CN115926224A - High-thermal-conductivity prepreg for packaging carrier plate and manufacture of copper-clad plate using prepreg - Google Patents
High-thermal-conductivity prepreg for packaging carrier plate and manufacture of copper-clad plate using prepreg Download PDFInfo
- Publication number
- CN115926224A CN115926224A CN202211287466.5A CN202211287466A CN115926224A CN 115926224 A CN115926224 A CN 115926224A CN 202211287466 A CN202211287466 A CN 202211287466A CN 115926224 A CN115926224 A CN 115926224A
- Authority
- CN
- China
- Prior art keywords
- prepreg
- silicon carbide
- parts
- carbide fiber
- weight
- 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.)
- Granted
Links
- 238000004806 packaging method and process Methods 0.000 title claims abstract description 23
- 238000004519 manufacturing process Methods 0.000 title abstract description 10
- 239000004744 fabric Substances 0.000 claims abstract description 66
- 239000000835 fiber Substances 0.000 claims abstract description 62
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical group [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 claims abstract description 61
- 229920005989 resin Polymers 0.000 claims abstract description 60
- 239000011347 resin Substances 0.000 claims abstract description 60
- 229910010271 silicon carbide Inorganic materials 0.000 claims abstract description 52
- 238000012986 modification Methods 0.000 claims abstract description 15
- 230000004048 modification Effects 0.000 claims abstract description 15
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 13
- 239000000945 filler Substances 0.000 claims abstract description 13
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 12
- 239000011889 copper foil Substances 0.000 claims abstract description 11
- 239000003292 glue Substances 0.000 claims description 23
- 239000002904 solvent Substances 0.000 claims description 20
- 239000000843 powder Substances 0.000 claims description 16
- 239000013032 Hydrocarbon resin Substances 0.000 claims description 13
- 229920006270 hydrocarbon resin Polymers 0.000 claims description 13
- 238000000034 method Methods 0.000 claims description 13
- 239000003795 chemical substances by application Substances 0.000 claims description 12
- 239000004643 cyanate ester Substances 0.000 claims description 11
- 238000007598 dipping method Methods 0.000 claims description 11
- 238000001035 drying Methods 0.000 claims description 11
- 239000000853 adhesive Substances 0.000 claims description 10
- 230000001070 adhesive effect Effects 0.000 claims description 10
- 238000007731 hot pressing Methods 0.000 claims description 10
- 150000008442 polyphenolic compounds Chemical class 0.000 claims description 10
- 235000013824 polyphenols Nutrition 0.000 claims description 10
- 238000002791 soaking Methods 0.000 claims description 10
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 10
- 229910052582 BN Inorganic materials 0.000 claims description 9
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 claims description 9
- 239000002002 slurry Substances 0.000 claims description 7
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 6
- 238000003825 pressing Methods 0.000 claims description 6
- 238000001816 cooling Methods 0.000 claims description 5
- 238000004090 dissolution Methods 0.000 claims description 5
- 238000010438 heat treatment Methods 0.000 claims description 5
- 238000003756 stirring Methods 0.000 claims description 5
- WXTMDXOMEHJXQO-UHFFFAOYSA-N 2,5-dihydroxybenzoic acid Chemical compound OC(=O)C1=CC(O)=CC=C1O WXTMDXOMEHJXQO-UHFFFAOYSA-N 0.000 claims description 4
- YQUVCSBJEUQKSH-UHFFFAOYSA-N 3,4-dihydroxybenzoic acid Chemical compound OC(=O)C1=CC=C(O)C(O)=C1 YQUVCSBJEUQKSH-UHFFFAOYSA-N 0.000 claims description 4
- LNTHITQWFMADLM-UHFFFAOYSA-N gallic acid Chemical compound OC(=O)C1=CC(O)=C(O)C(O)=C1 LNTHITQWFMADLM-UHFFFAOYSA-N 0.000 claims description 4
- 238000001291 vacuum drying Methods 0.000 claims description 4
- 239000002245 particle Substances 0.000 claims description 3
- KSEBMYQBYZTDHS-HWKANZROSA-M (E)-Ferulic acid Natural products COC1=CC(\C=C\C([O-])=O)=CC=C1O KSEBMYQBYZTDHS-HWKANZROSA-M 0.000 claims description 2
- KOMNUTZXSVSERR-UHFFFAOYSA-N 1,3,5-tris(prop-2-enyl)-1,3,5-triazinane-2,4,6-trione Chemical compound C=CCN1C(=O)N(CC=C)C(=O)N(CC=C)C1=O KOMNUTZXSVSERR-UHFFFAOYSA-N 0.000 claims description 2
- TUSDEZXZIZRFGC-UHFFFAOYSA-N 1-O-galloyl-3,6-(R)-HHDP-beta-D-glucose Natural products OC1C(O2)COC(=O)C3=CC(O)=C(O)C(O)=C3C3=C(O)C(O)=C(O)C=C3C(=O)OC1C(O)C2OC(=O)C1=CC(O)=C(O)C(O)=C1 TUSDEZXZIZRFGC-UHFFFAOYSA-N 0.000 claims description 2
- XMNIXWIUMCBBBL-UHFFFAOYSA-N 2-(2-phenylpropan-2-ylperoxy)propan-2-ylbenzene Chemical compound C=1C=CC=CC=1C(C)(C)OOC(C)(C)C1=CC=CC=C1 XMNIXWIUMCBBBL-UHFFFAOYSA-N 0.000 claims description 2
- 239000001263 FEMA 3042 Substances 0.000 claims description 2
- LRBQNJMCXXYXIU-PPKXGCFTSA-N Penta-digallate-beta-D-glucose Natural products OC1=C(O)C(O)=CC(C(=O)OC=2C(=C(O)C=C(C=2)C(=O)OC[C@@H]2[C@H]([C@H](OC(=O)C=3C=C(OC(=O)C=4C=C(O)C(O)=C(O)C=4)C(O)=C(O)C=3)[C@@H](OC(=O)C=3C=C(OC(=O)C=4C=C(O)C(O)=C(O)C=4)C(O)=C(O)C=3)[C@H](OC(=O)C=3C=C(OC(=O)C=4C=C(O)C(O)=C(O)C=4)C(O)=C(O)C=3)O2)OC(=O)C=2C=C(OC(=O)C=3C=C(O)C(O)=C(O)C=3)C(O)=C(O)C=2)O)=C1 LRBQNJMCXXYXIU-PPKXGCFTSA-N 0.000 claims description 2
- BLRPTPMANUNPDV-UHFFFAOYSA-N Silane Chemical compound [SiH4] BLRPTPMANUNPDV-UHFFFAOYSA-N 0.000 claims description 2
