TW201224240A - Fiber reinforcing resin complex material - Google Patents

Fiber reinforcing resin complex material Download PDF

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Publication number
TW201224240A
TW201224240A TW100135137A TW100135137A TW201224240A TW 201224240 A TW201224240 A TW 201224240A TW 100135137 A TW100135137 A TW 100135137A TW 100135137 A TW100135137 A TW 100135137A TW 201224240 A TW201224240 A TW 201224240A
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TW
Taiwan
Prior art keywords
fiber
resin
composite material
reinforced
epoxy
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TW100135137A
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Chinese (zh)
Inventor
Asami Nakai
Misao Mori
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Daicel Chem
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Publication of TW201224240A publication Critical patent/TW201224240A/en

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    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M15/00Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment
    • D06M15/19Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment with synthetic macromolecular compounds
    • D06M15/37Macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds
    • D06M15/55Epoxy resins
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04Reinforcing macromolecular compounds with loose or coherent fibrous material
    • C08J5/06Reinforcing macromolecular compounds with loose or coherent fibrous material using pretreated fibrous materials
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/24Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • C08J5/248Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using pre-treated fibres
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M13/00Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with non-macromolecular organic compounds; Such treatment combined with mechanical treatment
    • D06M13/10Treating fibres, threads, yarns, fabrics or fibrous goods made from such materials, with non-macromolecular organic compounds; Such treatment combined with mechanical treatment with compounds containing oxygen
    • D06M13/11Compounds containing epoxy groups or precursors thereof
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2363/00Characterised by the use of epoxy resins; Derivatives of epoxy resins
    • DTEXTILES; PAPER
    • D06TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06MTREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M2101/00Chemical constitution of the fibres, threads, yarns, fabrics or fibrous goods made from such materials, to be treated
    • D06M2101/40Fibres of carbon
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/29Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
    • Y10T428/2913Rod, strand, filament or fiber
    • Y10T428/2918Rod, strand, filament or fiber including free carbon or carbide or therewith [not as steel]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/29Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
    • Y10T428/2913Rod, strand, filament or fiber
    • Y10T428/2933Coated or with bond, impregnation or core
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/29Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
    • Y10T428/2913Rod, strand, filament or fiber
    • Y10T428/2933Coated or with bond, impregnation or core
    • Y10T428/2964Artificial fiber or filament

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Textile Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Health & Medical Sciences (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Reinforced Plastic Materials (AREA)
  • Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)

Abstract

The fiber with reinforcing resin of the present invention is a fiber that is treated the surface by epoxyated polydiene based resin. Preferably, the aforementioned fiber is a carbon fiber or a glass fiber. The fiber reinforcing resin complex material of the present invention is constituted of the aforementioned fiber with reinforcing resin and matrix resin; preferably, the aforementioned matrix resin is an epoxy based thermosetting resin. According to the fiber with reinforcing resin of the present invention, the absorption energy(elasticity energy) until the most high loading of fiber reinforcing resin complex material and absorption energy(movement energy) after the most high loading of fiber reinforcing resin complex material can be enhanced simultaneously.

Description

201224240 六、發明說明: 【發明所屬之技術領域】 本發明係有關製造纖維強化複合材料時有用的樹脂 強化用纖維、使用該樹脂強化用纖維之纖維強化樹脂複 合材料、及由該纖維強化樹脂複合材料構成的構造物。 【先前技術】 纖維強化樹脂複合材料乃由強化纖維及基質樹脂形 成的複合材料,係於汽車零件、土木建築用品、風力發 電之葉片、運動用&、航空器、船舶、機器人、纜線材 料等領域中廣泛被利用。作為強化纖維,係使用玻璃纖 維、醯胺纖維、碳纖維、硼纖維等。作為基質樹脂則多 使用容易含浸於強化纖維中的熱固性樹脂。作為熱固性 樹脂係使用環氧樹脂、不飽和聚酯樹脂、乙烯酯樹脂、 酚樹脂、馬來醯亞胺樹脂、氰酸酯樹脂等,而其中最常 使用具優良的耐熱性、彈性率、耐化學藥品性 resistance),且硬化收縮小的環氧樹脂。 曰本專利第3 1 36883號公報(專利文獻丨)中以提供一 種对衝擊性優良的碳纖維強化樹脂複合材料為課題而 揭示-種碳纖維強化樹脂複合材料,其特徵為:比重為 1.75以下,拉伸彈性率、拉伸強度為特定値以 氮濃度N/C及表面氧濃度〇/c處於特定範圍,每碳纖维 單位重量含由具有多個環氧基之脂肪族化合物而成的環 氧糸上毁劑(sizing agent)0.01〜5%,並以板端剝離強度為 22kgf/mm2以上的碳纖維強化。前述環氧系上聚劑係使 用環氧基數目為2〜4個且分子量為1〇〇〜2〇〇〇的脂肪族化 201224240 合物。 曰本專利第300352 1號公報(專利文獻2)中 種附著有上漿劑、接著力的變動小、碳纖維與 之接著力得以提升’並可使複合材料之機械特 良好的叙纖維為課題而揭不有一種碳纖維,复 具有雙酚A二縮水甘油醚或多個環氧基之腊肪 構成的上漿劑,該上漿劑的厚度為特定範圍内 漿劑的厚度的最大値與最小値之比係處於特定 [先前技術文獻] [專利文獻] [專利文獻1]日本專利第3 1 36883號公報 [專利文獻2]曰本專利苐3003521號公報 【發明内容】 [發明所欲解決之課題] 惟,前述文獻所述之強化纖維中,附著於 漿劑的分子中的環氧基數目少,且上浆齊丨< 小,因而難以充分提高強化纖維與基質樹脂的 又,以往關於纖維強化樹脂複合材料之耐衝擊 以同時提高,最大荷重以下的吸收能(彈性能)與 荷重的吸收能(進展能)。即,存在所謂欲提高 質樹脂的密接性來提高最大荷重以下的吸收能 最大荷重的吸收能會降低;反之,欲提高大於 的吸收能時’最大荷重以下的吸收能則會降低 悖。 本發明之目的在於提供一種可同時提升纖 以提供一 基質樹脂 性穩定而 附者有由 族化合物 ’且該上 it圍内。 纖維之上 分子量亦 密接性。 性’係難 大於最大 纖維與基 時,大於 最大荷重 的二律相 維強化樹 -4- 201224240 月曰:复口材料之最大荷重以下的吸收能(彈性能)與大於最 :仃重的吸收忐(進展能)的樹脂強化用纖維、使用該樹 月曰強化用纖維之纖維強化樹脂複合材料、及由該纖維強 化樹脂複合材料構成的構造物。 [用以解決課題之手段] 本^明人等為達上述目的而戮力進行研討的結果發 見右使用對表面以環氧化聚二烯系樹脂實施處理的纖 隹:為強化纖維,則可同時提升纖維強化樹脂複合材料 之取大何重以下的吸收能與大於最大荷重的吸收能本 發明即臻完成。 t —即,本發明係提供一種對纖維以環氧化聚二烯系樹 脂實施表面處理而成之樹脂強化用纖維。 前述纖維係以碳纖維或玻璃纖維為佳。 本發明又提供一種由前述樹脂強化用纖維及基質樹 脂構成的纖維強化樹脂複合材料。 前述基質樹脂係以環氧系熱固性樹脂為佳。 本發明進一步提供一種由前述纖維強化樹脂複合材 料構成的構造物。 [發明之效果] 根據本發明樹脂強化用纖維,因纖維表面係經分子 主鏈本身具橡膠彈性且分子内具有多個環氧基的環氧化 聚二烯系樹脂處理,故將其用作纖維強化樹脂複合材料 時,在纖維與基質樹脂之間形成對基質樹脂之接著性(密 接生)極南’且柔軟性特別優良的界面相。因此,纖維強 化樹脂複合材料之最大荷重以下的吸收能(彈性能)及大 201224240 於最大荷重的吸收能(進展能) 她、,站 v辰此)仔以同時提升,即’迄今 難以兼備的動態強度及靜態強 〜速!件以同時改善。由卟, 相對於以往可耐瞬間衝擊者一 , 〇 , # #般具有党衝擊後脆化之缺 點,本發明之纖維強化蔣[Technical Field] The present invention relates to a resin-reinforcing fiber useful for producing a fiber-reinforced composite material, a fiber-reinforced resin composite material using the resin-reinforcing fiber, and a composite of the fiber-reinforced resin. A structure made of materials. [Prior Art] The fiber-reinforced resin composite material is a composite material composed of a reinforcing fiber and a matrix resin, and is used in automobile parts, civil construction products, blades for wind power generation, sports &, aircraft, ships, robots, cable materials, and the like. Widely used in the field. As the reinforcing fiber, glass fiber, guanamine fiber, carbon fiber, boron fiber or the like is used. As the matrix resin, a thermosetting resin which is easily impregnated into the reinforcing fibers is often used. As the thermosetting resin, an epoxy resin, an unsaturated polyester resin, a vinyl ester resin, a phenol resin, a maleimide resin, a cyanate resin, or the like is used, and among them, the most commonly used one has excellent heat resistance, elastic modulus, and resistance. Chemical resistance, and epoxy resin with small shrinkage. In the carbon fiber reinforced resin composite material having excellent impact properties, a carbon fiber reinforced resin composite material is disclosed in the patent document No. 3 1 36883 (Patent Document No.), and the carbon fiber reinforced resin composite material is characterized in that the specific gravity is 1.75 or less. The elastic modulus and the tensile strength are specific enthalpy, and the nitrogen concentration N/C and the surface oxygen concentration 〇/c are in a specific range, and the carbon fiber unit weight includes an epoxy oxime composed of an aliphatic compound having a plurality of epoxy groups. The sizing agent is 0.01 to 5%, and is reinforced with carbon fibers having a sheet end peel strength of 22 kgf/mm2 or more. The above epoxy-based polymerization agent is an aliphaticated 201224240 compound having a number of epoxy groups of 2 to 4 and a molecular weight of 1 Å to 2 Å. In Japanese Patent No. 3003521 (Patent Document 2), a sizing agent is adhered to the sizing agent, and the change in the force is small, and the carbon fiber and the adhesive force are improved, and the mechanical properties of the composite material are excellent. There is no carbon fiber, a sizing agent composed of bisphenol A diglycidyl ether or a plurality of epoxy groups, and the thickness of the sizing agent is the maximum 値 and minimum thickness of the slurry in a specific range. The prior art document [Patent Document] [Patent Document 1] Japanese Patent No. 3 1 36883 [Patent Document 2] Japanese Patent Publication No. 3003521 [Abstract] [Problems to be Solved by the Invention] However, in the reinforced fiber described in the above document, the number of epoxy groups in the molecule attached to the slurry is small, and the sizing is small, and it is difficult to sufficiently increase the reinforcing fiber and the matrix resin. The impact resistance of the resin composite material is simultaneously increased, and the absorption energy (elastic energy) below the maximum load and the absorption energy of the load (progressive energy). That is, there is a so-called enhancement of the adhesion of the resin to increase the absorption energy of the maximum load below the maximum load, and the absorption energy of the maximum load is decreased. On the contrary, when the absorption energy is larger than the maximum load, the absorption energy below the maximum load is lowered. SUMMARY OF THE INVENTION An object of the present invention is to provide a matrix resin which can be simultaneously provided to provide a matrix resin stability and which is attached to the compound. The molecular weight above the fibers is also in close contact. When the sex is more than the maximum fiber and the base, the bipolar phase strengthening tree larger than the maximum load is -4- 201224240. The absorption energy (elastic energy) below the maximum load of the doubled material is greater than the maximum: the absorption of the weight A resin for reinforcing fibers of 忐 (progressive energy), a fiber-reinforced resin composite material using the fiber for reinforcing eucalyptus, and a structure composed of the fiber-reinforced resin composite material. [Means for Solving the Problem] The results of the study of the above-mentioned purpose, such as the use of the epoxidized polydiene resin on the surface: At the same time, the absorption energy below the weight of the fiber-reinforced resin composite material and the absorption energy greater than the maximum load are improved. T—that is, the present invention provides a resin-reinforced fiber obtained by subjecting a fiber to an epoxidized polydiene resin. The aforementioned fibers are preferably carbon fibers or glass fibers. Further, the present invention provides a fiber-reinforced resin composite material comprising the resin reinforcing fiber and a matrix resin. The matrix resin is preferably an epoxy thermosetting resin. The present invention further provides a structure comprising the aforementioned fiber-reinforced resin composite material. [Effects of the Invention] The fiber for fiber reinforcement according to the present invention is used as a fiber because the surface of the fiber is treated by an epoxidized polydiene resin having a rubber core elasticity and a plurality of epoxy groups in the molecule. When the resin composite material is reinforced, an interface phase which is extremely excellent in adhesion to the matrix resin (close contact) and which is particularly excellent in flexibility is formed between the fiber and the matrix resin. Therefore, the absorption energy (elastic energy) below the maximum load of the fiber-reinforced resin composite material and the absorption energy (progressive energy) of the maximum load of 201224240 at the maximum load of the fiber-reinforced resin composite material are simultaneously improved, that is, it is difficult to achieve at the same time. Dynamic strength and static strength ~ speed! To improve at the same time. As a result, compared with the previous ones that can withstand transient impacts, 〇, ##like has the disadvantage of embrittlement after party impact, the fiber strengthening Jiang of the present invention

