CN106046783B - A kind of boride ceramics filling in situ cyanate resin base composite material and preparation method thereof - Google Patents

A kind of boride ceramics filling in situ cyanate resin base composite material and preparation method thereof Download PDF

Info

Publication number
CN106046783B
CN106046783B CN201610611960.0A CN201610611960A CN106046783B CN 106046783 B CN106046783 B CN 106046783B CN 201610611960 A CN201610611960 A CN 201610611960A CN 106046783 B CN106046783 B CN 106046783B
Authority
CN
China
Prior art keywords
cyanate ester
ester resin
situ
composite material
metal boride
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201610611960.0A
Other languages
Chinese (zh)
Other versions
CN106046783A (en
Inventor
于志强
何延楠
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fudan University
Original Assignee
Fudan University
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Fudan University filed Critical Fudan University
Priority to CN201610611960.0A priority Critical patent/CN106046783B/en
Publication of CN106046783A publication Critical patent/CN106046783A/en
Application granted granted Critical
Publication of CN106046783B publication Critical patent/CN106046783B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/38Boron-containing compounds
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G73/00Macromolecular compounds obtained by reactions forming a linkage containing nitrogen with or without oxygen or carbon in the main chain of the macromolecule, not provided for in groups C08G12/00 - C08G71/00
    • C08G73/06Polycondensates having nitrogen-containing heterocyclic rings in the main chain of the macromolecule
    • C08G73/0622Polycondensates containing six-membered rings, not condensed with other rings, with nitrogen atoms as the only ring hetero atoms
    • C08G73/0638Polycondensates containing six-membered rings, not condensed with other rings, with nitrogen atoms as the only ring hetero atoms with at least three nitrogen atoms in the ring
    • C08G73/0644Poly(1,3,5)triazines
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G73/00Macromolecular compounds obtained by reactions forming a linkage containing nitrogen with or without oxygen or carbon in the main chain of the macromolecule, not provided for in groups C08G12/00 - C08G71/00
    • C08G73/06Polycondensates having nitrogen-containing heterocyclic rings in the main chain of the macromolecule
    • C08G73/0622Polycondensates containing six-membered rings, not condensed with other rings, with nitrogen atoms as the only ring hetero atoms
    • C08G73/0638Polycondensates containing six-membered rings, not condensed with other rings, with nitrogen atoms as the only ring hetero atoms with at least three nitrogen atoms in the ring
    • C08G73/065Preparatory processes
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K2201/00Specific properties of additives
    • C08K2201/002Physical properties
    • C08K2201/003Additives being defined by their diameter

Abstract

The invention belongs to advanced compound materials science domain, specially a kind of boride ceramics filling in situ cyanate resin base composite material and preparation method thereof.Bisphenol-A is first dissolved in benzene class or alkanes organic solvent by situ aggregation method, a certain amount of cyanogen halides is added, mechanical stirring obtains mixed solution in -10 ~ 0 DEG C of environment by the present invention;Under strong stirring, metal boride ceramic powder is added into mixed solution, continues to stir;At -10 ~ 0 DEG C, triethylamine is added dropwise in Xiang Shangshu system, system polymerize, and obtains metal diboride powder filling in situ cyanate ester resin after distillation removes organic solvent;Then catalyst stirring is added, curing molding at high temperature after Fruit storage.Metal boride filling in situ cyanate ester resin composite material produced by the present invention has material structure uniform, heat-resisting, excellent thermal conductivity structural behaviour feature, can be used as aerospace industry, aerospace industry electronic equipment in printed circuit board baseplate material, encapsulating material etc..

