WO2017163129A1 - Composition de résine époxy, préimprégné, et matériau en plastique renforcé par des fibres - Google Patents

Composition de résine époxy, préimprégné, et matériau en plastique renforcé par des fibres Download PDF

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Publication number
WO2017163129A1
WO2017163129A1 PCT/IB2017/000376 IB2017000376W WO2017163129A1 WO 2017163129 A1 WO2017163129 A1 WO 2017163129A1 IB 2017000376 W IB2017000376 W IB 2017000376W WO 2017163129 A1 WO2017163129 A1 WO 2017163129A1
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Prior art keywords
epoxy resin
resin composition
groups
component
composition according
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PCT/IB2017/000376
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English (en)
Inventor
Swezin Than TUN
Jonathan Hughes
Nobuyuki Arai
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Toray Industries, Inc.
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Publication of WO2017163129A1 publication Critical patent/WO2017163129A1/fr

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    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • C08J5/241—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres
    • C08J5/243—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs using inorganic fibres using carbon fibres
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/40—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the curing agents used
    • C08G59/50—Amines
    • C08G59/56—Amines together with other curing agents
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/20—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the epoxy compounds used
    • C08G59/22—Di-epoxy compounds
    • C08G59/226—Mixtures of di-epoxy compounds
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/40—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the curing agents used
    • C08G59/4007—Curing agents not provided for by the groups C08G59/42 - C08G59/66
    • C08G59/4014—Nitrogen containing compounds
    • C08G59/4021—Ureas; Thioureas; Guanidines; Dicyandiamides
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/40—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the curing agents used
    • C08G59/50—Amines
    • C08G59/504—Amines containing an atom other than nitrogen belonging to the amine group, carbon and hydrogen
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/68—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the catalysts used
    • C08G59/686—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the catalysts used containing nitrogen
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/04—Reinforcing macromolecular compounds with loose or coherent fibrous material
    • C08J5/0405—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres
    • C08J5/042—Reinforcing macromolecular compounds with loose or coherent fibrous material with inorganic fibres with carbon fibres
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • C08J5/249—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs characterised by the additives used in the prepolymer mixture
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2363/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins

Definitions

  • the present application provides an epoxy resin composition for fiber-reinforced composite materials that are well-suitable for aerospace applications, sports applications, and general industrial applications.
  • Fiber Reinforced Plastic (FRP) materials comprising a
  • reinforced fiber and a matrix resin have excellent mechanical properties such as strength and rigidity while being lightweight, and therefore are widely used as aircraft members, spacecraft members, automobile members, railway car members, ship
  • reinforcement fibers are in the form of woven cloth or continuous filaments.
  • FRP materials can be produced using filament winding methods, prepreg lamination methods, molding methods, pultrusion methods or the like, but the prepreg lamination method is predominantly used to obtain high performance FRP materials.
  • Prepreg lamination is a method in which a prepreg or prepregs produced by
  • thermosetting resin composition impregnating a reinforcing fiber with a thermosetting resin composition is or are formed and laminated, followed by curing of the resin through the application of heat and pressure to obtain the FRP material.
  • the FRPs' properties depend on both the reinforcement fiber and the matrix resin.
  • the important design properties include tensile strength and modulus, compression strength and modulus, impact resistance, damage tolerance, and toughness.
  • the FRP materials are composed of about 60% by weight of the reinforcing fibers, which govern the majority of the properties, whereas the matrix resin has greatest effect on compression strength and transverse tensile properties.
  • performance composites are typically based on ⁇ , ⁇ , ⁇ ', ⁇ '- tetrag lycidyl 4,4'-diaminodiphenyl methane and 4,4'- diaminodiphenyl sulfone. These resins produce high tensile strength and tensile moduli.
  • Epoxy resin systems providing higher matrix properties than state-of-the-art formulations are also known. For example, epoxy resin systems which use naphthalene- based epoxy resin systems in combination with amine curing agents provide higher compression strength and higher heat resistance than the start-of-the art resin system, as disclosed in a number of patent publications, for example, U.S. Pat. Publication Nos. 20110049426 and 20130217283. Another epoxy resin system using a naphthalene-based epoxy resin system with a
  • dicyclopentadiene-modified phenolic as a curing agent provides higher heat resistance, low water absorption, and good adhesion, as disclosed in U.S. Pat. No. 5312878.
  • these systems are designed for high cure temperatures of above 150°C for at least 2 hours to achieve the desired maximum properties.
  • more than one curing agent can be used for low temperature cure or out-of-autoclave cure.
  • U.S. Pat. Publication No. 20140100320 disclosed that an epoxy resin composition with aromatic amine and aliphatic amine in
  • the present invention therefore seeks to provide an epoxy resin composition that can be cured at a low temperature of below 150°C to form a cured product excellent in matrix resin modulus and heat resistance that prior attempts have failed to achieve.
  • Another object is to provide an FRP material that is excellent under hot/wet conditions. It has been found that a composition containing a naphthalene-based epoxy resin having at least two naphthalene moieties and at least one glycidyl ether group per molecule and a combination of aromatic and aliphatic amine hardeners exhibits excellent flexural modulus, low water
  • an epoxy resin composition for a fiber-reinforced composite material comprising components (A), (B), (C), (D), and (E), wherein the epoxy resin composition has a degree of cure of at least 90% and a water absorption of at most 3.0 wt% after being cured at 132°C for 2 hours, wherein the components (A), (B), (C), (D), and (E) com prise :
  • This invention further includes a cured epoxy resin obtained by curing the abovementioned epoxy resin composition, a prepreg obtained by impregnating a reinforcing fiber matrix with the abovementioned epoxy resin composition, a fiber-reinforced composite material obtained by curing the prepreg, and a fiber- reinforced composite material comprising a cured product obtained by curing the abovementioned epoxy resin composition and a reinforcing fiber base prepreg.
  • the inventors have surprisingly discovered that when a naphthalene- based epoxy resin containing two or more naphthalene moieties per molecule is employed in an epoxy resin composition, it is possible to maintain a high modulus in a cured resin obtained by curing the epoxy resin composition at a low temperature of below 150°C while reducing the tendency of the cured resin to absorb water, thus obtaining a better overall hot/wet modulus when tested.
  • a Afunctional epoxy resin will reduce the overall modulus of the system so that even if the water absorption is reduced the hot/wet modulus will be impaired.
  • a dicyclopentadiene-based epoxy resin a well-known material for reducing water absorption
  • the water absorption of the cured resin is reduced but room temperature dry modulus is lower. Even though the lower water absorption helps retain a higher percentage of the dry modulus when tested under hot wet
  • the hot/wet modulus is not significantly increased since the dry modulus has been lowered due to the presence of the dicyclopentadiene-based epoxy resin.