取芦强化树月曰複合材料具有黏著強度,JL 不僅可耐受強烈衝擊,在#強 '、 , 罕在又強烈衝擊後仍可保持高強度。 【實施方式】 [樹脂強化用纖維] 本發明樹脂強化用纖維為對纖維以環氧化聚二烯系 樹脂實施表面處理而成者。作為纖維,只要是一般使用 於纖維強化樹脂複合材料的纖維則未特別限$,可例舉 如碳纖維、玻璃纖維、醯胺纖維、硼纖維等。此等當中 特佳為碳纖維、玻璃纖維。纖維可以丨種單獨使用或2 種以上組合使用。 作為前述碳纖維,可使用例如聚丙烯腈(pAN)系碳纖 維瀝月糸石反纖維、氣相成長碳纖維等。玻璃纖維則可 使用一般使用於樹脂強化用的玻璃纖維。 作為環氧化聚一烯糸樹脂,可使用例如聚丁二稀、 聚異戊二烯或分子中具有丁二烯構造或異戊二烯構造之 化合物的共聚物之環氧化物。作為分子中具有丁二烯構 造或異戊二烯構造之化合物的共聚物之環氧化物,可例 示真有丁二烯構造之共聚合多烯之環氧化物(例如苯乙 烯/ 丁二烯/苯乙烯共聚物之環氧化物等)、具有異戊二稀 構造之共聚合多烯之環氧化物(例如苯乙烯/異戊二烯/苯 乙烯共聚物之環氧化物等)等。前述聚丁二烯、聚異戊二 烯、分子中具有丁二烯構造或異戊二烯構造之化合物的 201224240 共聚物的末端基團除氫原子外,還可為羥基、 末端基團特佳為氫原子、羥基。作為環氧化聚 脂,此等當中較佳為環氧化聚丁二烯、環氧化 烯、環氧化苯乙烯/丁二烯/苯乙烯共聚物、環 烯/異戊二烯/苯乙烯共聚物,特佳為環氧化聚 環氧化聚二烯系樹脂可以1種單獨使用或2種 使用。 環氧化聚二烯系樹脂可由聚丁二烯、聚異 为子中具有丁二烯構造或異戊二烯構造之化合 物與環氧化劑反應而製得。 在作為原料之聚丁二烯、聚異戊二烯、分 丁一烯構1«_或異戊二烯構造之化合物的共聚物 部位的立體結構可為順-1,4、反-丨,4、反_丨,2、 任一種。又,彼等之比例為任意者。 作為環氧化劑可例舉過氧乙酸、過氧甲 曱酸、三敗過氧乙酸、㉟氧丙酸等有機過氧 化氫、過氧化三級丁基、氰過氧化異丙苯等 化物類等。作為有機過氧酸,為提高標的物 的氧濃度,則以實質上未含水者(例 為〇·8重量%以下)為佳。上述環氧化劑當中 業上以廉價購得且穩定度高之觀點言之’ 酸。 付 進行環氧化之際可使用觸媒。 為環氧化劑時,可使用碳酸鈉等鹼 又使用過氧化氫作為環氧化劑時, 當使用有機 、硫酸等酸另 可使用鎢酸 鼠基等。 一婦系樹 聚異戊二 氧化苯乙 丁二稀。 以上組合 戊二烯、 物的共聚 子中具有 中,雙鍵 順-1,2的 、過氧苯 類、過氧 機氫過氧 環氧乙烷 水分含量 由可於工 為過氧乙 過氧酸作 ,當觸媒。 與氫氧化 201224240 鈉之混合物、或有機酸充當觸媒。更且,使用過氧化三 級丁基等有機氫過氧化物類時,則可使用六羰鉬充當觸 媒。 環氧化反應可於惰性溶劑中進行。作為惰性溶劑可 例舉如己烷、庚烷等脂肪烴;環己烷等脂環烴;苯、甲 笨、二曱苯等芳香烴;醚類;乙酸乙酯等酯類;氯仿、 四氯化碳等齒化烴;此等之混合溶劑等。 環氧化之反應溫度可依環氧化劑的種類來適當選 擇。當使用過氧乙酸作為環氧化劑時,反應溫度為例如 2 0〜8 0 °C。而使用過氧化三級丁基作為環氧化劑時,反應 溫度則為例如2 0 ~ 1 5 0。(3。 環氧化劑對原料(聚丁二烯、聚異戊二烯、分子中具 有丁二烯構造或異戊二烯構造之化合物的共聚物)的添 加莫耳比可依目標環氧化度來適當選擇。相對原料所具 有的雙鍵1莫耳,係以加入環氧化劑.,1〜2莫耳為佳。 生成之環氧化聚二烯系樹脂可由適當方法,例如以 不良溶劑(poor solvent)予以沉澱之方法、將聚合物於攪 拌下置入熱水中並蒸餾去除溶劑之方法、直接去溶劑之 方法等來分離。 遍^氧化聚二稀系樹脂之數量平均分子量例如為 500〜50000’ 較伟发 , 佳為2500〜30000,更佳為3500〜20000。 %氧化聚二、说备& α , 烯系树脂之環氧乙烷的氧濃度例如為 3〜15%,較佳盘 < ,。 又列如构 倘以分子中的環氧基數目較佳為5 個以上。 個更佳為1 0個以上,再更佳為20 201224240 [樹脂強化用纖維 本發明樹脂ί 烯系樹脂實施表 定,可例如為單 (knit)、魅(mat)、 法並未特別限定 烯系樹脂溶液或 系樹脂溶液或分 纖維表面之方法 當溫度予以乾燥 來適當選擇,例: 作為調製環 用之溶劑,可例 醢胺、二曱基乙 或内酯;此等之 擬調製環氧 需求(特別是使月 劑、分散劑等。 活性劑、非離子 之任一種。界面 使用或2種以上 處理時,環氧化 散液。 樹脂強化用 量(附著量)而言 的調製] 凌化用纖維可藉由對纖維以環氧化聚二 面處理來製得。纖維形態並未特別限 纖維、紗、股線(strand)、織物、針織 父織(braid)等任一種形態。表面處理方 ,可使用例如將纖維浸潰於環氧化聚二 分散液中、或對纖維噴灑環氧化聚二烯 散液,以使環氧化聚二烯系樹脂附著於 等。實施浸潰、噴灑等操作之後,以適 去除/谷劑。乾燥溫度可依溶劑種類等 如為35〜3 5 0 °C,較佳為40〜250。(:左右。 氧化聚二烯系樹脂溶液或分散液時所使 舉如水;曱醇、乙醇等醇類;二甲基甲 醯胺等醯胺或内醯胺;丙酮等g同類;酷 混合液等。 化聚一稀系樹脂溶液或分散液時,可視 3水作為溶劑時)使用界面活性劑、乳化 作為界面活性劑’可採用陰離子系界面 系界面活性劑、陽離子系界面活性劑等 活性劑、乳化劑、分散劑等可1種單獨 組合使用。此外,實施前述纖維之表面 ^ 一稀糸樹脂亦可使用經膠囊乳化之分 纖維中,就環氧化聚二烯系樹脂的處理 ’相對纖維1 0 0重量份,例如為〇. 〇 1〜5 201224240 重Ϊ份,較佳為0.1〜4重量份,更佳為〇 3〜3重量份。 量若過於製造纖維強化樹脂複合材料之際,纖維 了,貝树月曰的接著性容易降低,若過多則環氧化聚二烯 系樹脂之硬化物的厚層便占據於纖維與基質樹脂之間, 而有作為複合材料之特性發生變化之虞。 [纖維強化樹脂複合材料] 3月纖維強化樹脂複合材料係由前述樹脂強化用 戴二基貝樹脂構成。基質樹脂可為熱固性樹脂、熱塑 樹知的任一種,而由易於含浸於強化纖維之觀點言 :,佳為熱固性樹脂。作為熱固性樹脂’可使用環氧 J月::不飽和聚醋樹脂、乙烯醋樹脂、酴樹脂、馬來醯 乂女树脂、氰酸S旨樹脂等。就基質樹脂而言,上述樹脂 :小之=耐?性、彈性率、耐化學藥品性優良且硬化收 a 點S之,較佳為環氧系熱固性樹脂。 述%氧系熱固性樹脂並未特別 刖之環氧化合物,較佳為分子内具 二::化 環氧化合物。針、+、户^ 百2個以上裱氧基之 述衣氧化合物可以1種單獨I # 以上組合使用。 性干倜便用或2種 則述分子内具有2個以上環氧美之璟备 特別限定,可# H y &氣基之丨衣氧化合物並未 氧化合物、脂肪故夕_ > 衣軋化口物、雙酚型二環 型環氧樹脂等。、夕疋醇聚縮水甘油醚、聚縮水甘油胺 狀脂肪族骨架及2個以 ㈣定’惟較佳為⑴環 ,只要是分子内具有環 之化合物即可,並未特 環狀脂肪族骨架、含有 -10- 201224240 相鄰之兩碳原子而形成之具有2個以上月旨環環氧基的環 氧化合物。此種脂環族環氧化合物可例舉以下述式(1)表 示之化合物。The reinforced tree sapwood composite has adhesive strength, and JL can not only withstand strong impact, but also maintain high strength after strong and strong impact. [Embodiment] [Resin reinforcing fiber] The resin reinforcing fiber of the present invention is obtained by subjecting a fiber to an epoxidized polydiene resin. The fiber is not particularly limited as long as it is a fiber generally used for the fiber-reinforced resin composite material, and examples thereof include carbon fiber, glass fiber, guanamine fiber, and boron fiber. Among them, carbon fiber and glass fiber are particularly preferred. The fibers may be used singly or in combination of two or more. As the carbon fiber, for example, polyacrylonitrile (pAN)-based carbon fiber montmorillonite anti-fiber, vapor-grown carbon fiber or the like can be used. As the glass fiber, glass fiber generally used for resin reinforcement can be used. As the epoxidized polyalkylene oxime resin, for example, an epoxide of a copolymer of a polybutadiene, a polyisoprene or a compound having a butadiene structure or an isoprene structure in the molecule can be used. As an epoxide of a copolymer having a butadiene structure or an isoprene structure in a molecule, an epoxide of a copolymerized polyene having a butadiene structure (for example, styrene/butadiene/benzene) can be exemplified. An epoxide of an ethylene copolymer or the like, an epoxide of a copolymerized polyene having an isoprene structure (for example, an epoxide of a styrene/isoprene/styrene copolymer, etc.). The terminal group of the 201224240 copolymer of the above polybutadiene, polyisoprene, a compound having a butadiene structure or an isoprene structure in the molecule may have a hydroxyl group and a terminal group in addition to a hydrogen atom. It is a hydrogen atom or a hydroxyl group. As the epoxidized polyester, preferred among these are epoxidized polybutadiene, epoxidized alkene, epoxidized styrene/butadiene/styrene copolymer, cycloolefin/isoprene/styrene copolymer, It is particularly preferable that the epoxidized polyepoxidized polydiene resin may be used singly or in combination of two or more. The epoxidized polydiene resin can be obtained by reacting a compound having a butadiene structure or an isoprene structure in polybutadiene or polyisomer with an epoxidizing agent. The steric structure of the copolymer portion of the compound of polybutadiene, polyisoprene, butadiene-structured or isoprene as a raw material may be cis-1,4, anti-purine, 4, anti-丨, 2, any one. Also, the ratio of them is any. The epoxidizing agent may, for example, be an organic hydrogen peroxide such as peroxyacetic acid, peroxyformic acid, tris-peroxyacetic acid or 35 oxypropionic acid, a tertiary butyl peroxide or a cumene cyanide or the like. As the organic peroxyacid, in order to increase the oxygen concentration of the target, it is preferred that the organic peroxyacid is substantially free of water (for example, 8% by weight or less). Among the above epoxidizing agents, the acid is commercially available at a low cost and has a high degree of stability. Catalyst can be used for epoxidation. When the epoxidizing agent is used, an alkali such as sodium carbonate or hydrogen peroxide can be used as the epoxidizing agent. When an organic acid or an acid such as sulfuric acid is used, a tungstic acid azole group or the like can be used. A gynecological tree polyisobutyl benzene butyl bromide. The above-mentioned combined pentadiene, the copolymer of the copolymer has medium, double-bond-1, 2, peroxybenzene, peroxygen hydroperoxide ethylene oxide moisture content can be used as peroxyethylene peroxygen Acidic, when the catalyst. Mixture with sodium hydroxide 201224240 or organic acid as a catalyst. Further, when an organic hydroperoxide such as a tertiary butyl peroxide is used, molybdenum hexacarbonyl can be used as a catalyst. The epoxidation reaction can be carried out in an inert solvent. The inert solvent may, for example, be an aliphatic hydrocarbon such as hexane or heptane; an alicyclic hydrocarbon such as cyclohexane; an aromatic hydrocarbon such as benzene, methyl benzene or diphenyl; an ether; an ester such as ethyl acetate; chloroform or tetrachloro Toxic hydrocarbons such as carbon; such mixed solvents and the like. The reaction temperature of the epoxidation can be appropriately selected depending on the kind of the epoxidizing agent. When peracetic acid is used as the epoxidizing agent, the reaction temperature is, for example, 20 to 80 °C. When a tertiary butyl peroxide is used as the epoxidizing agent, the reaction temperature is, for example, 20 to 150. (3. The molar ratio of the epoxidizing agent to the raw material (polybutadiene, polyisoprene, copolymer having a butadiene structure or a isoprene structure in the molecule) may be based on the target epoxidation degree. Appropriately selected. Relative to the raw material, the double bond 1 mole is added with an epoxidizing agent, preferably 1 to 2 moles. The epoxidized polydiene resin formed can be formed by a suitable method, for example, a poor solvent. The method of precipitating, separating the polymer into hot water under stirring, distilling off the solvent, directly removing the solvent, etc., and separating the oxidized polydiphenyl resin by a number average molecular weight of, for example, 500 to 50000' More weifa, preferably 2500~30000, more preferably 3500~20000. % Oxidation poly, said & alpha, the oxygen concentration of ethylene oxide of the olefinic resin is, for example, 3 to 15%, preferably disk < Further, if the number of epoxy groups in the molecule is preferably 5 or more, more preferably 10 or more, and even more preferably 20 201224240 [Resin reinforcing fiber, resin of the invention) The implementation table can be, for example, single (knit), charm (mat) The method of not specifically limiting the surface of the olefinic resin solution or the resin solution or the fiber surface is appropriately selected when the temperature is dried, and examples thereof: as a solvent for preparing the ring, a guanamine, a dimercapto or a lactone; Such as the preparation of epoxy requirements (especially for the use of monthly agents, dispersants, etc.. Active agent, non-ionic any. Interface or two or more treatments, epoxidized dispersion. Resin strengthening amount (attachment) Modulation] The fiber for aging can be obtained by treating the fiber with epoxidized polyhedral. The fiber form is not limited to any of fibers, yarns, strands, fabrics, braids, and the like. For the surface treatment, for example, the fibers may be impregnated into the epoxidized polydispersion liquid, or the fibers may be sprayed with an epoxidized polydiene dispersion to adhere the epoxidized polydiene resin to the like. After spraying, etc., it is suitable to remove/treat. The drying temperature may be 35 to 350 ° C, preferably 40 to 250 depending on the type of solvent. (: 左右. Oxidized polydiene resin solution or dispersion Liquid time Such as water; alcohols such as decyl alcohol and ethanol; decylamine or decylamine such as dimethylformamide; g-like such as acetone; cool mixed liquid, etc. When concentrating a rare resin solution or dispersion, it can be regarded as 3 water. In the case of a solvent, a surfactant and emulsification may be used as a surfactant. An active agent such as an anionic interface surfactant or a cationic surfactant, an emulsifier, a dispersant, or the like may be used alone or in combination. The surface of the fiber ^ A thin resin can also be used in the capsule-emulsified fiber, the treatment of the epoxidized polydiene resin '100 parts by weight of the fiber, for example, 〇. 〇1~5 201224240 It is preferably 0.1 to 4 parts by weight, more preferably 3 to 3 parts by weight. When the amount of the fiber-reinforced resin composite material is too large, the adhesion of the shellfish is likely to decrease. If too much, the thick layer of the cured product of the epoxidized polydiene resin occupies between the fiber and the matrix resin. And there is a change in the characteristics of the composite material. [Fiber-reinforced resin composite material] The March fiber-reinforced resin composite material is composed of the above-mentioned resin-reinforced dicar resin. The matrix resin may be any of thermosetting resins and thermoplastics, and is preferably a thermosetting resin from the viewpoint of being easily impregnated with reinforcing fibers. As the thermosetting resin, an epoxy J:: an unsaturated polyester resin, an ethylene vinegar resin, a enamel resin, a male virgin resin, a cyanic acid S resin, or the like can be used. In terms of matrix resin, the above resin: small = resistant? It is excellent in properties, modulus of elasticity, chemical resistance, and hardening, and is preferably an epoxy-based thermosetting resin. The % oxygen-based thermosetting resin is not particularly preferred as an epoxy compound, and preferably has a two-component epoxy compound in the molecule. Needle, +, household ^ More than two or more decyloxy groups The oxygenate can be used in combination of one type of I alone or more. For dry sputum or two kinds, there are two or more epoxies in the molecule, which are specifically limited, and can be used as a #H y & gas-based oxime compound, an oxygen compound, and a fat _ > Rolled material, bisphenol type bicyclic epoxy resin, and the like. , cerium alcohol polyglycidyl ether, polyglycidamine amine-like aliphatic skeleton and two (4) fixed 'only preferred (1) ring, as long as it is a compound having a ring in the molecule, there is no special cyclic aliphatic skeleton An epoxy compound having two or more valence ring epoxy groups formed by containing two adjacent carbon atoms of -10-201224240. The alicyclic epoxy compound may, for example, be a compound represented by the following formula (1).

