示す。 Table 1 also shows the performance of the obtained film material.
実施例 4 Example 4
実施例 2において、 テ トラフルォロエチレン一エチレン共重合体 フィルムに代えて、 厚さ 6 0 μ ιταの、 メタロセン触媒を用いて重合 されたポリエチレンフィルム (宇部興産製「ュメ リ ッ ト J ) を使用し た以外は実施例 2と同様に実施した。 ' In Example 2, in place of the tetrafluoroethylene-ethylene copolymer film, a polyethylene film having a thickness of 60 μιτα and polymerized using a metallocene catalyst (“Umerit J” manufactured by Ube Industries) The procedure was performed in the same manner as in Example 2 except for using.
得られた膜材の性能を併せて表 1に示す。 ' 比較例 1〜 2 Table 1 also shows the performance of the obtained film material. '' Comparative Examples 1-2
実施例 1 において、 テ トラフルォロエチレン一エチレン共重合体 フィルムに代えて、 厚さ 3 0 μ mのポリ塩化ビュルフィルム又はポ リウレタンフィルムを使用した以外は実施例 1と同様に実施した。 得られた膜材の性能を併せて表 1に示す。 Example 1 was carried out in the same manner as in Example 1 except that a tetrachloroethylene-ethylene copolymer film was replaced by a 30 µm-thick polychlorinated vinyl film or a polyurethane film. Table 1 also shows the performance of the obtained film material.
比較例 4〜 5 Comparative Examples 4 to 5
実施例 2において、 テ トラフルォロエチレン一エチレン共重合体 フィルムに代えて、 厚さ 3 0 μ mのポリ塩化ビュルフィルム又はポ リ ウレタンフィルムを使用した以外は実施例 2と同様に実施した。 Example 2 was carried out in the same manner as in Example 2 except that a polychlorinated vinyl film or a polyurethane film having a thickness of 30 μm was used instead of the tetrafluoroethylene-ethylene copolymer film.
得られた膜材の性能を表 1に示す。 Table 1 shows the performance of the obtained film material.
比較例 3、 比較例 6 Comparative Example 3, Comparative Example 6
表 1 に示す繊維からなる、 繊度 4 4 0 d t e Xの糸条を経緯に配 し、 織密度が 2 0本/ 2 . 5 4 c mの平織物からなる基布を得た。 得られた基布の強力利用率を表 1に示す。 A yarn having a fineness of 450 dteX composed of the fibers shown in Table 1 was arranged in the course, and a base fabric made of a plain weave having a weave density of 20 yarns / 2.54 cm was obtained. Table 1 shows the strength utilization rate of the obtained base cloth.
上記基布に、 エチレン一ビニルアルコール系共重合体フイノレム (厚さ 1 2 μ m、 クラレ製 : Γェバール」 ) を貼り合わせ、 さらに その両面に、 厚さ 3 0 mのテ トラフルォロエチレン一エチレン共 重合体フィルム (旭硝子製 : 「ァフレックス」 ) を貼り合わせて膜 材を得た。 An ethylene-vinyl alcohol copolymer finolem (12 μm thick, made by Kuraray Co., Ltd .: Jeval) is attached to the above base cloth, and a 30-m-thick tetrafluoroethylene Ethylene A polymer film (manufactured by Asahi Glass: “Aflex”) was attached to obtain a film material.
得られた膜材の性能を併せて表 1に示す。 Table 1 also shows the performance of the obtained film material.
