CN115160540A - High-modulus high-activity epoxy resin and synthesis method and application thereof - Google Patents
High-modulus high-activity epoxy resin and synthesis method and application thereof Download PDFInfo
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- CN115160540A CN115160540A CN202210952271.1A CN202210952271A CN115160540A CN 115160540 A CN115160540 A CN 115160540A CN 202210952271 A CN202210952271 A CN 202210952271A CN 115160540 A CN115160540 A CN 115160540A
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- 239000003822 epoxy resin Substances 0.000 title claims abstract description 51
- 229920000647 polyepoxide Polymers 0.000 title claims abstract description 51
- 230000000694 effects Effects 0.000 title description 11
- 238000001308 synthesis method Methods 0.000 title description 2
- 239000003795 chemical substances by application Substances 0.000 claims abstract description 46
- 239000000178 monomer Substances 0.000 claims abstract description 28
- 238000006243 chemical reaction Methods 0.000 claims abstract description 9
- 239000000463 material Substances 0.000 claims abstract description 9
- 238000010146 3D printing Methods 0.000 claims abstract description 6
- PISLZQACAJMAIO-UHFFFAOYSA-N 2,4-diethyl-6-methylbenzene-1,3-diamine Chemical compound CCC1=CC(C)=C(N)C(CC)=C1N PISLZQACAJMAIO-UHFFFAOYSA-N 0.000 claims description 21
- 239000004593 Epoxy Substances 0.000 claims description 17
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 claims description 15
- 239000003054 catalyst Substances 0.000 claims description 11
- 239000002131 composite material Substances 0.000 claims description 11
- IBOFVQJTBBUKMU-UHFFFAOYSA-N 4,4'-methylene-bis-(2-chloroaniline) Chemical compound C1=C(Cl)C(N)=CC=C1CC1=CC=C(N)C(Cl)=C1 IBOFVQJTBBUKMU-UHFFFAOYSA-N 0.000 claims description 9
- 150000001412 amines Chemical group 0.000 claims description 9
- 239000003085 diluting agent Substances 0.000 claims description 9
- 238000000034 method Methods 0.000 claims description 8
- WZCQRUWWHSTZEM-UHFFFAOYSA-N 1,3-phenylenediamine Chemical group NC1=CC=CC(N)=C1 WZCQRUWWHSTZEM-UHFFFAOYSA-N 0.000 claims description 6
- BRLQWZUYTZBJKN-UHFFFAOYSA-N Epichlorohydrin Chemical compound ClCC1CO1 BRLQWZUYTZBJKN-UHFFFAOYSA-N 0.000 claims description 6
- AWMVMTVKBNGEAK-UHFFFAOYSA-N Styrene oxide Chemical group C1OC1C1=CC=CC=C1 AWMVMTVKBNGEAK-UHFFFAOYSA-N 0.000 claims description 6
- CHQVQXZFZHACQQ-UHFFFAOYSA-M benzyl(triethyl)azanium;bromide Chemical group [Br-].CC[N+](CC)(CC)CC1=CC=CC=C1 CHQVQXZFZHACQQ-UHFFFAOYSA-M 0.000 claims description 6
- ZZTCPWRAHWXWCH-UHFFFAOYSA-N diphenylmethanediamine Chemical class C=1C=CC=CC=1C(N)(N)C1=CC=CC=C1 ZZTCPWRAHWXWCH-UHFFFAOYSA-N 0.000 claims description 6
- 125000003700 epoxy group Chemical group 0.000 claims description 6
- 229940018564 m-phenylenediamine Drugs 0.000 claims description 6
- MCTWTZJPVLRJOU-UHFFFAOYSA-N 1-methyl-1H-imidazole Chemical group CN1C=CN=C1 MCTWTZJPVLRJOU-UHFFFAOYSA-N 0.000 claims description 5
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 5
- 229910052739 hydrogen Inorganic materials 0.000 claims description 5
- 239000001257 hydrogen Substances 0.000 claims description 5
- 239000011159 matrix material Substances 0.000 claims description 5
- 238000001816 cooling Methods 0.000 claims description 4
- 229910052736 halogen Inorganic materials 0.000 claims description 4
- 125000005843 halogen group Chemical group 0.000 claims description 4
- 150000008065 acid anhydrides Chemical class 0.000 claims description 3
- LTVUCOSIZFEASK-MPXCPUAZSA-N (3ar,4s,7r,7as)-3a-methyl-3a,4,7,7a-tetrahydro-4,7-methano-2-benzofuran-1,3-dione Chemical group C([C@H]1C=C2)[C@H]2[C@H]2[C@]1(C)C(=O)OC2=O LTVUCOSIZFEASK-MPXCPUAZSA-N 0.000 claims description 2
- ZMPZWXKBGSQATE-UHFFFAOYSA-N 3-(4-aminophenyl)sulfonylaniline Chemical compound C1=CC(N)=CC=C1S(=O)(=O)C1=CC=CC(N)=C1 ZMPZWXKBGSQATE-UHFFFAOYSA-N 0.000 claims description 2
