JP4748383B2 - Impact resistant fiber reinforced plastic and multilayer structure - Google Patents
Impact resistant fiber reinforced plastic and multilayer structure Download PDFInfo
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本発明は、高速の飛来物に対して優れた耐衝撃性を発揮できる耐衝撃性繊維強化プラスチック、及びそれを用いてなる多層構造体に関する。本発明は主として、高速の飛来物に対する耐衝撃性の向上に特に有用である。 The present invention, impact-resistant fiber reinforced plastic which can exhibit excellent impact resistance for the high-speed flying objects, and a multilayer structure using the same. The present invention is particularly useful mainly for improving impact resistance against high-speed flying objects.
従来より、高強度繊維からなる繊維強化プラスチックとして、耐衝撃ヘルメット用途においてガラス繊維層を外層に、有機繊維層を内層とした耐衝撃性繊維強化プラスチックや、異種の高強度繊維からなる層を組み合わせた耐衝撃性繊維強化プラスチックが提案されている（例えば、特許文献１、２）。かかる耐衝撃性繊維強化プラスチックは、通常、製造工程が煩雑になり、また、異素材を複合化するため、使用できる樹脂、接着剤が限定され、層間接着性が悪く、耐衝撃性低下の問題があった。また、同一の高強度繊維からなる繊維強化プラスチックとして、均一な樹脂量のものが提案されている（例えば、特許文献３）。かかる耐衝撃性繊維強化プラスチックは、剛性に優れるが、耐衝撃性に劣る問題があった。 Conventionally, as a fiber reinforced plastic made of high-strength fibers, in impact-resistant helmet applications, a combination of impact-resistant fiber-reinforced plastics with a glass fiber layer as the outer layer and an organic fiber layer as the inner layer, or layers made of different types of high-strength fibers Further, an impact resistant fiber reinforced plastic has been proposed (for example, Patent Documents 1 and 2). Such impact-resistant fiber-reinforced plastics usually have a complicated manufacturing process, and because different materials are combined, the resins and adhesives that can be used are limited, the interlayer adhesion is poor, and the impact resistance is reduced. was there. Moreover, the thing of the uniform resin amount is proposed as a fiber reinforced plastic which consists of the same high strength fiber (for example, patent document 3). Such an impact-resistant fiber-reinforced plastic has excellent rigidity but has a problem of poor impact resistance.
また、繊維強化プラスチックを接着剤を介して、セラミックスまたは金属と積層してなる多層構造体が提案されている（例えば、特許文献４、５）。特許文献４、５に記載の多層構造体には、本発明のような耐衝撃性繊維強化プラスチックの詳細な記載もなく、本発明に係る耐衝撃性繊維強化プラスチックより耐衝撃性が劣るため、耐衝撃性を有する多層構造体に構成する場合、耐衝撃性繊維強化プラスチック部分の厚みを増さざるをえず、多層構造体の重量が増加してしまうので、身体等に装着する場合には、動きにくく、また疲労しやすいといった問題があった。
本発明の課題は、かかる従来技術に鑑み、高速の飛来物に対し優れた耐衝撃性を有し、かつ、軽量であって身体等への装着物を構成する場合にも所望の機能を阻害せずに構成できる耐衝撃性繊維強化プラスチック及び多層構造体を提供することにある。 An object of the present invention, the prior art in view of the has against excellent impact resistance at a high speed of flying objects, and inhibit the desired function even when configuring the mounting of a light weight to the body, etc. It is an object of the present invention to provide an impact-resistant fiber-reinforced plastic and a multilayer structure that can be constructed without using the same.
上記課題を解決するために、本発明に係る耐衝撃性繊維強化プラスチックは、高速の飛来物に対する、高強度繊維を含む耐衝撃性繊維強化プラスチックであって、同種の高強度繊維の織物からなるが、曲げ弾性率の異なる層を２つ以上有し、前記層のうち高曲げ弾性率層での高強度繊維布帛への樹脂付着量が低曲げ弾性率層への付着量よりも高いことを特徴とし、かつ、高速の飛来物の衝突面側に高曲げ弾性率層を積層してなることを特徴とするものからなる。 In order to solve the above-mentioned problems, the impact-resistant fiber-reinforced plastic according to the present invention is an impact-resistant fiber-reinforced plastic containing high-strength fibers for high- speed flying objects, and is made of a woven fabric of the same type of high-strength fibers. However, it has two or more layers having different bending elastic moduli, and the amount of resin attached to the high-strength fiber fabric in the high bending elastic modulus layer among the layers is higher than the amount attached to the low bending elastic modulus layer. It is characterized in that a high bending elastic modulus layer is laminated on the collision surface side of a high-speed flying object .
この耐衝撃性繊維強化プラスチックにおいては、高曲げ弾性率層と低曲げ弾性率層の曲げ弾性率の比が１：０．２〜１：０．８の範囲にあることが好ましい。また、耐衝撃性繊維強化プラスチックの厚みに対して、１つの曲げ弾性率層の厚みの比率が、０．０５〜０．８の範囲にあることが好ましい。 In this impact-resistant fiber reinforced plastic, the ratio of the flexural modulus of the high flexural modulus layer to the low flexural modulus layer is preferably in the range of 1: 0.2 to 1: 0.8. Moreover, it is preferable that the ratio of the thickness of one bending elastic modulus layer with respect to the thickness of an impact-resistant fiber reinforced plastic exists in the range of 0.05-0.8.
また、２層以上の曲げ弾性率の異なる層からなる耐衝撃性繊維強化プラスチックであって、最高曲げ弾性率層から最低曲げ弾性率層にかけて各層の曲げ弾性率が順に小さくなっているのも好ましい態様の一つである。 Moreover, it is also an impact-resistant fiber reinforced plastic composed of two or more layers having different bending elastic moduli, and it is also preferable that the bending elastic moduli of each layer sequentially decrease from the highest bending elastic modulus layer to the lowest bending elastic modulus layer. This is one of the embodiments.
また、高曲げ弾性率層、低曲げ弾性率層、高曲げ弾性率層の弾性率以下で低曲げ弾性率を超える曲げ弾性率を有する層（ａ）の順になっており、耐衝撃性繊維強化プラスチックの厚みに対して、層（ａ）の厚みの比率が０．０５〜０．２の範囲にあるのも、好ましい態様の一つである。 In addition, the high bending elastic modulus layer, the low bending elastic modulus layer, the layer having the bending elastic modulus below the elastic modulus of the high bending elastic modulus layer and exceeding the low bending elastic modulus (a) are in order, and the impact-resistant fiber reinforced It is also a preferred embodiment that the ratio of the thickness of the layer (a) to the thickness of the plastic is in the range of 0.05 to 0.2.
