CN111410817A - Epoxy resin composition, preparation method and application thereof in hot-melt prepreg - Google Patents
Epoxy resin composition, preparation method and application thereof in hot-melt prepreg Download PDFInfo
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- CN111410817A CN111410817A CN201911389498.4A CN201911389498A CN111410817A CN 111410817 A CN111410817 A CN 111410817A CN 201911389498 A CN201911389498 A CN 201911389498A CN 111410817 A CN111410817 A CN 111410817A
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- 239000003822 epoxy resin Substances 0.000 title claims abstract description 107
- 229920000647 polyepoxide Polymers 0.000 title claims abstract description 107
- 239000012943 hotmelt Substances 0.000 title claims abstract description 54
- 239000000203 mixture Substances 0.000 title claims abstract description 53
- 238000002360 preparation method Methods 0.000 title claims abstract description 7
- 229920005989 resin Polymers 0.000 claims abstract description 32
- 239000011347 resin Substances 0.000 claims abstract description 32
- 239000003795 chemical substances by application Substances 0.000 claims abstract description 16
- 239000004831 Hot glue Substances 0.000 claims abstract description 11
- 229920005992 thermoplastic resin Polymers 0.000 claims abstract description 9
- 239000004744 fabric Substances 0.000 claims abstract description 4
- 239000012783 reinforcing fiber Substances 0.000 claims abstract description 4
- 239000011159 matrix material Substances 0.000 claims description 21
- PXKLMJQFEQBVLD-UHFFFAOYSA-N bisphenol F Chemical compound C1=CC(O)=CC=C1CC1=CC=C(O)C=C1 PXKLMJQFEQBVLD-UHFFFAOYSA-N 0.000 claims description 18
- QGBSISYHAICWAH-UHFFFAOYSA-N dicyandiamide Chemical compound NC(N)=NC#N QGBSISYHAICWAH-UHFFFAOYSA-N 0.000 claims description 13
- 238000000227 grinding Methods 0.000 claims description 11
- GYZLOYUZLJXAJU-UHFFFAOYSA-N diglycidyl ether Chemical compound C1OC1COCC1CO1 GYZLOYUZLJXAJU-UHFFFAOYSA-N 0.000 claims description 9
- 229920002037 poly(vinyl butyral) polymer Polymers 0.000 claims description 8
- 239000004695 Polyether sulfone Substances 0.000 claims description 3
- 229920006393 polyether sulfone Polymers 0.000 claims description 3
- 239000000126 substance Substances 0.000 claims description 3
- DGUJJOYLOCXENZ-UHFFFAOYSA-N 4-[2-[4-(oxiran-2-ylmethoxy)phenyl]propan-2-yl]phenol Chemical compound C=1C=C(OCC2OC2)C=CC=1C(C)(C)C1=CC=C(O)C=C1 DGUJJOYLOCXENZ-UHFFFAOYSA-N 0.000 claims description 2
- 239000011248 coating agent Substances 0.000 claims description 2
- 238000000576 coating method Methods 0.000 claims description 2
- 239000004843 novolac epoxy resin Substances 0.000 claims description 2
- AFEQENGXSMURHA-UHFFFAOYSA-N oxiran-2-ylmethanamine Chemical compound NCC1CO1 AFEQENGXSMURHA-UHFFFAOYSA-N 0.000 claims description 2
- 238000003756 stirring Methods 0.000 claims description 2
- 229920002554 vinyl polymer Polymers 0.000 claims description 2
- 238000013329 compounding Methods 0.000 claims 1
- 239000002131 composite material Substances 0.000 abstract description 18
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 abstract description 2
- 229910052760 oxygen Inorganic materials 0.000 abstract description 2
- 239000001301 oxygen Substances 0.000 abstract description 2
- 230000009257 reactivity Effects 0.000 abstract description 2
- ITZGNPZZAICLKA-UHFFFAOYSA-N bis(oxiran-2-ylmethyl) 7-oxabicyclo[4.1.0]heptane-3,4-dicarboxylate Chemical compound C1C2OC2CC(C(=O)OCC2OC2)C1C(=O)OCC1CO1 ITZGNPZZAICLKA-UHFFFAOYSA-N 0.000 description 8
- 238000003860 storage Methods 0.000 description 8
- 238000010438 heat treatment Methods 0.000 description 7
- 229920003002 synthetic resin Polymers 0.000 description 7
- 239000000057 synthetic resin Substances 0.000 description 7
- 229920000049 Carbon (fiber) Polymers 0.000 description 6
- 239000004917 carbon fiber Substances 0.000 description 6
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 238000000465 moulding Methods 0.000 description 6
- 238000004321 preservation Methods 0.000 description 6
- XSQUKJJJFZCRTK-UHFFFAOYSA-N Urea Chemical compound NC(N)=O XSQUKJJJFZCRTK-UHFFFAOYSA-N 0.000 description 5
- 150000001299 aldehydes Chemical class 0.000 description 5
- 239000004202 carbamide Substances 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 3
- XXOYNJXVWVNOOJ-UHFFFAOYSA-N fenuron Chemical compound CN(C)C(=O)NC1=CC=CC=C1 XXOYNJXVWVNOOJ-UHFFFAOYSA-N 0.000 description 3
- 238000005507 spraying Methods 0.000 description 3
- 125000002723 alicyclic group Chemical group 0.000 description 2
- 125000003118 aryl group Chemical group 0.000 description 2
- 206010040844 Skin exfoliation Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- UHZZMRAGKVHANO-UHFFFAOYSA-M chlormequat chloride Chemical compound [Cl-].C[N+](C)(C)CCCl UHZZMRAGKVHANO-UHFFFAOYSA-M 0.000 description 1
- 239000000805 composite resin Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 125000005843 halogen group Chemical group 0.000 description 1
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
Classifications