Description

A kind of boride ceramics filling in situ cyanate resin base composite material and its preparation Method
Technical field
The invention belongs to technical field of composite materials, and in particular to a kind of boride ceramics filling in situ cyanate resin base is multiple Condensation material and preparation method thereof.
Background technique
With the high power of modern microelectronics devices, highly integrated and micromation development, in industrial application electronic equipment The timely heat dissipation of baseplate material, encapsulating material etc. and stability seem most important.Cyanate (Cyanate Ester, CE) Resin is as a kind of important high-performance thermosetting resin, since it is with good heat resistance, lower dielectric constant and Jie The comprehensive performances such as electrical loss and good weatherability, in high performance print circuit board, aerospace structure member, stealth material, radar The advanced technologies such as antenna house and artificial satellite field has broad application prospects.Cyanate ester monomer is after solidification crosslinking, knot There is high structural stability, low polar 1,3,5-triazines ring structure in structure, even compact structure makes cyanate ester resin solid Brittleness is big after change, heating conduction is poor, generates violent temperature rise because that cannot radiate in time under high loading conditions and then leads to material Structure and performance failure, it is difficult to meet hot environment flowering structure to the actual requirement of material property, make its application by certain Limitation.To cyanate resin modifier, thermosetting resin, thermoplastic resin, rubber elastomer, chemical combination containing unsaturated double-bond are such as utilized Object and inorganic filler etc. have been carried out a large amount of research work, and research focuses mostly on to toughening modification of cyanate ester resin.Wherein Using inorganic ceramic filling modifier cyanate organic resin hot property, especially improves the mechanical property under its high temperature, leads Hot property is a kind of more effective method.Studies have shown that inorganic ceramic filling modifier organic resin has merged inorganic pottery It is negative in height that the excellent thermally conductive heat resistance of porcelain and high flexibility, the machinability of organic resin can significantly improve organic resin material Heating conduction under lotus.From the point of view of previous research, the inorganic filler for filling-modified cyanate ester resin is concentrated mainly on carbon Nanotube, graphene, SiO2、TiO2With BN etc., the method that material preparation is mainly blended using physical mechanical, and for benefit It is then rarely reported with the research of boride ceramics especially metal boride ceramic filler modified cyanic acid ester, especially by original position The research that polymerization prepares the filling-modified cyanate ester resin composite material of high-thermal conductive metal boride ceramics is not yet shown in so far Report.
Bibliography:
[1] Caifei Han, Aijuan Gu, Guozheng Liang, Li Yuan. Carbon nanotubes/ cyanate ester composites with low percolation threshold, high dielectric constant and outstanding thermal property[J].Composites: Part A, 2010,41: 1321-1328
[2] Qilang Lin, Lijuan Qu, Qiufeng lu. Preparation and properties of graphene oxide nanosheets/cyanate ester resin composites[J]. Polymer Testing, 2013, 32: 330-337
[3] Tim J. Wooster, Simmi Abrol, Jeffrey M. Hey, Douglas R. MacFarlane. The effect of particle matrix adhesion on the mechanical properties of silica filled cyanate ester composites[J]. Macromol. Mater. Eng. 2004, 289:872-879
[4] Jingwen Li, Zhixiong Wu, Chuanjun Huang, etc.Mechanical properties of cyanate ester/epoxy nanocomposites modified with plasma functionalized MWCNTs[J]. Composites Science and Technology, 2014,90:166-173
[5] John N. Suman, John Kathi, Shekharam Tammishetti.Thermoplastic modification of monomeric and partially polymerized bisphenol A dicyanate ester[J]. European Polymer Journal, 2005, 41:2963-2972。
Summary of the invention
It is multiple that the purpose of the present invention is to provide the metal boride ceramic filler cyanate ester resins of a kind of high heat resistance, high thermal conductivity Condensation material and preparation method thereof, to meet the field of engineering technology such as aerospace industry, aerospace structure part to heat-resisting material Actual demand.