  • substantially may refer to an amount that is within less than 10% of, within less than 5% of, within less than 1 % of, within less than 0.1 % of, or within less than 0.01 % of the stated amount.
  • room temperature as used herein has its ordinary meaning as known to those skilled in the art and may include temperatures within the range of about 15°C to 43°C.
  • low temperature cure includes curing at temperatures within the range of about 110°C to about 150°C.
  • Component (A) comprises one or more epoxy resins
  • naphthalene-based epoxy resins containing at least two naphthalene moieties and at least one glycidyl ether per molecule.
  • epoxy resins are referred to herein as "naphthalene-based epoxy resins.”
  • naphthalene as used herein describes a structure of two benzene rings which are conjugated to each other directly.
  • Any of the naphthalene-based monomer precursors (such as hydroxyl- substituted bi-naphthalene) may be formed into a glycidyl epoxy resin, such as glycidyl ether epoxy resins.
  • the diglycidyl ethers of the precursors may be formed by reacting the precursor with epichlorohydrin in the presence of a basic catalyst.
  • naphthalene-based epoxy resins which form part of an epoxy resin composition as described herein, provide low water absorption, high flexural modulus and high heat resistance once the epoxy resin composition has been cured.
  • component (A) is an essential component for an epoxy resin composition to successfully provide excellent performance, particularly under hot/wet conditions.
  • the naphthalene-based epoxy resin may comprise one bi- naphthalene moiety to which at least one glycidyl ether substituent is bonded, More than one glycidyl ether substituent may be bonded to the bi-naphthalene moiety at any suitable position in any suitable combination.
  • the bi-naphthalene moiety may also have a non-glycidyl either substituent bonded at any of the non-glycidyl ether substituted sites of either naphthalene ring.
  • Suitable non- glycidyl ether substituent groups include, without limitation, hydrogen atom, halogen atoms, Ci to C 6 alkyl groups, C x to C 6 alkoxyl groups, Cj to C 6 fluoroalkyl groups, cycloalkyl groups, aryl groups, and aryloxyl groups and combinations thereof.
  • Such non- glycidyl ether substituent groups may be straight, branched, cyclic, or polycyclic substituents, wherein these groups are optionally employed individually or different groups are optionally employed in combination thereof.
  • the naphthalene-based epoxy resin may contain two, three, four or more naphthalene rings linked to each other either directly or through a linking (bridging) moiety, such as a methylene group (-CH 2 -), with at least one glycidyl ether group (preferably at least two glycidyl ether groups) being bonded to (substituted on) a naphthalene ring (or multiple naphthalene rings, where two or more glycidyl ether groups are present).
  • the multiple naphthalene rings may optionally be substituted with one or more further su bstituents, including any of the aforementioned types of
  • component (A) may be comprised of one or more naphthalene- based epoxy resins represented by the following Formula (I):
  • R 1 to R 8 are each independently selected from the group consisting of a hydrogen atom, halogen atoms, Cj. to C 6 alkyl groups, C x to C 6 alkoxyl groups, Ci to C 6 fluoroalkyl groups, cycloalkyl groups, aryl groups, and aryloxyl groups wherein these groups are optionally employed individually or different groups are optionally employed in combination as each of Ri to R 8 ;
  • component (A) may be comprised of epoxy resin represented by the following Formula (II):
  • Ri to R 12 are each independently selected from the group consisting of hydrogen atoms, halogen atoms, CI to CIO alkyl groups, CI to CIO alkoxyl groups, CI to CIO fluoroalkyl groups, cycloalkyl groups, aryl groups, aryloxyl groups, and glycidoxy groups
  • Y 1 to Y 7 are each independently selected from the group consisting of hydrogen atoms, halogen atoms, CI to CIO alkyl groups, CI to CIO alkoxyl groups, CI to CIO fluoroalkyl groups, cycloalkyl groups, aryl groups, aryloxyl groups, and glycidoxy groups, wherein each benzene nucleus may be substituted with one or more Y groups, n is 0 or an integer of 1 to 5, k is 0 or an integer of 1 to 3, wherein the Y groups may be attached to either or both rings of each naphthalene nucleus; and each
  • the glycidyl ether groups on the naphthalene moieties may be bonded to any of the carbon atoms of each naphthalene ring in any combination.
  • the glycidyl ether groups may therefore be present at the 2, 3, 4, 5, 6, and/or 7 positions of any of the naphthalene rings present, and where there is more than one glycidyl ether group may be present in any suitable combination on any of the naphthalene rings of the epoxy resin.
  • Specific precursors which may be used for producing the naphthalene-based epoxy resin having two or more naphthalene moieties per molecule include l-(2-hydroxy- naphthalen-l-ylmethyl)- naphthalene- 2-ol, l-(2-hydroxy- naphthalen-l-ylmethyl)-naphthalene-2,7-diol, l-(2-hydroxy- naphthalen-l-ylmethyl)-naphthalene-7-ol, 1 - ( 7 - hyd roxy- naphthalen-l-ylmethyl)-naphthalene-7-ol, l-(2,7-dihydroxy- naphthalen-l-ylmethyl)-naphthalene-2,7-diol, or any combination thereof.
  • Such precursors may be reacted with epichlorohydrin, using base catalysis, to introduce the desired glycidyl ether groups as
  • n is the number of repeating units and an integer of 1 or more.
  • the amount of component (A) may be in the range of 20 to 70phr per lOOphr of total epoxy resin. In certain embodiments, the amount of naphthalene- based epoxy resin may be in the range of 25 to 40phr or 25 to 35phr per lOOphr of total epoxy resin If the amount is less than 20phr, water absorption may be high and hot/wet flexural modulus may be low. If the amount is greater than 70phr, the resin
  • viscosity may be very high and handling and processing of the FRP material may be difficult.
  • component (A) examples include "Epiclon (registered trademark)" HP4700, HP4710, HP4770, EXA4701, EXA4750, and EXA7240 (manufactured by Dainippon Ink and Chemicals, Inc.), NC-7000L and NC-7300L (manufactured by Nippon Kayaku Co., Ltd.) and ESN-175 and ESN- 375 (manufactured by Tohto Kasei Epoxy Co., Ltd.), etc., as well as combinations thereof.
  • the epoxy resin composition comprising component (A) is capable of being cured at 132°C for 2 hours to achieve the degree of cure of at least 90%. If the degree of cure is less than 90%, the FRP material obtained will have low compression strength and heat resistance.