- DAKWPKUUDNSNPN-UHFFFAOYSA-N Trimethylolpropane triacrylate Chemical compound C=CC(=O)OCC(CC)(COC(=O)C=C)COC(=O)C=C DAKWPKUUDNSNPN-UHFFFAOYSA-N 0.000 claims description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 2
- 238000000498 ball milling Methods 0.000 claims description 2
- 229910052796 boron Inorganic materials 0.000 claims description 2
- -1 boron aluminate Chemical class 0.000 claims description 2
- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 claims description 2
- KSEBMYQBYZTDHS-HWKANZROSA-N ferulic acid Chemical compound COC1=CC(\C=C\C(O)=O)=CC=C1O KSEBMYQBYZTDHS-HWKANZROSA-N 0.000 claims description 2
- 229940114124 ferulic acid Drugs 0.000 claims description 2
- KSEBMYQBYZTDHS-UHFFFAOYSA-N ferulic acid Natural products COC1=CC(C=CC(O)=O)=CC=C1O KSEBMYQBYZTDHS-UHFFFAOYSA-N 0.000 claims description 2
- 235000001785 ferulic acid Nutrition 0.000 claims description 2
- 235000004515 gallic acid Nutrition 0.000 claims description 2
- 229940074391 gallic acid Drugs 0.000 claims description 2
- 229960005219 gentisic acid Drugs 0.000 claims description 2
- 229910000077 silane Inorganic materials 0.000 claims description 2
- RMAQACBXLXPBSY-UHFFFAOYSA-N silicic acid Chemical compound O[Si](O)(O)O RMAQACBXLXPBSY-UHFFFAOYSA-N 0.000 claims description 2
- 235000012239 silicon dioxide Nutrition 0.000 claims description 2
- 238000004381 surface treatment Methods 0.000 claims description 2
- 235000015523 tannic acid Nutrition 0.000 claims description 2
- LRBQNJMCXXYXIU-NRMVVENXSA-N tannic acid Chemical compound OC1=C(O)C(O)=CC(C(=O)OC=2C(=C(O)C=C(C=2)C(=O)OC[C@@H]2[C@H]([C@H](OC(=O)C=3C=C(OC(=O)C=4C=C(O)C(O)=C(O)C=4)C(O)=C(O)C=3)[C@@H](OC(=O)C=3C=C(OC(=O)C=4C=C(O)C(O)=C(O)C=4)C(O)=C(O)C=3)[C@@H](OC(=O)C=3C=C(OC(=O)C=4C=C(O)C(O)=C(O)C=4)C(O)=C(O)C=3)O2)OC(=O)C=2C=C(OC(=O)C=3C=C(O)C(O)=C(O)C=3)C(O)=C(O)C=2)O)=C1 LRBQNJMCXXYXIU-NRMVVENXSA-N 0.000 claims description 2
- 229940033123 tannic acid Drugs 0.000 claims description 2
- 229920002258 tannic acid Polymers 0.000 claims description 2
- QURCVMIEKCOAJU-UHFFFAOYSA-N trans-isoferulic acid Natural products COC1=CC=C(C=CC(O)=O)C=C1O QURCVMIEKCOAJU-UHFFFAOYSA-N 0.000 claims description 2
- 238000005253 cladding Methods 0.000 claims 1
- 238000005538 encapsulation Methods 0.000 claims 1
- 239000012783 reinforcing fiber Substances 0.000 claims 1
- 239000011159 matrix material Substances 0.000 abstract description 8
- 230000001965 increasing effect Effects 0.000 abstract description 4
- 230000002411 adverse Effects 0.000 abstract description 3
- 230000000694 effects Effects 0.000 abstract description 3
- 239000012776 electronic material Substances 0.000 abstract description 2
- 239000002131 composite material Substances 0.000 description 9
- 239000000463 material Substances 0.000 description 9
- 230000000052 comparative effect Effects 0.000 description 8
- 239000003365 glass fiber Substances 0.000 description 7
- 238000002360 preparation method Methods 0.000 description 5
- 239000011521 glass Substances 0.000 description 4
- 238000001465 metallisation Methods 0.000 description 4
- 229920000642 polymer Polymers 0.000 description 4
- 239000000758 substrate Substances 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000017525 heat dissipation Effects 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 150000004760 silicates Chemical class 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- 208000036758 Postinfectious cerebellitis Diseases 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000007667 floating Methods 0.000 description 2
- 238000005470 impregnation Methods 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 230000000704 physical effect Effects 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000004132 cross linking Methods 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000003989 dielectric material Substances 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 238000009776 industrial production Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000004377 microelectronic Methods 0.000 description 1
- 239000005022 packaging material Substances 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
Images
Landscapes
- Reinforced Plastic Materials (AREA)
- Laminated Bodies (AREA)
Abstract
The invention discloses a prepreg for a high-thermal-conductivity packaging carrier plate and a manufacturing method of a copper-clad plate using the prepreg, and belongs to the technical field of electronic materials. The prepreg comprises a reinforced fiber cloth core and a resin layer coated outside the reinforced cloth core; the reinforced cloth core is silicon carbide fiber cloth, and the silicon carbide fiber cloth is modified silicon carbide fiber cloth subjected to surface reinforcing modification treatment; according to the invention, the silicon carbide fiber cloth is modified, so that adverse effects caused by high dielectric constant of silicon carbide are reduced, the bonding force between the silicon carbide fiber and matrix resin, and the compatibility and the cohesiveness between the heat-conducting filler and the matrix resin and between the heat-conducting filler and the silicon carbide fiber are increased, the peeling strength of the prepreg and the copper foil can be improved, and the heat conductivity coefficient of the copper-clad plate can be further improved.