Metal boride Situ of Ceramics provided by the invention fills cyanate ester resin composite material, is by cyanate resin High performance metal boride ceramic packing is added in rouge, cyanate ester resin high-temperature heat-conductive heat resistance is improved, specifically by metal Boride one-component ceramic powder, cyanate ester resin and catalyst composition;According to the mass fraction, the dosage of each component is as follows:
Cyanate ester resin: 85 ~ 95;
Metal boride ceramic powder: 5 ~ 15;
Catalyst: 0.01 ~ 0.05.
In the present invention, the metal boride ceramic powder is titanium diboride, zirconium diboride, niobium dioxide or two boronations Tantalum powder body, average grain diameter are 1 μm ~ 50 μm, wherein zirconium diboride and titanium diboride are best.
In the present invention, the cyanate ester resin be bisphenol A cyanate ester resin, average molecular mass be 500 ~ 2000;The resin as bisphenol-A in organic solvent, existing for the organic base under the conditions of react and obtain with cyanogen halides.Wherein, bis-phenol A: cyanogen halides: organic base: the quality proportioning of organic solvent is (1 ~ 1.1): (1.1 ~ 1.2): (0.9 ~ 1.1): (5 ~ 10).
Wherein, the organic solvent is alkane, benzene class or acetone, ethyl alcohol etc..
The organic base is the organic base tertiary amine that can receive Bronsted acid, preferably triethylamine.
The cyanogen halides is cyanogen chloride, cyanogen bromide or cyanogen iodide.It is preferred that cyanogen bromide.
In the present invention, the catalyst is major catalyst/synergistic catalyst, and major catalyst is organo-metallic compound The carboxylate of Cu, Co, Zn or Mn, synergistic catalyst are compatible reaction reagent, wherein preferred Zn/nonyl phenol, Co/nonyl phenol.
The preparation method of boride ceramics filling cyanate resin base composite material provided by the invention, using in-situ polymerization Method, specific steps are as follows:
(1) bisphenol-A, cyanogen halides organic solution are prepared and bisphenol-A, cyanogen halides, organic solvent is placed in -10 by quality proportioning In ~ 0 DEG C of environment, mechanical stirring;Then metal boride ceramic powder is added, controls stirring rate in 800 ~ 1500r/min;
(2) it at -10 ~ 0 DEG C, is added dropwise organic base (such as triethylamine), strong to stir, rate of addition is 0.1 ~ 0.5 drop/s, It is added dropwise within 2.5 ~ 3.5 hours.Insulated and stirred 1 ~ 3 hour, obtain suspension.It is washed to neutrality with distilled water, by the hydrogen of flocculence The separation of amine bromide salt, the hydrogen bromination amine salt isolated filter out remaining cyanate ester resin with acetone soak.It finally rotates, removing has Solvent obtains metal boride ceramic powder filling in situ cyanate ester resin;
(3) catalyst is added, 5 ~ 10min of high-speed stirred, Fruit storage injects rapidly mold, be warming up to 120 DEG C ~ 200 DEG C, solidify 5 ~ 7 hours, demoulding fills cyanate ester resin composite material to get metal boride Situ of Ceramics.
Metal boride Situ of Ceramics provided by the invention fills cyanate ester resin composite material, adds into cyanate ester resin Add boride ceramics to improve the research of cyanate ester resin performance, yet there are no report.Compared with existing similar research, utilize In-situ polymerization filled composite materials more obtained than mechanical-physical blend method have more uniform tissue signature, thus Guarantee that prepared material has more excellent performance;In addition, boride ceramics has high fusing point, splendid energy against corrosion Therefore power and thermal shock resistance and the high capacity of heat transmission utilize the cyanate ester resin of high-performance boride ceramics filling in situ Composite material will have the higher thermally conductive performances such as heat-resisting, have a extensive future in high-temperature-resistant structure and functor application field.
Specific embodiment
Embodiment 1
100g bisphenol-A, cyanogen bromide 105g and 400ml acetone soln are added in 1000ml there-necked flask, and there-necked flask is set In ice water or ice salt bath, under 1000r/min mechanical stirring, 6g zirconium diboride (ZrB is added2), in entire synthesis process In, temperature should be controlled at 0 DEG C or less.90g triethylamine is added dropwise under 1200r/min stirring by separatory funnel, rate of addition It for 0.5 drop/s, is added dropwise within about 3.5 hours, continues to stir 1h, obtain suspension.Then suspension is washed to neutrality with distilled water, The hydrogen bromination amine salt isolated filters out remaining cyanate ester resin with acetone soak and refunds former suspension.Hydrogen amine bromide will be separated After salt suspension system revolving, remove acetone solvent, obtain zirconium diboride powder filling in situ cyanate ester resin, then to 0.014gZn/nonyl phenol catalyst, high-speed stirred 6min are added into resin