- MBMUWELGNWWSKI-UHFFFAOYSA-N 4-(oxiran-2-ylmethoxy)phenol Chemical compound C1=CC(O)=CC=C1OCC1OC1 MBMUWELGNWWSKI-UHFFFAOYSA-N 0.000 claims description 2
- ULKLGIFJWFIQFF-UHFFFAOYSA-N 5K8XI641G3 Chemical compound CCC1=NC=C(C)N1 ULKLGIFJWFIQFF-UHFFFAOYSA-N 0.000 claims description 2
- WPYCRFCQABTEKC-UHFFFAOYSA-N Diglycidyl resorcinol ether Chemical compound C1OC1COC(C=1)=CC=CC=1OCC1CO1 WPYCRFCQABTEKC-UHFFFAOYSA-N 0.000 claims description 2
- FQYUMYWMJTYZTK-UHFFFAOYSA-N Phenyl glycidyl ether Chemical compound C1OC1COC1=CC=CC=C1 FQYUMYWMJTYZTK-UHFFFAOYSA-N 0.000 claims description 2
- LGRFSURHDFAFJT-UHFFFAOYSA-N Phthalic anhydride Natural products C1=CC=C2C(=O)OC(=O)C2=C1 LGRFSURHDFAFJT-UHFFFAOYSA-N 0.000 claims description 2
- 230000009471 action Effects 0.000 claims description 2
- 239000003513 alkali Substances 0.000 claims description 2
- 239000002585 base Substances 0.000 claims description 2
- JHIWVOJDXOSYLW-UHFFFAOYSA-N butyl 2,2-difluorocyclopropane-1-carboxylate Chemical compound CCCCOC(=O)C1CC1(F)F JHIWVOJDXOSYLW-UHFFFAOYSA-N 0.000 claims description 2
- 238000001914 filtration Methods 0.000 claims description 2
- YVWGMAFXEJHFRO-UHFFFAOYSA-N halopropane Chemical compound FC(F)C(F)(F)CBr YVWGMAFXEJHFRO-UHFFFAOYSA-N 0.000 claims description 2
- 229950000188 halopropane Drugs 0.000 claims description 2
- ZZYXNRREDYWPLN-UHFFFAOYSA-N pyridine-2,3-diamine Chemical compound NC1=CC=CN=C1N ZZYXNRREDYWPLN-UHFFFAOYSA-N 0.000 claims description 2
- 239000006228 supernatant Substances 0.000 claims description 2
- 150000008064 anhydrides Chemical class 0.000 claims 1
- CQRYARSYNCAZFO-UHFFFAOYSA-N salicyl alcohol Chemical compound OCC1=CC=CC=C1O CQRYARSYNCAZFO-UHFFFAOYSA-N 0.000 claims 1
- 229920005989 resin Polymers 0.000 abstract description 22
- 239000011347 resin Substances 0.000 abstract description 22
- 238000002360 preparation method Methods 0.000 abstract description 19
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 230000009257 reactivity Effects 0.000 abstract description 5
- 230000000930 thermomechanical effect Effects 0.000 abstract description 5
- 229920006253 high performance fiber Polymers 0.000 abstract description 4
- 239000003733 fiber-reinforced composite Substances 0.000 abstract 1
- 239000000047 product Substances 0.000 description 27
- 230000000052 comparative effect Effects 0.000 description 10
- IAZDPXIOMUYVGZ-UHFFFAOYSA-N Dimethylsulphoxide Chemical compound CS(C)=O IAZDPXIOMUYVGZ-UHFFFAOYSA-N 0.000 description 9
- 241001112258 Moca Species 0.000 description 6
- 229920000642 polymer Polymers 0.000 description 6
- 239000004918 carbon fiber reinforced polymer Substances 0.000 description 5
- XCXKODUKOQLZHO-UHFFFAOYSA-N 3-[(4-hydroxyphenyl)iminomethyl]phenol Chemical compound C1=CC(O)=CC=C1N=CC1=CC=CC(O)=C1 XCXKODUKOQLZHO-UHFFFAOYSA-N 0.000 description 4
- 125000003277 amino group Chemical group 0.000 description 4
- 238000002474 experimental method Methods 0.000 description 4
- 125000004435 hydrogen atom Chemical group [H]* 0.000 description 4
- 238000002156 mixing Methods 0.000 description 4
- 238000006116 polymerization reaction Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 3
- RAXXELZNTBOGNW-UHFFFAOYSA-N imidazole Natural products C1=CNC=N1 RAXXELZNTBOGNW-UHFFFAOYSA-N 0.000 description 3
- 230000002194 synthesizing effect Effects 0.000 description 3
- 229920001187 thermosetting polymer Polymers 0.000 description 3
- LRWZZZWJMFNZIK-UHFFFAOYSA-N 2-chloro-3-methyloxirane Chemical compound CC1OC1Cl LRWZZZWJMFNZIK-UHFFFAOYSA-N 0.000 description 2
- JMFHJQBJQSFWGM-UHFFFAOYSA-N 3,5-dihydroxy-n-(4-hydroxyphenyl)benzamide Chemical group C1=CC(O)=CC=C1NC(=O)C1=CC(O)=CC(O)=C1 JMFHJQBJQSFWGM-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- 238000005033 Fourier transform infrared spectroscopy Methods 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000007809 chemical reaction catalyst Substances 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 239000008367 deionised water Substances 0.000 description 2