このような耐衝撃性繊維強化プラスチックにおいては、高曲げ弾性率層の高強度繊維のヤング率が低曲げ弾性率層の繊維のヤング率よりも高い構成とすることができる。 In such an impact-resistant fiber reinforced plastic, the Young's modulus of the high-strength fiber of the high bending elastic modulus layer can be higher than the Young's modulus of the fiber of the low bending elastic modulus layer.
本発明に係る多層構造体は、上記のような耐衝撃性繊維強化プラスチックに接着剤を介してセラミックスまたは金属を積層してなることを特徴とするものからなる。この場合、積層されたセラミックスまたは金属の表面側を、高速の飛来物に対する衝突面側とすればよい。 The multilayer structure according to the present invention is formed by laminating ceramics or metal with the above-mentioned impact-resistant fiber reinforced plastic via an adhesive. In this case, the surface of the laminated ceramic or metal, may be the collision surface side against a high-speed flying objects.
上記のような本発明に係る耐衝撃性繊維強化プラスチックは、例えば、防護チョッキ（防弾チョッキや防刃チョッキ等）やヘルメット、車輌、艦船、航空機の付加装甲に用いることができ、さらに防弾板等にも用いることができる。また、上記のような本発明に係る多層構造体も、防護チョッキ（防弾チョッキや防刃チョッキ等）やヘルメット、車輌、艦船、航空機の付加装甲に用いることができ、さらに防弾板等にも用いることができる。 The impact-resistant fiber-reinforced plastic according to the present invention as described above can be used, for example, in protective vests (such as bulletproof vests and blade-proof vests), helmets, vehicles, ships, and additional armor of aircraft, and for bulletproof plates, etc. Can also be used. Moreover, the multilayer structure according to the present invention as described above can also be used in protective vests (such as bulletproof vests and blade-proof vests), helmets, vehicles, ships, and additional armor of aircraft, and also used in bulletproof plates and the like. Can do.
本発明によれば、従来のものに比べ、軽量で、かつ高速の飛来物に対し優れた耐衝撃性を有する耐衝撃性繊維強化プラスチック及び多層構造体を提供できる。したがって、身体等への装着物を構成する場合にも所望の機能を発揮させることが可能になり、かつ、車輌、艦船、航空機の付加装甲に用いるには、極めて優れた耐衝撃性を発揮させることができる。 According to the present invention, it is possible to provide an impact-resistant fiber-reinforced plastic and a multilayer structure that are lighter and have higher impact resistance against high-speed flying objects than conventional ones. Therefore, it is possible to exhibit a desired function even when constituting an attachment to the body, etc., and to exhibit extremely excellent impact resistance when used for additional armor of a vehicle, a ship, or an aircraft. be able to.
以下に、本発明について、望ましい実施の形態とともに詳細に説明する。
本発明に係る耐衝撃性繊維強化プラスチックに用いられる高強度繊維としては、引張強度が１７ｃＮ／ｄｔｅｘ以上のものが好ましく、１７〜４５ｃＮ／ｄｔｅｘｓのものがより好ましく、１９〜４０ｃＮ／ｄｔｅｘのものがさらに好ましい。また、高強度繊維の弾性率としては、３００〜２０００ｃＮ／ｄｔｅｘが好ましく、３５０〜１８００ｃＮ／ｄｔｅｘがさらに好ましい。このような特性を備えた高強度繊維としては、特に限定されるものではなく、例えば、芳香族ポリアミド（アラミド）、芳香族ポリエーテルアミド、全芳香族ポリエステル、超高分子量ポリエチレン、ポリビニルアルコール、ポリパラフェニレンベンゾビスオキサゾール、ポリベンズイミダゾール、ポリイミド、ポリエーテルエーテルケトン、ポリエーテルイミド、ポリフェニレンサルファイド、ノボロイド、ポリピリドビスイミダゾール、ポリアリレート、ポリケトン、ポリテトラフルオロエチレン、ポリオキシメチレン、ポリアクリロニトリル、ポリアミドイミド、ポリエーテルケトンなどからなる繊維、炭素繊維、セラミック繊維、ガラス繊維などが好ましく使用でき、耐衝撃性、生産性、価格などからアラミド繊維、超高分子量ポリエチレン、ポリパラフェニレンベンゾビスオキサゾール、ポリピリドビスイミダゾール、ガラス繊維がさらに好ましく使用できる。また、これら高強度繊維の繊度としては、１００〜７０００ｄｔｅｘであることが好ましく、２００〜３５００ｄｔｅｘの範囲がさらに好ましいが、特に限定されるものではない。
Hereinafter, the present invention will be described in detail together with preferred embodiments.
The high-strength fiber used in the impact-resistant fiber-reinforced plastic according to the present invention preferably has a tensile strength of 17 cN / dtex or more, more preferably 17 to 45 cN / dtex, and 19 to 40 cN / dtex. Further preferred. Moreover, as an elastic modulus of a high strength fiber, 300-2000 cN / dtex is preferable and 350-1800 cN / dtex is further more preferable. The high-strength fiber having such characteristics is not particularly limited. For example, aromatic polyamide (aramid), aromatic polyether amide, wholly aromatic polyester, ultrahigh molecular weight polyethylene, polyvinyl alcohol, poly Paraphenylene benzobisoxazole, polybenzimidazole, polyimide, polyetheretherketone, polyetherimide, polyphenylene sulfide, novoloid, polypyridobisimidazole, polyarylate, polyketone, polytetrafluoroethylene, polyoxymethylene, polyacrylonitrile, polyamide Fibers made of imide, polyetherketone, etc., carbon fibers, ceramic fibers, glass fibers, etc. can be preferably used. Aramid fibers, ultra-high molecular weight poly- Styrene, polyparaphenylenebenzobisoxazole, polypyridobisimidazole, glass fiber is more preferably used. Further, the fineness of these high-strength fibers is preferably 100 to 7000 dtex, more preferably 200 to 3500 dtex, but is not particularly limited.
さらに高強度繊維を用いて高強度繊維布帛を作製し、耐衝撃性繊維強化プラスチックの材料とすることができる。該高強度繊維布帛としては、織物、編物、不織布、フェルト、一方向性シート（ＵＤ〔一方向に引き揃えられたもの〕）、及びＵＤを０°／９０°に積層したもの、３次元構造物などが好ましく使用でき、寸法安定性、強度から織物、ＵＤがさらに好ましく使用できる。該織物には、平織、綾織、朱子織、畝織、斜子織、杉綾、二重織などを用いることができる。かかる繊維及び布帛は、原糸の製造工程や加工工程での生産性あるいは特性改善のために通常使用されている各種添加剤を含んでいてもよい。例えば熱安定剤、酸化防止剤、光安定剤、平滑剤、耐電防止剤、可塑剤、増粘剤、顔料、難燃剤、油剤などを含有、または付着せしめることができる。 Furthermore, a high-strength fiber fabric can be produced using high-strength fibers and used as a material for impact-resistant fiber-reinforced plastic. The high-strength fiber fabric includes woven fabric, knitted fabric, non-woven fabric, felt, unidirectional sheet (UD [aligned in one direction]), and UD laminated at 0 ° / 90 °, three-dimensional structure Goods can be preferably used, and woven fabric and UD can be more preferably used in view of dimensional stability and strength. As the woven fabric, plain weave, twill weave, satin weave, cocoon weave, oblique weave, sugi twill, double weave and the like can be used. Such fibers and fabrics may contain various additives usually used for improving the productivity or properties in the production process and processing process of the raw yarn. For example, a heat stabilizer, an antioxidant, a light stabilizer, a smoothing agent, an antistatic agent, a plasticizer, a thickener, a pigment, a flame retardant, and an oil agent can be contained or adhered.