  • the cured epoxy resin composition also has a water absorption of at most 3.0 wt% after immersing in boiling water for 24 hours. If the water absorption is more than 3.0 wt%, the FRP material obtained will have low compression strength and heat resistance, particularly under hot/wet conditions. The water absorption is measured by the difference in the weight of the epoxy resin composition before and after immersion.
  • the cured epoxy resin composition comprising component (A) may have a room temperature flexural modulus of at least 4.0 GPa and a hot/wet flexural modulus of at least 3.0 GPa.
  • the room temperature flexural modulus refers to the sample being tested without immersion and the hot/wet flexural modulus refers to the sample being tested at 82°C after immersing in boiling water for 24 hours. If the hot/wet flexural modulus is less than 3.0GPa, the FRP material obtained may have low compression strength.
  • the flexural modulus of the cured epoxy resin can be determined by 3- point bending test in accordance with ASTM D 7264 using an
  • the epoxy resin composition also comprises the component (B) wherein the component (B) comprises or is an epoxy or more than one epoxy resin other than a naphthalene-based epoxy resin as defined herein and used as component (A), to improve the cross linking and processability .
  • These epoxy resins may be prepared from precursors such as amines (e.g., epoxy resins prepared using diamines and compounds containing at least one amine group and at least one hydroxyl group such as tetrag lycidy I diaminodiphenyl methane, tetraglycidyl diaminodiphenylether, tetrag lycidy I
  • phenols e.g., bisphenol A epoxy resins, bisphenol F epoxy resins, bisphenol S epoxy resins, bisphenol R epoxy resins, phenol-novolac epoxy resins, cresol- novolac epoxy resins, resorcinol epoxy resins and
  • triphenylmethane epoxy resins dicyclopentadiene epoxy resins, naphthalene epoxy resins (epoxy resins containing only a single naphthalene moiety per molecule), epoxy resins having a biphenyl skeleton, isocya na te- mod if ied epoxy resins, epoxy resins having a fluorene skeleton, and compounds having a carbon-carbon double bond (e.g., alicyclic epoxy resins).
  • the epoxy resins suitable for use in component (B) are not restricted to the examples above. Halogenated epoxy resins prepared by halogenating these epoxy resins can also be used. Furthermore, mixtures of two or more of these epoxy resins, and compounds having one epoxy group or monoepoxy compounds such as glycidylaniline, glycidyl toluidine or other g lycidy la m i nes
  • amine base epoxy such as YH434L (manufactured by Nippon Steel
  • bisphenol F epoxy resins such as " j E R (registered trademark)” 806, 807, 4002P, 4004P, 4007P, 4009P and 4010P (manufactured by Mitsubishi Chemical Corporation), and "Epotohto (registered trademark)” YDF2001 and YDF2004 (manufactured by Nippon Steel Chemical Co., Ltd.); tetramethyl-bisphenol F epoxy resin such as YSLV-80XY (manufactured by Nippon Steel Chemical Co., Ltd.); bisphenol S epoxy resins such as "Epiclon (registered trademark)” EXA-154 (manufactured by Dainippon Ink and Chemicals, Inc.); phenol-novolac epoxy resins such as "jER (registered trademark)” 152 and 154 (manufactured by Mitsubishi Chemical Corporation), and “Epiclon (registered trademark)” N-740, N-770, and N-775 (manufactured by Dainippon In
  • naphthalene epoxy resins (containing a single naphthalene moiety per
  • HP4032 and HP4032D manufactured by
  • triphenylmethane epoxy resins such as "jER (registered trademark)" 1032S50 (manufactured by Mitsubishi Chemical
  • the abovementioned component (B) may comprise component (Bl) and component (B2) which are epoxy resins different from each other, wherein component (Bl) is an epoxy resin having more than two epoxy-functional groups per molecule and component (B2) is an epoxy resin different from component (Bl) and having less than three epoxy-functional groups per molecule.
  • component (Bl) epoxy resin provides high cross linking and high strength once the composition has been cured.
  • component (B2) epoxy resin provides high elongation and low viscosity resin for handleability and tackiness.
  • “Handleability” refers to the ability to easily handle and process the material.
  • the amount of component (Bl) may be in the range of 30 to
  • the amount is less than 30phr, the strength of the FRP material obtained may be impaired. If the amount is greater than 80phr, the water absorption may be high and the FRP material obtained may have low compression strength .
  • component (Bl) examples include: amine base epoxy resins such as
  • the component (B2) epoxy resin may have an epoxy equivalent weight of less than 205 g/eq to achieve high elongation.
  • Examples of commercially available products suitable for use as component (B2) having an EEW of less than 205 g/eq include: bisphenol A epoxy resins such as "jER (registered trademark)" 825, 828 and 834 (manufactured by Mitsubishi
  • the component (B2) may have an epoxy equivalent weight of less than 170 g/eq to achieve even higher elongation. Additionally, these epoxies can provide lower resin viscosity for handieability, processability, and tackiness.
  • component (B2) having an epoxy equivalent weight of less than 170 g/eq include: GAN (manufactured by Nippon Kayaku Co., Ltd.) and cycloaliphatic epoxy resins such as "Celloxide (registered trademark)" 2021P, 8000, 8010, and 8200 (manufactured by Daicel Chemical Industries).
  • the amount of component (B2) may be at most 30phr per lOOphr of total epoxy resin. If the amount is greater than 30phr, the water absorption may be high and the FRP material obtained may have low compression strength.
  • the viscosity of the epoxy resin composition comprising the component (B2) at 40°C may be between 1 x 10 3 and 3 x 10 4 Pa-s, in order to achieve both handieability and processability of the FRP while maintaining the mechanical properties. If the viscosity at 40°C is too low, the handieability may be compromised because the tack may be too high. If the viscosity at 40°C is too high, the moldability of the FRP may be unsatisfactory because the tack may be too low.
  • the viscosity of the epoxy resin composition was measured using a dynamic viscoelasticity measuring device (ARES, manufactured by TA Instruments) using parallel plates with a diameter of 40 mm while increasing the temperature at a rate of 2°C/min, with a strain of 10%, frequency of 0.5 Hz, and plate interval of 1 mm, from 40°C to 150°C.
  • AOS dynamic viscoelasticity measuring device
  • a combination of amine-based curing agents is suitable for curing the epoxy resin composition.
  • An amine-based curing agent is a compound that contains a nitrogen atom in the molecule and can react with epoxy groups for curing. Without wishing to be bound by theory, it is believed that the combination of amine-based curing agents utilized in the present invention provides high heat resistance and storage stability.