⑴ 以上述式(1)表示之脂環族環氧化合物係藉由將相 應之脂環族烯烴化合物以脂肪族過氧羧酸等氧化來製 造,使用貫質上無水之脂肪族過氧羧酸所製造者,以具 有高環氧化率觀點而言係較佳。 八 上述式(1)中’ γ表示單鍵或連結基團。作為連結基 團可例舉如2價烴基、羰基(-CO-)、醚鍵(-0-)、酯鍵 (-COO-)、酿胺鍵(_c〇NH_)、羧酸酯鍵( 〇c〇〇 )及連結 有多個此等基團之基團等。作為上述2價烴基,可較佳 例不奴數1〜18(特別為1〜6)之直鏈狀或支鏈狀伸烷基、2 價脂環烴基(特別A 1 ^ 引马2價伸環烷基)等,前述直鏈狀或支 鏈狀伸烧基可你丨與;^ m J舉亞甲基、甲基亞曱基、二曱基亞曱基' 伸乙基、伸丙某、一 签 二亞甲基等。又,2價脂環烴基可例 舉1,2 -伸環戊基、 i,3、伸環戊基、伸環丁基、1,2-伸環己 基、1,3 -伸環己其 , 丞 丨,4-伸環己基、伸環己基等。 作為以式(1彳矣_ V J衣不之脂環族環氧化合物,具體上可例 示下述化合物。 -11 - 201224240(1) The alicyclic epoxy compound represented by the above formula (1) is produced by oxidizing a corresponding alicyclic olefin compound with an aliphatic peroxycarboxylic acid or the like, and a perhydrate-free aliphatic peroxycarboxylic acid is used. The manufacturer is preferred from the viewpoint of having a high epoxidation ratio. VIII In the above formula (1), γ represents a single bond or a linking group. The linking group may, for example, be a divalent hydrocarbon group, a carbonyl group (-CO-), an ether bond (-0-), an ester bond (-COO-), a urethane bond (_c〇NH_), or a carboxylate bond (〇) C〇〇) and a group in which a plurality of such groups are linked. As the above-mentioned divalent hydrocarbon group, a linear or branched alkyl group or a divalent alicyclic hydrocarbon group having a number of from 1 to 18 (particularly from 1 to 6) can be preferably used (particularly A 1 ^ 引马2 price extension) Cycloalkyl), etc., the above-mentioned linear or branched extension group can be used; ^ m J methylene, methyl fluorenylene, dimethyl fluorenyl group , a sign of dimethylene and so on. Further, the divalent alicyclic hydrocarbon group may, for example, be a 1,2-cyclopentyl group, an i, 3, a cyclopentyl group, a cyclopentene group, a 1,2-extended cyclohexyl group, a 1,3-extension ring,丞丨, 4-cyclohexyl group, cyclohexyl group, etc. As the alicyclic epoxy compound of the formula (1彳矣_ V J), the following compounds can be specifically exemplified. -11 - 201224240