耐衝撃性繊維強化プラスチックを構成する樹脂（マトリックス樹脂）としては、熱硬化性樹脂や熱可塑性樹脂を用いることができ、特に限定されるものではないが、熱硬化性樹脂としては、例えば、フェノール樹脂、メラミン樹脂、ユリア樹脂、不飽和ポリエステル樹脂、エポキシ樹脂、ポリウレタン樹脂、ジアリルフタレート樹脂、珪素樹脂、ポリイミド樹脂、ビニルエステル樹脂などやその変性樹脂など、熱可塑性樹脂であれば塩化ビニル樹脂、ポリスチレン、ＡＢＳ樹脂、ポリエチレン、ポリプロピレン、フッ素樹脂、ポリアミド樹脂、ポリアセタール樹脂、ポリカーボネート樹脂、ポリエステル、ポリアミドなど、さらには熱可塑性ポリウレタン、ブタジエンゴム、ニトリルゴム、ネオプレン、ポリエステル等の合成ゴム又はエラストマーなどが好ましく使用できるが、特に限定されるものではない。中でも、フェノール樹脂とポリビニルブチラール樹脂を主成分とする樹脂、不飽和ポリエステル樹脂、ビニルエステル樹脂、ポリエチレン、ポリプロピレン等のポリオレフィン系樹脂、ポリエステル樹脂が耐衝撃性、寸法安定性、強度、価格などから好ましく使用できる。かかる熱硬化性樹脂及び熱可塑性樹脂には、工業的にその目的、用途、製造工程や加工工程での生産性あるいは特性改善のため通常使用されている各種添加剤を含んでいてもよい。例えば、変性剤、可塑剤、充填剤、離型剤、着色剤、希釈剤などを含有せしめることができる。 As the resin (matrix resin) constituting the impact-resistant fiber reinforced plastic, a thermosetting resin or a thermoplastic resin can be used, and is not particularly limited, but examples of the thermosetting resin include phenol. Resin, melamine resin, urea resin, unsaturated polyester resin, epoxy resin, polyurethane resin, diallyl phthalate resin, silicon resin, polyimide resin, vinyl ester resin, etc. and its modified resins such as vinyl chloride resin, polystyrene , ABS resin, polyethylene, polypropylene, fluororesin, polyamide resin, polyacetal resin, polycarbonate resin, polyester, polyamide, etc., and also synthetic rubber or elastomer such as thermoplastic polyurethane, butadiene rubber, nitrile rubber, neoprene, polyester, etc. Such mer can be preferably used, but it is not particularly limited. Among them, resins mainly composed of phenolic resins and polyvinyl butyral resins, unsaturated polyester resins, vinyl ester resins, polyolefin resins such as polyethylene and polypropylene, and polyester resins are preferable in terms of impact resistance, dimensional stability, strength, price, etc. Can be used. Such thermosetting resins and thermoplastic resins may contain various additives which are usually used for industrial purposes, applications, productivity in production steps and processing steps, or improvement of properties. For example, a modifier, a plasticizer, a filler, a release agent, a colorant, a diluent, and the like can be included.
高強度繊維布帛強化プラスチックの作製に必要なプリプレグを得る方法は特に限定されるものではないが、熱硬化性樹脂の場合、熱硬化性樹脂を溶剤に溶解してワニスに調整し、該布帛をワニス漕に通しバーコーターやクリアランスロールなどにて余分な樹脂を掻き取る方法や、コーティング、スプレーを用いた塗工が一般的に行われる。一方、熱可塑性樹脂の場合、樹脂エマルジョンや溶融あるいは溶剤に溶解してナイフやグラビアなどにてコーティングする方法や、溶融した樹脂を直接布帛にラミネートする方法が一般的に行われる。 The method for obtaining the prepreg necessary for the production of the high-strength fiber fabric reinforced plastic is not particularly limited. However, in the case of a thermosetting resin, the thermosetting resin is dissolved in a solvent to prepare a varnish, and the fabric is obtained. A method of scraping excess resin with a bar coater or a clearance roll through a varnish basket, coating using a coating or spraying is generally performed. On the other hand, in the case of a thermoplastic resin, a method of coating with a resin emulsion, melting or solvent and coating with a knife or gravure, or a method of laminating a molten resin directly on a fabric is generally performed.
本発明に係る耐衝撃性繊維強化プラスチックは、２つ以上の曲げ弾性率の異なる層を有するものである。その製造方法としては、ヤング率の異なる高強度繊維布帛を２種類以上準備し、樹脂量を同一または変化させたプリプレグを上記方法により製作し、複数枚積層後、加熱加圧する方法や同一のヤング率からなる高強度繊維布帛に樹脂量を変化させたプリプレグを上記方法により製作し、複数枚積層後、加熱加圧する方法がある。また、ヤング率の異なる高強度繊維布帛を２種類以上準備し、重量（厚み）の同一または異なるフィルムとを交互に複数枚積層して、加熱加圧する成形法や同一のヤング率からなる高強度繊維布帛と重量（厚み）の異なるフィルムを交互に複数枚積層して、加熱加圧する成形法、樹脂量の異なる耐衝撃性繊維強化プラスチックを個別に加熱加圧成形後、接着剤を介して貼り合わせる方法などがある。 The impact-resistant fiber-reinforced plastic according to the present invention has two or more layers having different flexural moduli. As a manufacturing method thereof, two or more types of high-strength fiber fabrics having different Young's moduli are prepared, a prepreg having the same or changed resin amount is manufactured by the above method, and a plurality of layers are laminated and heated and pressed, or the same Young There is a method in which a high-strength fiber fabric having a ratio is made by changing the amount of resin by the above method, and a plurality of layers are laminated and heated and pressed. In addition, two or more types of high-strength fiber fabrics with different Young's moduli are prepared, and a plurality of alternately laminated films with the same or different weight (thickness) are heated and pressed. A method of laminating multiple fabrics and films with different weights (thicknesses) alternately, heating and pressing, and impact-resistant fiber-reinforced plastics with different amounts of resin are individually heat-pressed and pasted via an adhesive There are ways to match them.