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L63/00—Compositions of epoxy resins; Compositions of derivatives of epoxy resins
-
- 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
- C08G59/68—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
- C08J5/24—Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
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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
- C08J2363/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
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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
- C08J2429/00—Characterised by the use of homopolymers or copolymers of compounds having one or more unsaturated aliphatic radicals, each having only one carbon-to-carbon double bond, and at least one being terminated by an alcohol, ether, aldehydo, ketonic, acetal, or ketal radical; Hydrolysed polymers of esters of unsaturated alcohols with saturated carboxylic acids; Derivatives of such polymer
- C08J2429/14—Homopolymers or copolymers of acetals or ketals obtained by polymerisation of unsaturated acetals or ketals or by after-treatment of polymers of unsaturated alcohols
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- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
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- C08J2463/00—Characterised by the use of epoxy resins; Derivatives of epoxy resins
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- 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
- C08J2481/00—Characterised by the use of macromolecular compounds obtained by reactions forming in the main chain of the macromolecule a linkage containing sulfur with or without nitrogen, oxygen, or carbon only; Polysulfones; Derivatives of such polymers
- C08J2481/06—Polysulfones; Polyethersulfones
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Abstract
本发明创造涉及一种环氧树脂组合物、制备方法及其在热熔预浸料中的应用,根据复合材料对固化温度、反应活性、工艺性和外观特性的要求,设计中温固化反应平缓的热熔环氧树脂的主体树脂及各个组分的比例,将主体环氧树脂、热塑性树脂、固化剂和促进剂,在一定条件下制备得到满足使用要求的环氧树脂组合物;然采用上述环氧树脂体系进行热熔胶膜的涂制,然后与增强纤维或织物进行复合得到热熔预浸料,采用该热熔环氧树脂制备的复合材料产品的表面外观饱满度和无孔洞。The invention of the invention relates to an epoxy resin composition, a preparation method and its application in hot-melt prepreg. According to the requirements of the composite material for curing temperature, reactivity, processability and appearance characteristics, a medium-temperature curing reaction is designed to be gentle. The main resin of the hot-melt epoxy resin and the proportion of each component, the main epoxy resin, thermoplastic resin, curing agent and accelerator are prepared under certain conditions to obtain an epoxy resin composition that meets the requirements for use; The hot-melt adhesive film is coated with the oxygen resin system, and then compounded with reinforcing fibers or fabrics to obtain a hot-melt prepreg.
Description
技术领域technical field
本发明属于结构复合材料用热熔预浸料制造技术领域,具体涉及一种环氧树脂组合物、制备方法及其在热熔预浸料中的应用。The invention belongs to the technical field of manufacturing hot-melt prepregs for structural composite materials, and particularly relates to an epoxy resin composition, a preparation method and its application in hot-melt prepregs.
背景技术Background technique
树脂基复合材料由于轻质高强的特点,已在航空航天、轨道交通等领域得到大量应用,近年来,大尺寸超厚度的复合材料构件越来越广泛,例如氢气运输复合材料罐体的局部厚度达到210mm,这种大壳体、变厚度结构件对树脂基体和成形工艺要求提出了更为苛刻的要求,如固化过程相对平缓但必须在130℃完成固化、成形制品表面无孔洞,无需额外进行喷涂等。Resin matrix composites have been widely used in aerospace, rail transit and other fields due to their light weight and high strength. Reaching 210mm, this kind of large shell and variable thickness structural parts put forward more stringent requirements for the resin matrix and the forming process. For example, the curing process is relatively gentle but must be cured at 130 °C, and the surface of the formed product has no holes, and no additional processing is required. spraying etc.
现有的中温固化体系多为潜伏型树脂体系,多采用1,1-二甲基-3-苯基脲为促进剂,在90-130℃范围时,潜伏型固化剂迅速被激发,反应放出较大的热量,在成形大尺度大厚度复合材料时需要人为的设置多个保温台阶,但产品质量的一致性仍然不能保证。且目前的树脂体系制造的复合材料产品外观质量经常出现微小的空洞,需要后续进行喷涂工序,由于涂料体系与复合材料界面结合较差,存在随时剥落的风险。The existing medium-temperature curing systems are mostly latent resin systems, and 1,1-dimethyl-3-phenylurea is used as the accelerator. When the temperature is in the range of 90-130 °C, the latent curing agent is rapidly excited and the reaction is released. Larger heat, multiple thermal insulation steps need to be artificially set when forming large-scale and large-thickness composite materials, but the consistency of product quality is still not guaranteed. Moreover, the appearance quality of the composite products manufactured by the current resin system often has tiny voids, which requires a subsequent spraying process. Due to the poor bonding between the coating system and the composite material interface, there is a risk of peeling off at any time.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于克服现有技术的上述缺陷,提供一种中温固化低放热的环氧树脂组合物。The purpose of the present invention is to overcome the above-mentioned defects of the prior art, and to provide a medium-temperature curing and low exothermic epoxy resin composition.