- 229910021641 deionized water Inorganic materials 0.000 description 2
- 238000000113 differential scanning calorimetry Methods 0.000 description 2
- 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 2
- 125000002887 hydroxy group Chemical group [H]O* 0.000 description 2
- 239000011259 mixed solution Substances 0.000 description 2
- 239000012299 nitrogen atmosphere Substances 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229920003002 synthetic resin Polymers 0.000 description 2
- 239000000057 synthetic resin Substances 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 238000002411 thermogravimetry Methods 0.000 description 2
- 239000004634 thermosetting polymer Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- NIXOWILDQLNWCW-UHFFFAOYSA-M Acrylate Chemical compound [O-]C(=O)C=C NIXOWILDQLNWCW-UHFFFAOYSA-M 0.000 description 1
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 1
- 238000002679 ablation Methods 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 238000009739 binding Methods 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010292 electrical insulation Methods 0.000 description 1
- 239000012776 electronic material Substances 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000011151 fibre-reinforced plastic Substances 0.000 description 1
- 230000009477 glass transition Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000011031 large-scale manufacturing process Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000010189 synthetic method Methods 0.000 description 1
Images
Classifications
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- 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
- C08G59/28—Di-epoxy compounds containing acyclic nitrogen atoms
-
- C—CHEMISTRY; METALLURGY
- C07—ORGANIC CHEMISTRY
- C07D—HETEROCYCLIC COMPOUNDS
- C07D303/00—Compounds containing three-membered rings having one oxygen atom as the only ring hetero atom
- C07D303/02—Compounds containing oxirane rings
- C07D303/12—Compounds containing oxirane rings with hydrocarbon radicals, substituted by singly or doubly bound oxygen atoms
- C07D303/18—Compounds containing oxirane rings with hydrocarbon radicals, substituted by singly or doubly bound oxygen atoms by etherified hydroxyl radicals
- C07D303/20—Ethers with hydroxy compounds containing no oxirane rings
- C07D303/24—Ethers with hydroxy compounds containing no oxirane rings with polyhydroxy compounds
- C07D303/27—Ethers with hydroxy compounds containing no oxirane rings with polyhydroxy compounds having all hydroxyl radicals etherified with oxirane containing 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
- C08G59/20—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
- C08G59/32—Epoxy compounds containing three or more epoxy groups
- C08G59/3227—Compounds containing acyclic nitrogen atoms
-
- 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
- C08G59/5033—Amines aromatic
-
- 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
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- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Epoxy Resins (AREA)
Abstract
The invention provides a polar epoxy resin monomer containing a typical structure shown in formula I, a synthetic preparation method and a curing system thereof. The polar epoxy resin monomer has high reactivity and can realize rapid curing, and an epoxy resin cured material obtained by the reaction of the polar epoxy resin monomer and a curing agent has high modulus and excellent thermo-mechanical property, and has important application value in the fields of conventional application of epoxy resin, rapid manufacturing of high-performance fiber reinforced composite materials, 3D printing of resin and the like.