system, Fruit storage injects rapidly mould Tool, is solidified and is post-processed according to+180 DEG C/1h+200 DEG C/4h of+150 DEG C/1h of 120 DEG C/1h.Demould to obtain zirconium diboride Filling in situ cyanate ester resin composite material about 127g.Test result shows that the glass transition temperature Tg of the composite material is 310.8 DEG C (under identical experiment condition, the cyanate ester resin glass transition temperature Tg of synthesis is 278.5 DEG C, general ceramics Powder such as SiO2、Al2O3The glass transition temperature Tg for filling cyanate ester resin composite material is 294 ~ 302 DEG C);In room temperature item Under part, the thermal conductivity of the composite material is that (under the same test conditions, the cyanate ester resin of synthesis is 0.22 to 0.38W/mK W/mK, general ceramic powder such as SiO2、Al2O3The thermal conductivity for filling cyanate ester resin composite material is 0.28 ~ 0.32 W/m K)。
Embodiment 2
50g bisphenol-A, cyanogen bromide 52.5g and 200ml acetone soln are added in 500ml there-necked flask, and there-necked flask is set In ice water or ice salt bath, under 800r/min mechanical stirring, 3g titanium diboride (TiB is added2), in entire synthesis process In, temperature should be controlled at 0 DEG C or less.45g triethylamine is added dropwise under 1000r/min stirring by separatory funnel, rate of addition It for 0.3 drop/s, is added dropwise within about 3.0 hours, continues to stir 1h, obtain suspension.Then suspension is washed to neutrality with distilled water, The hydrogen bromination amine salt isolated filters out remaining cyanate ester resin with acetone soak and refunds former suspension.Hydrogen amine bromide will be separated After salt suspension system revolving, remove acetone solvent, obtain titanium diboride powder filling in situ cyanate ester resin, then to 0.01gZn/nonyl phenol catalyst, high-speed stirred 5min are added into resin system, Fruit storage injects rapidly mold, Solidified and post-processed according to+180 DEG C/1h+200 DEG C/4h of+150 DEG C/1h of 120 DEG C/1h.Demould to obtain titanium diboride original position Fill cyanate ester resin composite material about 65g.Test result shows that the glass transition temperature Tg of the composite material is 308.8 ℃;At room temperature, the thermal conductivity of the composite material is 0.378W/mK.
Embodiment 3
25g bisphenol-A, cyanogen bromide 26.25g and 100ml acetone soln are added in 250ml there-necked flask, and there-necked flask is set In ice water or ice salt bath, under 800r/min mechanical stirring, 3.05g zirconium diboride (ZrB is added2), it was synthesized entirely Cheng Zhong, temperature should be controlled at 0 DEG C or less.22.5g triethylamine is added dropwise under 900r/min stirring by separatory funnel, speed is added dropwise Degree is 0.1 drop/s, is added dropwise within about 3.0 hours, continues to stir 1h, obtains suspension.Then with distilled water washing suspension into Property, the hydrogen bromination amine salt isolated filters out remaining cyanate ester resin with acetone soak and refunds former suspension.Hydrogen bromine will be separated Suspension system revolving after changing amine salt, removes acetone solvent, obtains zirconium diboride powder filling in situ cyanate ester resin, then To addition 0.01gZn/nonyl phenol catalyst in resin system, high-speed stirred 5min is obtained, Fruit storage injects rapidly Mold is solidified and is post-processed according to+180 DEG C/1h+200 DEG C/4h of+150 DEG C/1h of 120 DEG C/1h.Demould to obtain two boronations Zirconium filling in situ cyanate ester resin composite material about 33.5g.Test result shows the glass transition temperature Tg of the composite material It is 312.4 DEG C;At room temperature, the thermal conductivity of the composite material is 0.43W/mK.
Embodiment 4
50g bisphenol-A, cyanogen bromide 55g and 250ml acetone soln are added in 500ml there-necked flask, and there-necked flask is placed in In ice water or ice salt bath, under 800r/min mechanical stirring, 7.315g zirconium diboride (ZrB is added2), in entire synthesis process In, temperature should be controlled at 0 DEG C or less.50g triethylamine is added dropwise under 1000r/min stirring by separatory funnel, rate of addition It for 0.3 drop/s, is added dropwise within about 3.0 hours, continues to stir 1h, obtain suspension.Then suspension is washed to neutrality with distilled water, The hydrogen bromination amine salt isolated filters out remaining cyanate ester resin with acetone soak and refunds former suspension.Hydrogen amine bromide will be separated After salt suspension system revolving, remove acetone solvent, obtain zirconium diboride powder filling in situ cyanate ester resin, then to 0.01gCo/nonyl phenol catalyst, high-speed stirred 8min are added into resin system, Fruit storage injects rapidly mold, Solidified and post-processed according to+180 DEG C/1h+200 DEG C/4h of+150 DEG C/1h of 120 DEG C/1h.Demould to obtain zirconium diboride original position Fill cyanate ester resin composite material about 68g.Test result shows that the glass transition temperature Tg of the composite material is 314.2 ℃;At room temperature, the thermal conductivity of the composite material is 0.48W/mK.