本发明的另外一个目的在于提供一种中温固化低放热的热熔环氧树脂组合物的制备方法。Another object of the present invention is to provide a preparation method of a medium-temperature curing and low exothermic hot-melt epoxy resin composition.
本发明的再一个目的在于提供包含该热熔环氧树脂组合物的热熔预浸料。Still another object of the present invention is to provide a hot-melt prepreg comprising the hot-melt epoxy resin composition.
本发明的上述目的主要是通过如下技术方案予以实现的:The above-mentioned purpose of the present invention is mainly achieved through the following technical solutions:
本发明技术方案是:根据复合材料对固化温度、反应活性、工艺性和外观特性的要求,设计中温固化反应平缓的热熔环氧树脂的主体树脂及各个组分的比例,将主体环氧树脂、热塑性树脂、固化剂和促进剂,在一定条件下制备得到满足使用要求的热熔环氧树脂。采用上述环氧树脂体系进行热熔胶膜的涂制,然后与增强纤维或织物进行复合得到热熔预浸料。The technical scheme of the present invention is: according to the requirements of the composite material for curing temperature, reactivity, manufacturability and appearance characteristics, the main resin and the proportion of each component of the hot-melt epoxy resin with gentle curing reaction at medium temperature are designed, and the main epoxy resin is , thermoplastic resin, curing agent and accelerator, under certain conditions, a hot-melt epoxy resin that meets the requirements of use can be prepared. The hot-melt adhesive film is coated with the above epoxy resin system, and then compounded with reinforcing fibers or fabrics to obtain a hot-melt prepreg.
本发明的具体方法是:The concrete method of the present invention is:
(1)将主体环氧树脂中的多官能环氧树脂与热塑性树脂在100-150℃溶解,保温搅拌30-120min至均已透明状态,得到组分A;(1) Dissolving the multifunctional epoxy resin and thermoplastic resin in the main epoxy resin at 100-150° C., stirring for 30-120 minutes at a temperature until both are transparent, and obtaining component A;
(2)将主体环氧树脂中的低粘度环氧树脂与固化剂、促进剂按比例加入预混合,通过三辊研磨设备研磨20-40min,得到组分B;(2) adding the low-viscosity epoxy resin in the main epoxy resin, the curing agent and the accelerator in proportion to premix, and grinding by three-roll grinding equipment for 20-40min to obtain component B;
(3)将(1)中的组分A和(2)中的组分B在60-90℃进行共混10-40min得到中温固化低放热的热熔环氧树脂组合物。(3) The component A in (1) and the component B in (2) are blended at 60-90° C. for 10-40 minutes to obtain a medium-temperature curing and low exothermic hot-melt epoxy resin composition.
具体地,所述主体环氧树脂、热塑性树脂、固化剂、促进剂的质量百分含量分别为74%-92%:4%-16%:2.3%-8.6%:0.8%-4.4%,且上述各组分的百分含量之和为100%。当各组分按照上述比例配比时,既能保证树脂体系在中温范围内平缓固化完全,又能保证采用上述树脂制备的复合材料制品表面无孔洞和无需喷涂等。Specifically, the mass percentages of the main epoxy resin, thermoplastic resin, curing agent, and accelerator are respectively 74%-92%: 4%-16%: 2.3%-8.6%: 0.8%-4.4%, and The sum of the percentages of the above components is 100%. When each component is proportioned according to the above ratio, it can not only ensure that the resin system is completely cured in a medium temperature range, but also ensure that the surface of the composite product prepared with the above resin has no holes and no need to spray.