Description
Technical Field
The invention belongs to the field of advanced materials, and particularly relates to a high-modulus high-activity epoxy resin, a synthetic method and application thereof.
Background
Due to the characteristics of good processability, excellent adhesive property, mechanical property, electrical insulation property, chemical stability and the like, the epoxy resin is widely applied to pouring and packaging of electronic materials and in coatings, adhesives and composite material matrixes.
When the epoxy resin is used as a matrix of a composite material, the epoxy resin needs a long-time high-temperature curing condition, so that the large-scale production and preparation of the composite material taking the epoxy resin as the matrix are restricted. Currently, high performance fiber reinforced thermoset polymer Composites (CFRP) rely on forming in large, expensive autoclave or oven. For example, the CFRP fuselage of boeing 787 is estimated to require 350 Gigajoules (GJ) of energy in an 8 hour cure cycle and produces over 80 tons of carbon dioxide. Therefore, the fast curing epoxy resin has an important application prospect in the commercial field for the purpose of reducing production energy consumption and manufacturing cost, and has attracted great research interest. In addition, the fast curing epoxy resin has potential application value in the fields of 3D printing and the like, and is beneficial to further widening the application direction of the epoxy resin.
Self-curing forward polymerization is an important molding strategy for resin curing, and the resin is promoted to be cured spontaneously by using the exothermic heat of the polymerization process to provide continuous chemical power without more external energy, so that the manufacturing cost is greatly reduced. However, to date, most self-initiated polymers have failed to meet high performance requirements due to poor performance. For example, while acrylate monomers have the necessary energy density and reactivity to undergo rapid forward polymerization, the resulting polymers have much lower mechanical properties than the matrix polymers used in structural fiber reinforced polymer composites. In contrast, epoxy monomers can produce polymers with strong mechanical properties, but rapid polymerization remains challenging due to their low reactivity (Journal of Polymer Science Part A: polymer Chemistry,2010,48 (9): 2000-2005).
CFRP puts higher demands on mechanical properties in addition to the ability of epoxy resins to cure rapidly and spontaneously. The modulus of the fast curing materials is generally low, and the current CFRP facing unbalanced compression and tension conditions limits the wider application of the CFRP. Therefore, in order to better cope with various complicated application environments, epoxy resins with higher modulus are also becoming one of the hot fields of research.
In summary, in order to improve the compression performance of the composite material and promote the improvement of the manufacturability of the composite material, the fast-curing high-modulus epoxy resin is one of the necessary development directions in the field.
Disclosure of Invention
The invention aims to provide an epoxy resin with high modulus and high activity.
The invention provides an epoxy resin curing system, which comprises an epoxy resin monomer containing a structure shown in a formula I and a curing agent:
wherein R is 1 、R 2 、R 3 Are each independently selected from hydrogen orAnd R is 1 、R 2 、R 3 At least one of which is
Further, the structure shown in formula I is:
further, the curing agent is an amine curing agent, an acid anhydride curing agent or an accelerator curing agent, wherein the amine curing agent is m-phenylenediamine, halogen substituted or unsubstituted diaminodiphenylmethane, 3,4' -diaminodiphenyl sulfone, diethyltoluenediamine or diaminopyridine; the acid anhydride curing agent is methyl nadic anhydride or phthalic anhydride; the accelerator curing agent is 1-methylimidazole or 2-ethyl-4-methylimidazole.
Further, the curing agent is an amine curing agent, preferably a halogen substituted or unsubstituted diaminodiphenylmethane, more preferably 3,3 '-dichloro-4, 4' -diaminodiphenylmethane or diethyltoluenediamine.