Description
Technical Field
The invention belongs to the technical field of electronic materials, and particularly relates to a prepreg for a high-thermal-conductivity packaging carrier plate and a manufacturing method of a copper-clad plate using the prepreg.
Background
With the continuous development of microelectronic technology, the variety of electronic devices is diversified, the integration density is increased, and heat dissipation becomes one of important influencing factors in the design and manufacture of high-density devices, particularly high-power devices such as LEDs, power modules, cameras and the like, and the requirements on heat dissipation are higher than those of common devices. The thermal conductivity of the package carrier is improved, which is one of the main approaches for high power applications.
The prepreg and the copper-clad plate are basic materials for manufacturing the packaging carrier plate, and the prepreg and the copper-clad plate are prepared by taking glass fiber cloth as a reinforcing framework material at present, but the glass fiber cloth has low thermal conductivity which is usually 0.2-2.2W/m.K, and is difficult to meet the heat dissipation requirement. Wong C P, bollamparyr S, journal of Applied Polymer Science,2015,74 (14): 3396-3403 describes a method for improving the thermal conductivity of a resin substrate by changing the molecular chain structure of the Polymer itself to improve the order of the physical structure, reduce the phonon scattering and reduce the thermal resistance of the Polymer itself, but this method is not easy to implement, and has high cost and is not suitable for industrial production. Documents Chen H, ginzburg V, progress in Polymer Science,2016,59, and Gao J S, shiu S C, journal of Composite Materials,2013,47 (4): 449-458: the common heat-conducting fillers such as silicon carbide and boron nitride are added, the heat-conducting performance of the composite material can be improved by utilizing the interaction of the resin base material and the heat-conducting fillers, but the method needs to be filled with a large amount of heat-conducting filler powder, the heat-conducting filler powder is poor in dispersion uniformity, physical properties such as resin dielectric, hardness and thermal expansion and contraction rate can be changed, and processes such as drilling, pressing and hole metallization in carrier plate manufacturing are influenced.
In recent years, various composite materials with an isolation structure show excellent heat conduction and electric conductivity, such as silicon carbide fiber materials, which have the advantages of strong high-temperature bearing capacity, high hardness, oxidation resistance, wear resistance, large heat conductivity, small thermal expansion coefficient, chemical corrosion resistance and the like, and the heat conductivity of the materials can reach 16.7W/m.K, and specific values are shown in Table 1. The composite material has a larger length-diameter ratio, can effectively contact with each other to form a heat-conducting network, and the compounding of the silicon carbide fiber and the heat-conducting filler can not only increase the contact area of the silicon carbide fiber and the matrix resin, but also effectively promote the directional distribution of the heat-conducting particles so as to improve the heat-conducting property of the composite material.
TABLE 1 physical properties such as thermal conductivity of each material
Patent CN202210170426 discloses a high-frequency copper-clad plate of high heat conduction hydrocarbon resin base prepreg and preparation thereof, adopts carborundum fiber cloth to simply replace glass fiber cloth, obtains the high-frequency copper-clad plate through impregnating hydrocarbon resin glue solution, and this high-frequency copper-clad plate has advantages such as low dielectric constant, low dielectric loss, high heat conductivility, high peel strength. However, since silicon carbide has a dielectric constant of 9.66 to 10.03 (300K, table 1), it is a high dielectric material and is not suitable for high-frequency and high-speed signal transmission. Secondly, the prepreg and the copper-clad plate thereof have high chemical stability, so that the catalyst is difficult to adsorb during the metallization of through holes and blind holes which are interconnected among layers, copper deposition is not facilitated, and the silicon carbide fiber cloth has the problems of poor bonding force with resin and the like, so that the application of the silicon carbide prepreg and the copper-clad plate in a packaging carrier plate is limited.
Disclosure of Invention
The invention aims to: the prepreg for the high-heat-conduction packaging carrier plate is characterized in that surface enhancement modification treatment is carried out on the silicon carbide fiber cloth, adverse effects caused by high dielectric constant and high chemical stability of silicon carbide are reduced, the binding force between the silicon carbide fiber and matrix resin, the compatibility and the cohesiveness between the heat-conduction filler and the matrix resin and between the heat-conduction filler and the silicon carbide fiber are increased, and the peel strength, the tensile strength and the heat-conduction performance of a copper-clad plate of the silicon carbide fiber cloth and a copper foil are improved.
Another object of the invention is: the prepared silicon carbide fiber copper-clad plate has high heat-conducting property, low dielectric constant and dielectric loss and better through hole metallization characteristic, and is particularly suitable for manufacturing the carrier plate for packaging high-power devices such as LEDs, PICs and the like. .