  • components (C) and (D) are used together as curing agents. Said combination provides the FRP material with low temperature curability while simultaneously providing superior compression strength, heat resistance, and storage stability.
  • the suitable amine curing agents for component (C) and (D) are dicyandiamide and diaminodiphenyl sulfone, respectively. Specific illustrative examples of suitable
  • diaminodiphenyl sulfones include, but are not limited to, 4,4'- diaminodiphenyl sulphone (4,4'-DDS) and 3 , 3 '-d ia m i n od i p he ny I sulphone (3,3'-DDS) and combinations thereof.
  • the amount of component (C) may be in the range of 2 to 7phr per lOOphr of total epoxy resin. If the amount is less than 2phr, the heat resistance and mechanical properties of FRP material obtained may be impaired. If the amount is greater than 7phr, the water absorption may be high from unreactive amine and the FRP material obtained may have low compression strength under hot/wet conditions.
  • the amount of component (D) may be in the range of 5 to 30phr per lOOphr of total epoxy resin. If the amount is less than 5phr, the heat resistance and mechanical properties of FRP material obtained may be impaired. If the amount is greater than 30phr, the viscosity of the epoxy resin composition may become too high; the processing and moldability of the FRP material may also be adversely affected.
  • component (C) examples include DICY-7 and DICY-15 (manufactured by Mitsubishi Chemical Corporation) and "Dyhard (registered
  • dicyandiamide 100S (manufactured by AlzChem Trostberg GmbH).
  • a micronized grade of dicyandiamide is utilized in one embodiment of the present invention.
  • These curing agents may be supplied as a powder or can be employed in the form of a mixture with a liquid epoxy resin composition.
  • Examples of commercially available products suitable for component (D) include "Aradur (registered trademark)” 9664-1 and 9791-1 (manufactured by Huntsman Advanced Materials).
  • any curing agents other than the abovementioned components (C) and (D) may be added to the epoxy resin composition, as long as the effect of the invention is not deteriorated.
  • other curing agents include polyamides, aromatic amidoamines (e.g., aminobenzamides, aminobenzanilides, and aminobenzene sulfonamides), aromatic diamines (e.g., diamino diphenylmethane, and m- phenylenediamine), tertiary amines (e.g., N-N-dimethylaniline, ⁇ , ⁇ -dimethylbenzylamine, and 2,4,6-tris(dimethylaminomethyl) phenol), aminobenzoates (e.g., trimethylene glycol di-p- aminobenzoate and neopentyl glycol di-p-amino-benzoate), aliphatic amines (e.g., diethylenetriamine, triethylenetetramine, is
  • a latent curing agent can be also be used since it makes the storage stability of the epoxy resin composition excellent.
  • a latent curing agent is a curing agent capable of exhibiting activity owing to the phase change or chemical change, etc. caused by certain stimulation such as heat or light.
  • an amine adduct type latent curing agent, microcapsule type latent curing agent, dicyandiamide derivatives, thereof, can be used.
  • An amine adduct type latent curing agent is a product having a high molecular weight and made insoluble at the storage temperature, obtained by reacting an active ingredient such as a compound having a primary, secondary or tertiary amine or any of various imidazole derivatives react with a compound capable of reacting with those compounds.
  • microcapsule type latent curing agent is a product obtained by using a curing agent as a nucleus and covering the nucleus with a shell such as a high molecular substance, for example, an epoxy resin, polyurethane resin, polystyrene-based compound or polyimide, etc., or cyclodextrin, etc., to decrease the contact between the epoxy resin and the curing agent.
  • a dicyandiamide derivative is obtained by combining dicyandiamide with any of various compounds, and a product obtained by reaction with an epoxy resin and a product obtained by reaction with a vinyl compound or acrylic compound, etc. can be enumerated.
  • Examples of commercially available products of the amine adduct type latent curing agent includes: “Amicure (registered Trademark)" PN-23, PN-H, PN-40, PN-50, PN-F, MY-24 and MY-H (manufactured by Ajinomoto Fine-Techno Co., Inc.), "Adeka Hardener (registered trademark)” EH-3293S, EH-3615S and EH- 4070S (manufactured by Adeka Corporation). Examples of
  • microcapsule type latent curing agent examples include "Novacure (registered trademark)" HX-3721 and HX-3722 (manufactured by Asahi Kasei Chemicals Corporation.
  • examples of commercially available products of dicyandiamide derivative include DICY-7 and DICY-15 (manufactured by Japan Epoxy Resins Co., Ltd. Any of the abovementioned curing agents can be used more than two in combination, as long as the effect of the invention is not deteriorated.
  • the relative amounts of curing agent and epoxy resin in the epoxy resin composition are selected such that there is a molar excess of epoxy groups relative to active hydrogens.
  • components (A), (B), (C) and (D) may each be present in an amount effective to provide a molar ratio of active
  • hyd rogens epoxy groups of from 0.4:1 to 0.8:1.
  • Formulations having a ratio lower than 0.4:1 may have low heat resistance and reduced properties, whereas formulations having a ratio higher than 0.8:1 may have lower reactivity and may not reach a high degree of cure at lower temperatures.
  • the epoxy resin composition must be used with at least one curing catalyst to accelerate curing of the epoxy resin composition, so that the capability of achieving a high degree of cure (e.g., at least 90%) at a relatively low temperature (e.g., 132°C) within a short period of time (two hours) is plausible.
  • a high degree of cure e.g., at least 90%
  • a relatively low temperature e.g., 132°C
  • the component (E) is the curing catalyst, wherein the curing catalyst is one or more urea- based compounds that can accelerate the reaction of epoxy resin with any curing agents and/or the self-polymerization of epoxy resin.
  • the epoxy resin composition using urea-based catalysts as the curing catalyst has high storage stability and high heat resistance.
  • the amount of the component (E) may be in the range of 1 to 8phr per lOOphr of total epoxy resin. If the amount is less than lphr, the acceleration effect may be insufficient; the heat
  • the resistance of the FRP material obtained may be impaired. If the amount of is greater than 8phr, the accelerating effect may be excessive, the storage stability of the epoxy resin composition and the mechanical properties of the FRP material obtained may be impaired.
  • Suitable urea-based catalysts include: N,N-dimethyl-N'-(3,4- dichlorophenyl) urea, toluene bis(dimethylurea), 4,4'-methylene bis (phenyl d i methyl u rea ) , N-(4-chlorophenyl) N,N-dimethyl urea and 3-phenyl-l, 1-dimethylurea, and combinations thereof.