本発明に係る耐衝撃性繊維強化プラスチックにおいては、同種の高強度繊維からなり、単糸繊度や総繊度の異なる布帛を使用できる。異種の高強度繊維を組み合わせた場合、上記成形時において、収縮差の違いにより寸法安定性に問題が生じる。また、個別成形後、接着剤を介して貼り合わせる方法もあるが、工程が煩雑になるほか接着剤の選定が必要となり、場合によっては満足できる接着性を得られない。また、２つ以上の曲げ弾性率の異なる層は、少なくとも高曲げ弾性率層と低曲げ弾性率層からなり、その曲げ弾性率は、例えばヤング率の異なる高強度繊維布帛の組み合わせや高強度繊維布帛と樹脂の接着性や樹脂付着量に依存する。各層の樹脂付着量は、耐衝撃性繊維強化プラスチックの場合、高強度有機繊維布帛に対し３〜３０ｗｔ％が好ましい。さらに好ましくは５〜２０ｗｔ％である。３ｗｔ％未満であれば、高速の飛来物が衝突した際、剛性が低いため形態保持性が低く、３０ｗｔ％を超えると、繊維の自由度を奪うため耐衝撃性に劣る。さらに、高曲げ弾性率層と低曲げ弾性率層の曲げ弾性率の比が１：０．２〜１：０．８であることが好ましい。低曲げ弾性率層の曲げ弾性率の比が０．２未満であれば高速の飛来物が衝突した際、剛性が低く変形量が大きいため、人体に悪影響を及ぼす可能性がある。逆に０．８を超えると、全体的に剛性の均一な繊維強化プラスチックと性能に大差がなくなり、本発明による曲げ弾性率差を設けたことによる効果が小さくなる。 In the impact-resistant fiber reinforced plastic according to the present invention, fabrics made of the same kind of high-strength fiber and having different single yarn fineness and total fineness can be used. When different types of high-strength fibers are combined, a problem arises in dimensional stability due to the difference in shrinkage during the molding. In addition, there is a method of bonding through an adhesive after individual molding, but the process becomes complicated and the selection of an adhesive is necessary, and in some cases, satisfactory adhesiveness cannot be obtained. Further, the two or more layers having different bending elastic moduli are composed of at least a high bending elastic modulus layer and a low bending elastic modulus layer, and the bending elastic modulus is, for example, a combination of high strength fiber fabrics having different Young's moduli or high strength fibers. It depends on the adhesiveness between the fabric and the resin and the amount of resin adhered. In the case of impact-resistant fiber reinforced plastic, the resin adhesion amount of each layer is preferably 3 to 30 wt% with respect to the high-strength organic fiber fabric. More preferably, it is 5-20 wt%. If it is less than 3 wt%, when high-speed flying objects collide, the rigidity is low and the shape retention is low, and if it exceeds 30 wt%, the freedom of the fibers is lost and the impact resistance is poor. Furthermore, the ratio of the flexural modulus of the high flexural modulus layer to the low flexural modulus layer is preferably 1: 0.2 to 1: 0.8. If the ratio of the flexural modulus of the low flexural modulus layer is less than 0.2, when a high-speed flying object collides, it has a low rigidity and a large amount of deformation, which may adversely affect the human body. On the other hand, if it exceeds 0.8, there is no great difference in performance from the fiber reinforced plastic having uniform rigidity as a whole, and the effect of providing the difference in flexural modulus according to the present invention becomes small.
また、高曲げ弾性率層と低曲げ弾性率層の間で、順に曲げ弾性率が傾斜していることが好ましく、高速の飛来物の衝突面に高曲げ弾性率層が来るのが好ましい。逆になった場合（低曲げ弾性率層が衝突面側）、低曲げ弾性率層の自由度が低くなるため、耐弾性能（高速の飛来物〔例えば、弾丸〕に対する耐衝撃性）を阻害する。１つの曲げ弾性率層の厚みの比率は、耐衝撃性繊維強化プラスチックの厚みに対して、０．０５〜０．８の範囲にあることが好ましい。０．０５未満であれば耐衝撃性繊維強化プラスチックが多層となるため、耐衝撃性は良好であるが作業、工程が煩雑になる。高曲げ弾性率層の厚み比率が０．８を超えると均一な耐衝撃性繊維強化プラスチックと性能に大差がなくなり、低曲げ弾性率層が０．８を超えると剛性が低く変形量が大きくなる。また、人体側に配置する低曲げ弾性率層の変形量が大きい場合には、人体と低曲げ弾性率層との間に、高曲げ弾性率層の弾性率以下で低曲げ弾性率を超える曲げ弾性率を有する層（ａ）を積層することができる。その場合、耐衝撃性を低下しない範囲で変形を低減させる必要があり、耐衝撃性繊維強化プラスチックの厚みに対して、（ａ）の厚みの比率が０．０５〜０．２の範囲内にあることが好ましい。０．０５未満であれば変形を低減できないし、０．２を超えると低曲げ弾性率層の自由度が下がり、耐衝撃性が低下する。 In addition, it is preferable that the bending elastic modulus inclines in order between the high bending elastic modulus layer and the low bending elastic modulus layer, and it is preferable that the high bending elastic modulus layer comes to the collision surface of the high-speed flying object. If it is reversed (low flexural modulus layer is on the impact surface side), the flexibility of the low flexural modulus layer is low, which impedes ballistic performance (impact resistance against high-speed flying objects (for example, bullets)) To do. The thickness ratio of one flexural modulus layer is preferably in the range of 0.05 to 0.8 with respect to the thickness of the impact-resistant fiber reinforced plastic. If it is less than 0.05, the impact-resistant fiber reinforced plastic has a multilayer structure, so that the impact resistance is good, but the work and process become complicated. When the thickness ratio of the high flexural modulus layer exceeds 0.8, there is no significant difference in performance from the uniform impact-resistant fiber reinforced plastic, and when the low flexural modulus layer exceeds 0.8, the rigidity is low and the deformation becomes large. . In addition, when the deformation amount of the low bending elastic modulus layer arranged on the human body side is large, the bending between the human body and the low bending elastic modulus layer is less than the elastic modulus of the high bending elastic modulus layer and exceeds the low bending elastic modulus. A layer (a) having an elastic modulus can be laminated. In that case, it is necessary to reduce deformation within a range where the impact resistance is not lowered, and the ratio of the thickness of (a) is within the range of 0.05 to 0.2 with respect to the thickness of the impact resistant fiber reinforced plastic. Preferably there is. If it is less than 0.05, deformation cannot be reduced, and if it exceeds 0.2, the degree of freedom of the low bending elastic modulus layer is lowered, and impact resistance is lowered.