其中,所述主体环氧树脂为低粘度环氧树脂和多官能环氧树脂的混合物,优选地,低粘度环氧树脂与多官能环氧树脂的质量比为10:90-90:10;Wherein, the main epoxy resin is a mixture of low viscosity epoxy resin and multifunctional epoxy resin, preferably, the mass ratio of low viscosity epoxy resin to multifunctional epoxy resin is 10:90-90:10;
所述低粘度环氧树脂为双酚A缩水甘油醚(DYD128,岳阳石化树脂厂)、双酚F缩水甘油醚(830s,无锡树脂厂)中的一种或其组合;The low-viscosity epoxy resin is one of bisphenol A glycidyl ether (DYD128, Yueyang Petrochemical Resin Factory) and bisphenol F glycidyl ether (830s, Wuxi Resin Factory) or a combination thereof;
所述多官能环氧树脂为缩水甘油胺(AG-80,市售)、酚醛型环氧树脂(638s,市售)、多官能缩水甘油酯脂环族环氧树脂(TDE-85,市售)中的一种或其组合;The multifunctional epoxy resins are glycidylamine (AG-80, commercially available), novolac epoxy resin (638s, commercially available), multifunctional glycidyl ester alicyclic epoxy resin (TDE-85, commercially available) ), or a combination thereof;
所述热塑性树脂为在环氧树脂中可以溶解的热塑性塑料,优选为聚乙烯醇缩甲醛、聚乙烯醇缩丁醛、聚醚砜中的一种或几种的组合,采用上述热塑性树脂可以保证后续复合材料制品的外观平整无孔洞;The thermoplastic resin is a thermoplastic that can be dissolved in an epoxy resin, preferably one or a combination of polyvinyl formal, polyvinyl butyral, and polyethersulfone. The appearance of the subsequent composite products is smooth without holes;
所述固化剂为双氰胺(Dicy,市售)或改性双氰胺(HT2833,市售)的一种或其组合;Described curing agent is a kind of or its combination of dicyandiamide (Dicy, commercially available) or modified dicyandiamide (HT2833, commercially available);
所述促进剂为具有以下化学结构IA(Ecure20,市售)和IB(UR800,市售)的组合物,优选地,IA:IB组合物的质量比为1:0.2~1:1.0,即可以保证热熔环氧树脂体系可以在中温范围内完成固化,同时由于特殊的化学结构,反应放热平缓。The accelerator is a composition with the following chemical structures IA (Ecure20, commercially available) and IB (UR800, commercially available). Preferably, the mass ratio of the IA:IB composition is 1:0.2 to 1:1.0, that is, It is guaranteed that the hot melt epoxy resin system can be cured in the medium temperature range, and at the same time, due to the special chemical structure, the reaction exotherm is gentle.
采用上述热熔环氧树脂组合物作为树脂基体进行热熔胶膜的涂制,与然后与增强纤维或织物进行复合制备得到热熔预浸料。其中,上述热熔预浸料中树脂基体的百分比质量含量为30%~40%。Using the above-mentioned hot-melt epoxy resin composition as a resin matrix to coat a hot-melt adhesive film, and then compound it with reinforcing fibers or fabrics to prepare a hot-melt prepreg. Wherein, the percentage mass content of the resin matrix in the hot-melt prepreg is 30% to 40%.
按照上述方法制备得到的中温固化的热熔环氧树脂组合物及热熔预浸料在制备树脂基复合材料中的应用,也属于本发明的保护范围。The application of the medium-temperature-cured hot-melt epoxy resin composition and the hot-melt prepreg prepared according to the above method in the preparation of resin-based composite materials also belongs to the protection scope of the present invention.
本发明创造的有益效果:Beneficial effects created by the present invention:
(1)本发明提供的热熔环氧树脂组合物,采用芳香族脲类(IA)和脂环族脲类(IB)两种促进剂混用,其中,IA芳香族脲含有卤原子的吸电子诱导效应,使得在双氰胺存在时催化活性较1,1-二甲基-3-苯基脲降低;IB为脂环族脲类,作为双氰胺的催化剂时固化更为平缓且可赋予预浸料更多的贮存周期,即可保证树脂体系在90-130℃可以固化又能保证低的反应放热量和固化平缓难以兼备的技术难题,最终获得了中温固化低放热的热熔环氧树脂体系。(1) The hot-melt epoxy resin composition provided by the present invention adopts two kinds of accelerators, aromatic urea (IA) and alicyclic urea (IB), to be mixed, wherein, the IA aromatic urea contains electron-withdrawing halogen atoms. Induction effect, which makes the catalytic activity lower than that of 1,1-dimethyl-3-phenylurea in the presence of dicyandiamide; IB is an alicyclic urea, which cures more gently and can impart More storage periods of prepreg can ensure that the resin system can be cured at 90-130 ° C, and can ensure low reaction heat and smooth curing. Oxygen resin system.
(2)本发明提供的热熔环氧树脂组合物采用特定热塑性树脂溶解改性,在室温下具有良好的贴合性,且采用该热熔环氧树脂组合物制备的复合材料产品的表面外观饱满度和无孔洞。(2) The hot-melt epoxy resin composition provided by the present invention is dissolved and modified by a specific thermoplastic resin, has good adhesion at room temperature, and the surface appearance of the composite product prepared by using the hot-melt epoxy resin composition Fullness and no holes.
(3)本发明提供的热熔环氧树脂组合物及其预浸料已经在大型超尺寸复合材料制品中得到应用,产品表面无需进行二次喷涂即可满足指标要求。(3) The hot-melt epoxy resin composition and its prepreg provided by the present invention have been used in large and super-sized composite products, and the surface of the product can meet the index requirements without secondary spraying.
具体实施方式Detailed ways
需要说明的是,在不冲突的情况下,本发明创造中的实施例及实施例中的特征可以相互组合。It should be noted that the embodiments of the present invention and the features of the embodiments may be combined with each other under the condition of no conflict.