In order to realize the purpose, the invention adopts the following technical scheme:
a prepreg for a high-thermal-conductivity packaging carrier plate comprises a reinforced fiber cloth core and a resin layer coated outside the reinforced cloth core;
the reinforced cloth core is silicon carbide fiber cloth, and the silicon carbide fiber cloth is modified silicon carbide fiber cloth subjected to surface reinforcing modification treatment;
the resin layer is obtained by curing and drying a resin glue solution, and the resin glue solution comprises the following components in parts by weight: cyanate ester: 15-30 parts by weight of hydrocarbon resin: 30-60 parts by weight of heat-conducting powder: 5-10 parts by weight of curing agent: 5-15 parts by weight, solvent: 30 to 50 parts by weight.
Further, the preparation method of the modified silicon carbide fiber cloth comprises the following steps:
s1, soaking silicon carbide fiber pulp in 0.1-3 mg/mL polyphenol water solution A for 20-30 min, adding a solution containing a water-based adhesive, papermaking and forming, and performing vacuum drying to obtain a silicon carbide fiber cloth core;
s2, putting the reinforced cloth core into dipping slurry C, dipping for 30-60 min, taking out, and vacuum drying to obtain the modified silicon carbide fiber cloth core, wherein the dipping slurry C is 20-30 parts by mass of silicate solution and 30-60K 2 Ti 6 O 13 The pH value of the dipping slurry C is controlled within the range of 7 to 9 by using silicic acid.
Furthermore, the polyphenol solution A is one or a mixture of more of tannic acid, gentisic acid, ferulic acid, gallic acid and protocatechuic acid.
Further, the curing agent is one or more of triallyl isocyanurate, dicumyl peroxide and trimethylolpropane triacrylate.
Further, the heat-conducting powder is one or more of hexagonal boron nitride, alumina, spherical aluminum nitride and boron aluminate whiskers, and the particle size of the heat-conducting filler is 0.5-5 um.
Further, the prepreg for the high-thermal-conductivity packaging carrier plate is prepared by the following steps:
s1, adding 15-30 parts by weight of cyanate ester and 30-60 parts by weight of hydrocarbon resin into a solvent at the temperature of 70-110 ℃ for full dissolution, heating the solvent to 100-130 ℃, adding 5-10 parts by weight of heat-conducting powder, 1-5 parts by weight of curing agent and the rest solvent, keeping the temperature at 100-130 ℃, and stirring until the mixture is uniform to obtain a resin glue solution;
and S2, placing the reinforced cloth core into the resin glue solution obtained in the step S1, soaking for 10-30 min, curing at 120-200 ℃ for 1-10 h, and cooling to room temperature after curing to obtain the high-thermal-conductivity resin-based prepreg.
Furthermore, the heat-conducting powder is hexagonal boron nitride, and is added into the resin glue solution after ball milling, drying and silane surface treatment in sequence.
The invention also provides a copper-clad plate prepared by using the prepreg for the high-thermal-conductivity packaging carrier plate, and the copper-clad plate is prepared by the following steps: the high-thermal-conductivity resin-based prepreg and the copper foil are symmetrically overlapped, then the prepreg and the copper foil are placed into a hot press, and the copper-clad plate is obtained by hot pressing after vacuumizing, wherein the conditions of the hot pressing process are as follows: the temperature is 150-350 ℃, the pressing time is 2-8 h, and the pressure is 1-50 MPa.
Due to the adoption of the technical scheme, the invention has the following advantages:
1. the prepreg for the high-thermal-conductivity packaging carrier plate comprises a reinforcing cloth core and a resin layer, wherein the reinforcing cloth core is a silicon carbide fiber cloth core, and the silicon carbide fiber has excellent performances of high thermal conductivity coefficient, high strength, high modulus, high temperature resistance, oxidation resistance, low thermal expansion coefficient and the like, and is beneficial to design and manufacture of high-power and high-density devices.
2. The treatment liquid used in the modification treatment process of the reinforced cloth core comprises silicate solution, composite glass powder and acetone solution. Silicates are the most widely used materials in inorganic adhesives, havingRegular tetrahedronThe structure improves the porosity of a matrix and reduces the density of the material by introducing air pores, so that the number of polarized molecules in unit volume is reduced, and the dielectric constant of the material is reduced. Meanwhile, the adhesive has good adhesion, and can meet the adhesion requirements of silicon carbide and common materials such as ceramics, glass, packaging materials, metals and the like. However, with a single silicate adhesive, the bond strength tends to decrease over time, and K is 2 Ti 6 O 13 The whisker modified silicate solution can improve the stability of the silicate adhesive to a certain extent. The glass powder also has good affinity and good compatibility with resin, and is a good adhesive. Silicon carbide fibers have the advantage of high thermal conductivity, while also having the disadvantages of high dielectric constant and poor bonding to resins. The solution such as silicate is utilized to carry out surface enhancement coating modification treatment, thus reducing the adverse effect caused by the high dielectric constant of the silicon carbide, increasing the bonding force between the silicon carbide fiber and matrix resin, the compatibility and the cohesiveness between the heat-conducting filler and the matrix resin and between the heat-conducting filler and the silicon carbide fiber, and further improving the heat conductivity coefficient of the copper-clad plate.
3. According to the invention, the reinforcing cloth core is preferably prepared by taking polyphenol as a modified solution, after impregnation, the polyphenol is attached to the surface of the composite fiber, and when a prepreg is prepared, the polyphenol on the surface of the composite fiber can participate in the cross-linking curing reaction of hydrocarbon resin and cyanate ester, so that the bonding force between the silicon carbide fiber and the resin can be further enhanced.