多層構造体に使用されるセラミックスとしては、ファインセラミックスであれば問題なく使用できる。特性として、例えば圧縮強度１５００ＭＰａ以上、曲げ強度３００ＭＰａ以上、ビッカース強度１０００ｋｇ／ｍｍ2以上のものであれば特に限定されるものではないが、アルミナ類、窒化類、珪石類、ボロン類、マグネシア類などや、これらセラミックスの混合焼成物、セラミックスが金属補強された構成物、セラミックスが繊維補強された構成物、炭素繊維等の耐熱性繊維でセラミックスを強靱化した繊維複合セラミックスやセラミックス粒子、ウィスカ、短繊維、連続長繊維で強化したセラミックス基複合材料（例えば、炭化珪素繊維／炭化珪素マトリックス複合材）などが好ましく使用できる。耐衝撃性、軽量性、強度、価格などからアルミナ類、窒化類、珪石類、ボロン類がさらに好ましく使用できる。アルミナ類であれば、純度が８５％以上であることが好ましい。純度が８５％未満であれば添加物の量の関係から、高速の飛来物衝突時のエネルギー吸収性能が低下する。 As the ceramic used for the multilayer structure, fine ceramics can be used without any problem. The properties are not particularly limited as long as the compressive strength is 1500 MPa or more, the bending strength is 300 MPa or more, and the Vickers strength is 1000 kg / mm 2 or more, but aluminas, nitrides, silicas, borons, magnesias, etc. Also, mixed fired products of these ceramics, ceramic-reinforced components, ceramic-reinforced components, fiber composite ceramics made of toughened ceramics with heat-resistant fibers such as carbon fibers, ceramic particles, whiskers, short A ceramic matrix composite material (for example, silicon carbide fiber / silicon carbide matrix composite material) reinforced with fibers or continuous long fibers can be preferably used. From the viewpoint of impact resistance, lightness, strength, price, etc., aluminas, nitrides, silicas, and borons can be more preferably used. In the case of aluminas, the purity is preferably 85% or more. If the purity is less than 85%, the energy absorption performance at the time of high-speed flying object collision is lowered due to the amount of additive.
また、多層構造体に使用される金属としては、鉄、銅、アルミニウム、マグネシウム、チタン、ニッケル、亜鉛、鉛、すずなどの純金属や、物性を改質するため、２種類以上の金属または炭素などの非金属を溶かし合わせた合金、例えば炭素鋼、高張力鋼、クロム鋼、クロムモリブデン鋼、ニッケルクロム鋼、ニッケルクロムモリブデン鋼、ジューコール鋼、ハッドフィールド鋼、超強靱鋼、ステンレス鋼、鋳鉄、銅合金（真鍮、すず青銅、アルミニウム青銅、ベリリウム銅など）、アルミニウム合金（Ａｌ−Ｃｕ系合金、Ｃｕ合金、Ａｌ−Ｓｉ系合金、Ａｌ−Ｍｇ系合金、ジュラルミンなど）、マグネシウム合金（Ｍｇ−Ａｌ−Ｚｎ合金、Ｍｇ−Ｚｎ−Ｚｒ合金、Ｍｇ−希土類元素合金、Ｍｇ−Ｔｈ系合金、Ｍｇ−Ｍｎ合金、Ｍｇ−Ｔｈ−Ｍｎ合金、Ｍｇ−Ｚｎ−Ｒ．Ｅ．合金など）、チタン合金、ニッケル合金（Ｎｉ−Ｍｎ合金、Ｎｉ−Ｃｕ合金、Ｎｉ−Ｍｏ合金、Ｎｉ−Ｃｒ合金など）、亜鉛合金、鉛合金、すず合金、また、アルミ、チタン、銅などの金属マトリックスを金属やセラミックスの粒子、ウィスカ、短繊維、連続長繊維で強化した金属基複合材料（例えば、ボロン繊維強化アルミ、炭化珪素／チタン）などが好ましく使用できる。軽量性、硬度、耐力、耐衝撃性などからチタン、ステンレス鋼、ジュラルミン、チタン合金がさらに好ましく使用できる。また、かかる金属には製造工程や加工工程での生産性から常識の範囲内で不純物を含んでいてもよい。 In addition, the metal used in the multilayer structure may be pure metal such as iron, copper, aluminum, magnesium, titanium, nickel, zinc, lead, tin, or two or more kinds of metals or carbon to modify physical properties. Non-metal alloys such as carbon steel, high strength steel, chrome steel, chrome molybdenum steel, nickel chrome steel, nickel chrome molybdenum steel, jucoal steel, hadfield steel, super tough steel, stainless steel, cast iron , Copper alloys (brass, tin bronze, aluminum bronze, beryllium copper, etc.), aluminum alloys (Al—Cu alloys, Cu alloys, Al—Si alloys, Al—Mg alloys, duralumin, etc.), magnesium alloys (Mg— Al—Zn alloy, Mg—Zn—Zr alloy, Mg—rare earth element alloy, Mg—Th alloy, Mg—Mn alloy, Mg—Th— n alloy, Mg—Zn—RE alloy, etc.), titanium alloy, nickel alloy (Ni—Mn alloy, Ni—Cu alloy, Ni—Mo alloy, Ni—Cr alloy, etc.), zinc alloy, lead alloy, tin Alloys, and metal matrix composites (for example, boron fiber reinforced aluminum, silicon carbide / titanium) in which a metal matrix such as aluminum, titanium, or copper is reinforced with metal or ceramic particles, whiskers, short fibers, or continuous long fibers. It can be preferably used. Titanium, stainless steel, duralumin, and titanium alloy can be more preferably used because of lightness, hardness, proof stress, impact resistance, and the like. Moreover, the metal may contain impurities within the range of common sense from the productivity in the manufacturing process and processing process.