实施例1Example 1
步骤(1):将主体环氧树脂中的多官能缩水甘油酯脂环族环氧树脂(TDE-85,天津晶东化学有限公司)17.1kg加热到120℃熔化,加入1kg聚乙烯醇缩丁醛,保温30-90min至完全溶解透明状态,得到组分A;Step (1): 17.1 kg of the polyfunctional glycidyl ester alicyclic epoxy resin (TDE-85, Tianjin Jingdong Chemical Co., Ltd.) in the main epoxy resin was heated to 120° C. to melt, and 1 kg of polyvinyl butyral was added. Aldehyde, heat preservation for 30-90min to completely dissolved and transparent state to obtain component A;
步骤(2):将主体环氧树脂中的低粘度环氧树脂双酚F缩水甘油醚(830s,上海合成树脂厂)3.1kg与固化剂(改性双氰胺,HT2833,市售)1kg、促进剂(IA:IB=5:1)0.24kg份按比例加入预混合,通过三辊研磨设备研磨40min,得到组分B;Step (2): 3.1kg of low-viscosity epoxy resin bisphenol F glycidyl ether (830s, Shanghai Synthetic Resin Factory) in the main epoxy resin and 1kg of curing agent (modified dicyandiamide, HT2833, commercially available), 0.24kg of accelerator (IA:IB=5:1) was added in proportion to premix, and ground for 40min by three-roll grinding equipment to obtain component B;
步骤(3):将(1)中的组分A和(2)中的组分B在70℃进行共混30min得到中温固化低放热的热熔环氧树脂组合物。Step (3): The component A in (1) and the component B in (2) are blended at 70° C. for 30 minutes to obtain a medium-temperature curing and low exothermic hot-melt epoxy resin composition.
采用上述热熔环氧树脂组合物作为树脂基体进行热熔胶膜的涂制,然后与T300碳纤维进行复合得到热熔预浸料,控制树脂基体质量百分含量为36%。The hot-melt epoxy resin composition was used as the resin matrix to coat the hot-melt adhesive film, and then compounded with T300 carbon fiber to obtain a hot-melt prepreg, and the mass percentage of the resin matrix was controlled to be 36%.
采用DSC(DSC2500,TA公司)进行10℃/min升温速率扫描,扫描反应放热为150J/g。采用上述热熔环氧树脂组合物及其预浸料制备的复合材料制品表面无孔洞,外观平整,成型质量良好。预浸料贮存周期为60天。A DSC (DSC2500, TA company) was used to scan at a heating rate of 10°C/min, and the reaction exotherm was 150 J/g. The composite material product prepared by using the above-mentioned hot-melt epoxy resin composition and its prepreg has no holes on the surface, smooth appearance and good molding quality. The prepreg storage period is 60 days.
实施例2Example 2
步骤(1):将主体环氧树脂中的多官能缩水甘油酯脂环族环氧树脂(TDE-85,天津晶东化学有限公司)17.5kg加热到120℃熔化,加入2kg聚乙烯醇缩丁醛,保温30-90min至完全溶解透明状态,得到组分A;Step (1): 17.5kg of polyfunctional glycidyl ester alicyclic epoxy resin (TDE-85, Tianjin Jingdong Chemical Co., Ltd.) in the main epoxy resin was heated to 120° C. to melt, and 2kg of polyvinyl butyral was added. Aldehyde, heat preservation for 30-90min to completely dissolved and transparent state to obtain component A;
步骤(2):将主体环氧树脂中的低粘度环氧树脂双酚F缩水甘油醚(830s,上海合成树脂厂)3kg份与固化剂(双氰胺,市售)1.6kg份、促进剂(IA:IB=4:1)0.4kg按比例加入预混合,通过三辊研磨设备研磨40min,得到组分B;Step (2): 3kg parts of low-viscosity epoxy resin bisphenol F glycidyl ether (830s, Shanghai Synthetic Resin Factory) in the main epoxy resin, 1.6kg parts of curing agent (dicyandiamide, commercially available), accelerator (IA:IB=4:1) 0.4kg was added to the premix in proportion, and ground for 40min by three-roll grinding equipment to obtain component B;
步骤(3):将(1)中的组分A和(2)中的组分B在70℃进行共混30min得到中温固化低放热的热熔环氧树脂组合物。Step (3): The component A in (1) and the component B in (2) are blended at 70° C. for 30 minutes to obtain a medium-temperature curing and low exothermic hot-melt epoxy resin composition.
采用上述热熔环氧树脂组合物作为树脂基体进行热熔胶膜的涂制,然后与EW400玻璃纤维进行复合得到热熔预浸料,控制树脂基体质量百分含量为36%。The hot-melt epoxy resin composition was used as the resin matrix to coat the hot-melt adhesive film, and then compounded with EW400 glass fiber to obtain a hot-melt prepreg, and the mass percentage of the resin matrix was controlled to be 36%.