  • urea-based catalysts suitable for use as component (E) include: DCMU99 (manufactured by Hodogaya Chemical Co., Ltd.), "Dyhard (registered trademark)" UR200, UR300, UR400, UR500, URAccl3 and URAcc57
  • urea-based catalysts having more than one urea group per molecule may be used in order to attain particularly rapid curing properties.
  • any curing catalyst(s) other than the urea-based catalysts may also be added, as long as the effect of the invention is not deteriorated.
  • curing catalysts include boron trifluoride piperidine, p-t-butylcatechol, sulfonate compounds (e.g., ethyl p-toluenesulfonate, isopropyl p- toluenesu Ifonate or methyl p-toluenesulfonate), tertiary amines and salts thereof, imidazoles and salts thereof, phosphorus curing accelerators, metal carboxylates and Lewis and Bronsted acids and salts thereof.
  • Examples of commercially available imidazole compounds or derivatives thereof include 2MZ, 2PZ and 2E4MZ (manufactured by Shikoku Chemicals Corporation).
  • suitable Lewis acid catalysts include complexes of a boron trihalide and a base, such as a boron trifluoride piperidine complex, boron trifluoride monoethyl amine complex, boron trifluoride triethanol amine complex, or boron trichloride octyl amine complex. Any two or more of the abovementioned curing catalysts can be used in combination as long as the effect of the invention is not
  • the epoxy resin composition comprising the abovementioned components (A)-(E) have a degree of cure (DoC) of at least 90 % after heating at 132°C for 2 hours.
  • DoC degree of cure
  • the DoC of an epoxy resin composition can be determined by Differential Scanning calorimeter (DSC, manufactured by TA Instruments).
  • the DoC value is obtained by empirically comparing the exothermic reaction peak area of an uncured resin (AH unC ure d ) against the residual exothermic reaction peak area of a cured resin (AH cureC i)-
  • An epoxy resin composition may exhibit more than one exothermic reaction peak; in such cases, the total areas of such peaks are compared.
  • the DoC can be calculated by the following formula:
  • ⁇ H cfug red exothermic reaction peak area of an cured resin
  • the epoxy resin composition comprising the abovementioned components (A)-(E) may have a dry Tg (glass transition
  • Said "fully cured" epoxy resin is a cured epoxy resin where the degree of cure degree is 90% or more after
  • the dry Tg refers to the glass transition temperature of a sample being tested without immersion and the wet Tg refers to the glass transition temperature of sample being tested after immersing in boiling water for 24hours. If the wet Tg is less than 115°C, the FRP material will have low heat resistance and low compression strength. In certain embodiments, the cure profile is not particularly limited, as long as the effect of the invention is not deteriorated. If a higher Tg is desired, the epoxy resin composition can be cured at higher temperature. For example, the epoxy resin composition may have a dry Tg of 170°C and a wet Tg of 150°C when the composition is cured at 180°C for 2 hours. The Tg of a cured epoxy resin can be determined by torsional Dynamic Mechanical Analyzer (ARES, manufactured by TA Instruments).
  • ARES torsional Dynamic Mechanical Analyzer
  • thermoplastic resin may be added to the epoxy resin composition, as long as the effect of the invention is not deteriorated. Without wishing to be bound by theory, it is believed that thermoplastic resins provide maximum fracture toughness and impact resistance. Such thermoplastic resins include, but are not limited to, elastomers, branched polymers,
  • thermoplastic resins include thermoplastic resins that are soluble in an epoxy resin and organic particles such as rubber particles and thermoplastic resin particles.
  • a thermoplastic resin having a hydrogen-binding functional group which may have an effect of improving the adhesion between a cured epoxy resin and a reinforcing fiber, may be used.
  • thermoplastic resins having hydroxyl groups examples include polyvinyl acetal resins such as polyvinyl formal and
  • thermoplastic resins having amide bonds include polyamide, polyimide and polyvinyl pyrrolidone.
  • thermoplastic resin having one or more sulfonyl groups is
  • the polyamide, the polyimide and the polysulfone may have a functional group such as an ether bond and a carbonyl group in the main chain thereof.
  • the polyamide may have a substituent on a nitrogen atom in the amide group.
  • thermoplastic resins soluble in an epoxy resin and having a hydrogen-binding functional group examples include: polyvinyl acetal resins such as "Denkabutyral
  • phenoxy resin such as "UCAR (registered trademark)” PKHP (manufactured by Union Carbide Corporation); polyamide resins such as "Macromelt (registered trademark)” (manufactured by Henkel-Hakusui Corporation) and "Amilan (registered
  • polyimides such as "Ultem (registered trademark)" 1000P
  • Suitable polyethersulfones for example, may have a number average molecular weight of from about 10,000 to about 75,000 g/mol.
  • any type(s) of additive(s) may be added, as long as the effect of the present invention is not
  • Rubber particles may be added.
  • the rubber particles crosslinked rubber particles and core-shell rubber particles produced by the graft polymerization of different
  • polymers on the surfaces of crosslinked rubber particles may be used, from the viewpoint of handling properties.
  • crosslinked rubber particles examples include FX501P (manufactured by Japan Synthetic Rubber Corporation), which comprises a crosslinked product of a carboxyl- modified butadiene-acrylonitrile copolymer, and CX-MN series (manufactured by Nippon Shokubai Co., Ltd.) and YR-500 series (manufactured by Nippon Steel Chemical Co., Ltd.), each of which comprises acrylic rubber microparticles.
  • FX501P manufactured by Japan Synthetic Rubber Corporation
  • CX-MN series manufactured by Nippon Shokubai Co., Ltd.
  • YR-500 series manufactured by Nippon Steel Chemical Co., Ltd.
  • Examples of commercially available core-shell rubber particle products include "Paraloid (registered trademark)” EXL-2655
  • the acrylic resin has high incompatibility with an epoxy resin, and therefore may be used suitably for controlling viscoelasticity .
  • Examples of commercially available acrylic resin products include "Dianal (registered trademark)" BR series (manufactured by
  • thermoplastic resin particles polyamide particles and polyimide particles may be used.
  • Polyamide particles are most preferable for greatly increasing the impact resistance due to their excellent toughness.
  • nylon 12 nylon 11, nylon 6, nylon 6/12 copolymer, and a nylon (semi-IPN nylon) modified to have a semi-IPN (interpenetrating polymer network) with an epoxy compound as disclosed in Example 1 of Japanese Patent Application Laid-open No. 1-104624 impart particularly good adhesive strength in combination with the epoxy resin.
  • suitable commercially available polyamide particles include SP-500 (manufactured by Toray Industries Inc.) and
  • any type of inorganic particle such as clay may be added, as long as the effect of the present invention is not deteriorated.