上記のようなセラミックスまたは金属は、単独、あるいは複数枚の組み合わせでもよく、複数の組み合わせの場合、１種類あるいは２種類以上組み合わせてもよい。形状としては三角形、長方形、正方形、台形、六角形等の多角形であり、複数片を隙間なく配列できる形状が好ましい。厚み方向については、平面板、曲面板に限らず、均一な厚みのものや接合部の耐衝撃性向上のために平面形状における端部の厚みが中央部に対し厚いもの等を採用でき、重量面からは均一厚みのものが好ましい。このような形状のセラミックス片、または金属片を本発明に係る耐衝撃性繊維強化プラスチック上に例えば千鳥状に配置することにより、高速の飛来物に対し優れた耐衝撃性能を有する多層構造体を構成できる。例えば、形状が正方形の場合、その一辺の長さは３〜１０ｃｍの範囲内にあることが好ましく、さらには、４〜７ｃｍの範囲内にあることが好ましい。セラミックス、または金属の厚みは、対象とする高速の飛来物の構造や重量、速度、安全率などにより適宜選択するものとする。例えば、高速の飛来物が３０−０６Ｍ２ＡＰ弾の場合、アルミナセラミックスであれば７〜１３ｍｍの範囲内にあることが好ましく、ＮＡＴＯ Ｍ８０弾の場合、アルミナセラミックスであれば４〜９ｍｍの範囲内にあることが好ましく、ＮＡＴＯ ＳＳ−１０９弾であれば３．０〜７ｍｍの範囲内にあることが好ましい。各飛来物に対し上記厚み未満であれば、十分な耐衝撃性能を付与できない。また、上記厚みを超えると満足できる耐衝撃性能を付与できるものの、多層構造体の重量が増す。 The ceramics or metals as described above may be used alone or in combination of a plurality of pieces, and in the case of a plurality of combinations, one kind or two or more kinds may be combined. The shape is a polygon such as a triangle, a rectangle, a square, a trapezoid, or a hexagon, and a shape that allows a plurality of pieces to be arranged without gaps is preferable. Regarding the thickness direction, not only flat plates and curved plates, but also those with uniform thickness and the thickness of the end in the planar shape that is thicker than the center to improve the impact resistance of the joint, etc., can be used. The thing of uniform thickness is preferable from a surface. A multilayer structure having excellent impact resistance against high-speed flying objects can be obtained by arranging such shaped ceramic pieces or metal pieces on the impact-resistant fiber-reinforced plastic according to the present invention in a staggered manner, for example. Can be configured. For example, when the shape is a square, the length of one side thereof is preferably in the range of 3 to 10 cm, and more preferably in the range of 4 to 7 cm. The thickness of the ceramic or metal is appropriately selected according to the structure, weight, speed, safety factor, etc. of the target high-speed flying object. For example, when the high-speed projectile is a 30-06M2AP bullet, it is preferably in the range of 7 to 13 mm for alumina ceramics, and in the case of NATO M80 bullet, it is within the range of 4 to 9 mm for alumina ceramics. In the case of NATO SS-109, it is preferably within a range of 3.0 to 7 mm. If it is less than the above thickness for each flying object, sufficient impact resistance performance cannot be imparted. Moreover, although the impact resistance performance which can be satisfied when it exceeds the said thickness can be provided, the weight of a multilayered structure increases.
さらに、耐衝撃性繊維強化プラスチックをセラミックス、または金属に固定する方法は、プリプレグ作製に用いられる樹脂や合成ゴム、エポキシ樹脂、ウレタン樹脂等の接着剤で接着し、セラミックスや金属と高強度繊維布帛強化プラスチックの間を密着させる。このようにして得られたセラミックスや金属と耐衝撃性繊維強化プラスチックの積層品（多層構造体）の形状は使用目的に応じ、平板、曲面板等適宜選択できる。 Furthermore, the method for fixing the impact-resistant fiber reinforced plastic to ceramics or metal is to bond the ceramics or metal to a high-strength fiber fabric by bonding with an adhesive such as resin, synthetic rubber, epoxy resin or urethane resin used for prepreg production. Adhere between reinforced plastics. The shape of the laminate (multilayer structure) of ceramics, metal and impact-resistant fiber reinforced plastic obtained as described above can be appropriately selected according to the purpose of use, such as a flat plate or a curved plate.
また、該積層品において、高速飛来物の耐衝撃性をさらに向上させるため、接着剤を介して高強度繊維布帛、または樹脂が付着した高強度繊維布帛をセラミックス、または金属側に１〜２枚積層する方法や一般的な熱可塑性樹脂で被覆する方法などがある。布帛を積層する場合、積層する高強度繊維布帛は同種あるいは異種のものであってもかまわない。また、高強度繊維布帛を積層する場合、耐衝撃性繊維強化プラスチックの変形を抑制しない範囲で高強度繊維布帛を耐衝撃性繊維強化プラスチックの一部に積層できる。これによって、多層構造体周辺部に高速の飛来物が衝突した際、セラミックスや金属と耐衝撃性繊維強化プラスチックの層間剥離を抑制でき耐衝撃性が向上する。該接着剤としてはプリプレグ作製に用いられる樹脂や合成ゴム、エポキシ樹脂、ウレタン樹脂等を用いることができる。セラミックスや金属の表面に高強度繊維布帛を積層しない場合、衝突時のセラミックス片が飛び散るばかりでなく、応力を緩和できないため耐衝撃性に劣ることがある。 Further, in the laminated product, in order to further improve the impact resistance of the high-speed flying object, one or two high-strength fiber fabrics or high-strength fiber fabrics to which a resin is attached via an adhesive are provided on the ceramic or metal side. There are a method of laminating and a method of coating with a general thermoplastic resin. When the fabrics are laminated, the high-strength fiber fabrics to be laminated may be the same type or different types. When a high-strength fiber fabric is laminated, the high-strength fiber fabric can be laminated on a part of the impact-resistant fiber reinforced plastic as long as deformation of the impact-resistant fiber-reinforced plastic is not suppressed. As a result, when a high-speed flying object collides with the periphery of the multilayer structure, delamination of ceramics or metal and the impact-resistant fiber reinforced plastic can be suppressed, and the impact resistance is improved. As the adhesive, resins used for prepreg production, synthetic rubber, epoxy resins, urethane resins, and the like can be used. When a high-strength fiber fabric is not laminated on the surface of ceramics or metal, not only the ceramic pieces at the time of collision are scattered, but also the impact resistance may be inferior because stress cannot be relaxed.
本発明に係る耐衝撃性繊維強化プラスチック及び多層構造体は、どのようなものにも使用でき、特に限定されるものではなく、例えば、防護チョッキ（チョッキ内部の防護材料）やヘルメット及びその装着板、防弾板（防護チョッキへの挿入板）、車輌、艦船、航空機への付加装甲に使用されるのが好ましい。その場合、耐衝撃性繊維強化プラスチックや多層構造体は、製品形状や使用環境にあった状態で常法に従い製造後着用、施工される。例えば、防護チョッキは、外衣を裁断後、該繊維強化プラスチック、または多層構造体とを常法に従い縫製、あるいは防護チョッキに挿入できる部分を作成することにより製造される。ヘルメットは、必要な形状に裁断後、該繊維強化プラスチック、または多層構造体を常法に従い成型加工することにより製造される。また、繊維強化プラスチック製ヘルメットに必要な大きさの多層構造体を付加することもできる。車輌、艦船、航空機用付加装甲は、所定のサイズに該繊維強化プラスチック、または多層構造体を常法に従い成形することにより製造される。さらに、機械加工によるボルト止めや面ファスナーなどにより車輌、艦船、航空機に施工される。 The impact-resistant fiber-reinforced plastic and the multilayer structure according to the present invention can be used for anything, and are not particularly limited. For example, a protective waistcoat (protective material inside the waistcoat), a helmet, and a mounting plate thereof It is preferably used for additional armor to bulletproof plates (insertion plates for protective vests), vehicles, ships and aircraft. In that case, the impact-resistant fiber-reinforced plastic and the multilayer structure are worn and applied after production according to a conventional method in a state suitable for the product shape and use environment. For example, the protective vest is manufactured by cutting the outer garment and then sewing the fiber reinforced plastic or the multilayer structure according to a conventional method, or creating a portion that can be inserted into the protective vest. The helmet is manufactured by cutting the fiber-shaped plastic into a required shape and then molding the fiber-reinforced plastic or multilayer structure according to a conventional method. In addition, a multilayer structure having a size required for the fiber-reinforced plastic helmet can be added. Additional armor for vehicles, ships, and aircraft is manufactured by molding the fiber-reinforced plastic or multilayer structure into a predetermined size according to a conventional method. Furthermore, it is applied to vehicles, ships, and aircraft by bolting and hook-and-loop fasteners by machining.