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〇Jn〇Jn

ο 上述式中,η為整數1〜3 0。 作為脂環族環氧化合物,除上述(i)之外,還可使用 (ii)僅2個環氧基當中的1個構成環狀脂肪族骨架且含有 相鄰之兩碳原子而形成之作為脂環環氧基的環氧化合物 (例如檸烯二環氧化物)、(iii)構成環氧基之碳原子與構成 環狀脂肪族骨架之碳原子以單鍵鍵結的環氧化合物、(iv) 縮水甘油醚化合物(例如具有環狀脂肪族骨架與縮水甘 -12- 201224240 油醚基之縮水甘油醚型環氧化合物等)。作為上述化合 物,具體上可例示下述化合物。ο In the above formula, η is an integer of 1 to 3 0. As the alicyclic epoxy compound, in addition to the above (i), (ii) one of only two epoxy groups may be used to form a cyclic aliphatic skeleton and contain two adjacent carbon atoms. An epoxy compound having an alicyclic epoxy group (for example, a limonene diepoxide), (iii) an epoxy compound constituting an epoxy group and a carbon atom constituting the cyclic aliphatic skeleton bonded by a single bond, ( Iv) a glycidyl ether compound (for example, a glycidyl ether type epoxy compound having a cyclic aliphatic skeleton and a glycidyl-12-201224240 oleyl ether group). Specific examples of the above compounds include the following compounds.