采用DSC(DSC2500,TA公司)进行10℃/min升温速率扫描,扫描反应放热为170J/g。采用上述热熔环氧树脂组合物及其预浸料制备的复合材料制品表面无孔洞,外观平整,成型质量良好。预浸料贮存周期为60天。A DSC (DSC2500, TA company) was used to scan at a heating rate of 10°C/min, and the reaction exotherm was 170 J/g. The composite material product prepared by using the above-mentioned hot-melt epoxy resin composition and its prepreg has no holes on the surface, smooth appearance and good molding quality. The prepreg storage period is 60 days.
实施例3Example 3
步骤(1):将主体环氧树脂中的多官能缩水甘油酯脂环族环氧树脂(TDE-85,天津晶东化学有限公司)18kg加热到120℃熔化,加入1kg聚乙烯醇缩丁醛,保温30-90min至完全溶解透明状态,得到组分A;Step (1): 18kg of the polyfunctional glycidyl ester alicyclic epoxy resin (TDE-85, Tianjin Jingdong Chemical Co., Ltd.) in the main epoxy resin was heated to 120°C to melt, and 1kg of polyvinyl butyral was added. , heat preservation for 30-90min to completely dissolved and transparent state to obtain component A;
步骤(2):将主体环氧树脂中的低粘度环氧树脂双酚F缩水甘油醚(830s,上海合成树脂厂)3kg与固化剂(双氰胺,市售)2kg、促进剂(IA:IB=3:1)0.48kg按比例加入预混合,通过三辊研磨设备研磨40min,得到组分B;Step (2): 3kg of low-viscosity epoxy resin bisphenol F glycidyl ether (830s, Shanghai Synthetic Resin Factory) in the main epoxy resin, 2kg of curing agent (dicyandiamide, commercially available), accelerator (IA: IB=3:1) 0.48kg was added in proportion to premix, and ground for 40min by three-roll grinding equipment to obtain component B;
步骤(3):将(1)中的组分A和(2)中的组分B在70℃进行共混30min得到中温固化低放热的热熔环氧树脂组合物。Step (3): The component A in (1) and the component B in (2) are blended at 70° C. for 30 minutes to obtain a medium-temperature curing and low exothermic hot-melt epoxy resin composition.
采用上述热熔环氧树脂组合物作为树脂基体进行热熔胶膜的涂制,然后与T700碳纤维进行复合得到熔预浸料,控制树脂基体质量百分含量为35%。The hot-melt epoxy resin composition was used as the resin matrix to coat the hot-melt adhesive film, and then compounded with T700 carbon fiber to obtain a molten prepreg, and the mass percentage of the resin matrix was controlled to be 35%.
采用DSC(DSC2500,TA公司)进行10℃/min升温速率扫描,扫描反应放热为175J/g。采用上述热熔环氧树脂组合物及其预浸料制备的复合材料制品表面无孔洞,外观平整,成型质量良好。预浸料贮存周期为50天。DSC (DSC2500, TA company) was used to scan at a heating rate of 10°C/min, and the reaction exotherm was 175 J/g. The composite material product prepared by using the above-mentioned hot-melt epoxy resin composition and its prepreg has no holes on the surface, smooth appearance and good molding quality. The prepreg storage period is 50 days.
实施例4Example 4
步骤(1):将主体环氧树脂中的多官能缩水甘油酯脂环族环氧树脂(TDE-85,天津晶东化学有限公司)16.5kg加热到120℃熔化,加入4kg聚醚砜,保温30-90min至完全溶解透明状态,得到组分A;Step (1): 16.5kg of the polyfunctional glycidyl ester alicyclic epoxy resin (TDE-85, Tianjin Jingdong Chemical Co., Ltd.) in the main epoxy resin was heated to 120°C to melt, 4kg of polyethersulfone was added, and the temperature was kept warm. 30-90min to completely dissolved and transparent state to obtain component A;
步骤(2):将主体环氧树脂中的低粘度环氧树脂双酚F缩水甘油醚(830s,上海合成树脂厂)3kg与固化剂(双氰胺,市售)1.25kg、促进剂(IA:IB=2:1)0.65kg按比例加入预混合,通过三辊研磨设备研磨40min,得到组分B;Step (2): 3kg of low-viscosity epoxy resin bisphenol F glycidyl ether (830s, Shanghai Synthetic Resin Factory) in the main epoxy resin, 1.25kg of curing agent (dicyandiamide, commercially available), accelerator (IA : IB=2:1) 0.65kg was added in proportion to pre-mix, and ground for 40min by three-roll grinding equipment to obtain component B;
步骤(3):将(1)中的组分A和(2)中的组分B在70℃进行共混30min得到中温固化低放热的热熔环氧树脂组合物。Step (3): The component A in (1) and the component B in (2) are blended at 70° C. for 30 minutes to obtain a medium-temperature curing and low exothermic hot-melt epoxy resin composition.
采用上述热熔环氧树脂组合物作为树脂基体进行热熔胶膜的涂制,然后与T800碳纤维进行复合得到热熔预浸料,控制树脂基体质量百分含量为34%。The hot-melt epoxy resin composition was used as the resin matrix to coat the hot-melt adhesive film, and then compounded with T800 carbon fiber to obtain a hot-melt prepreg, and the mass percentage of the resin matrix was controlled to be 34%.