Drawings
FIG. 1 is a comparison of samples of silicon carbide fiber substrate subjected to reinforcing modification treatment and samples of silicon carbide fiber substrate not subjected to reinforcing modification treatment, wherein A is cracking of the silicon carbide fiber substrate after tin floating of the samples which are not subjected to reinforcing modification treatment; b is that the sample is not cracked after tin floating of the sample is treated by the silicon carbide fiber for enhancing and modifying;
FIG. 2 is a diagram of an actual product prepared by using the copper-clad plate obtained by the method of the present invention, wherein A is a diagram of an actual product of a power management chip carrier plate prepared by using the copper-clad plate obtained by the method; b is a real object diagram of the packaging carrier plate prepared by the copper-clad plate obtained by the method.
Detailed Description
The invention is further illustrated by the following examples, which are not intended to limit the scope of the invention as claimed.
Example 1
The prepreg for the high-thermal-conductivity packaging carrier plate provided by the embodiment comprises a reinforced fiber cloth core and a resin layer coated outside the reinforced cloth core; the reinforced cloth core is silicon carbide fiber cloth, and the silicon carbide fiber cloth is modified silicon carbide fiber cloth with the surface subjected to surface reinforcing modification treatment; the resin layer is obtained by drying resin glue solution, and the resin glue solution comprises the following components in parts by weight: cyanate ester: 25 parts by weight, hydrocarbon resin: 30 parts by weight, heat conductive powder: 5 parts by weight, curing agent: 5 parts by weight, solvent: 30 parts by weight.
The preparation method of the modified silicon carbide fiber cloth comprises the following steps:
s1, soaking silicon carbide fiber pulp in 0.1mg/mL polyphenol water solution for 20min, adding a water-based adhesive, making paper, forming, and drying in vacuum to obtain a silicon carbide fiber cloth core;
s2, placing the reinforced cloth core into the dipping slurry for dipping for 30min, and drying in vacuum to obtain the modified silicon carbide fiber cloth core, wherein the dipping solution is 40 parts by mass of K 2 Ti 6 O 13 Whisker modified silicate solution and 20 parts by mass of composite glass powder. . The pH of the impregnation solution was 8.
The prepreg for the high-thermal-conductivity packaging carrier plate is prepared by the following steps:
s1, adding 15 parts by mass of cyanate ester and 30 parts by mass of hydrocarbon resin into a 100-DEG C solvent for sufficient dissolution, heating the solvent to 110 ℃, adding 8 parts by mass of hexagonal boron nitride, 3 parts by weight of a curing agent and the rest of the solvent, keeping the temperature at 110 ℃, and stirring until the mixture is uniform to obtain a resin glue solution;
and S2, placing the reinforced cloth core into the resin glue solution obtained in the step S1, soaking for 30min, curing at 185 ℃ for 3h, and cooling to room temperature after curing to obtain the high-thermal-conductivity resin-based prepreg.
The invention also provides a copper-clad plate prepared by using the prepreg for the high-thermal-conductivity packaging carrier plate, and the copper-clad plate is prepared by the following steps: the high-thermal-conductivity resin-based prepreg and the copper foil are symmetrically overlapped, then the prepreg and the copper foil are placed into a hot press, and the copper-clad plate is obtained by hot pressing after vacuumizing, wherein the conditions of the hot pressing process are as follows: the temperature is 210 ℃, the pressing time is 3.5h, and the pressure is 25MPa.
Comparative example 1
The prepreg for the package carrier provided by the embodiment comprises a reinforced fiber cloth core and a resin layer coated outside the reinforced fiber cloth core; the reinforced cloth core is made of silicon carbide fiber cloth, the resin layer is obtained by drying resin glue liquid, and the resin glue liquid comprises the following components in parts by weight: cyanate ester: 25 parts by weight, hydrocarbon resin: 30 parts by weight, heat conductive powder: 5 parts by weight, curing agent: 5 parts by weight, solvent: 30 parts by weight.
The preparation method of the silicon carbide fiber cloth comprises the following steps:
s1, soaking silicon carbide fiber pulp in 0.1mg/mL polyphenol water solution for 20min, adding a water-based adhesive, making paper, molding, and drying in vacuum to obtain a silicon carbide fiber cloth core;
the prepreg for the high-thermal-conductivity packaging carrier plate is prepared by the following steps:
s1, adding 15 parts by mass of cyanate ester and 30 parts by mass of hydrocarbon resin into a 100-DEG C solvent for full dissolution, heating the solvent to 110 ℃, adding 8 parts by mass of hexagonal boron nitride, 3 parts by mass of a curing agent and the rest of the solvent, keeping the temperature at 110 ℃, and stirring until the mixture is uniform to obtain a resin glue solution;
and S2, placing the reinforced cloth core into the resin glue solution obtained in the step S1, soaking for 30min, curing at 185 ℃ for 3h, and cooling to room temperature after curing to obtain the high-thermal-conductivity resin-based prepreg.
The invention also provides a copper-clad plate prepared by using the prepreg for the high-thermal-conductivity packaging carrier plate, and the copper-clad plate is prepared by the following steps: the high-thermal-conductivity resin-based prepreg and the copper foil are symmetrically overlapped, then the prepreg and the copper foil are placed into a hot press, and the copper-clad plate is obtained by hot pressing after vacuumizing, wherein the conditions of the hot pressing process are as follows: the temperature is 210 ℃, the pressing time is 3.5h, and the pressure is 25MPa.
Comparative example 2
The prepreg for the package carrier board provided by the embodiment comprises a reinforced fiber cloth core and a resin layer coated outside the reinforced cloth core; the reinforced cloth core is glass fiber cloth, the resin layer is obtained by drying resin glue solution, and the resin glue solution comprises the following components in parts by weight: cyanate ester: 25 parts by weight of a hydrocarbon resin: 30 parts by weight, heat conductive powder: 5 parts by weight, curing agent: 5 parts by weight, solvent: 30 parts by weight.
The preparation method of the glass fiber cloth comprises the following steps:
s1, soaking glass fiber pulp in 0.1mg/mL polyphenol water solution for 20min, adding a water-based adhesive, making and molding, and performing vacuum drying to obtain a glass fiber cloth core;
the prepreg for the high-thermal-conductivity packaging carrier plate is prepared by the following steps:
s1, adding 15 parts by mass of cyanate ester and 30 parts by mass of hydrocarbon resin into a 100-DEG C solvent for sufficient dissolution, heating the solvent to 110 ℃, adding 8 parts by mass of hexagonal boron nitride, 3 parts by weight of a curing agent and the rest of the solvent, keeping the temperature at 110 ℃, and stirring until the mixture is uniform to obtain a resin glue solution;
and S2, placing the reinforced cloth core into the resin glue solution obtained in the step S1, soaking for 30min, curing at 185 ℃ for 3h, and cooling to room temperature after curing to obtain the high-thermal-conductivity resin-based prepreg.
And symmetrically superposing the resin-based prepregs prepared in the comparative example 1 and the resin-based prepregs prepared in the comparative example 2 with the copper foil, putting the prepregs into a hot press, vacuumizing and carrying out hot pressing to obtain the copper-clad plate. The hot pressing process meets the following conditions: the temperature is 210 ℃, the pressing time is 3.5h, and the pressure is 25Mpa.
The test methods of comparative examples 1 and 2 were performed according to the IPC-TM 650 related requirements.
And comparing the performance of the copper-clad plates in the example 1, the comparative example 1 and the comparative example 2. The comparative results are shown in Table 2.
Table 2 shows a comparison of the properties of the three examples
Therefore, it is easy to find that the silicon carbide fiber copper-clad plate subjected to surface enhancement modification treatment provided by the embodiment has good comprehensive performance, has high heat conductivity, can achieve a heat conductivity coefficient of 12.8W/m.K, and also has low dielectric constant and dielectric loss, and better through hole metallization characteristics (the highest copper rear backlight index). In addition, the silicon carbide fiber copper-clad plate subjected to the surface enhancement modification treatment provided by the embodiment is not easy to crack, and the copper-clad plate not subjected to the surface enhancement modification treatment is easy to crack inside, as shown in fig. 1, which illustrates that the silicon carbide fiber surface enhancement modification treatment enhances the bonding capability of the silicon carbide fiber and the resin. Therefore, the improved copper-clad plate provided by the embodiment is particularly suitable for manufacturing the carrier plate for packaging high-power devices such as an LED, a PIC and the like, as shown in fig. 2.
The foregoing embodiments are provided merely to illustrate the principles and efficacy of the invention, and not to limit the invention, but rather to facilitate an understanding of the principles of the invention, and the scope of the invention is not limited to the configurations and embodiments described above, and those skilled in the art can make various other specific modifications and combinations without departing from the spirit of the invention, and still be within the scope of the invention.
Claims (8)
1. The utility model provides a high thermally conductive encapsulation prepreg for carrier plate, includes reinforcing fiber cloth core and the cladding at the outside resin layer of reinforcing cloth core, its characterized in that:
the reinforced cloth core is silicon carbide fiber cloth, and the silicon carbide fiber cloth is modified silicon carbide fiber cloth subjected to surface reinforcing modification treatment;
the resin layer is obtained by curing and drying resin glue solution, and the resin glue solution comprises the following components in parts by weight: cyanate ester: 15-30 parts by weight of hydrocarbon resin: 30-60 parts by weight of heat-conducting powder: 5-10 parts by weight of curing agent: 5-15 parts by weight, solvent: 30 to 50 portions.
2. The prepreg for the packaging carrier plate with high thermal conductivity according to claim 1, wherein the modified silicon carbide fiber cloth is prepared by the following steps:
s1, soaking silicon carbide fiber pulp in 0.1-3 mg/mL polyphenol water solution A for 20-30 min, adding a solution containing a water-based adhesive, papermaking, forming and vacuum drying to obtain a silicon carbide fiber cloth core;
s2, placing the reinforced cloth core into a dipping slurry C, dipping for 30-60 min, taking out, and drying in vacuum to obtain the modified silicon carbide fiber cloth core, wherein the dipping slurry C is 20-30 parts by mass of silicate solution and 30-60K 2 Ti 6 O 13 The pH value of the dipping slurry C is controlled within the range of 7 to 9 by using silicic acid.
3. The prepreg according to claim 2, wherein: the polyphenol solution A is one or more of tannic acid, gentisic acid, ferulic acid, gallic acid and protocatechuic acid.
4. The prepreg according to claim 1, wherein: the curing agent is one or more of triallyl isocyanurate, dicumyl peroxide and trimethylolpropane triacrylate.
5. The prepreg according to claim 1, wherein: the heat-conducting powder is one or more of hexagonal boron nitride, alumina, spherical aluminum nitride and boron aluminate whiskers, and the particle size of the heat-conducting filler is 0.5-5 um.
6. The prepreg according to claim 1, wherein: the prepreg for the high-thermal-conductivity packaging carrier plate is prepared by the following steps:
s1, adding 15-30 parts by weight of cyanate ester and 30-60 parts by weight of hydrocarbon resin into a solvent at the temperature of 70-110 ℃ for full dissolution, heating the solvent to 100-130 ℃, adding 5-10 parts by weight of heat-conducting powder, 1-5 parts by weight of curing agent and the rest solvent, keeping the temperature at 100-130 ℃, and stirring until the mixture is uniform to obtain a resin glue solution;
and S2, placing the reinforced cloth core into the resin glue solution obtained in the step S1, soaking for 10-30 min, curing at 120-200 ℃ for 1-10 h, and cooling to room temperature after curing to obtain the high-thermal-conductivity resin-based prepreg.