Further, the molar ratio of the active hydrogen of the amine-based curing agent to the epoxy group of the epoxy resin monomer is (0.8 to 2): 1, preferably 1.
Further, the curing system also comprises a diluent; the diluent is styrene oxide, phenyl glycidyl ether, resorcinol glycidyl ether or hydroquinone glycidyl ether, preferably styrene oxide;
preferably, the diluent is used in an amount of 5% to 10% w/w of the epoxy resin curing system.
The invention also provides an epoxy resin cured product, which is prepared by reacting the epoxy resin cured system at 130-140 ℃ for 2-5 hours and then reacting at 170-190 ℃ for 2-5 hours.
The invention also provides application of the epoxy resin cured product as a composite material matrix or a 3D printing material.
The invention also provides an epoxy resin monomer, which contains the following structure:
the invention also provides a preparation method of the epoxy resin monomer, which comprises the following steps:
(1) Under the action of catalyst, the epoxy halopropane and salicylaminol react at 90-110 deg.c for 4-12 hr;
(2) Cooling to below 70 ℃, adding alkali for reaction for 4-12 hours, cooling, filtering, standing for layering, and removing the catalyst and epihalohydrin in the supernatant to obtain the catalyst;
preferably, the epihalohydrin of step (1) is epichlorohydrin; the catalyst is benzyltriethylammonium bromide or 1-methylimidazole; and/or the base of step (2) is sodium hydroxide, preferably solid sodium hydroxide.
The invention has the beneficial effects that: the polar epoxy resin with a typical structure has high reactivity, the epoxy resin condensate obtained by the reaction with the curing agent has high modulus, particularly, the condensate prepared by a TEBAM curing system has good thermal mechanical property, and the polar epoxy resin has important application value in the fields of rapid manufacturing of high-performance fiber reinforced thermosetting polymer composite materials, resin 3D printing and the like.
Obviously, many modifications, substitutions, and variations are possible in light of the above teachings of the invention, without departing from the basic technical spirit of the invention, as defined by the following claims.
The present invention will be described in further detail with reference to the following examples. This should not be understood as limiting the scope of the above-described subject matter of the present invention to the following examples. All the technologies realized based on the above contents of the present invention belong to the scope of the present invention.
Drawings
FIG. 1 shows DSC spectra of DEBIM/MPD (comparative example 2) and TEBAM/DETDA (example 2) curing processes.
FIG. 2 is a plot of DMA performance for a DEBAM cured article (example 1) and a TEBAM cured article (example 2) versus E51 (comparative example 1).
FIG. 3 is a plot of heat residual weight for DEBAM cured (example 1) and TEBAM cured (example 2) versus E51 (comparative example 1).
Detailed Description
The raw materials and equipment used in the invention are known products, and are obtained by purchasing products sold in the market. The epoxy equivalent of the epoxy resin is determined according to the measurement results of GB/T4612-2008.
Example 1 preparation of resin monomer DEBAM of the invention and cured product thereof
1. Preparation of DEBAM
Adding epoxy chloropropane and salicylaminol into the flask, wherein the mass ratio of the epoxy chloropropane to the hydroxyl is 15. Benzyl triethyl ammonium bromide is selected as a reaction catalyst, and the addition amount of the benzyl triethyl ammonium bromide is 2.5-3% of the mass of the 3-hydroxybenzaldehyde- (4-hydroxy-phenylimine). The reaction is carried out at 100 ℃ for 4 to 12 hours. The flask was cooled to below 70 ℃, sodium hydroxide particles were added in portions, and the mixed solution was continuously stirred for 4-12 hours, cooled, and filtered. After standing and layering, the catalyst in the solution was extracted with deionized water, and epichlorohydrin was removed by concentration to obtain DEBAM.
1 H NMR(400MHz,DMSO,DEBAM)δ10.01(s,0H),7.76-7.61(m,2H),7.49(dd,J=8.4,7.3,1.8Hz,1H),7.19(dd,J=8.4,1.0Hz,1H),7.18-6.87(m,3H),6。87-6.63(m,1H),4.56-4.45(m,1H),4.31(dd,J=11.4,2.7Hz,1H),4.26-3.99(m,1H),3.95-3.59(m,2H),3.59-3.28(m,1H),2.91-2.60(m,4H)。
FTIR(DEBAM)(KBr):ν(O=CN-H)=3396cm -1 ,νAr(C β -H)=3003,2921,2848cm -1 ,ω(C=O)=1706cm -1 , νepoxy(C-O-C)=909cm -1 。
Determination of the epoxy equivalent E according to GB/T4612-2008 q =166.9, epoxy value E v =0.515 (close to the theoretical epoxy value of 0.585), and the weight average molecular weight was measured to be 333.8.
