A kind of preparation method of epoxy resin/silicon nitride composite material
Technical field
The present invention relates to a kind of preparation method of LED encapsulation heat-conducting resin, especially a kind of epoxy resin/silicon nitride is multiple
The preparation method of condensation material.
Background technology
Epoxy resin (Epoxy Resin, EP) has that cementability is high, shrinking percentage is low, heat resistance is high, good manufacturability and price
Low advantage, therefore it is widely used in the encapsulation of electronic component.But the thermal conductivity of EP is bad, cause EP encapsulating materials
Poor radiation, so as to influence the service life of electronic product, has been difficult in adapt to the fast development of encapsulation technology.
In order to improve the thermal conductivity of epoxy resin encapsulating material, at present researcher's most study be select graphene or
Carbon nanotubes is as heat filling, but graphene or carbon nanotubes higher price, and needs in preparation process to use oxygen
Strong oxidizing property, corrosive chemical reagent used in graphite, treatment process are more complicated.
The content of the invention
In order to solve epoxy resin encapsulating material of the prior art using graphene or carbon nanotubes as heat filling
The deficiency brought, there is provided a kind of preparation method of epoxy resin/silicon nitride composite material, it uses modified nano-silicon nitride
As heat filling, the thermal conductivity of material is improved, and the price of nano-silicon nitride is far below graphene and carbon nanotubes, changes
Property process and aftertreatment technology it is more simple and convenient than graphite, without using the strong oxygen used in graphite oxide in preparation process
The property changed, corrosive chemical reagent.
The present inventor is innovated on the basis of conventional thermal conductive filler, has used modified nano-silicon nitride as heat conduction
Filler, for improving the heat conductivility of epoxy resin, but since Nano powder of silicon nitride has higher surface energy, is polymerizeing
It is dispersed poor in thing.In order to which silicon nitride can be evenly dispersed in resin system and is kept well with basis material
Compatibility, researcher carry out surface modification to it, improve the hot property and other performances of composite material.
Technical solution
A kind of preparation method of epoxy resin/silicon nitride composite material, includes the following steps:
(1) preparation of modified silicon nitride
Take new alkoxy three (p-aminophenyl epoxide) zirconate to be uniformly mixed with solvent at 55-65 DEG C, then add and receive
Rice silicon nitride, and magnetic agitation reflux 20-30h is carried out at 65-85 DEG C, obtained reflux system is centrifuged, and
With absolute ethyl alcohol centrifuge washing, finally obtained material is dried, is ground.
(2) preparation of composite material
Epoxy resin is heated to 55-65 DEG C, the ethanol solution of modified silicon nitride is then added, is mixed at 55-65 DEG C equal
It is even, and 1-2h is stirred in 75-85 DEG C, curing agent is added after being then cooled to 55-65 DEG C, injection molding is placed on vacuum tank exhaust, so
After cured, to obtain the final product.
In step (1), the dosage of new alkoxy three (p-aminophenyl epoxide) zirconate is the 40- of nano-silicon nitride
70wt%.
In step (2), the epoxy resin is bisphenol A type epoxy resin, epoxide equivalent 210-240g/eq.
In step (2), the additive amount of modified silicon nitride is the 0.5-6% of epoxy resin quality.
In step (2), the additive amount of curing agent accounts for the 1-6wt% of epoxy resin.
Further, in step (1), the solvent be selected from dimethylformamide (DMF), acetone, formamide, methyl formate or
Any one in ethyl acetate.
Further, in step (1), the dosage of solvent is calculated by 35-45ml solvents/g silicon nitrides.
Further, in step (1), the rotating speed of the centrifugally operated is 10000-12000r/min.
Further, in step (1), the drying process is:Prior to 50-60 DEG C air blast drying, then the vacuum at 55-65 DEG C
Dry 8-12h.
Further, in step (2), the concentration of the ethanol solution of modified silicon nitride is modified silicon nitride/10-14ml second for 1g
Alcohol.
Further, in step (2), the dosage of the ethanol solution of modified silicon nitride is molten for the ethanol of 3-20mL modification silicon nitrides
Liquid/10g epoxy resin.
Further, in step (2), the curing agent is in 2-ethyl-4-methylimidazole, ethylenediamine or triethylene tetramine
Any one.
Further, in step (2), curing operation flow is:70℃/1h+90℃/1h+120℃/1.5h+150℃/
1.5h。
Beneficial effect:The thermal conductivity factor of composite material of the present invention improves compared with the thermal conductivity factor of pure epoxy resin EP
44.2%, and the dosage of the modified nano-silicon nitride of heat filling is low, is only the 0.5-6% of epoxy resin quality.
Embodiment
In following embodiments, the epoxy resin of use is bisphenol A type epoxy resin, epoxide equivalent 210-240g/eq,
New (p-aminophenyl epoxide) zirconate of alkoxy three using Nanjing Neng De new material technologies Co., Ltd ZCA-N97.