上述式令,R表示由q元醇[R-(OH)q]除去q個OH 之基團,P表示整數1〜50,q表示整數1〜10。q個括弧 内之基團中,p 可各自相同或相異。作為 q 元醇 [R-(OH)q],可例舉曱醇、乙醇、1-丙醇、異丙醇、1-丁 醇等一元醇;乙二醇、1,2-丙二醇、1,3-丙二醇、1,4-丁 二醇、新戊二醇、1,6 -己二醇、二乙二醇、三乙二醇、 四乙二醇、二丙二醇、聚丙二醇等二元醇;甘油、二甘 油、赤藻糖醇、三羥甲基乙烷、三羥甲基丙烷、新戊四 醇、二新戊四醇、山梨醇等三元以上之醇。前述醇類亦 可為聚醚多醇、聚酯多醇、聚碳酸酯多醇、聚烯烴多醇 -13- 201224240 等。前述醇類較佳為碳數1〜10之脂肪族醇類(特別為三 羥甲基丙烷等脂肪族多元醇)。 更且,除此之外還可使用(V)具有3個以上環氧基的 多官能環氧化合物。具體而言可例示下述化合物。 C0-^0-(CH2>jC0^0-CH, co-f o-(ch2)^co ^0-CH, ch2—CO -f o —(ch2)^· co 0—CH, CH —C〇-{-〇 —(CH2)^-C0 〇—CHr CH—CO -f 0 —(CH2)^· CO ^ 0—CH, CH2—CO -f 0 —(CH2)^· CO 0—CH; 〇:In the above formula, R represents a group in which q OH groups are removed by a q-valent alcohol [R-(OH)q], P represents an integer of 1 to 50, and q represents an integer of 1 to 10. Among the groups in the q parentheses, p may be the same or different. The q-valent alcohol [R-(OH)q] may, for example, be a monohydric alcohol such as decyl alcohol, ethanol, 1-propanol, isopropanol or 1-butanol; ethylene glycol, 1,2-propanediol, 1, a glycol such as 3-propanediol, 1,4-butanediol, neopentyl glycol, 1,6-hexanediol, diethylene glycol, triethylene glycol, tetraethylene glycol, dipropylene glycol or polypropylene glycol; A trihydric or higher alcohol such as glycerin, diglycerin, erythritol, trimethylolethane, trimethylolpropane, pentaerythritol, dipentaerythritol or sorbitol. The aforementioned alcohols may also be polyether polyols, polyester polyols, polycarbonate polyols, polyolefin polyols -13-201224240, and the like. The above alcohol is preferably an aliphatic alcohol having 1 to 10 carbon atoms (particularly an aliphatic polyol such as trimethylolpropane). Further, (V) a polyfunctional epoxy compound having three or more epoxy groups may be used in addition to the above. Specifically, the following compounds can be exemplified. C0-^0-(CH2>jC0^0-CH, co-f o-(ch2)^co ^0-CH, ch2—CO -fo —(ch2)^· co 0—CH, CH—C〇- {-〇—(CH2)^-C0 〇—CHr CH—CO —f 0 —(CH2)^· CO ^ 0—CH, CH 2 —CO —f 0 —(CH 2 )^· CO 0—CH;

上述式中,a、b、c、d、e、f為整數0~30。 作為前述雙酚型二環氧化合物可採用習知品,可例 舉如雙酚A型環氧樹脂(雙酚A二縮水甘油醚;兩末端 具有縮水甘油醚基之雙酚A與環氧氯丙烷之縮合生成物 等)、雙酚F型環氧樹脂(雙酚F二縮水甘油醚;兩末端 具有縮水甘油醚基之雙酚F與環氧氯丙烷之縮合生成物 等)、雙酚S型環氧樹脂(雙酚S二縮水甘油醚;兩末端 具有縮水甘油醚基之雙酚S與環氧氯丙烷之縮合生成物 等)等。 -14- 201224240 前述脂肪族多元醇聚縮水甘油醚並未 — 為該脂肪族多元醇聚縮水甘油鍵中的「脂肪族?艮定。作 <例舉如乙二醇、丨,2_丙二醇、丨,3•丙二醇夕凡一」 ιλ 丁 1,3· 丁 二醇、 I,4-丁 一醇、1,5-戊二醇、新戊二醇、丨,。己二醇、二乙 二醇:,乙二醇、四乙二醇、聚乙二醇、二丙二醇:: 丙二醇等二元醇;甘油、二甘油' 如甘/由、赤藻糖醇、 三經甲基乙院、三經甲基丙烧、新戊四醇: 等三元以上之醇。 # —新戊四醇 油醚之代表性實例,可In the above formula, a, b, c, d, e, and f are integers 0 to 30. As the bisphenol type diepoxy compound, a conventional product may be used, and examples thereof include a bisphenol A type epoxy resin (bisphenol A diglycidyl ether; and a bisphenol A and an epichlorohydrin having a glycidyl ether group at both terminals). a condensed product, etc.), a bisphenol F type epoxy resin (bisphenol F diglycidyl ether; a condensation product of bisphenol F and epichlorohydrin having a glycidyl ether group at both ends), and a bisphenol S ring An oxygen resin (bisphenol S diglycidyl ether; a condensation product of bisphenol S and epichlorohydrin having a glycidyl ether group at both ends). -14- 201224240 The aforementioned aliphatic polyglycol polyglycidyl ether is not - is an "aliphatic" in the polyglycidyl bond of the aliphatic polyol. For example, such as ethylene glycol, hydrazine, 2-propylene glycol , 丨, 3 • propylene glycol 夕凡一” ιλ D 1,3 · butanediol, I, 4-butanol, 1,5-pentanediol, neopentyl glycol, hydrazine. Hexanediol, diethylene glycol: ethylene glycol, tetraethylene glycol, polyethylene glycol, dipropylene glycol: diol such as propylene glycol; glycerin, diglycerol' such as ganyl/yellow, erythritol, three It is a ternary or higher alcohol such as methyl ketone, trimethoprim, and neopentyl alcohol. #—a representative example of neopentyl alcohol ether