2. Preparation of the cured product
Taking the DEBAM prepared in the step 1, 3 '-dichloro-4, 4' -diaminodiphenylmethane (MOCA) curing agent, and mixing the DEBAM and the 3,3 '-dichloro-4, 4' -diaminodiphenylmethane (MOCA) curing agent according to the molar ratio of the hydrogen atom carried by the amino group to the epoxy group of 1:1, and adding styrene oxide diluent accounting for 5% of the total mixed amount of the resin and the curing agent to dilute, reacting at 110 ℃ for 3 hours, 150 ℃ for 3 hours, and 200 ℃ for 3 hours, and curing to prepare a product (DEBAM +5% SO/MOCA).
Example 2 preparation of resin monomer TEBAM of the invention and cured product thereof
1. Preparation of TEBAM
Referring to the preparation method of example 1, salicylaminophenol was replaced with 3, 5-dihydroxy-N- (4-hydroxyphenyl) benzamide, and the catalyst was replaced with 1-methylimidazole in an amount of 1% of 3, 5-dihydroxy-N- (4-hydroxyphenyl) benzamide; thus obtaining TEBAM.
1 H NMR(400MHz,DMSO,TEBAM)δ10.06(s,1H),δ7.71-7.62(m,1H),7.16(dd,J=12.8,2.4Hz,1H),7.01-6.93(m,1H),6.93-6.71(m,1H),6.43(s,1H),4.42(ddd,J=11.4,2.7,1.0Hz,1H),4.36-4。14(m,1H),4.03-3.90(m,1H),3.90(dd,J=5.6,3.7Hz,1H),3.90-3.74(m,1H),3.77-3.55(m,1H),3。58-3.50(m,1H),3.49-3.20(m,2H),2.90-2.78(m,3H),2.82-2.68(m,2H),2.72-2.61(m,1H)。
FTIR(TEBAM)(KBr):ν(O-H)=3397cm -1 ,νAr(C β -H)=3064,3001,2927cm -1 ,ω(C=O)=1718cm -1 , β(O=CN-H)=1594cm -1 , νepoxy(C-O-C)=909cm -1 .
Determination of the epoxy equivalent E according to GB/T4612-2008 q =194.0, epoxy value E v =0.515 (close to the theoretical epoxy value of 0.726), and the weight average molecular weight was measured to be 388.0.
2. Preparation of the cured product
Taking the TEBAM prepared in the step 1 and a diethyl toluene diamine (DETDA) curing agent, wherein the mixing ratio of the TEBAM curing agent to the diethyl toluene diamine (DETDA) curing agent is that the molar ratio of hydrogen atoms carried by amino groups to epoxy groups is 1:1, and adding styrene oxide diluent accounting for 10% of the total amount of the resin and curing agent mixed to dilute, reacting at 110 ℃ for 3 hours, at 150 ℃ for 3 hours, and at 200 ℃ for 3 hours, and curing to prepare a product (TEBAM +10% SO/DETDA).
Example 3 preparation of a resin monomer DEBAM cured product of the invention
Referring to the method of example 1, a cured product was prepared by adjusting the amount ratio of DEBAM and MOCA to 0.8.
Example 4 preparation of a resin monomer DEBAM cured product of the invention
Referring to the method of example 1, a cured product was prepared by adjusting the amount ratio of DEBAM and MOCA to 2 in terms of the molar ratio of hydrogen atoms carried by amino groups to epoxy groups.
Example 5 preparation of a cured product of a resin monomer TEBAM of the invention
Referring to the method of example 2, a cured product was prepared by adjusting the ratio of the amounts of TEBAM and DETDA to 0.8.
Example 6 preparation of a cured product of a resin monomer TEBAM of the invention
Referring to the procedure of example 2, a cured product was prepared by adjusting the ratio of the amounts of TEBAM and DETDA to 2.
