High-thermal-conductivity carbon fiber composite material with laminated hybrid structure and preparation method of high-thermal-conductivity carbon fiber composite material
A composite material, laminated structure technology, applied in the direction of carbon fiber, heat exchange materials, fiber processing, etc., can solve the limited improvement of the thermal conductivity of composite materials, the limited improvement of thermal conductivity of composite materials, and the interlaminar shear strength of carbon fiber composite materials. Rapid decline and other problems, to achieve the effect of improving thermal conductivity and mechanical properties, reducing thermal resistance in space, and efficient transmission
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Embodiment 1
[0034] In this example, the specific preparation parameters of the carbon fiber composite material with laminated hybrid structure are:
[0035] The carbon fiber is made of T700 orthogonal cloth in the form of fabric, the thickness of each layer of carbon fiber cloth is 0.6mm, the diameter of carbon fiber is 7μm, the number of monofilaments of carbon fiber tow is 12K, and the density is 1.8g / cm 3 .
[0036] The gas used to excite the plasma in the plasma treatment is air, and the plasma treatment time is 15 minutes.
[0037] The copper-containing material is made of spherical pure copper powder with a particle size of 500nm and a specific surface area of 20m 2 / g, bulk density is 2.3g / cm 3 .
[0038] Graphene is selected from graphene nanosheets prepared by oxidation-reduction method, the number of layers is 5 layers, the sheet diameter is 10 μm, and the thickness is 2 nm.
[0039] The spraying method is blended spraying, in which: the concentration of the copper-contain...
Embodiment 2
[0043] The difference from Example 1 is that in this example, the specific preparation parameters of the carbon fiber composite material with laminated hybrid structure are:
[0044] The carbon fiber is made of T700 orthogonal cloth in the form of fabric, the thickness of each layer of carbon fiber cloth is 0.6mm, the diameter of carbon fiber is 7μm, the number of monofilaments of carbon fiber tow is 12K, and the density is 1.8g / cm 3 .
[0045] The gas used to excite the plasma in the plasma treatment is air, and the plasma treatment time is 15 minutes.
[0046] The copper-containing material is flaky pure copper powder, with a diameter of 50 μm, a thickness of 4 nm, and a specific surface area of 5 m 2 / g, the bulk density is 2.5g / cm 3 .
[0047] Graphene is selected from graphene spheres prepared by a spray-drying method, and the particle size is 30 μm.
[0048] The spraying method is alternate spraying, wherein: the concentration of the copper-containing solution is 3...
Embodiment 3
[0052] The difference from Example 1 is that in this example, the specific preparation parameters of the carbon fiber composite material with laminated hybrid structure are:
[0053] The carbon fiber is made of T800 orthogonal cloth in the form of prepreg, the thickness of each layer of prepreg is 0.4mm, the diameter of carbon fiber is 7μm, the number of monofilaments of carbon fiber tow is 6K, and the density is 1.8g / cm 3 .
[0054] The gas used to excite the plasma in the plasma treatment is oxygen with a volume purity of 99.999%, and the plasma treatment time is 30 minutes.
[0055] The copper-containing material is made of spherical pure copper powder, with a particle size of 20 μm and a specific surface area of 6m 2 / g, bulk density is 2.4g / cm 3 .
[0056] Graphene is a graphene sheet prepared by the catalytic intercalation expansion exfoliation method, with 6 layers, a sheet diameter of 50 μm, and a thickness of 2.5 nm.
[0057] The spraying method is blended spray...
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