Embodiment 5
50g bisphenol-A, cyanogen bromide 55g and 250ml acetone soln are added in 500ml there-necked flask, and there-necked flask is placed in In ice water or ice salt bath, under 800r/min mechanical stirring, 7.315g titanium diboride (TiB is added2), in entire synthesis process In, temperature should be controlled at 0 DEG C or less.50g triethylamine is added dropwise under 1000r/min stirring by separatory funnel, rate of addition It for 0.3 drop/s, is added dropwise within about 3.0 hours, continues to stir 1h, obtain suspension.Then suspension is washed to neutrality with distilled water, The hydrogen bromination amine salt isolated filters out remaining cyanate ester resin with acetone soak and refunds former suspension.Hydrogen amine bromide will be separated After salt suspension system revolving, remove acetone solvent, obtain titanium diboride powder filling in situ cyanate ester resin, then to 0.01gCo/nonyl phenol catalyst, high-speed stirred 8min are added into resin system, Fruit storage injects rapidly mold, Solidified and post-processed according to+180 DEG C/1h+200 DEG C/4h of+150 DEG C/1h of 120 DEG C/1h.Demould to obtain titanium diboride original position Fill cyanate ester resin composite material about 68g.Test result shows that the glass transition temperature Tg of the composite material is 311.2 ℃;At room temperature, the thermal conductivity of the composite material is 0.436W/mK.
Embodiment 6
100g bisphenol-A, cyanogen bromide 105g and 500ml acetone soln are added in 1000ml there-necked flask, and there-necked flask is set In ice water or ice salt bath, under 1000r/min mechanical stirring, 19.51g zirconium diboride (ZrB is added2), entirely synthesizing In the process, temperature should be controlled at 0 DEG C or less.100g triethylamine is added dropwise under 1200r/min stirring by separatory funnel, is added dropwise Speed is 0.5 drop/s, is added dropwise within about 3.5 hours, continues to stir 1h, obtains suspension.Then extremely with distilled water washing suspension Neutrality, the hydrogen bromination amine salt isolated filter out remaining cyanate ester resin with acetone soak and refund former suspension.Hydrogen will be separated Suspension system revolving after bromination amine salt, removes acetone solvent, obtains zirconium diboride powder filling in situ cyanate ester resin, so It obtains adding 0.064gCo/nonyl phenol catalyst in resin system backward, high-speed stirred 10min, Fruit storage, rapidly Mold is injected, is solidified and is post-processed according to+180 DEG C/1h+200 DEG C/4h of+150 DEG C/1h of 120 DEG C/1h.Demould two Zirconium boride in-situ fills cyanate ester resin composite material about 141.4g.Test result shows the glass transition of the composite material Temperature Tg is 315.7 DEG C;At room temperature, the thermal conductivity of the composite material is 0.56W/mK.
Embodiment 7
50g bisphenol-A, cyanogen bromide 52.5g and 250ml acetone soln are added in 500ml there-necked flask, and there-necked flask is set In ice water or ice salt bath, under 800r/min mechanical stirring, 9.755g titanium diboride (TiB is added2), it was synthesized entirely Cheng Zhong, temperature should be controlled at 0 DEG C or less.50g triethylamine is added dropwise under 1000r/min stirring by separatory funnel, speed is added dropwise Degree is 0.3 drop/s, is added dropwise within about 3.0 hours, continues to stir 1h, obtains suspension.Then with distilled water washing suspension into Property, the hydrogen bromination amine salt isolated filters out remaining cyanate ester resin with acetone soak and refunds former suspension.Hydrogen bromine will be separated Suspension system revolving after changing amine salt, removes acetone solvent, obtains titanium diboride powder filling in situ cyanate ester resin, then To addition 0.01gZn/nonyl phenol catalyst in resin system, high-speed stirred 5min is obtained, Fruit storage injects rapidly Mold is solidified and is post-processed according to+180 DEG C/1h+200 DEG C/4h of+150 DEG C/1h of 120 DEG C/1h.Demould to obtain two boronations Titanium filling in situ cyanate ester resin composite material about 72g.Test result shows that the glass transition temperature Tg of the composite material is 312.8℃;At room temperature, the thermal conductivity of the composite material is 0.512W/mK.