Comparative examples 1,
Referring to the preparation method of example 1, the epoxy resin monomer was replaced with a commercially available epoxy resin E51, and the curing agent was replaced with diaminodiphenylmethane, in a mixing ratio of 1:1 (mass ratio of curing agent to resin 2.5.
Comparative examples 2,
1. Preparation of DEBIM
Epichlorohydrin and 3-hydroxybenzaldehyde- (4-hydroxyphenylimine) were added to the flask in a mass ratio of epichlorohydrin to hydroxyl of 15. Benzyl triethyl ammonium bromide is selected as a reaction catalyst, and the addition amount of the benzyl triethyl ammonium bromide is 2.5-3% of the mass of the 3-hydroxybenzaldehyde- (4-hydroxy-phenylimine). The reaction is carried out at 100 ℃ for 4 to 12 hours. The flask was cooled to below 70 ℃, the sodium hydroxide particles were added in portions, and the mixed solution was continuously stirred for 4-12 hours, cooled, and filtered. After standing and layering, extracting the catalyst in the solution with deionized water, and removing epichlorohydrin by concentration to obtain DEBIM.
Epoxy determination according to GB/T4612-2008Equivalent E q =168.8, epoxy value E v =0.592 (close to the theoretical epoxy value of 0.615) and the weight average molecular weight was measured to be 337.6.
1 H NMR(500MHz,CHCl 3 -d,DEBIM)δ8.42(s,1H),7.03(t,3H),6.68-6.93(t,3H),6.33-6.62(D,2H),4.89(s,1H),4.45(s,1H),3.11-3.34(DD,4H),3.44-3.32(M,3H),2.86-2.75(DD,2H),2.49(D,2H)。
Method for binding reaction raw material 3-hydroxybenzaldehyde- (4-hydroxyphenylimine) 1 HNMR (400MHz, DMSO) results: δ 9.62 (S, 1H), 9.48 (S, 1H), 8.50 (S, 1H), 7.32 (d, J =3.2hz, 1h), 7.31-7.26 (M, 2H), 7.21-7.14 (M, 2H), 6.91-6.85 (M, 1H), 6.82-6.76 (M, 2H), 2.54 (S, 1H).
2. Preparation of cured product
And (2) adding a m-phenylenediamine curing agent into the DEBIM prepared in the step (1) and uniformly mixing, wherein the proportion of the DEBIM to the m-phenylenediamine curing agent satisfies that the molar ratio of hydrogen atoms (namely active hydrogen) carried by amino groups to epoxy groups is 1:1 (i.e., the mass ratio of m-phenylenediamine to DEBIM is 1.6. Cured at 135 ℃ for 3 hours and 180 ℃ for 3 hours to obtain a cured product (DEBIM/MPD).
The beneficial effects of the present invention are demonstrated by the following experimental examples.
Experimental example 1 Activity of resin monomer
In the process of selecting the curing agent, the TEBAM and DEBAM epoxy resin monomer of the invention is found to be easy to implode at room temperature by using a common amine curing agent (m-phenylenediamine or diaminodiphenylmethane) or an imidazole curing agent. Only with the use of less active curing agents such as DETDA and MOCA, and the use of diluents, can the expected cured products be successfully synthesized, reflecting the high activity of the TEBAM and DEBAM epoxy resin monomers of the invention.
The preparation of the cured products of example 2 and comparative example 2 was further monitored by Differential Scanning Calorimetry (DSC) and the results are shown in figure 1. The peak curing temperature of the resin monomer DEBIM and the high-activity curing agent MPD in comparative example 2 is 149.4 ℃, and the curing temperature of the resin monomer TEBAM and the low-activity curing agent DETDA in example 2 is 148.8 ℃. The peak exotherm temperature for the less reactive curing agent is lower than for the more reactive curing agent.
The initial exothermic temperature (total exothermic amount is 5%) of the DEBIM and the high-activity curing agent MPD is 88.8 ℃, the initial exothermic temperature of the TEBAM and the low-activity curing agent DETDA is 53.5 ℃, and the exothermic peak of the reaction is very wide, so that the TEBAM and DEBAM resins of the embodiment 1 and the embodiment 2 have extremely high reactivity.