=醇二縮水甘油 作為脂肪族多元醇聚縮水甘 例舉1,6 -已二醇二縮水甘油喊、 鍵、二起甲基丙烷聚縮水甘油醚、二乙二醇二縮水甘油 醚、新戊二醇二縮水甘油醚、丙二醇二縮水甘油醚、聚 丙二醇二縮水甘油醚、聚乙二醇二縮水甘油醚等。 聚縮水甘油胺梨環氧樹脂可例舉如N,N,N,,N,_四縮 水甘油-4,4’-亞曱基-雙苯曱胺等。 由提高調合時及纖維強化樹脂複合材料製造時之作 業性之觀點言之,前述環氧化合物係以呈液狀為佳。惟, 即便單體為固體環氧化合物,就摻混各成分後之硬化性 組成物的黏度(25。〇而言,只要是為例如20〇〇〇mPa· s 以下者仍可能使用。環氧化合物(所使用之所有環氧化合 物的/昆合物)的黏度(2 5 )例如為5 0 0 0 0 m P a · s以下,較 佳為300 00mpa · s以下,更佳為2〇〇〇〇mPa · s以下。此 黏度若過大則作業性等容易降低。 [纖維強化樹脂複合材料的製造] 若基質樹脂為熱固性樹脂時’則本發明纖維強化樹 -15- 201224240 脂複合材料可藉由使前述本發明樹脂強化用纖維與形成 基質樹脂之硬化性組成物(硬化前之組成物)構成的混合 材料硬化來製造。硬化一般係藉由加熱來進行》擬製造 纖維強化樹脂複合材料時,可應用習知方法,例如預浸 (prepreg)法、手積法(hand lay up method)、繞絲製胚法、 RTM(Hesin Transfer Molding,樹脂轉注成形)法、拉擠成 形法、真空吸入(vacuuminfusion)法等方法。 前述硬化性組成物一般係由硬化性化合物(環氧化 合物等)、硬化劑及硬化促進劑或硬化觸媒、視需求摻混 之各種添加劑構成。 硬化劑並未特別限定,可依硬化性化合物的種類等 來適當選擇。當硬化性化合物為環氡化合物等時,作為 硬化劑係較佳使用酸酐、多胺等。硬化劑可以丨種單獨 使用或2種以上組合使用。 酸酐可由 選擇、使用。 而言可例舉如 甲酸酐、十二 曱酸酐等。此 不良影響的範 苯二曱酸酐、 曱基環己缚二 時’係以予以 呈液狀之混合 使用商品名「 般慣用為%_氧樹脂用硬化劑者之中任意 作為酸酐’較佳為常溫下呈液狀者,具體 甲基四氫鄰笨二甲酸酐、甲基六氫鄰苯二 稀基琥拍酸酐、曱基内亞曱基四氫鄰笨二 外’在未對環氧樹脂組成物之含浸性造成 圍内可使用常溫下呈固體之酸酐,例如鄰 四氫鄰笨二曱酸酐、六氫鄰苯二曱酸酐、 ‘羧酸酐等。當使用常溫下呈固體之酸酐 溶解於常溫下呈液狀之酸酐中作成常溫下 物來使用為佳。作為酸酐系硬化劑,亦可 RIKACID MH-700」(新日本理化公司製)、 -16- 201224240 商品名「RIKACID ΜΗ」(新曰本理化公司製)、商品名 「ΗΝ-5 5 00」(曰立化成工業公司製)等市售品。 多胺可由一般慣用為環氧樹脂用硬化劑者之中任意 選擇、使用。作為多胺,較佳為常溫下呈液狀者。當使 用常溫下呈固體之多胺時,係以予以溶解於常溫下呈液 狀之多胺中形成常溫下呈液狀之混合物來使用為佳。作 為多胺之具體實例,可例舉如二伸乙三胺、三伸乙四胺、 四伸乙五胺、二伸丙二胺、二乙胺基丙胺等鏈狀脂肪族 多胺;Ν-胺基乙基旅啡、薄荷烯二胺(menthene diamine)、異佛爾酮二胺等環狀脂肪族多胺;聚醚多胺[例 如商品名「JEFFAMINE D-230」、「JEFFAMINE D-400」、 「JEFFAMINE D-2000」、「JEFFAMINE D-4000」、 「JEFFAMINE ED-600」、「JEFFAMINE ED-900」、 「JEFFAMINE ED-2003」、「JEFF AMINE EDR-1 48」、 「JEFFAMINE EDR-176」、「JEFFAMINE T-403」、 「JEFFAMINE T-3000」、「JEFFAMINE T-5000」(以上 為Huntsman公司製)等]等。 酸酐系硬化劑、多胺系硬化劑等硬化劑之摻混量較 佳以可發揮作為硬化劑之效果的有效量,即一般按環氧 樹脂組成物中環氧化合物之每1當量之環氧基,係以如 0.5〜1.5酸酐當量(或胺當量等)之比例來使用。 前述硬化促進劑只要是促進環氧化合物等的硬化時 一般所使用的硬化促進劑則無特殊限制,可使用例如三 級胺、三級胺鹽、咪唑類、有機磷系化合物、四級銨鹽、 四級鎮鹽、有機金屬鹽、硼化合物等。硬化促進劑可以 -17- 201224240 1種單獨使用或2種以上組合使用。 作為三級胺可例舉如月桂基二曱胺、N,N-二曱基環 己胺、Ν,Ν-二甲基苯曱胺、Ν,Ν-二曱基苯胺、(Ν,Ν-二甲 胺甲基)酚、2,4,6-三(Ν,Ν-二甲胺曱基)酚、1,8-二氮雜雙 環[5_4.0]十一碳-7-烯(DBU)、1,5-二氮雜雙環[4.3.0]壬 -5-烯(DBN)等。 作為三級胺鹽可例舉如前述三級胺之羧酸鹽、磺酸 鹽、無機酸鹽等。羧酸鹽可例舉辛酸鹽等碳數1〜30(特別 為碳數1〜10)之羧酸之鹽(特別為脂肪酸之鹽)等。磺酸鹽 可例舉對曱苯磺酸鹽、苯磺酸鹽、曱磺酸鹽、乙磺酸鹽 等。三級胺鹽之代表性實例則可例舉 1,8-二氮雜雙環 [5.4.0]十一碳-7-烯(DBU)之鹽(例如對甲苯磺酸鹽、辛酸 鹽)等。 作為咪唑類可例舉如2-曱基咪唑、2-乙基咪唑、1,2-二曱基咪唑、2-乙基-4-甲基咪唑、2-苯基咪唑、2-苯基 -4-甲基咪唑、1-苯甲基-2-甲基咪唑等。 作為有機磷系化合物可例舉如三苯基膦、亞磷酸三 苯酯等。 作為四級銨鹽可例舉如四乙基溴化銨、四丁基溴化 銨等。 作為四級鱗鹽可例舉如四丁基鱗癸酸鹽、四丁基鎮 月桂酸鹽、四丁基鐫肉豆蔻酸鹽、四丁基鎮棕櫚酸鹽、 四丁基鱗陽離子與雙環[2.2.1]庚烷-2,3-二羧酸及/或甲 基雙環[2.2.1]庚烷-2,3-二羧酸之陰離子形成之鹽;四丁 基鱗陽離子與1,2,4,5-環己烷四羧酸之陰離子形成之 201224240 鹽;四丁基鱗陽離子與甲磺酸之陰離子形成之鹽 基鐫陽離子與笨磺酸之陰離子形 :,丁 對甲本Μ之陰離子形成之鹽;四丁基鱗陽離子血 枣κ夂之陰離子形成之鹽’四丁基鱗陽離子 — 烧基苯磺酸之陰離子形成之鹽等。 — 作為有機金屬鹽可例舉如辛酸錫'辛酸鋅、 酸二丁基錫、乙醯丙酮鋁錯合物等。 作為硼化合物可例舉如三氟化硼、三苯硼烷等。 作為硬化促進劑亦可使用商品名「^ S A - 5 〇 6」、「U-C A T S A 1 η 7 r CAT SA·102」、「U_CAT 5003」(以上 馬San-Apr〇公司製)等市售品。 硬化促進劑之掺混量亦因硬化劑(酸肝系硬化劑等 的種類而異’-般相對硬化齊"〇〇重量份,係為0.01〜15 重量份,較佳為°·1〜10重量份,更佳為0.5〜8重量份。 作為硬化觸媒可使用例如陽離子聚合起始劑。陽離 子聚合起始劑乃為透過加熱而釋出起始陽離子聚合反應 之物質的起始劑。作為陽離子聚合起始劑可例舉如芳基 二重氮鹽[例如PP_33(ADEKA(股)製)]、芳基錤鹽、^ 錄鹽[例如 FC.509(3M(股)製)、UVEi〇14(g e (股)製)、 66 CP-77(以上為 ADEKA(股)製)、si-60L、SI-80L、 I 100L、SI-ll〇L(以上為三新化學工業(股)製)]等。 、相對例如硬化性化合物(環氧化合物等)100重量 伤,硬化觸媒之用量係為0 01〜15重量份,較佳為〇 〇5〜12 重量份’更佳為0.1〜10重量份。 作為前述各種添加劑可例舉如具有羥基的低分子量 -19- 201224240 化合物。透過摻混具有窥基的低分子化合物 進行硬化反應。具有經基之化合物可 勿’即可緩緩 二醇、丙三醇等多元醇。 —醇、二乙 此外,在硬化性組成物中,除此之 化物(纖維強化樹脂複合材料)之物隹土成艰可於未斟硬 圍内摻混各種添加劑。作為此種添加:可:c範 活性劑、内部脫模劑、著色劑、阻辦 ::如界面 偶合劑、填充劑、抗氧化劑、 //包劑、矽烷 H 外線吸收劑辇 化性組成物,以重量為基準’此等各種添加劑之: 較佳為10%以下(特別為5%以下)。 摻混置 硬化性組成物之硬化、、+ m 更化/皿度亦因硬化性化合物 而異,例如為40〜25〇t,較佳為8〇〜2〇(rc。 種類 如此所得之纖維強化樹脂複合材料(硬 轉移溫度例如為9(TC以上,較佳為i2〇t以上。玻璃 此外’纖.准強化樹脂複合材料中的纖維體積 (Vf)亦因用途而異,惟〜8G%,較佳為35〜7〇%。 本發明纖維強化樹脂複合材料其彈性能及進展能得 以同時提升’不僅耐衝擊,還可保持衝擊後的強度從 而適用於航空器之機體、主翼、尾翼、飛行操縱裝置、 整流罩(fairing)、機罩(cowl)、P1等、太空飛行器之馬達 外殼(motor case)、主翼等、人工衛星之本體結構、汽車 之底盤等汽車零件、鐵路車輛之車身結構、自行車之車 身結構、船舶之船身結構、風力發電之葉片、壓力容器、 釣竿、網球拍、高爾夫球桿、機械+ f、纜料構造物。 [實施例] -20- 201224240 以下’以實施例對本發明具體進行說明,惟本發明 未由此等所限定。 實施例1 將碳纖維布[東麗(股)製,以碳纖維Τ70〇所製之平 紋織物]浸潰於1 〇〇重量份丙酮中溶有2重量份之環氧化 聚 丁二稀[Daicel Chemical Industries(股)製,商品名 「EPOLEAD PB3 6 00」’環氧乙烷之氧濃度7.8%,數量 平均分子量5 9 0 0 ]的溶液中約1 〇秒後取出,於乾燥機 内、6 0 C之温度下乾燥3 0分鐘。乾燥後之碳纖維布的重 量相較於浸潰前係增加1 ·5%,可確認環氧化聚丁二烯既 已塗布於碳纖維上。 次之,以手積法使相對3,4-環氧環己基曱基(3,4-環 氧)環己烧缓酸6旨[Daicel Chemical Industries(股)製,商 品名「CELLOXIDE 2021P」]1〇〇重量份,混有13〇重量 份之4-甲基六氫鄰苯二甲酸酐與六氫鄰苯二甲酸酐之混 合物[新曰本理化(股)製’商品名r RIKACId MH-700」]、 〇. 6 5重量份之乙二醇、0.6 5重量份之作為硬化促進劑之 1,8-二氮雜雙環[5.4.0]十一碳-7-烯(DBU)之辛酸鹽 [San-Apiro(股)製,商品名「SA-102」]的液體(硬化性組 成物)含浸於浸潰乾燥後之碳纖維布的單層體或丨2層積 層體中’再於加熱爐中以11 0°C硬化2小時後,進一步 以1 7 0 °C硬化2小時’即製得碳纖維強化樹脂。 測疋所传之峡纖維強化樹脂的纖維體積含有率(V【) 的結果,單層體為54.0%’ 12層積層體為6〇9%。 -21 - 201224240 比較例1 除未進行將碳纖維布浸潰於環氧化聚丁二烯溶液 之操作以外’係以與實施例1同樣的方式來製作單層 體、1 2層積層體之碳纖維強化樹脂。 測疋所得之碳纖維強化樹脂的纖維體積含有率(Vf) 的果,單層體為54·0%,12層積層體為64_3%。 [評定試驗1丨 對實轭例1及比較例丨中所得之單層體之碳纖維強 化樹月曰進仃拉伸試驗,並測定彈性率⑷叫及拉伸強声 (MPa)心申試驗係依據日本工業標準κ7〇73之方 進行。此外,單層體之試片 尺寸為長200mm、寬2〇mm、 4 0_35mm。結果係示於表 求得。 、表1。表1中,增加率係由下式 之値-比較例1之値)/比較例 增加率(%)=[(實施例 1之値]X 1 0 0 [評定試驗21 對實施例1及比較例1中自θ ^ Α Τ所侍之積層有1 2層之破镳 維強化樹脂進行落錘衝擊試給、 禮I反纖 ’並測定最大荷童以丁认 吸收能(彈性能)及大於最大科击 Π置以下的 ° Ϊ的吸收能(進展泸、。铉# 衝擊試驗係依據日本工業桿m ν 展此)洛錘 、+ K7085之方法來推;。心 外,12層積層體之試驗片尺寸 水進订此 厚2mm。結果係示於表2。表:長l〇〇mrn '寬10〇mm、 得。 中,增加率係由下式求 之値]X 10 增加率(%)=[(實施例1之 値·比較例1之値)/比較例 22- 201224240 [表1]= alcohol diglycidyl as an aliphatic polyol polycondensed water, exemplified 1,6-hexanediol diglycidyl shunt, bond, two methyl propane polyglycidyl ether, diethylene glycol diglycidyl ether, neopentyl Glycol diglycidyl ether, propylene glycol diglycidyl ether, polypropylene glycol diglycidyl ether, polyethylene glycol diglycidyl ether, and the like. The polyglycidylamine pear epoxy resin may, for example, be N, N, N, N, _tetraglycidyl-4, 4'-fluorenylene-dibenzoguanamine or the like. From the viewpoint of improving the workability at the time of blending and the production of the fiber-reinforced resin composite material, the epoxy compound is preferably liquid. However, even if the monomer is a solid epoxy compound, the viscosity of the curable composition after blending the respective components (25. 〇 may be used as long as it is, for example, 20 〇〇〇 mPa·s or less. The viscosity (25) of the compound (all the epoxy compound/ester compound used) is, for example, 5,000 mPa·s or less, preferably 300 00 mPa·s or less, more preferably 2 Å. 〇〇mPa · s or less. If the viscosity is too large, the workability and the like are easily lowered. [Production of fiber-reinforced resin composite material] If the matrix resin is a thermosetting resin, the fiber-reinforced tree of the present invention can be borrowed from the present invention. The resin for reinforcing the above-mentioned resin of the present invention is produced by curing a mixed material comprising a curable composition (a composition before curing) of a matrix resin. The curing is generally carried out by heating when the fiber-reinforced resin composite material is to be produced. Conventional methods such as a prepreg method, a hand lay up method, a wire-making method, an RTM (Hesin Transfer Molding) method, a pultrusion method, a vacuum suction method can be applied. A method such as a vacuum infusion method. The curable composition is generally composed of a curable compound (such as an epoxy compound), a curing agent, a curing accelerator, or a curing catalyst, and various additives blended as required. When the curable compound is a cyclic ruthenium compound or the like, an acid anhydride, a polyamine or the like is preferably used as the curing agent. The curing agent may be used singly or in combination of two or more kinds. The anhydride can be selected and used. For example, it can be exemplified by formic anhydride, dodecanoic anhydride, etc. The adverse effects of the phthalic anhydride and the fluorenyl ring-bonded two-times are used in a liquid form. The product name "usually used as an acid anhydride for the curing agent for %_oxy resin" is preferably liquid at room temperature, specifically methyltetrahydrophthalic anhydride, methylhexahydrophthalic acid Anhydrous anhydride, fluorenyl fluorenyl sulfhydryl tetrahydron-butyrene can be used as an acid anhydride at room temperature in the absence of impregnation of the epoxy resin composition, such as o-tetrahydro-o-stup An anhydride, a hexahydrophthalic anhydride, a 'carboxylic acid anhydride, etc.. It is preferably used as a solid acid anhydride at room temperature in a liquid anhydride at room temperature, and is preferably used as an acid anhydride hardener. RIKACID MH-700" (manufactured by Nippon Chemical and Chemical Co., Ltd.), -16-201224240 Trade name "RIKACID ΜΗ" (manufactured by Shin Sakamoto Chemical Co., Ltd.), trade name "ΗΝ-5 5 00" (manufactured by Kyori Chemical Co., Ltd.) Commercially available products The polyamine can be arbitrarily selected and used as a curing agent for epoxy resins, and the polyamine is preferably liquid at normal temperature. When a polyamine which is solid at a normal temperature is used, it is preferably used in a polyamine which is dissolved in a liquid at a normal temperature to form a liquid mixture at normal temperature. As a specific example of the polyamine, a chain aliphatic polyamine such as diethylenetriamine, triethylenetetramine, tetraethyleneamine, dipropylenediamine or diethylaminopropylamine can be exemplified; a cyclic aliphatic polyamine such as aminoethyl phenanthrene, menthene diamine or isophorone diamine; polyether polyamine [e.g., trade name "JEFFAMINE D-230", "JEFFAMINE D-400" "JEFFAMINE D-2000", "JEFFAMINE D-4000", "JEFFAMINE ED-600", "JEFFAMINE ED-900", "JEFFAMINE ED-2003", "JEFF AMINE EDR-1 48", "JEFFAMINE EDR-" 176", "JEFFAMINE T-403", "JEFFAMINE T-3000", "JEFFAMINE T-5000" (above, manufactured by Huntsman), etc. The blending amount of the curing agent such as the acid anhydride-based curing agent or the polyamine-based curing agent is preferably an effective amount which can exert the effect as a curing agent, that is, generally 1 equivalent of the epoxy compound in the epoxy resin composition. The base is used in a ratio of, for example, 0.5 to 1.5 anhydride equivalents (or amine equivalents, etc.). The hardening accelerator is not particularly limited as long as it is a curing accelerator which is generally used for curing an epoxy compound or the like, and for example, a tertiary amine, a tertiary amine salt, an imidazole, an organophosphorus compound, or a quaternary ammonium salt can be used. , four grades of salt, organic metal salts, boron compounds, etc. The hardening accelerator may be used -17-201224240 alone or in combination of two or more. The tertiary amine may, for example, be lauryl diamine, N,N-didecylcyclohexylamine, hydrazine, hydrazine-dimethylphenyl guanamine, hydrazine, hydrazine-didecyl aniline, (Ν, Ν- Dimethylaminomethyl)phenol, 2,4,6-tris(Ν,Ν-dimethylaminodecyl)phenol, 1,8-diazabicyclo[5_4.0]undec-7-ene (DBU , 1,5-diazabicyclo[4.3.0]non-5-ene (DBN), and the like. The tertiary amine salt may, for example, be a carboxylate, a sulfonate or a mineral acid salt of the above tertiary amine. The carboxylate may, for example, be a salt of a carboxylic acid having a carbon number of 1 to 30 (particularly a carbon number of 1 to 10) such as an octanoate (particularly a salt of a fatty acid). The sulfonate may, for example, be p-toluenesulfonate, besylate, sulfonate or ethanesulfonate. A representative example of the tertiary amine salt is, for example, a salt of 1,8-diazabicyclo [5.4.0]undec-7-ene (DBU) (e.g., p-toluenesulfonate, octoate) or the like. The imidazoles may, for example, be 2-mercaptoimidazole, 2-ethylimidazole, 1,2-dimercaptoimidazole, 2-ethyl-4-methylimidazole, 2-phenylimidazole, 2-phenyl- 4-methylimidazole, 1-benzyl-2-methylimidazole, and the like. The organophosphorus compound may, for example, be triphenylphosphine or triphenylphosphite. The quaternary ammonium salt may, for example, be tetraethylammonium bromide or tetrabutylammonium bromide. The fourth-order scale salt may, for example, be tetrabutyl sulphonate, tetrabutyl laurate, tetrabutyl sulfonium myristate, tetrabutyl palmitate, tetrabutyl cation and bicyclo [ 2.2.1] a salt formed by the anion of heptane-2,3-dicarboxylic acid and/or methylbicyclo[2.2.1]heptane-2,3-dicarboxylic acid; tetrabutyl squaride and 1,2 a 201224240 salt formed by an anion of 4,5-cyclohexanetetracarboxylic acid; an anionic form of a salt sulfonium cation and a sulfonic acid formed by an anion of a tetrabutyl cation and a methanesulfonic acid: a salt formed by an anion; a salt formed by an anion of tetrabutyl cation cation blood κ 夂 四 'tetrabutyl cation cation — a salt formed by an anion of a benzene sulfonic acid. — The organic metal salt may, for example, be a zinc octylate, zinc octoate, dibutyltin acid or an aluminum acetonate complex. The boron compound may, for example, be boron trifluoride or triphenylborane. Commercially available products such as "^ S A - 5 〇 6", "U-C A T S A 1 η 7 r CAT SA·102", and "U_CAT 5003" (manufactured by Ma-Apr Co., Ltd.) can be used as the hardening accelerator. The blending amount of the hardening accelerator is also 0.01 to 15 parts by weight, preferably °·1~, depending on the type of the hardening agent (the acid liver hardener or the like). 10 parts by weight, more preferably 0.5 to 8 parts by weight. As the curing catalyst, for example, a cationic polymerization initiator may be used. The cationic polymerization initiator is an initiator which releases a substance which initiates cationic polymerization by heating. The cationic polymerization initiator may, for example, be an aryldiazonium salt [for example, PP_33 (manufactured by ADEKA Co., Ltd.), an arylsulfonium salt, a salt (for example, FC.509 (made by 3M), UVEi). 〇14 (ge (share) system), 66 CP-77 (above ADEKA (share) system), si-60L, SI-80L, I 100L, SI-ll〇L (above is Sanxin Chemical Industry Co., Ltd.) )), etc., relative to, for example, a curable compound (epoxy compound, etc.) 100 weight damage, the amount of the hardening catalyst is 0 01 to 15 parts by weight, preferably 〇〇 5 to 12 parts by weight 'more preferably 0.1 〜10 parts by weight. As the above various additives, a low molecular weight -19 to 201224240 compound having a hydroxyl group can be exemplified. The molecular compound is subjected to a hardening reaction. The compound having a trans-group can be used to retard a polyol such as a diol or a glycerin. Alcohol, diethylene, and, in addition, in a curable composition, a fiber-reinforced resin The composite material) can be mixed with various additives in the hard shell. As such, it can be: c-fan active agent, internal mold release agent, colorant, and resistance: such as interface coupling agent, Filler, antioxidant, //packaging agent, decane H external absorbent, deuterated composition, based on the weight of the various additives: preferably 10% or less (especially 5% or less). The hardening of the curable composition, the + m refining/dish degree is also different depending on the curable compound, and is, for example, 40 to 25 Torr, preferably 8 Å to 2 Torr (rc. The fiber reinforced resin compound thus obtained The material (hard transfer temperature is, for example, 9 (TC or more, preferably i2 〇t or more. The glass fiber volume in the quasi-reinforced resin composite material is also different depending on the use, but ~8 G%, preferably 35 to 7〇%. The fiber-reinforced resin composite material of the present invention The elastic energy and progress can be simultaneously improved. 'Not only impact resistance, but also the strength after impact, which is suitable for the aircraft body, main wing, tail wing, flight control device, fairing, cowl, P1, etc. Motor case, main wing, etc., body structure of artificial satellite, automobile parts such as chassis of automobile, body structure of railway vehicle, body structure of bicycle, hull structure of ship, blade of wind power generation, pressure vessel , fishing rods, tennis rackets, golf clubs, mechanical + f, cable construction. [Examples] -20-201224240 Hereinafter, the present invention will be specifically described by way of examples, but the present invention is not limited thereto. Example 1 A carbon fiber cloth [made of Toray Co., Ltd., a plain weave fabric made of carbon fiber Τ70〇] was impregnated with 1 part by weight of acetone in 2 parts by weight of epoxidized polybutadiene [Daicel Chemical Industries] (Stock) system, the product name "EPOLEAD PB3 6 00" 'Ethylene oxide oxygen concentration 7.8%, number average molecular weight 5 9000' of the solution is taken out after about 1 〇 seconds, in the dryer, 6 0 C Dry at temperature for 30 minutes. The weight of the dried carbon fiber cloth was increased by 1.5% compared with that before the impregnation, and it was confirmed that the epoxidized polybutadiene was coated on the carbon fiber. Secondly, the 3,4-epoxycyclohexyldecyl (3,4-epoxy)cyclohexanone acid 6 is used by hand method [Daicel Chemical Industries, Ltd., trade name "CELLOXIDE 2021P"] 1 part by weight, mixed with 13 parts by weight of a mixture of 4-methylhexahydrophthalic anhydride and hexahydrophthalic anhydride [New 曰 理 理 ( ' ' 商品 商品 商品 R R R R R R R R R R R R R R R R R R R R 700"], 〇. 6 5 parts by weight of ethylene glycol, 0.6 parts by weight of octanoic acid of 1,8-diazabicyclo[5.4.0]undec-7-ene (DBU) as a hardening accelerator The liquid (curable composition) of salt [San-Apiro Co., Ltd., trade name "SA-102"] is impregnated into a single layer or a two-layer laminate of carbon fiber cloth after dipping and drying. After hardening at 11 ° C for 2 hours in the furnace and further hardening at 170 ° C for 2 hours, a carbon fiber reinforced resin was obtained. As a result of measuring the fiber volume fraction (V [) of the chiral fiber reinforced resin, the monolayer was 54.0%', and the 12-layer laminate was 6〇9%. -21 - 201224240 Comparative Example 1 Carbon fiber reinforced with a single layer and a 12 layer laminate in the same manner as in Example 1 except that the carbon fiber cloth was not impregnated with the epoxidized polybutadiene solution. Resin. The fiber volume content (Vf) of the carbon fiber-reinforced resin obtained by the measurement was 5·0% for the single layer and 64 to 3% for the 12-layer laminate. [Evaluation Test 1) The carbon fiber reinforced tree 曰 曰 tensile test of the single layer body obtained in the yoke example 1 and the comparative example ,, and the elastic modulus (4) and the tensile strong sound (MPa) heart test system were measured. It is carried out according to the Japanese Industrial Standard κ7〇73. In addition, the test piece size of the single layer body is 200 mm long, 2 mm wide, and 40 mm 35 mm. The results are shown in the table. ,Table 1. In Table 1, the increase rate is 値 from the following formula - 比较 of Comparative Example 1 / Comparative Example Increasing Rate (%) = [(Example 1 値) X 1 0 0 [Assessment Test 21 vs. Example 1 and Comparison In Example 1, the layer of the θ ^ Α 侍 has 12 layers of ruthenium-reinforced reinforced resin for the drop hammer impact test, and the remedy of the maximum energy of the children. The absorption energy of the maximum Π 以下 以下 ( ( 泸 泸 泸 泸 泸 泸 泸 泸 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 、 The test piece size water was set to a thickness of 2 mm. The results are shown in Table 2. Table: Length l〇〇mrn 'width 10 〇 mm, obtained. Medium, the increase rate is obtained by the following formula] X 10 increase rate (% ) = [(Example 1 / Comparative Example 1) / Comparative Example 22 - 201224240 [Table 1]