  • suitable inorganic particles include metallic oxide particles, metallic particles and mineral particles.
  • the inorganic particles may be used to improve some functions of the cured epoxy resin composition and to impart one or more functions to the cured epoxy resin composition. Examples of such functions include surface hardness, anti-blocking property, heat resistance, barrier property, conductivity, antistatic property, electromagnetic wave absorption, UV shield, toughness, impact resistance, and low coefficient of linear thermal expansion.
  • Examples of other suitable inorganic materials include aluminum hydroxide, magnesium hydroxide, glass beads, glass flakes and glass balloons.
  • suitable metallic oxides include silicon oxide, titanium oxide, zirconium oxide, zinc oxide, tin oxide, indium oxide, aluminum oxide, antimony oxide, cerium oxide, magnesium oxide, iron oxide, tin-doped indium oxide (ITO), antimony-doped tin oxide and fluorine-doped tin oxide.
  • suitable metals include gold, silver, copper, aluminum, nickel, iron, zinc and stainless.
  • suitable minerals include montmorillonite, talc, mica, boehmite, kaoline, smectite, xonotlite, vermiculite and sericite.
  • Examples of other suitable carbonaceous materials include carbon black, acetylene black, Ketjen black, carbon nanotubes, graphenes, carbon nanofibers, carbon nanobeads, fullerenes, etc.
  • any size of inorganic particles may be used; for example, the inorganic particles may have a size which is in the range of 1 nm to 10 ⁇ .
  • Any shape inorganic particles may be used; for example, the inorganic particles may be spherical, needle, plate, balloon or hollow in shape.
  • the inorganic particles may be just used as powder or used as a dispersion in a solvent like sol or colloid.
  • the surface of the inorganic particle may be treated by a coupling agent to improve the dispersibility and the
  • the epoxy resin composition may contain one or more other materials in addition to the
  • Examples of other materials include mold release agents, surface treatment agents, flame retardants, antibacterial agents, leveling agents, antifoaming agents,
  • thixotropic agents heat stabilizers, light stabilizers, UV absorbers, pigments, coupling agents and metal alkoxides.
  • the components of the epoxy resin composition may be mixed in a kneader, planetary mixer, triple roll mill, twin screw extruder, and the like.
  • the epoxy resins and any thermoplastic resins, excluding curing agents and catalysts, are added in the selected equipment.
  • the mixture is then heated to a temperature in the range of 130 to 180°C while being stirred so as to uniformly dissolve the epoxy resins.
  • the mixture is cooled down to a temperature of no more than 100°C, while being stirred, followed by the addition of the curing agent and catalysts and kneading to disperse those components.
  • This method may be used to provide an epoxy resin composition with excellent storage stability.
  • a reinforcing fiber there are no specific limitations or restrictions on the type of a reinforcing fiber can be used, as long as the effects of the invention are not deteriorated.
  • examples include glass fibers, carbon fibers, and graphite fibers such as S glass, S-l glass, S-2 glass, S-3 glass, E-glass, L-glass organic fibers such as aramid fibers, boron fibers, metal fibers such as alumina fibers, silicon carbide fibers, tungsten carbide fibers, and natural/bio fibers.
  • Particularly carbon fiber may provide the FRP materials
  • carbon fibers are those from Toray Industries having a standard modulus of about 200-250 GPa (Torayca® T300, T300J, T400H, T600S, T700S, T700G), an intermediate modulus of about 250-300 GPa (Torayca® T800H, T800S, T1000G, T1100G, M30S,
  • M30G or a high modulus of greater than 300 GPa
  • Torayca® M40, M35J, M40J, M46J, M50J, M55J, M60J a high modulus of greater than 300 GPa
  • the form and the arrangement of a layer of reinforcing fibers used are not specifically limited. Any of the forms and spatial arrangements of the reinforcing fibers known in the art such as long fibers in a direction, chopped fibers in random orientation, single tow, narrow tow, woven fabrics, mats, knitted fabrics, and braids may be employed.
  • the term "long fiber” as used herein refers to a single fiber that is substantially continuous over 10 mm or longer or a fiber bundle comprising the single fibers.
  • short fibers refers to a fiber bundle comprising fibers that are cut into lengths of shorter than 10 mm.
  • a form wherein a reinforcing fiber bundle is arranged in one direction may be most suitable.
  • a clothlike (woven fabric) form is also suitable for the present invention.
  • the FRP materials of the present invention may be any FRP materials of the present invention.
  • the resin transfer molding method is a method in which a reinforcing fiber base material is directly impregnated with a liquid thermosetting resin composition and cured. Since this method does not involve an intermediate product, such as a prepreg, it has great potential for molding cost reduction and is advantageously used for the manufacture of structural materials for spacecraft, aircraft, rail vehicles, automobiles, marine vessels and so on.
  • the prepreg lamination and molding method is a method in which a prepreg or prepregs, produced by impregnating a
  • composition is/are formed and/or laminated, followed by the curing of the resin through the application of heat and pressure to the formed and/or laminated prepreg/prepregs to obtain a FRP material .
  • the filament winding method is a method in which one to several tens of reinforcing fiber rovings are drawn together in one direction and impregnated with a thermosetting resin composition as they are wrapped around a rotating metal core (mandrel) under tension at a predetermined angle. After the wraps of rovings reach a predetermined thickness, it is cured and then the metal core is removed.
  • the pultrusion method is a method in which reinforcing fibers are continuously passed through an impregnating tank filled with a liquid thermosetting resin composition to impregnate them with the thermosetting resin composition, followed by a squeeze die and heating die for molding and curing, by continuously drawing them using a tensile machine. Since this method offers the advantage of continuously molding FRP materials, it is used for the
  • FRP materials for fishing rods, rods, pipes, sheets, antennas, architectural structures, and so on.
  • the prepreg lamination and molding method may be used to give excellent stiffness and strength to the FRP materials obtained.
  • Prepregs may contain the epoxy resin composition and reinforcing fibers. Such prepregs may be obtained by
  • Impregnation methods include the wet method and hot melt method (dry method).
  • the wet method is a method in which reinforcing fibers are first immersed in a solution of an epoxy resin composition, created by dissolving the epoxy resin composition in a solvent, such as methyl ethyl ketone or methanol, and retrieved, followed by the removal of the solvent through evaporation via an oven, etc. to impregnate reinforcing fibers with the epoxy resin composition.
  • a solvent such as methyl ethyl ketone or methanol
  • the hot-melt method may be implemented by impregnating reinforcing fibers directly with an epoxy resin composition, made fluid by heating in advance, or by first coating a piece or pieces of release paper or the like with an epoxy resin composition for use as resin film and then placing a film over one or either side of reinforcing fibers as configured into a flat shape, followed by the application of heat and pressure to impregnate the reinforcing fibers with the resin.