7. The prepreg according to claim 6, wherein: the heat conducting powder is hexagonal boron nitride, and the hexagonal boron nitride is added into resin glue solution after ball milling, drying and silane surface treatment in sequence.
8. The copper-clad plate prepared by using the prepreg for the high-thermal-conductivity packaging carrier plate according to claim 1 is characterized by being prepared by the following steps: the high-thermal-conductivity resin-based prepreg and the copper foil are symmetrically overlapped, then the prepreg and the copper foil are placed into a hot press, and the copper-clad plate is obtained by hot pressing after vacuumizing, wherein the conditions of the hot pressing process are as follows: the temperature is 150-350 ℃, the pressing time is 2-8 h, and the pressure is 1-50 MPa.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202211287466.5A CN115926224B (en) | 2022-10-20 | 2022-10-20 | Prepreg for packaging carrier plate with high heat conductivity and manufacturing of copper-clad plate using prepreg |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202211287466.5A CN115926224B (en) | 2022-10-20 | 2022-10-20 | Prepreg for packaging carrier plate with high heat conductivity and manufacturing of copper-clad plate using prepreg |
Publications (2)
Publication Number | Publication Date |
---|---|
CN115926224A true CN115926224A (en) | 2023-04-07 |
CN115926224B CN115926224B (en) | 2024-05-14 |
Family
ID=86696638
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202211287466.5A Active CN115926224B (en) | 2022-10-20 | 2022-10-20 | Prepreg for packaging carrier plate with high heat conductivity and manufacturing of copper-clad plate using prepreg |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN115926224B (en) |
Citations (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101735456A (en) * | 2009-11-24 | 2010-06-16 | 广东生益科技股份有限公司 | High weather-proof thermosetting resin composite and prepreg and copper-clad laminate prepared thereby |
CN102850726A (en) * | 2012-09-07 | 2013-01-02 | 广东生益科技股份有限公司 | Composite material, high frequency circuit substrate produced by using composite material, and production method of high frequency circuit substrate |
WO2014036712A1 (en) * | 2012-09-07 | 2014-03-13 | 广东生益科技股份有限公司 | Composite material, high frequency circuit substrate made from the same, and production method thereof |
JP2015048452A (en) * | 2013-09-04 | 2015-03-16 | 信越化学工業株式会社 | Cyanate ester resin prepreg, laminate substrate, cyanate ester resin metal-clad laminate, and led mounting substrate |
US20150181707A1 (en) * | 2012-06-12 | 2015-06-25 | Mitsubishi Gas Chemical Company, Inc. | Resin composition, prepreg, metal foil-clad laminate and printed wiring board |
CN104844241A (en) * | 2015-04-13 | 2015-08-19 | 安徽省含山瓷业股份有限公司 | High strength carbon fiber reinforced silicon carbide ceramic matrix composite material and preparation method thereof |
CN105860758A (en) * | 2016-05-09 | 2016-08-17 | 安徽爱莱特照明灯具有限公司 | Antibacterial and waterproof insulating paint with high heat conductivity for LED lamp holders and method for manufacturing antibacterial and waterproof insulating paint |
CN108382047A (en) * | 2018-04-01 | 2018-08-10 | 苏州欣天新精密机械有限公司 | A kind of hot melt preparation method of copper-clad plate |
US20210340067A1 (en) * | 2017-03-20 | 2021-11-04 | Government Of The United States As Represented By The Secretary Of The Air Force | Oxidation-resistant fiber coatings and related methods |
WO2022000629A1 (en) * | 2020-06-30 | 2022-01-06 | 瑞声声学科技(深圳)有限公司 | Resin composition, prepreg, laminated board, preparation method for prepreg, preparation method for laminated board and application thereof |
CN114368196A (en) * | 2022-01-10 | 2022-04-19 | 江苏耀鸿电子有限公司 | Epoxy IC packaging support plate and preparation method thereof |
CN114437435A (en) * | 2022-02-24 | 2022-05-06 | 无锡睿龙新材料科技有限公司 | High-thermal-conductivity hydrocarbon resin-based prepreg and high-frequency copper-clad plate prepared from same |
CN114889273A (en) * | 2022-03-23 | 2022-08-12 | 电子科技大学 | Glass fiber-free ceramic/hydrocarbon resin-based microwave medium substrate and preparation method thereof |
CN114932727A (en) * | 2022-05-27 | 2022-08-23 | 江苏耀鸿电子有限公司 | Heat-resistant hydrocarbon resin-based copper-clad plate and preparation method thereof |
-
2022
- 2022-10-20 CN CN202211287466.5A patent/CN115926224B/en active Active
Patent Citations (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101735456A (en) * | 2009-11-24 | 2010-06-16 | 广东生益科技股份有限公司 | High weather-proof thermosetting resin composite and prepreg and copper-clad laminate prepared thereby |
US20150181707A1 (en) * | 2012-06-12 | 2015-06-25 | Mitsubishi Gas Chemical Company, Inc. | Resin composition, prepreg, metal foil-clad laminate and printed wiring board |
CN102850726A (en) * | 2012-09-07 | 2013-01-02 | 广东生益科技股份有限公司 | Composite material, high frequency circuit substrate produced by using composite material, and production method of high frequency circuit substrate |
WO2014036712A1 (en) * | 2012-09-07 | 2014-03-13 | 广东生益科技股份有限公司 | Composite material, high frequency circuit substrate made from the same, and production method thereof |