由表1及表2得知,使用經環氧化聚二稀系樹脂表 -理之,脂強化用纖維的複合材料(實施存")相較於 用未、.k %氧化聚二烯系樹脂表面處理之樹脂強化用纖 勺複σ材料(比較例丨),拉伸強度大幅改善,且彈性能 及進展能亦同時增大。 [產業上之可利用性] 入本發明樹脂強化用纖維可同時提升纖維強化樹脂複 合材料之最大荷重以下的吸收能(彈性能)及大於最大荷 重的吸收能(進展能),係有用於作為汽車零件、土木建 築用品、風力發電之葉片、運動用品、航空器、船舶、 機器人、纜線材料等領域中所利用之纖維強化複合材料 -23- 201224240 的製造原料。 【圖式簡單說明】 無。 【主要元件符號說明】It is known from Tables 1 and 2 that the composite material of the resin for fat strengthening (execution) is used in comparison with the oxidized polydiene resin. Resin-treated resin-reinforced resin-reinforced sigma material (comparative example), the tensile strength is greatly improved, and the elastic energy and progress can be simultaneously increased. [Industrial Applicability] The resin for reinforcing fibers of the present invention can simultaneously increase the absorption energy (elastic energy) below the maximum load of the fiber-reinforced resin composite material and the absorption energy (progressive energy) larger than the maximum load, and is used as Manufacturing materials for fiber reinforced composite materials -23- 201224240 used in the fields of automotive parts, civil engineering supplies, blades for wind power generation, sporting goods, aircraft, ships, robots, and cable materials. [Simple description of the diagram] None. [Main component symbol description]