Claims (8)

1. a kind of metal boride Situ of Ceramics fills cyanate ester resin composite material, which is characterized in that the composite material be by Metal boride one-component ceramic powder, cyanate ester resin and catalyst composition;According to the mass fraction, the dosage of each component is as follows:
Cyanate ester resin: 85 ~ 95;
Metal boride ceramic powder: 5 ~ 15;
Catalyst: 0.01 ~ 0.05.
2. metal boride Situ of Ceramics according to claim 1 fills cyanate ester resin composite material, which is characterized in that The metal boride ceramic powder is titanium diboride, zirconium diboride, niobium dioxide or tantalum diboride powder, and average grain diameter is 1 μ m~50μm。
3. metal boride Situ of Ceramics according to claim 1 or 2 fills cyanate ester resin composite material, feature exists In the cyanate ester resin is bisphenol A cyanate ester resin, and average molecular mass is 500 ~ 2000;The resin is by bisphenol-A In organic solvent, it reacts and obtains with cyanogen halides under the conditions of existing for the organic base;Wherein, bisphenol-A: cyanogen halides: organic base: have The quality proportioning of solvent is (1 ~ 1.1): (1.1 ~ 1.2): (0.9 ~ 1.1): (5 ~ 10).
4. metal boride Situ of Ceramics according to claim 3 fills cyanate ester resin composite material, which is characterized in that The organic solvent is alkane, benzene class or acetone or ethyl alcohol.
5. metal boride Situ of Ceramics according to claim 3 fills cyanate ester resin composite material, which is characterized in that The organic base is the organic base tertiary amine that can receive Bronsted acid.
6. metal boride Situ of Ceramics according to claim 3 fills cyanate ester resin composite material, which is characterized in that The cyanogen halides is cyanogen chloride, cyanogen bromide or cyanogen iodide.
7. according to claim 1, metal boride Situ of Ceramics described in one of 2,4,5,6 fills cyanate ester resin composite wood Material, which is characterized in that the catalyst is major catalyst/synergistic catalyst, wherein major catalyst is organo-metallic compound The carboxylate of Cu, Co, Zn or Mn, synergistic catalyst are necleophilic reaction reagent.
8. a kind of system of the metal boride Situ of Ceramics filling cyanate ester resin composite material as described in one of claim 1-7 Preparation Method, using situ aggregation method, which is characterized in that specific steps are as follows:
(1) bisphenol-A, cyanogen halides organic solution are prepared and bisphenol-A, cyanogen halides, organic solvent is placed in -10 ~ 0 DEG C by quality proportioning In environment, mechanical stirring;Then metal boride ceramic powder is added, controls stirring rate in 800 ~ 1500r/min;
(2) at -10 ~ 0 DEG C, organic base, stirring is added dropwise, rate of addition is 0.1 ~ 0.5 drop/s, is added dropwise within 2.5 ~ 3.5 hours; Insulated and stirred 1 ~ 3 hour, obtain suspension;It is washed to neutrality with distilled water, the hydrogen amine bromide salt of flocculence is separated, is isolated Hydrogen bromination amine salt filters out remaining cyanate ester resin with acetone soak;It finally rotates, removes organic solvent, obtain metal boride Ceramic powder filling in situ cyanate ester resin;
(3) catalyst, 5 ~ 10min of high-speed stirred is added, Fruit storage injects rapidly mold, is warming up to 120 DEG C ~ 200 DEG C, solidify 5 ~ 7 hours, demoulding fills cyanate ester resin composite material to get metal boride Situ of Ceramics.
CN201610611960.0A 2016-07-31 2016-07-31 A kind of boride ceramics filling in situ cyanate resin base composite material and preparation method thereof Active CN106046783B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610611960.0A CN106046783B (en) 2016-07-31 2016-07-31 A kind of boride ceramics filling in situ cyanate resin base composite material and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610611960.0A CN106046783B (en) 2016-07-31 2016-07-31 A kind of boride ceramics filling in situ cyanate resin base composite material and preparation method thereof

