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Preparation method of silicon carbide ceramic-based composite material based on regulation and control of infiltration preform pore structure

A technology of silicon carbide ceramic matrix and composite materials, which is applied in the direction of ceramic products, other household appliances, household appliances, etc., can solve the fiber space obstruction, it is difficult to obtain a uniform pore structure, and it is difficult to obtain silicon carbide ceramic composite materials with low residual silicon and other problems, to achieve the effect of reducing the residual silicon content of the material and improving the overall performance

Inactive Publication Date: 2022-07-01
SHANGHAI INST OF CERAMIC CHEM & TECH CHINESE ACAD OF SCI
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  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the main technical methods for regulating the pore structure of preforms are chemical vapor infiltration, slurry impregnation, and organic precursor impregnation and cracking methods. Due to the steric hindrance effect of fibers, these methods are difficult to obtain a uniform pore structure and carbonization with low residual silicon. Silicon Ceramic Composite

Method used

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  • Preparation method of silicon carbide ceramic-based composite material based on regulation and control of infiltration preform pore structure
  • Preparation method of silicon carbide ceramic-based composite material based on regulation and control of infiltration preform pore structure
  • Preparation method of silicon carbide ceramic-based composite material based on regulation and control of infiltration preform pore structure

Examples

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Embodiment 1

[0047] An infiltration preform pore structure regulation and preparation method of a silicon carbide ceramic matrix composite material, the specific steps of which are:

[0048] (1) Ball milling the silicon carbide powder, the binder and the solvent to obtain a uniform and stable slurry: the particle size of the silicon carbide powder is 2 μm, and polyvinyl alcohol and ethanol are the binder and the solvent, respectively. The mass ratio of silicon carbide powder, polyvinyl alcohol and ethanol is 30:10:60, the ball milling speed is 90 rpm, and the time is 24 hours;

[0049] (2) Immerse the above slurry into carbon fiber cloth to obtain a fiber impregnated sheet, and the impregnated sheet is cut, dried, pressurized and cured, and subjected to a first pyrolysis treatment to obtain a preform. The thickness of the obtained fiber-impregnated sheet was 0.5 mm. After the fiber-impregnated sheets are laminated (8 layers in total), the curing temperature is 100° C., the curing holding ...

Embodiment 2

[0053] Similar to the steps in Example 1, the difference is: in step (1), the particle size of the silicon carbide powder is 5 μm, and polyvinyl butyral is the binder, wherein the silicon carbide powder, the binder and the The mass ratio of the solvent was 40:10:50. The volume fraction of silicon carbide powder in the obtained infiltration preform is 40 vol%, and the volume fraction of pore-forming carbon in the infiltration preform is 15 vol%.

Embodiment 3

[0055] Similar to the steps in Example 1, the difference is: (1) silicon carbide fiber cloth; (2) the components of the pore-forming slurry are epoxy resin, polyvinylpyrrolidone and ethanol, and the mass ratio is 40:20: 40. The volume fraction of silicon carbide powder in the obtained infiltration preform is 40 vol%, and the volume fraction of pore-forming carbon in the infiltration preform is 10 vol%.

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Abstract

The invention relates to a preparation method of a silicon carbide ceramic-based composite material based on regulation and control of an infiltration preform pore structure, which comprises the following steps: (1) impregnating fiber cloth in silicon carbide slurry and taking out to obtain a fiber impregnated sheet, and then carrying out cutting, drying, pressurized curing and first pyrolysis treatment to obtain a preform; (2) mixing organic resin, a pore-forming agent and a solvent to obtain pore-forming slurry; (3) carrying out vacuum impregnation on the obtained preform in pore-forming slurry, taking out the preform, and carrying out curing and secondary pyrolysis treatment to obtain an infiltration preform; and (4) embedding the obtained infiltration preform with silicon powder or / and silicon alloy powder, and carrying out reactive sintering to obtain the silicon carbide ceramic-based composite material.

Description

technical field [0001] The invention relates to a preparation method of a silicon carbide ceramic matrix composite material based on the regulation of the pore structure of an infiltration preform, and belongs to the technical field of aerospace thermal structure ceramic matrix composite materials. Background technique [0002] The new generation of high thrust-to-weight ratio aero-engines have a high temperature take-off gas temperature before the turbine as high as about 1700 °C, far exceeding the temperature limit (~1100 °C) that the nickel-based superalloy with the best heat resistance can withstand. Compared with superalloys, fiber-reinforced silicon carbide ceramic matrix composites have high specific strength, high specific modulus, non-brittle fracture, and excellent high temperature resistance and oxidation resistance. The best choice for high-temperature structural materials for first-generation aero-engines. [0003] The preparation methods of silicon carbide cer...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C04B38/06C04B35/80C04B35/565C04B35/622
CPCC04B38/06C04B38/068C04B35/565C04B35/622C04B2235/6567C04B2235/6581
Inventor 陈小武张俊敏董绍明张翔宇杨金山阚艳梅胡建宝廖春景
Owner SHANGHAI INST OF CERAMIC CHEM & TECH CHINESE ACAD OF SCI