Embodiment 1
(1) preparation of modified silicon nitride
Take 0.1010g ZCA-N97 to be uniformly mixed with 60mL solvent DMFs at 60 DEG C, then add 2.0015g nanometers of nitrogen
SiClx, and magnetic agitation reflux 24h is carried out at 80 DEG C, obtained reflux system is centrifuged, and use absolute ethyl alcohol
Centrifuge washing 3 times, finally dries obtained material in 55 DEG C of air blast, then 12h is dried in vacuo at 60 DEG C, grinds 30min.
(2) preparation of composite material
By epoxy resin 29.56g, then oil bath heating adds ethanol solution (the 1g modification nitrogen of modified silicon nitride to 60 DEG C
SiClx:13mL ethanol) 10mL, it is uniformly mixed at 60 DEG C, and 2h are stirred in 80 DEG C, curing agent 2- is added after being then cooled to 55 DEG C
Ethyl -4-methylimidazole 0.8878g, injection molding are placed on vacuum tank exhaust 1.5h, then cure by following technique:70℃/1h+90
DEG C/1h+120 DEG C/1.5h+150 DEG C/1.5h, up to epoxy resin/modification silicon nitride composite material.
Embodiment 2
(1) preparation of modified silicon nitride
Take 0.5023g ZCA-N97 to be uniformly mixed with 300mL solvent DMFs at 60 DEG C, then add 3.0115g nanometers of nitrogen
SiClx, and magnetic agitation reflux 24h is carried out at 80 DEG C, obtained reflux system is centrifuged, and use absolute ethyl alcohol
Centrifuge washing 4 times, finally dries obtained material in 60 DEG C of air blast, then 12h is dried in vacuo at 60 DEG C, grinds 30min.
(2) preparation of composite material
By epoxy resin 28.5673g, then oil bath heating adds ethanol solution (the 1g modifications of modified silicon nitride to 60 DEG C
Silicon nitride:12mL ethanol) 20mL, it is uniformly mixed at 60 DEG C, and 2.5h are stirred in 80 DEG C, add and cure after being then cooled to 60 DEG C
Agent 2-ethyl-4-methylimidazole 0.8588g, injection molding are placed on vacuum tank exhaust 2h, then cure by following technique:70℃/1h+
90 DEG C/1h+120 DEG C/1.5h+150 DEG C/1.5h, up to epoxy resin/modification silicon nitride composite material.
Embodiment 3
(1) preparation of modified silicon nitride
Take 0.3023g ZCA-N97 to be uniformly mixed with 180mL solvent ethyl acetates at 60 DEG C, then add 2.6815g
Nano-silicon nitride, and magnetic agitation reflux 24h is carried out at 70 DEG C, obtained reflux system is centrifuged, and use nothing
Water-ethanol centrifuge washing 4 times, finally dries obtained material in 60 DEG C of air blast, then is dried in vacuo 12h at 60 DEG C, grinding
40min。
(2) preparation of composite material
By epoxy resin 56.82g, then oil bath heating adds ethanol solution (the 1g modification nitrogen of modified silicon nitride to 60 DEG C
SiClx:14mL ethanol) 8mL, it is uniformly mixed at 60 DEG C, and 3h are stirred in 80 DEG C, curing agent 2- is added after being then cooled to 65 DEG C
Ethyl -4-methylimidazole 0.8648g, injection molding are placed on vacuum tank exhaust 2h, then cure by following technique:70℃/1h+90
DEG C/1h+120 DEG C/1.5h+150 DEG C/1.5h, up to epoxy resin/modification silicon nitride composite material.
Comparative example 1
It is added to using carbon nanotubes in epoxy resin and prepares composite material, in technical process and parameter and embodiment 1
Step (2) is similar, and modified silicon nitride therein simply is changed to carbon nanotubes.
Comparative example 2
It is added to using KH550 (3- aminopropyl triethoxysilanes) modified graphite oxide in epoxy resin and prepares composite wood
Material, technical process and parameter are similar with the step (2) in embodiment 1, and modified silicon nitride therein simply is changed to KH550 is modified
Graphite oxide.
Performance test
Epoxy resin made from embodiment 1-3/modification silicon nitride composite material carries out to the test of heat conductivility, and with it is pure
Epoxy resin and comparative example 1, the heat conductivility of comparative example 2 are contrasted, and are tested limited using Xiangtan, Hunan Province double happiness instrument
Company DRL-III type heat conduction coefficient testers, and measured with the uniform coating composite materials surface of heat-conducting silicone grease.
Test result see the table below:
|
Thermal conductivity factor W/ (mK), |
Embodiment 1 |
0.4471 |
Embodiment 2 |
0.4460 |
Embodiment 3 |
0.4437 |
Pure epoxy resin |
0.31 |
Comparative example 1 |
0.3536 |
Comparative example 2 |
0.3504 |
As can be seen from the above table, compared with pure epoxy resin, the thermal conductivity factor of composite material of the invention improves 44%,
With the composite material prepared with identical technique addition carbon nanotubes into epoxy resin and with KH550 (three second of 3- aminopropyls
Oxysilane) modified graphite oxide is added to the composite material prepared in epoxy resin and compares, and thermal conductivity factor has by a relatively large margin
Raising.