JP2015048452A (en) * | 2013-09-04 | 2015-03-16 | 信越化学工業株式会社 | Cyanate ester resin prepreg, laminate substrate, cyanate ester resin metal-clad laminate, and led mounting substrate |
CN104844241A (en) * | 2015-04-13 | 2015-08-19 | 安徽省含山瓷业股份有限公司 | High strength carbon fiber reinforced silicon carbide ceramic matrix composite material and preparation method thereof |
CN105860758A (en) * | 2016-05-09 | 2016-08-17 | 安徽爱莱特照明灯具有限公司 | Antibacterial and waterproof insulating paint with high heat conductivity for LED lamp holders and method for manufacturing antibacterial and waterproof insulating paint |
US20210340067A1 (en) * | 2017-03-20 | 2021-11-04 | Government Of The United States As Represented By The Secretary Of The Air Force | Oxidation-resistant fiber coatings and related methods |
CN108382047A (en) * | 2018-04-01 | 2018-08-10 | 苏州欣天新精密机械有限公司 | A kind of hot melt preparation method of copper-clad plate |
WO2022000629A1 (en) * | 2020-06-30 | 2022-01-06 | 瑞声声学科技(深圳)有限公司 | Resin composition, prepreg, laminated board, preparation method for prepreg, preparation method for laminated board and application thereof |
CN114368196A (en) * | 2022-01-10 | 2022-04-19 | 江苏耀鸿电子有限公司 | Epoxy IC packaging support plate and preparation method thereof |
CN114437435A (en) * | 2022-02-24 | 2022-05-06 | 无锡睿龙新材料科技有限公司 | High-thermal-conductivity hydrocarbon resin-based prepreg and high-frequency copper-clad plate prepared from same |
CN114889273A (en) * | 2022-03-23 | 2022-08-12 | 电子科技大学 | Glass fiber-free ceramic/hydrocarbon resin-based microwave medium substrate and preparation method thereof |
CN114932727A (en) * | 2022-05-27 | 2022-08-23 | 江苏耀鸿电子有限公司 | Heat-resistant hydrocarbon resin-based copper-clad plate and preparation method thereof |
Non-Patent Citations (2)
Title |
---|
JJ DONG,等: "Hydrocarbon Resin-Based Composites with Low Thermal Expansion Coefficient and Dielectric Loss for High-Frequency Copper Clad Laminates", 《POLYMERS》, vol. 14, no. 11, 30 June 2022 (2022-06-30), pages 2200 * |
张文根,等: "偶联剂表面处理纳米SiC改性氰酸酯树脂的耐热性研究", 《工程塑料应用》, vol. 40, no. 6, 31 December 2012 (2012-12-31), pages 21 - 24 * |
Also Published As
Publication number | Publication date |
---|---|
CN115926224B (en) | 2024-05-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2016078432A1 (en) | Modified aluminium oxide composite material, copper-coated substrate and preparation method thereof | |
WO2022104949A1 (en) | Thermally conductive composite material and preparation method therefor | |
CN111844951B (en) | High-frequency heat-conducting substrate and preparation method thereof | |
CN109988409B (en) | Boron nitride aggregate, thermosetting resin composition containing boron nitride aggregate and application of thermosetting resin composition | |
CN108570202B (en) | Preparation method of polytetrafluoroethylene composite substrate material | |
Li et al. | Surface modification of boron nitride via poly (dopamine) coating and preparation of acrylonitrile‐butadiene‐styrene copolymer/boron nitride composites with enhanced thermal conductivity | |
Zhai et al. | Cyanate ester resin based composites with high toughness and thermal conductivity | |
CN114621543A (en) | High-frequency prepreg, high-frequency copper-clad plate and preparation method thereof | |
JPH0145417B2 (en) | ||
CN113043680A (en) | High-heat-dissipation aluminum-based copper-clad plate | |
CN108659457A (en) | A kind of boron nitride cladding sulfonated graphene-epoxy resin composite material and preparation method thereof | |
CN114905813A (en) | Low-dielectric-constant high-thermal-conductivity high-frequency metal foil-clad laminated board and manufacturing method thereof | |
CN113150484B (en) | COC-based composite substrate material for high-frequency copper-clad plate and preparation method | |
Ge et al. | Enhancing thermal conductivity of the insulating layer of high-frequency copper clad laminates via incorporating surface modified spherical hBN fillers | |
CN114148048A (en) | High-heat-dissipation aluminum-based copper-clad plate and preparation method thereof | |
CN115926224B (en) | Prepreg for packaging carrier plate with high heat conductivity and manufacturing of copper-clad plate using prepreg | |
CN111825955B (en) | Prepreg for high frequency, preparation method thereof and copper-clad plate and preparation method thereof | |
CN111605267B (en) | Flame-retardant olefin substrate and preparation method thereof | |
CN115322687B (en) | High-heat-conductivity phosphate-based inorganic insulating adhesive and bonding method thereof | |
CN1392219A (en) | High heat conductivity composite material and its preparing method | |
CN114437435A (en) | High-thermal-conductivity hydrocarbon resin-based prepreg and high-frequency copper-clad plate prepared from same | |
CN115483112A (en) | Silicon nitride ceramic copper-clad plate and preparation process thereof | |
CN116042093B (en) | Silicone grease heat dissipation coating, preparation method thereof and electronic product | |
KR20170123394A (en) | Coating composition with improved thermal conductivity and method of forming coating film | |
CN110184008A (en) | A kind of preparation method of epoxy group heat conductive insulating compound cutan |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | 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 |