Experimental example 2 mechanical and thermomechanical properties of the cured product of synthetic resin
1. Experimental methods
The cured products of examples 1, 2 and comparative example 1 were subjected to flexural and tensile properties according to the test standards and sample specifications of table 1, and subjected to dynamic thermo-mechanical analysis (DMA).
Table 1 test standards and sample specifications
2. Results of the experiment
As shown in table 2.
TABLE 2 comparison of the composition and Properties of the different curing systems
It can be seen that the average flexural modulus and tensile modulus of the cured resin products of examples 1 and 2 are significantly improved as compared with those of a cured product of a conventional epoxy resin E51 (comparative example 1).
In particular, as shown in FIG. 2, it can be seen that the glass transition temperature of the cured TEBAM and DETDA are higher than 220 ℃. Meanwhile, the modulus of DEBAM cured material is higher than that of E51 cured material before 150 ℃, and the storage modulus of TEBAM cured material is still 1408MPa (single cantilever mode) at 200 ℃. Reflecting that the cured TEBAM and DETDA of example 2 of the present invention also have excellent thermo-mechanical properties.
Experimental example 3 thermal residual weight of cured synthetic resin
1. Experimental method
Thermogravimetric analysis (TGA) was performed on the cured resin of examples 1 and 2 and the cured resin of comparative example 1 at 800 ℃ in a nitrogen atmosphere.
2. Results of the experiment
As shown in fig. 3. It can be seen that the residual carbon content of E51 is only 11.8% at 800 ℃ under a nitrogen atmosphere. Under the same condition, the residual carbon content of DEBAM and TEBAM cured products can reach 18.5 percent and 25.2 percent, which shows that the resin has better heat resistance and ablation resistance than E51.
In conclusion, the invention provides a polar epoxy resin monomer with a typical structure and a curing system thereof. The polar epoxy resin monomer has high reaction activity, and an epoxy resin condensate obtained by the reaction of the polar epoxy resin monomer and a curing agent has high modulus and good thermomechanical property. The preparation method has important application value in the fields of rapid manufacturing of high-performance fiber reinforced thermosetting polymer composite materials, resin 3D printing and the like.
Claims (10)
3. the epoxy curing system of claim 1, wherein the curing agent is an amine curing agent, an anhydride curing agent, or an accelerator curing agent, and the amine curing agent is m-phenylenediamine, a halogen substituted or unsubstituted diaminodiphenylmethane, 3,4' -diaminodiphenylsulfone, diethyltoluenediamine, or diaminopyridine; the acid anhydride curing agent is methyl nadic anhydride or phthalic anhydride; the accelerator curing agent is 1-methylimidazole or 2-ethyl-4-methylimidazole.
4. The epoxy curing system of claim 3, wherein the curing agent is an amine curing agent, preferably a halogen substituted or unsubstituted diaminodiphenylmethane, more preferably 3,3 '-dichloro-4, 4' -diaminodiphenylmethane or diethyltoluenediamine.
5. The epoxy resin curing system of claim 4, wherein the molar ratio of active hydrogen of the amine-based curing agent to epoxy groups of the epoxy resin monomer is (0.8-2): 1, preferably 1.
6. The epoxy curing system of claim 1, further comprising a diluent; the diluent is styrene oxide, phenyl glycidyl ether, resorcinol glycidyl ether or hydroquinone glycidyl ether, preferably styrene oxide;
preferably, the diluent is used in an amount of 5% to 10% w/w of the epoxy resin curing system.
7. A cured epoxy resin which is obtained by reacting the epoxy resin curing system according to any one of claims 1 to 6 at 130 to 140 ℃ for 2 to 5 hours and then at 170 to 190 ℃ for 2 to 5 hours.
8. Use of the cured epoxy resin according to claim 7 as a matrix for composite materials or as a 3D printing material.
10. the method of preparing an epoxy resin monomer according to claim 9, comprising the steps of:
(1) Under the action of catalyst, the epoxy halopropane and saligenin react for 4-12 hours at 90-110 ℃;
(2) Cooling to below 70 ℃, adding alkali for reaction for 4-12 hours, cooling, filtering, standing for layering, and removing the catalyst and epihalohydrin in the supernatant to obtain the catalyst;
preferably, the epihalohydrin of step (1) is epichlorohydrin; the catalyst is benzyltriethylammonium bromide or 1-methylimidazole; and/or the base of step (2) is sodium hydroxide.
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