Publications (2)

Publication Number Publication Date
CN106046783A CN106046783A (en) 2016-10-26
CN106046783B true CN106046783B (en) 2019-05-31

Family

ID=57196696

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610611960.0A Active CN106046783B (en) 2016-07-31 2016-07-31 A kind of boride ceramics filling in situ cyanate resin base composite material and preparation method thereof

Country Status (1)

Country Link
CN (1) CN106046783B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114806084A (en) * 2021-01-29 2022-07-29 北大方正集团有限公司 Composite material, preparation method and circuit board

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102719097A (en) * 2012-07-06 2012-10-10 苏州大学 Titanium diboride oxide/thermosetting resin composite material and preparation method thereof
CN104231624A (en) * 2014-08-22 2014-12-24 南京信息职业技术学院 Modified cyanate resin heat-conducting composite material and preparation method thereof
CN104961652A (en) * 2015-05-30 2015-10-07 扬州天启新材料股份有限公司 Bisphenol A type cyanate resin monomer preparation method

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102719097A (en) * 2012-07-06 2012-10-10 苏州大学 Titanium diboride oxide/thermosetting resin composite material and preparation method thereof
CN104231624A (en) * 2014-08-22 2014-12-24 南京信息职业技术学院 Modified cyanate resin heat-conducting composite material and preparation method thereof
CN104961652A (en) * 2015-05-30 2015-10-07 扬州天启新材料股份有限公司 Bisphenol A type cyanate resin monomer preparation method

Also Published As

Publication number Publication date
CN106046783A (en) 2016-10-26

Similar Documents

Publication Publication Date Title
CN105399959B (en) A kind of alkyd resin moulding material additive and preparation method thereof based on polyphosphazene microspheres
Wang et al. Combining alumina particles with three-dimensional alumina foam for high thermally conductive epoxy composites
CN102337007B (en) High-performance epoxy resin composition for sheet molding compound (SMC)
Song et al. Thermal conductivity enhancement of alumina/silicone rubber composites through constructing a thermally conductive 3D framework
CN101508824B (en) Oxatyl-containing lateral group polyarylether cured modified epoxy resin composition and method for producing the same
CN102286207A (en) Thermoplastic polymer based thermal conductive composite and preparation method thereof
CN109181134A (en) A kind of thermal-conductive polymer matrix composites and preparation method thereof
TWI540171B (en) A resin composition, a resin sheet, a resin cured product, and a substrate
CN103304999B (en) The silsesquioxane composition of cyanate ester resin/containing metal aluminium or titanium
CN105368046B (en) Cyanate ester resin/heat conduction filler composition, prepreg and its application
CN104231631A (en) High-performance thermal conductive silicone rubber and preparation method thereof
CN102977556A (en) High-performance epoxy resin composition for vacuum infusion molding and preparation method thereof
CN104559061A (en) High-thermal conductivity insulated carbon filler, high-thermal conductivity insulated epoxy resin composite material and preparation method thereof
CN107001584A (en) Low-thermal-expansion halogen-free flame-retardant composition for high density printed circuit board
Liu et al. A Full-component recyclable Epoxy/BN thermal interface material with anisotropy high thermal conductivity and interface adaptability
CN113402847A (en) Low-filling high-thermal-conductivity polymer composite material and preparation method thereof
CN104031355A (en) Epoxy resin composition cured and modified by carboxyl-containing polyether nitrile sulphone ketone copolymer as well as preparation method and application of epoxy resin composition
CN106046783B (en) A kind of boride ceramics filling in situ cyanate resin base composite material and preparation method thereof
CN102634165A (en) Epoxy resin composition
CN108410134A (en) A kind of fibrous composite composition epoxy resin and its application
CN110845828A (en) Modified heat-conducting filler for polymer and preparation method of composite material of modified heat-conducting filler
KR102427035B1 (en) A composition for a cured resin, a cured product of the composition, a method for manufacturing the composition and the cured product, and a semiconductor device
Wang et al. The influence of carbon spheres on thermal and mechanical properties of epoxy composites
CN106661194B (en) Epoxy resin composition for carbon-fiber-reinforced composite material, resin sheet, prepreg, carbon fibre reinforced composite
CN104045978A (en) Polyarylether nitrile/epoxy resin copolymerized modified composition and preparation method and application thereof

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant