Preparation method of CEM-3 copper clad plate with high heat conductivity
A technology of copper-clad laminates and high thermal conductivity, which is applied in the direction of chemical instruments and methods, printed circuit manufacturing, circuit substrate materials, etc., can solve the problems of shortened life, large thermal expansion coefficient, and increased power consumption, and achieve the effect of improving heat dissipation
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Embodiment 1
[0027] Embodiment 1: A kind of preparation method of CEM-3 copper-clad laminate
[0028] a. prepare core material resin, its component parts by weight are:
[0029] 90 parts of bisphenol A type epoxy resin, 10 parts of novolak type epoxy resin,
[0030] 30 parts of phenolic resin, 240 parts of filler Al2O3,
[0031] 10 parts of filler titanium dioxide, 20 parts of filler talcum powder
[0032] 4.5 parts of coupling agent KH-560 0.03 parts of curing accelerator 2-ethyl-4-methylimidazole,
[0033] b. The above materials are prepared into a resin solution for the core material with methyl ethyl ketone;
[0034] c. Impregnate the glass fiber paper with the above resin solution, and make it into a semi-cured state at a temperature of 130-210°C to make a core material bonding sheet.
[0035] d. Prepare the fabric resin matrix, its components (parts by weight) are:
[0036] 70 parts of bisphenol A type epoxy resin, 30 parts of brominated epoxy resin,
[0037] Nitrogen-containin...
Embodiment 2
[0042] Embodiment 2: A kind of preparation method of CEM-3 copper-clad laminate
[0043] a. prepare core material resin, its component parts by weight are:
[0044] 90 parts of bisphenol A type epoxy resin, 10 parts of novolak type epoxy resin,
[0045] 20 parts of phenolic resin, filler Al(OH) 3 40 copies,
[0046] Filler boron nitride 80 parts, coupling agent KH-560 1.5 parts,
[0047] Curing accelerator 2-ethyl-4-methylimidazole 0.4 parts
[0048] b. The above materials are prepared into a resin solution for the core material with methyl ethyl ketone;
[0049] c. Impregnate the glass fiber paper with the above resin solution, dry it at 130-210°C, and slice it to make core material;
[0050] d. prepare fabric resin, its component (weight part) is:
[0051] 70 parts of bisphenol A epoxy resin, 30 parts of brominated epoxy resin,
[0052] Nitrogen-containing novolak type phenolic resin 30 parts Al(OH) 3 40 copies,
[0053] 60 parts of aluminum nitride, 0...
Embodiment 3
[0057] Embodiment 3: A kind of preparation method of CEM-3 copper clad laminate
[0058] A. prepare core material resin, its component (weight part) is:
[0059] 100 parts of bisphenol A type epoxy resin, 25 parts of phenolic resin,
[0060] Filler Al(OH) 3 80 parts, 20 parts of filler aluminum nitride,
[0061] 120 parts of filler magnesium oxide, 2.5 parts of coupling agent KH-560;
[0062] 0.1 part of curing accelerator 2-ethyl-4-methylimidazole.
[0063] b. The above materials are prepared into a resin solution for the core material with methyl ethyl ketone;
[0064] c. Impregnate the glass fiber paper with the above resin solution, dry it at 130-210°C, and slice it to make core material;
[0065] d. prepare fabric resin, its component is:
[0066] 70 parts of bisphenol A type epoxy resin, 30 parts of brominated epoxy resin,
[0067] Nitrogen-containing novolak type phenolic resin 25 parts Mg(OH) 3 30 servings,
[0068] 40 parts of aluminum nitride, 0.2 pa...
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