  • the hot-melt method may give the prepreg having virtually no residual solvent in it.
  • the prepreg may have a carbon fiber areal weight of between 40 to 350 g/m 2 . If the carbon fiber areal weight is less than 40 g/m 2 , there may be insufficient fiber content, and the FRP material may have low strength. If the carbon fiber areal weight is more than 350 g/m 2 , the drapability of the prepreg may be impaired.
  • the prepreg may also have a resin content of between 20 to 70wt%. If the resin content is less than 20 wt%, the impregnation may be unsatisfactory, creating large number of voids. If the resin content is more than 90 wt%, the FRP mechanical properties will be impaired.
  • Appropriate heat and pressure may be used under the prepreg lamination and molding method, the press molding method, autoclave molding method, bagging molding method, wrapping tape method, internal pressure molding method, or the like.
  • the autoclave molding method is a method in which prepregs are laminated on a tool plate of a predetermined shape and then covered with bagging film, followed by curing, performed through the application of heat and pressure while air is drawn out of the laminate. It may allow precision control of the fiber orientation, as well as providing high-quality molded materials with excellent mechanical characteristics, due to a minimum void content.
  • the pressure applied during the molding process may be 0.3 to 1.0 MPa, while the molding temperature may be in the 90 to 300°C range (in one embodiment of the invention, in the range of 110°C to 150°C, e.g., 120°C to 140°C).
  • the wrapping tape method is a method in which prepregs are wrapped around a mandrel or some other cored bar to form a tubular FRP material. This method may be used to produce golf shafts, fishing poles and other rod-shaped products. In more concrete terms, the method involves the wrapping of prepregs around a mandrel, wrapping of wrapping tape made of
  • thermoplastic film over the prepregs under tension for the purpose of securing the prepregs and applying pressure to them.
  • the cored bar is removed to obtain the tubular body.
  • the tension used to wrap the wrapping tape may be 20 to 100 N.
  • the curing temperature may be in the 80 to 300°C range (in one embodiment of the invention, in the range of 110°C to 150°C, e.g., 120°C to 140°C).
  • the internal pressure forming method is a method in which a preform obtained by wrapping prepregs around a thermoplastic resin tube or some other internal pressure applicator is set inside a metal mold, followed by the introduction of high pressure gas into the internal pressure applicator to apply pressure,
  • the pressure applied during the molding process may be 0.1 to 2.0 MPa.
  • the molding temperature may be between room temperature and 300°C or in the 180 to 275°C range (in one embodiment of the invention, in the range of 110°C to 150°C, e.g., 120°C to 140°C).
  • the FRP materials that contain cured epoxy resin that contain cured epoxy resin
  • compositions obtained from epoxy resin compositions of the present invention and reinforcing fibers are advantageously used in general industrial applications, and aeronautics and space applications.
  • the FRP materials may also be used in other
  • sports applications such as sports applications (e.g., golf shafts, fishing rods, tennis or badminton rackets, hockey sticks and ski poles) and structural materials for vehicles (e.g., automobiles, bicycles, marine vessels and rail vehicles, drive shafts, leaf springs, windmill blades, pressure vessels, flywheels, papermaking rollers, roofing materials, cables, and repair/reinforcement materials).
  • structural materials for vehicles e.g., automobiles, bicycles, marine vessels and rail vehicles, drive shafts, leaf springs, windmill blades, pressure vessels, flywheels, papermaking rollers, roofing materials, cables, and repair/reinforcement materials.
  • HP-4770 manufactured by Dainippon Ink and
  • Naphthalene-based epoxy resin "NC-7000L” (manufactured by Nippon Kayaku) having an epoxide equivalent weight (EEW) of 230 g/eq.
  • MY0816 manufactured by Huntsman Advanced Materials having a single naphthalene moiety per molecule and an epoxide equivalent weight (EEW) of 150 g/eq.
  • VW10700RFP polyethersulfone manufactured by Solvay Advanced Polymers having a number average molecular weight of 21,000 g/mol .
  • Plain Weave Carbon fiber "Torayca (registered trademark)" T700S-12K-50C having a fiber filament count of 12,000, tensile strength of 4.9 GPa, tensile elasticity of 230 GPa, and tensile elongation of 2.0% (manufactured by Toray Industries Inc.).
  • a mixture was created by dissolving prescribed amounts of all the components other than the curing agent and curing accelerator in a mixer, and then prescribed amounts of the curing agent were mixed into the mixture along with prescribed amounts of the accelerator to obtain the epoxy resin composition.
  • the cured epoxy resin composition was molded by the following method described in this section. After mixing, the epoxy resin composition prepared in (1) was injected into a mold set for a thickness of 2 mm using a 2 mm-thick "Teflon (registered trademark)" spacer. Then, the epoxy resin composition was heated at a rate of 1.7°C/min from room temperature to 132°C and then kept for 2 hours at 132°C to obtain 2 mm-thick cured epoxy resin composition plates.
  • Teflon registered trademark
  • the epoxy resin composition may be cured to have a certain degree of cure.
  • the percent cure or degree of cure (DoC) of an epoxy resin composition can be determined using a Differential Scanning
  • the degree of cure is empirically determined by comparing the exothermic reaction peak area of an uncured resin (AH uncured ) against the residual exothermic reaction peak area of a cured resin (AH cure( i), using a ramp rate of 10°/min.
  • the uncured resin obtained in (1) was subjected to a dynamic scan with a heating rate of 10°C/min from -50°C to a final temperature at which the exothermic reaction is completed and above which thermal degradation might occur.
  • the cured epoxy resin composition obtained in (2) was subjected to a dynamic scan with a heating rate of 10°C/min from 50°C to a final temperature at which the exothermic reaction is completed and above which thermal degradation might occur.
  • AH uncured exothermic reaction peak area of an uncured resi n
  • the epoxy resin composition may have a certain Tg (glass transition
  • the Tg may be determined using the following method. A specimen measuring 12.5 mm x 50 mm is cut from a cured epoxy resin composition obtained in (2). The specimen is then subjected to measurement of Tg in 1.0 Hz Torsion Mode using a dynamic viscoelasticity measuring device (ARES, manufactured by TA Instruments) by heating it to the temperatures of 50°C to 250°C at a rate of 5°C/min in accordance with SACMA SRM 18R-94.
