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A kind of anti-oxidation coating on the surface of carbon-silicon carbide composite material and its preparation method

An anti-oxidation coating and composite material technology, which is applied in the field of carbon-silicon carbide composite ceramic coatings, can solve the problems of high thermal stress, easy cracking, and mismatching thermal expansion coefficients of the coating, and achieve high-temperature oxidation resistance. Effect of reducing brittle fracture and improving fracture toughness

Active Publication Date: 2022-02-01
AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, the thermal expansion coefficient mismatch between the composite material and the ceramic coating and the microcracks in the coating lead to a large thermal stress in the coating, which is easy to crack during the high-low temperature transition process, and the high-temperature anti-oxidation effect still needs to be improved.

Method used

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  • A kind of anti-oxidation coating on the surface of carbon-silicon carbide composite material and its preparation method
  • A kind of anti-oxidation coating on the surface of carbon-silicon carbide composite material and its preparation method

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preparation example Construction

[0056] (c) Fabrication method of vertical graphene arrays

[0057] In some preferred embodiments of the present invention, the vertical graphene array layer is grown on the surface of the carbon-silicon carbide composite material by plasma-assisted chemical vapor deposition.

[0058] Specifically, the method includes the following steps: placing the carbon-silicon carbide composite material in the cavity of a chemical vapor deposition device, vacuuming, purging, and programming the temperature, and then turning on the carbon source and the plasma generating device, and the carbon source is cracked into Plasma, the plasma is deposited on the carbon-silicon carbide composite material to obtain a vertical graphene array layer.

[0059] The number of layers of graphene can be controlled and adjusted through the deposition conditions, and the size is positively correlated with the deposition time. Vertical graphene with different sizes can be prepared by controlling the deposition ...

Embodiment 1

[0085] S1. Grind and polish the carbon-silicon carbide composite material with No. 400, No. 800 and No. 1000 sandpaper respectively, then clean it with absolute ethanol, and then dry it in an oven at 80°C. Step S1 can provide a clean s surface.

[0086] S2, using plasma-assisted chemical vapor deposition to deposit a vertical graphene array layer on the surface of the carbon-silicon carbide composite material, specifically including the following steps:

[0087] Place the carbon-silicon carbide composite material treated by S1 in the plasma chamber, close the chamber, and use a mechanical pump to draw a vacuum to make the pressure in the chamber reach 0.2mbar; open the argon gas for scrubbing, and adjust the flow rate of the argon gas to 200sccm. The control valve adjusts the pressure in the plasma chamber to 50mbar and keeps it stable; then the temperature is raised to 550°C through program control; after the temperature in the chamber is stabilized, turn off the argon gas; t...

Embodiment 2

[0091] S1. Grind and polish the carbon-silicon carbide composite material with No. 400, No. 800 and No. 1000 sandpaper respectively, then clean it with absolute ethanol, and then dry it in an oven at 80°C. Step S1 can provide a clean s surface.

[0092] S2, using plasma-assisted chemical vapor deposition to deposit a vertical graphene array layer on the surface of the carbon-silicon carbide composite material, specifically including the following steps:

[0093] Place the carbon-silicon carbide composite material treated by S1 in the plasma chamber, close the chamber, and use a mechanical pump to draw a vacuum to make the pressure in the chamber reach 0.2mbar; open the argon gas for scrubbing, and adjust the flow rate of the argon gas to 200sccm. The control valve adjusts the pressure in the plasma chamber to 50mbar and keeps it stable; then the temperature is raised to 650°C through program control; after the temperature in the chamber is stable, turn off the argon gas; 6. Tu...

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Abstract

The invention relates to an anti-oxidation coating on the surface of a carbon-silicon carbide composite material and a preparation method thereof. The anti-oxidation coating includes: a vertical graphene array layer combined with a base carbon-silicon carbide composite material; and a ceramic coating formed by depositing on the vertical graphene array layer. The method comprises the following steps: (1) growing a vertical graphene array layer on the surface of a carbon-silicon carbide composite material by plasma-assisted chemical vapor deposition; and (2) depositing a ceramic coating on the vertical graphene array layer . The present invention adopts the vertical graphene array to toughen the carbon-silicon carbide composite ceramic coating, and the addition of the vertical graphene array improves the fracture toughness of the ceramic coating and reduces the brittleness of the ceramic coating during high-temperature friction Fracture, thereby improving the high temperature oxidation resistance of the coating.

Description

technical field [0001] The invention relates to the technical field of carbon-silicon carbide composite ceramic coatings, in particular to a carbon-silicon carbide composite surface oxidation-resistant coating and a preparation method thereof. Background technique [0002] At present, carbon-silicon carbide composite materials have excellent properties such as light weight, high specific strength, high specific modulus, and high temperature resistance, and are widely used in aerospace and other military fields. However, the high temperature and easy oxidation of carbon-silicon carbide composite materials is the biggest obstacle encountered in its practical application. The preparation of ceramic coatings on the surface of composite materials can effectively isolate the composite material from the external environment, protect the substrate from high temperature oxidation, and exert the excellent performance of the composite material. However, the thermal expansion coefficie...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C04B41/85
CPCC04B41/009C04B41/5001C04B41/85C04B41/5059C04B41/4531C04B41/4558
Inventor 杨良伟宋环君刘伟刘俊鹏于新民李晓东霍鹏飞于艺杨冰洋金鑫张昊
Owner AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH