High-thermal-conductivity composite material with embedded structure and preparation method for high-thermal-conductivity composite material
A high thermal conductivity, composite material technology, applied in the field of composite materials, can solve the problems of inability to use substrate materials, high cost of carbon nanotubes and highly oriented pyrolytic graphite, etc. Effect
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Embodiment 1
[0028] This embodiment provides a method for preparing a high thermal conductivity composite material with an embedded structure, including the following steps:
[0029] (1) Preparation of porous ceramics: pressing porous silicon carbide ceramic powder to obtain a green body; sintering the green body at 1700° C. under a nitrogen atmosphere (60% vol) and keeping it warm for 1 hour to form a porous ceramic;
[0030] (2) Importing ultra-high thermal conductivity materials: embedding nickel-plated diamond micropowder with an average particle size of 320 mesh into the porous ceramic core to obtain a preform;
[0031] (3) Metal smelting: select industrial pure aluminum, put it into a pit furnace for smelting at a temperature of 850°C, and obtain molten aluminum;
[0032] (4) Squeeze casting: put the prefabricated body into a vacuum box furnace for preheating, under argon protection, the preheating temperature is 800°C, and at the same time, the composite mold is preheated to 300°C. ...
Embodiment 2
[0035] This embodiment provides a method for preparing a high thermal conductivity composite material with an embedded structure, which is different from Embodiment 1 in that the embedded high thermal conductivity material is oriented pyrolytic graphite.
Embodiment 3
[0037] This example provides a method for preparing a high thermal conductivity composite material with an embedded structure. The difference from Example 1 is that the metal melting material is magnesium-aluminum alloy AZ81, the melting temperature is 700°C, about 75% air, about 24.8% CO 2 , about 0.2% SF 6 Mixed gas for protection.
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Abstract
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