基布強力利用率 耐候性 強度保持率 (%) 識維 IW尤 1玍樹 Us層 Base cloth strong utilization rate Weather resistance Strength retention rate (%) Knowledge IW like 1 玍 tree Us layer
( % ) - 8 0 °C 8 0 °C 比較例 1 テクノーラ 9 9 ポリ塩化ビュル 8 5 6 0 8 0 比較例 2 テクノーラ 9 9 ポリ ウレタン 8 0 5 0 7 0 実施例 1 テクノーラ 9 9 フッ素系 9 5 8 5 9 5 比較例 3 テクノーラ 8 0 表 9フッ素系 9 6 9 0 9 0 比較例 4 ザィ口ン 9 8 ポリ塩化ビュル 8 0 6 5 8 0 比較例 5 ザィ口ン 9 8 ポリ ウレタン 7 8 4 5 6 5 実施例 2 ザィ口ン 9 8 フッ素系 9 5 9 0 9 0 比較例 6 ザィ口ン 7 5 フッ素系 9 5 9 0 9 5 実施例 3 テクノ一ラ 9 9 ポリエチレン 9 0 9 0 9 0 実施例 4 ザィ口ン 9 9 ポリエチレン 9 0 9 0 9 0 (%)-80 ° C 80 ° C Comparative Example 1 Technora 9 9 Polychlorinated Bulb 8 5 6 0 8 0 Comparative Example 2 Technora 9 9 Polyurethane 8 0 5 0 7 0 Example 1 Technora 9 9 Fluorine 9 5 8 5 9 5 Comparative Example 3 Technora 8 0 Table 9 Fluorine 9 6 9 0 9 0 Comparative Example 4 Zain 98 8 Polychlorinated Bulk 8 0 6 5 8 0 Comparative Example 5 Zain 9 8 Polyurethane 7 8 4 5 6 5 Example 2 Zine 9 8 Fluorine 9 5 9 0 9 0 Comparative Example 6 Zine 7 5 Fluorine 9 5 9 0 9 5 Example 3 Technora 9 9 Polyethylene 9 Example 9 4 9 9 Polyethylene 9 0 9 0 9 0
産業上の利用可能性 Industrial applicability
本発明の膜材.は、 耐光性に優れ、 且つ軽量で高い強力を有してレ、 るので、 地球観測、 気象観測、 電波中継等に利用される軟式飛行船 の船体などの材料として好適に使用することができる。 The film material of the present invention has excellent light resistance, is lightweight and has high strength, and is therefore suitable as a material for the hull of a soft airship used for earth observation, weather observation, radio wave relay, and the like. Can be used.
Claims
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| JP2002-49562 | 2002-02-26 | ||
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| WO2003072350A1 true WO2003072350A1 (en) | 2003-09-04 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2010020073A1 (en) * | 2008-08-19 | 2010-02-25 | 昶闳科技股份有限公司 | An undilated waterproof and heat insulation geotextile |
| CN104309796A (en) * | 2014-09-25 | 2015-01-28 | 安徽科耀智能科技有限公司 | Unmanned plane with high security structure |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH04235035A (en) * | 1990-07-02 | 1992-08-24 | Mitsui Petrochem Ind Ltd | Membrane materials with excellent gas barrier properties and their uses |
| WO1996010666A1 (en) * | 1994-09-30 | 1996-04-11 | Lockheed Martin Corporation | Flexible material for use in an inflatable structure |
| JP2001239605A (en) * | 2000-02-29 | 2001-09-04 | Kuraray Co Ltd | Laminated sheet |
| JP2001277391A (en) * | 2000-04-04 | 2001-10-09 | Kuraray Co Ltd | Laminated sheet |
| JP2001334594A (en) * | 2000-05-29 | 2001-12-04 | Kuraray Co Ltd | Laminated sheet |
-
2003
- 2003-02-25 WO PCT/JP2003/002072 patent/WO2003072350A1/en not_active Ceased
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH04235035A (en) * | 1990-07-02 | 1992-08-24 | Mitsui Petrochem Ind Ltd | Membrane materials with excellent gas barrier properties and their uses |
| WO1996010666A1 (en) * | 1994-09-30 | 1996-04-11 | Lockheed Martin Corporation | Flexible material for use in an inflatable structure |
| JP2001239605A (en) * | 2000-02-29 | 2001-09-04 | Kuraray Co Ltd | Laminated sheet |
| JP2001277391A (en) * | 2000-04-04 | 2001-10-09 | Kuraray Co Ltd | Laminated sheet |
| JP2001334594A (en) * | 2000-05-29 | 2001-12-04 | Kuraray Co Ltd | Laminated sheet |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2010020073A1 (en) * | 2008-08-19 | 2010-02-25 | 昶闳科技股份有限公司 | An undilated waterproof and heat insulation geotextile |
| CN104309796A (en) * | 2014-09-25 | 2015-01-28 | 安徽科耀智能科技有限公司 | Unmanned plane with high security structure |
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