采用DSC(DSC2500,TA公司)进行10℃/min升温速率扫描,扫描反应放热为180J/g。采用上述热熔环氧树脂组合物及其预浸料制备的复合材料制品表面无孔洞,外观平整,成型质量良好。预浸料贮存周期为45天。DSC (DSC2500, TA company) was used to scan at a heating rate of 10°C/min, and the reaction exotherm was 180 J/g. The composite material product prepared by using the above-mentioned hot-melt epoxy resin composition and its prepreg has no holes on the surface, smooth appearance and good molding quality. The prepreg storage period is 45 days.
对比例1Comparative Example 1
步骤(1):将主体环氧树脂中的多官能缩水甘油酯脂环族环氧树脂(TDE-85,天津晶东化学有限公司)17.1kg加热到120℃熔化,加入1kg聚乙烯醇缩丁醛,保温30-90min至完全溶解透明状态,得到组分A;Step (1): 17.1 kg of the polyfunctional glycidyl ester alicyclic epoxy resin (TDE-85, Tianjin Jingdong Chemical Co., Ltd.) in the main epoxy resin was heated to 120° C. to melt, and 1 kg of polyvinyl butyral was added. Aldehyde, heat preservation for 30-90min to completely dissolved and transparent state to obtain component A;
步骤(2):将主体环氧树脂中的低粘度环氧树脂双酚F缩水甘油醚(830s,上海合成树脂厂)3.1kg与固化剂(改性双氰胺,市售)1kg、促进剂(1,1二甲基-3-苯基脲)0.24kg加入预混合,通过三辊研磨设备研磨40min,得到组分B;Step (2): 3.1 kg of low-viscosity epoxy resin bisphenol F glycidyl ether (830s, Shanghai Synthetic Resin Factory) in the main epoxy resin, 1 kg of curing agent (modified dicyandiamide, commercially available), accelerator (1,1 dimethyl-3-phenylurea) 0.24kg was added to the premix and ground for 40min by a three-roller grinding device to obtain component B;
步骤(3):将(1)中的组分A和(2)中的组分B在70℃进行共混30min得到中温固化低放热的热熔环氧树脂组合物。Step (3): The component A in (1) and the component B in (2) are blended at 70° C. for 30 minutes to obtain a medium-temperature curing and low exothermic hot-melt epoxy resin composition.
采用上述热熔环氧树脂组合物作为树脂基体进行热熔胶膜的涂制,然后与T300碳纤维进行复合得到热熔预浸料,控制树脂基体质量百分含量为36%。The hot-melt epoxy resin composition was used as the resin matrix to coat the hot-melt adhesive film, and then compounded with T300 carbon fiber to obtain a hot-melt prepreg, and the mass percentage of the resin matrix was controlled to be 36%.
采用DSC(DSC2500,TA公司)进行10℃/min升温速率扫描,扫描反应放热为252J/g。采用上述热熔环氧树脂组合物及其预浸料制备的复合材料制品表面有孔洞,成型质量良可。预浸料贮存周期为20天。A DSC (DSC2500, TA company) was used to scan at a heating rate of 10°C/min, and the reaction exotherm was 252 J/g. The composite material product prepared by using the above-mentioned hot-melt epoxy resin composition and its prepreg has holes on the surface, and the molding quality is good. The prepreg storage period is 20 days.
对比例2Comparative Example 2
步骤(1):将主体环氧树脂中的多官能缩水甘油酯脂环族环氧树脂(TDE-85,天津晶东化学有限公司)17.1kg加热到120℃熔化,加入1kg聚乙烯醇缩丁醛,保温30-90min至完全溶解透明状态,得到组分A;Step (1): 17.1 kg of the polyfunctional glycidyl ester alicyclic epoxy resin (TDE-85, Tianjin Jingdong Chemical Co., Ltd.) in the main epoxy resin was heated to 120° C. to melt, and 1 kg of polyvinyl butyral was added. Aldehyde, heat preservation for 30-90min to completely dissolved and transparent state to obtain component A;
步骤(2):将主体环氧树脂中的低粘度环氧树脂双酚F缩水甘油醚(830s,上海合成树脂厂)3.1kg与固化剂(改性双氰胺,市售)1kg、促进剂(IA)0.24kg加入预混合,通过三辊研磨设备研磨40min,得到组分B;Step (2): 3.1 kg of low-viscosity epoxy resin bisphenol F glycidyl ether (830s, Shanghai Synthetic Resin Factory) in the main epoxy resin, 1 kg of curing agent (modified dicyandiamide, commercially available), accelerator (IA) 0.24kg was added to premix and ground for 40min by three-roll grinding equipment to obtain component B;
步骤(3):将(1)中的组分A和(2)中的组分B在70℃进行共混30min得到中温固化低放热的热熔环氧树脂组合物。Step (3): The component A in (1) and the component B in (2) are blended at 70° C. for 30 minutes to obtain a medium-temperature curing and low exothermic hot-melt epoxy resin composition.