Claims (1)

201224240 201224240 七 、申請專利範圍·· 桝肝月曰強化用纖維’其係對纖維以環氧化聚二稀系 2树脂貫施表面處理而成。 纖维Γ專利乾圍第1項之樹脂強化用纖维’其中前述 3 、糸為碳纖維或玻璃纖維。 第1 ^維強化樹脂複合材料,其係由如申請專利範圍 4.如申ί 2項之樹脂強化用纖維及基質樹脂構成。 卜請專利範圍第3項之纖維強化樹脂複合材料,其 S一:述基質樹脂係為環氧系熱固性樹脂。 化椒冓&物’其係由如申請專利範圍帛4項之纖維強 匕树脂複合材料構成。 -25- 201224240 四、指定代表圖: (一) 本案指定代表圖為:無。 (二) 本代表圖之元件符號簡單說明: 無0 五、本案若有化學式時,請揭示最能顯示發明特徵的化學式:201224240 201224240 VII. Scope of application for patents·· 桝 曰 曰 曰 曰 ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ ’ 纤维 纤维 纤维 纤维 纤维 纤维 。 。 。 。 。 The fiber reinforced fiber of the first item of the fiber Γ patent dry circumference, wherein the above 3, 糸 is carbon fiber or glass fiber. The 1st-dimensional reinforced resin composite material is composed of a resin-reinforcing fiber and a matrix resin as claimed in the patent application. A fiber-reinforced resin composite material according to item 3 of the patent scope, wherein the matrix resin is an epoxy-based thermosetting resin. The scorpion scorpion &matter' is composed of a fiber reinforced resin composite material as disclosed in the patent application 帛4 item. -25- 201224240 IV. Designated representative map: (1) The representative representative of the case is: None. (2) A brief description of the symbol of the representative figure: None 0. If there is a chemical formula in this case, please disclose the chemical formula that best shows the characteristics of the invention:
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