以上のようにして得られた、耐衝撃性繊維強化プラスチック及び多層構造体は、軽量、かつ優れた耐衝撃性を有するという効果を奏する。 The impact-resistant fiber-reinforced plastic and the multilayer structure obtained as described above have an effect of being lightweight and having excellent impact resistance.
以下、実施例により本発明をさらに詳しく説明する。なお、本発明はこれら実施例に限定されるものではない。また、実施例中の特性については、次の測定法を用いた。 Hereinafter, the present invention will be described in more detail with reference to examples. The present invention is not limited to these examples. Moreover, the following measuring method was used about the characteristic in an Example.
原糸強度、弾性率、織布の目付、織り密度、厚さは、ＪＩＳ Ｌ１０９６による。高強度繊維強化プラスチックの曲げ弾性率は、ＪＩＳ Ｋ７０７４に準拠し、その際の条件として、試験片寸法を長さ６０ｍｍ、幅２０ｍｍ、支点間距離４０ｍｍ、試験速度３ｍｍ／ｍｉｎとする。高強度繊維強化プラスチック及び各曲げ弾性率層の厚みは、ノギスを使用し測定する。また、各曲げ弾性率層の厚み、曲げ弾性率は、各曲げ弾性率層単独で成形し測定した。 The raw yarn strength, elastic modulus, fabric weight, weave density, and thickness are in accordance with JIS L1096. The bending elastic modulus of the high-strength fiber reinforced plastic conforms to JIS K7074, and the test piece dimensions are a length of 60 mm, a width of 20 mm, a distance between fulcrums of 40 mm, and a test speed of 3 mm / min. The thickness of the high strength fiber reinforced plastic and each bending elastic modulus layer is measured using calipers. Moreover, the thickness of each bending elastic modulus layer and the bending elastic modulus were measured by molding each bending elastic modulus layer alone.
実施例１
原糸強度２０ｃＮ／ｄｔｅｘ、弾性率５００ｃＮ／ｄｔｅｘのアラミド繊維（総繊度３３００ｄｔｅｘ）を使用した平織織布（目付：４６０ｇ／ｍ2、織り密度１７本／２．５４ｃｍ、厚さ０．６４ｍｍ）にフェノール樹脂（ポリビニルブーチラール主成分）を含浸、乾燥して樹脂分１５ｗｔ％及び１０ｗｔ％のプリプレグを得た。１５ｗｔ％のプリプレグを７枚、１０ｗｔ％のプリプレグを７枚積層し、１５０℃、５０ｋｇ／ｃｍ2 、３０分加熱加圧成形して耐衝撃性繊維強化プラスチックを得た。曲げ弾性率及び厚みは次の通りである。
・繊維強化プラスチック（１４枚積層）：厚み５．５ｍｍ
・１５ｗｔ％プリプレグ（７枚積層）からの成形品：
曲げ弾性率：１．７３ＧＰａ、厚み：２．８ｍｍ、厚みの比率：０．５１
・１０ｗｔ％プリプレグ（７枚積層）からの成形品：
曲げ弾性率：１．１７ＧＰａ、厚み：２．７ｍｍ、厚みの比率：０．４９
・曲げ弾性率の比 １：０．６８
Example 1
Plain weave fabric (weight per unit: 460 g / m 2 , weaving density 17 / 2.54 cm, thickness 0.64 mm) using aramid fibers (total fineness 3300 dtex) with raw yarn strength 20 cN / dtex and elastic modulus 500 cN / dtex A prepreg having a resin content of 15 wt% and 10 wt% was obtained by impregnation with a phenol resin (polyvinyl butyral main component) and drying. Seven 15 wt% prepregs and seven 10 wt% prepregs were laminated and subjected to heat and pressure molding at 150 ° C. and 50 kg / cm 2 for 30 minutes to obtain an impact resistant fiber reinforced plastic. The flexural modulus and thickness are as follows.
・ Fiber reinforced plastic (14 sheets laminated): Thickness 5.5mm
・ Molded product from 15wt% prepreg (7 layers):
Flexural modulus: 1.73 GPa, thickness: 2.8 mm, thickness ratio: 0.51
・ Molded product from 10wt% prepreg (7 layers):
Flexural modulus: 1.17 GPa, thickness: 2.7 mm, thickness ratio: 0.49
・ Ratio of flexural modulus 1: 0.68
実施例２
実施例１のプリプレグの他に５ｗｔ％のプリプレグを作成し、１５ｗｔ％のプリプレグを５枚、１０ｗｔ％のプリプレグを５枚、５ｗｔ％のプリプレグを４枚順に積層し、実施例１の方法で耐衝撃性繊維強化プラスチックを得た。曲げ弾性率及び厚みは次の通りである。
・繊維強化プラスチック（１４枚積層）：厚み５．５ｍｍ
・１５ｗｔ％プリプレグ（５枚積層）からの成形品：
曲げ弾性率：１．７３ＧＰａ、厚み：２．０ｍｍ、厚みの比率：０．３６
・１０ｗｔ％プリプレグ（５枚積層）からの成形品：
曲げ弾性率：１．１７ＧＰａ、厚み：１．９ｍｍ、厚みの比率：０．３５
・５ｗｔ％プリプレグ（４枚積層）からの成形品：
曲げ弾性率：０．４５ＧＰａ、厚み：１．６ｍｍ、厚みの比率：０．２９
・曲げ弾性率の比 １：０．２６
Example 2
In addition to the prepreg of Example 1, 5 wt% prepreg was prepared, 5 sheets of 15 wt% prepreg, 5 sheets of 10 wt% prepreg, and 4 sheets of 5 wt% prepreg were laminated in order. An impact fiber reinforced plastic was obtained. The flexural modulus and thickness are as follows.
・ Fiber reinforced plastic (14 sheets laminated): Thickness 5.5mm
-Molded product from 15wt% prepreg (5 sheets laminated):
Flexural modulus: 1.73 GPa, thickness: 2.0 mm, thickness ratio: 0.36
-Molded product from 10 wt% prepreg (5 sheets laminated):
Flexural modulus: 1.17 GPa, thickness: 1.9 mm, thickness ratio: 0.35
・ Molded product from 5 wt% prepreg (4 layers):
Flexural modulus: 0.45 GPa, thickness: 1.6 mm, thickness ratio: 0.29
・ Ratio of flexural modulus 1: 0.26
実施例３
実施例１、２に記載の１５ｗｔ％及び５ｗｔ％のプリプレグを使用し、１５ｗｔ％のプリプレグを６枚、５ｗｔ％のプリプレグを６枚、１５ｗｔ％のプリプレグを２枚順に積層し、実施例１の方法で耐衝撃性繊維強化プラスチックを得た。曲げ弾性率及び厚みは次の通りである。
・繊維強化プラスチック（１４枚積層）：厚み５．５ｍｍ
・１５ｗｔ％プリプレグ（６枚積層）からの成形品：
曲げ弾性率：１．７３ＧＰａ、厚み：２．４ｍｍ、厚みの比率：０．４４
・５ｗｔ％プリプレグ（６枚積層）からの成形品：
曲げ弾性率：０．４５ＧＰａ、厚み：２．３ｍｍ、厚みの比率：０．４２
・１５ｗｔ％プリプレグ（２枚積層）からの成形品：
曲げ弾性率：１．７３ＧＰａ、厚み：０．８ｍｍ、厚みの比率：０．１４
・曲げ弾性率の比：１：０．２６
Example 3
Using 15 wt% and 5 wt% prepregs described in Examples 1 and 2, 6 sheets of 15 wt% prepregs, 6 sheets of 5 wt% prepregs, and 2 sheets of 15 wt% prepregs were laminated in order. The impact-resistant fiber reinforced plastic was obtained by the method. The flexural modulus and thickness are as follows.
・ Fiber reinforced plastic (14 sheets laminated): Thickness 5.5mm
-Molded product from 15 wt% prepreg (6 sheets laminated):
Flexural modulus: 1.73 GPa, thickness: 2.4 mm, thickness ratio: 0.44
・ Molded product from 5wt% prepreg (6 sheets laminated):
Flexural modulus: 0.45 GPa, thickness: 2.3 mm, thickness ratio: 0.42
-Molded product from 15 wt% prepreg (two-layer lamination):
Flexural modulus: 1.73 GPa, thickness: 0.8 mm, thickness ratio: 0.14
-Ratio of flexural modulus: 1: 0.26
実施例４
アルミナセラミックス（純度９２％、比重３．６ｇ／ｃｍ3、重量１８ｋｇ／ｍ2、大きさ１０ｃｍの正方形、厚み５ｍｍ）を実施例１の１５ｃｍ角の高強度繊維強化プラスチックにウレタン系接着剤で固定し多層構造体を得た。
Example 4
Alumina ceramics (purity 92%, specific gravity 3.6 g / cm 3 , weight 18 kg / m 2 , size 10 cm square, thickness 5 mm) were fixed to the 15 cm square high-strength fiber reinforced plastic of Example 1 with urethane adhesive. A multilayer structure was obtained.
比較例１
実施例１の１５ｗｔ％のプリプレグを１４枚積層し、実施例１の条件、方法で耐衝撃性繊維強化プラスチックを得た。
繊維強化プラスチック（１５ｗｔ％１４枚積層）、曲げ弾性率：１．７３ＧＰａ、厚み：５．５ｍｍ
Comparative Example 1
Fourteen 15 wt% prepregs of Example 1 were laminated, and an impact-resistant fiber-reinforced plastic was obtained under the conditions and method of Example 1.
Fiber reinforced plastic (15 wt% 14 sheets laminated), flexural modulus: 1.73 GPa, thickness: 5.5 mm
比較例２
比較例１の高強度繊維強化プラスチックと実施例３のアルミナセラミックスとをウレタン系接着剤で固定し多層構造体を得た。
Comparative Example 2
The high-strength fiber reinforced plastic of Comparative Example 1 and the alumina ceramic of Example 3 were fixed with a urethane-based adhesive to obtain a multilayer structure.
実施例１〜３、比較例１で得た高強度繊維強化プラスチックを、豊和工業（株）製小口径発射装置にて、ＭＩＬ−ＳＴＤ−６６２Ｆに準拠した１．１ｇの高速飛翔体でのＢａｌｌｉｓｔｉｃ Ｌｉｍｉｔ（Ｖ５０）を評価した。また、実施例４や比較例３で得た多層構造体は、住友石炭鉱業（株）製高速飛翔体試験装置「ＨＦＴ−１０１５」にて４．０ｇの高速飛翔体（ＮＡＴＯ ＳＳ−１０９模擬弾）を用い、約９００ｍ／ｓの速度で耐衝撃試験を実施し、高速飛翔体が衝突した際の貫通・不貫通を評価した。結果を表１に示す。実施例１〜４の高強度繊維強化プラスチック及び多層構造体は、高速の飛来物に対し良好な耐衝撃性を示した。 Ballistic in 1.1 g high-speed flying object based on MIL-STD-662F was obtained by using the high-strength fiber reinforced plastic obtained in Examples 1 to 3 and Comparative Example 1 with a small-aperture launcher manufactured by Toyoka Industries Co., Ltd. Limit (V50) was evaluated. In addition, the multilayer structure obtained in Example 4 and Comparative Example 3 is 4.0 g high-speed flying object (NATO SS-109 simulated bullets) using a high-speed flying object test apparatus “HFT-1015” manufactured by Sumitomo Coal Mining Co., Ltd. ), An impact resistance test was performed at a speed of about 900 m / s, and penetration / non-penetration when a high-speed flying object collided was evaluated. The results are shown in Table 1. The high-strength fiber reinforced plastics and multilayer structures of Examples 1 to 4 exhibited good impact resistance against high-speed flying objects.
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| US7674409B1 (en) * | 2006-09-25 | 2010-03-09 | Honeywell International Inc. | Process for making uniform high strength yarns and fibrous sheets |
| US7622405B1 (en) * | 2006-09-26 | 2009-11-24 | Honeywell International Inc. | High performance same fiber composite hybrids by varying resin content only |
| JP4869915B2 (en) * | 2006-12-28 | 2012-02-08 | 京セラケミカル株式会社 | Compound bulletproof board |
| US7964267B1 (en) * | 2007-04-13 | 2011-06-21 | Bae Systems Tensylon H.P.M., Inc. | Ballistic-resistant panel including high modulus ultra high molecular weight polyethylene tape |
| JP5185606B2 (en) * | 2007-12-17 | 2013-04-17 | 株式会社オーラ | Anti-blade material and protective clothing |
| JP5291376B2 (en) * | 2008-04-28 | 2013-09-18 | 京セラケミカル株式会社 | Compound bulletproof board |
| CN102387894A (en) * | 2009-04-13 | 2012-03-21 | 株式会社有恒商会 | Work clamp, wool material for brush, brush, and manufacturing method of work clamp and wool material for brush |
| EP3130457B1 (en) | 2014-04-11 | 2018-05-30 | Nissan Motor Co., Ltd | Shock absorption mechanism and vehicle exterior plate member provided with same |
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