  • ARES dynamic viscoelasticity measuring device
  • Tg was determined by finding the intersection between the tangent line of the glassy region and the tangent line of the transition region from the glassy region to the rubbery region on the temperature-storage elasticity modulus G' curve, and the temperature at that intersection was considered to be the glass transition temperature (Tg), commonly referred to as G' onset Tg. (5) Water absorption
  • the epoxy resin composition may have a certain water absorption. Water absorption is determined using the following procedure.
  • W t the initial weight of resin before immersion
  • W B the initial weight of resin after immersion
  • the epoxy resin composition may have a certain viscosity at 40°C,
  • viscosity refers to the complex viscoelastic modulus ⁇ * .
  • the viscosity of the epoxy resin composition was measured using a dynamic viscoelasticity measuring device (ARES,
  • the epoxy resin composition may have certain flexural properties. Flexural properties were measured in accordance with the following procedure. A specimen measuring 12.5 mm x 60 mm was cut from the cured epoxy resin composition obtained in (2). Then, the specimen is processed in a 3-point bend flexural test in accordance with ASTM D7264 using an Instron Universal Testing Machine (manufactured by Instron). In the case of room temperature properties, the test specimens are not immersed and are tested at room temperature to obtain the RTD flexural properties of the epoxy resin composition. In the case of hot/wet properties, the specimens are immersed under boiling water for 24 hours. Then the specimens are placed in the pre-heated test chamber at 82°C and held for 3-minute prior to starting the test. The ETW flexural properties of the epoxy resin composition can be obtained from this.
  • the FRP laminate comprising the epoxy resin composition was prepared to test Open Hole
  • the prepreg was cut into 350 mm x 350 mm samples. After layering 16 sheets of the fabric prepreg samples to produce a ( + 45°/0° Warp/-45°/90° Fill) 2S configuration laminate, vacuum bagging was carried out, and the laminate was cured at a rate of 1.7°C/min from room temperature to 132°C under pressure of 0.59 MPa using an autoclave to obtain a quasi- isotropic FRP material.
  • This test specimen was then subjected to open-hole compression testing as prescribed in ASTM-D6484 using an Instron Universal Testing Machine. Measurement was taken at the elevated temperature of 82°C wet (ETW) after immersing at 71°C water for 2 weeks and at room temperature dry (RTD).
  • the FRP laminate comprising the epoxy resin composition was prepared to test 90 ° F i 11 Tensile strength.
  • the prepreg was cut into 300 mm x 300 mm samples. After laying 12 sheets of the fabric prepreg samples to produce a (90°Fill) 12 configuration laminate and cured as described in method (8).
  • This test specimen was then subjected to Tensile testing as prescribed in ASTM-D3039 using an Instron Universal Testing Machine. Measurement was taken at room temperature dry (RTD).
  • RTD room temperature dry
  • compositions shown in Tables 1 and 2 were produced as described in method (1).
  • the properties for each example are stated in Tables 1 and 2. These properties of are achieved with the cure profile described in method (2).
  • a prepreg comprising a reinforcing fiber impregnated with the epoxy resin composition was obtained by the following method.
  • the epoxy resin composition obtained in method (1) was applied onto release paper using a knife coater to produce two sheets of 68.0 g/m 2 resin film.
  • the aforementioned two sheets of fabricated resin film were overlaid on both sides of plain weave carbon fibers (T700S-12K-50C) with a density of 1.8 g/cm 2 in the form of a sheet and the epoxy resin composition was impregnated using a roller temperature of 100 °C and a roller pressure of 0.07 MPa to produce a fabric prepreg with a carbon fiber areal weight of 190 g/m 2 and a resin content of 42wt%.
  • the FRP material was molded as described in method (8).
  • the TS and OHC results for some of the embodiments are stated in Tables 1 and 2.
  • the FRP materials were prepared by the abovementioned methods for working examples 4 and 6 comprising the
  • Vf can be obtained from acid digestion test ASTM D3171-90.
  • Vf can be obtained from acid digestion test ASTM D3171-90.

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Abstract

Les modes de réalisation de l'invention concernent une composition de résine époxy comprenant au moins une résine époxy à base de naphtalène contenant au moins deux fractions de naphtalène et au moins un groupe éther glycidique par molécule, un préimprégné et un matériau composite renforcé par des fibres. Les modes de réalisation de l'invention concernent plus spécifiquement une composition de résine époxy contenant une association de types spécifiques de résines époxy et d'agents de durcissement qui assurent un module de flexion élevé et une faible absorption d'eau, ladite composition étant appropriée pour préparer un matériau composite renforcé par des fibres capable de supporter des environnements d'utilisation extrême. Les modes de réalisation de l'invention concernent par ailleurs des systèmes de résine époxy capables d'atteindre un degré élevé de durcissement (par exemple 90 % ou plus) en un laps de temps relativement court (par exemple deux heures) à une température relativement basse (par exemple 132 °C).
PCT/IB2017/000376 2016-03-24 2017-03-22 Composition de résine époxy, préimprégné, et matériau en plastique renforcé par des fibres WO2017163129A1 (fr)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10472479B2 (en) 2018-02-01 2019-11-12 Hexcel Corporation Prepreg for use in making composite parts which tolerate hot and wet conditions
US10577472B2 (en) 2018-02-01 2020-03-03 Hexcel Corporation Thermoplastic particle-toughened prepreg for use in making composite parts which tolerate hot and wet conditions
EP3751032A1 (fr) * 2019-06-11 2020-12-16 Corex Materials Corporation Tissus tissés par dispersion de fils d'étoupe constitués de composite à matrice polymère et leur procédé de production
CN112739741A (zh) * 2018-09-21 2021-04-30 东丽株式会社 环氧树脂组合物、预浸料坯、以及纤维增强复合材料
EP3766926A4 (fr) * 2018-03-20 2022-01-26 Toray Industries, Inc. Préimprégné et matériau composite renforcé de fibres

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10472479B2 (en) 2018-02-01 2019-11-12 Hexcel Corporation Prepreg for use in making composite parts which tolerate hot and wet conditions
US10577472B2 (en) 2018-02-01 2020-03-03 Hexcel Corporation Thermoplastic particle-toughened prepreg for use in making composite parts which tolerate hot and wet conditions
EP3766926A4 (fr) * 2018-03-20 2022-01-26 Toray Industries, Inc. Préimprégné et matériau composite renforcé de fibres
CN112739741A (zh) * 2018-09-21 2021-04-30 东丽株式会社 环氧树脂组合物、预浸料坯、以及纤维增强复合材料
EP3751032A1 (fr) * 2019-06-11 2020-12-16 Corex Materials Corporation Tissus tissés par dispersion de fils d'étoupe constitués de composite à matrice polymère et leur procédé de production

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