采用上述热熔环氧树脂组合物作为树脂基体进行热熔胶膜的涂制,然后与T300碳纤维进行复合得到热熔预浸料,控制树脂基体质量百分含量为36%。The hot-melt epoxy resin composition was used as the resin matrix to coat the hot-melt adhesive film, and then compounded with T300 carbon fiber to obtain a hot-melt prepreg, and the mass percentage of the resin matrix was controlled to be 36%.
采用DSC(DSC2500,TA公司)进行10℃/min升温速率扫描,扫描反应放热为220J/g。采用上述热熔环氧树脂组合物及其预浸料制备的复合材料制品表面无孔洞,成型质量良可。预浸料贮存周期为30天。A DSC (DSC2500, TA company) was used to scan at a heating rate of 10°C/min, and the reaction exotherm was 220 J/g. The composite material product prepared by using the above-mentioned hot-melt epoxy resin composition and its prepreg has no holes on the surface, and the molding quality is good. The prepreg storage period is 30 days.
对比例3Comparative Example 3
步骤(1):将主体环氧树脂中的多官能缩水甘油酯脂环族环氧树脂(TDE-85,天津晶东化学有限公司)17.1kg加热到120℃熔化,加入1kg聚乙烯醇缩丁醛,保温30-90min至完全溶解透明状态,得到组分A;Step (1): 17.1 kg of the polyfunctional glycidyl ester alicyclic epoxy resin (TDE-85, Tianjin Jingdong Chemical Co., Ltd.) in the main epoxy resin was heated to 120° C. to melt, and 1 kg of polyvinyl butyral was added. Aldehyde, heat preservation for 30-90min to completely dissolved and transparent state to obtain component A;
步骤(2):将主体环氧树脂中的低粘度环氧树脂双酚F缩水甘油醚(830s,上海合成树脂厂)3.1kg与固化剂(改性双氰胺,市售)1kg、促进剂(IB)0.24kg加入预混合,通过三辊研磨设备研磨40min,得到组分B;Step (2): 3.1 kg of low-viscosity epoxy resin bisphenol F glycidyl ether (830s, Shanghai Synthetic Resin Factory) in the main epoxy resin, 1 kg of curing agent (modified dicyandiamide, commercially available), accelerator (IB) 0.24kg was added to premix, and ground for 40min by three-roll grinding equipment to obtain component B;
步骤(3):将(1)中的组分A和(2)中的组分B在70℃进行共混30min得到中温固化低放热的热熔环氧树脂组合物。Step (3): The component A in (1) and the component B in (2) are blended at 70° C. for 30 minutes to obtain a medium-temperature curing and low exothermic hot-melt epoxy resin composition.
采用上述热熔环氧树脂组合物作为树脂基体进行热熔胶膜的涂制,然后与T300碳纤维进行复合得到热熔预浸料,控制树脂基体质量百分含量为36%。The hot-melt epoxy resin composition was used as the resin matrix to coat the hot-melt adhesive film, and then compounded with T300 carbon fiber to obtain a hot-melt prepreg, and the mass percentage of the resin matrix was controlled to be 36%.
采用DSC(DSC2500,TA公司)进行10℃/min升温速率扫描,扫描反应放热为120J/g。采用上述热熔环氧树脂组合物及其预浸料制备的复合材料需要在150℃后处理才能固化,在130℃不能完全固化。预浸料贮存周期为90天。A DSC (DSC2500, TA company) was used to scan at a heating rate of 10°C/min, and the reaction exotherm was 120 J/g. The composite material prepared by using the above hot-melt epoxy resin composition and its prepreg needs to be post-treated at 150° C. to be cured, and cannot be completely cured at 130° C. The prepreg storage period is 90 days.
以上对本发明创造的一个实施例进行了详细说明,但所述内容仅为本发明创造的较佳实施例,不能被认为用于限定本发明创造的实施范围。凡依本发明创造申请范围所作的均等变化与改进等,均应仍归属于本发明创造的专利涵盖范围之内。An embodiment of the present invention has been described in detail above, but the content is only a preferred embodiment of the present invention, and cannot be considered to limit the implementation scope of the present invention. All equivalent changes and improvements made according to the application scope of the invention should still fall within the scope of the invention.
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Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
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JPH02302426A (en) * | 1989-05-17 | 1990-12-14 | Shin Etsu Chem Co Ltd | Epoxy resin composition |
CN101945916A (en) * | 2008-02-26 | 2011-01-12 | 东丽株式会社 | Epoxy resin composition, prepreg, abd fiber-reinforced composite material |
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JPH02302426A (en) * | 1989-05-17 | 1990-12-14 | Shin Etsu Chem Co Ltd | Epoxy resin composition |
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CN113698774A (en) * | 2021-08-27 | 2021-11-26 | 北京理工大学 | Preparation method of polycarbosilane blended resin hot-melt prepreg |
CN113698774B (en) * | 2021-08-27 | 2022-06-21 | 北京理工大学 | A kind of preparation method of polycarbosilane blend resin hot-melt prepreg |
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