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Bn nanotube interfacial phase strengthened and toughened carbon fiber reinforced ceramic matrix composite material and preparation method thereof

A composite material and fiber reinforced technology, applied in the field of composite materials, can solve the problems of reducing the comprehensive mechanical properties of materials, reducing fiber content, low mechanical properties, etc., and achieving the effect of improving synergistic bearing capacity, improving fatigue resistance, and short heat treatment time.

Active Publication Date: 2021-12-14
CENT SOUTH UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, the C / C-SiC composite materials prepared by the LSI process still have the following problems: (1) In high temperature environment, liquid silicon is very easy to corrode the carbon fibers in the C / C porous body, reducing the amount of material available for load-carrying per unit volume inside the material. At the same time, the chemical reaction between silicon and carbon also introduces strong interface bonds such as carbon fiber / SiC and matrix carbon / SiC, resulting in low strength and poor toughness of the prepared C / C-SiC composite material; figure 1 As shown, it is a schematic diagram of the interface reaction in the LSI process and the typical silicification damage morphology before and after the LSI reaction, indicating that the silicification damage of carbon fibers in the LSI process is more serious, which leads to lower mechanical properties; (2) in C / C-SiC composites , the micron-scale reinforcing phase of carbon fiber is difficult to toughen the micro-regions between carbon fiber bundles, within carbon fiber bundles, and between carbon fiber layers, resulting in the appearance of "weak areas" inside the material and reducing the comprehensive mechanical properties of the entire material; ( 3) During the long-term service of C / C-SiC composites, the fiber / matrix interface will experience interface wear and fiber strength decline due to interface debonding under long-term dynamic loads, resulting in material strength decline or even premature failure and fracture
However, the interfacial phase of carbon nanotubes can realize the toughening and interfacial strengthening of the internal micro-area of ​​the material, but this method cannot completely solve the corrosion damage of liquid silicon to carbon fibers.

Method used

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  • Bn nanotube interfacial phase strengthened and toughened carbon fiber reinforced ceramic matrix composite material and preparation method thereof
  • Bn nanotube interfacial phase strengthened and toughened carbon fiber reinforced ceramic matrix composite material and preparation method thereof
  • Bn nanotube interfacial phase strengthened and toughened carbon fiber reinforced ceramic matrix composite material and preparation method thereof

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Experimental program
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Embodiment 1

[0051] This embodiment provides a BN nanotube interface phase toughened carbon fiber reinforced ceramic matrix composite material, the specific preparation steps are as follows:

[0052] Degumming treatment: arrange the carbon fiber weaving in a vacuum sintering furnace, and under the protection of argon, heat up to 800℃ at a heating rate of 15°C / min. After the fiber is degummed, it is cooled to room temperature with the furnace to obtain a degummed carbon fiber woven cloth ;

[0053] S1. Preparation of impregnation solution: Boron oxide powder, boric acid powder, magnesium oxide powder and FeCl 3 The powder is mixed according to the ratio of 20:65:5:10 by mass percentage, and placed in a zirconia ceramic ball mill jar filled with isopropanol for ball milling to obtain an impregnation solution; wherein: the mass ratio of isopropanol to the mixed powder is 200: 10. The mass ratio of ball to material is 120:1, the ball milling speed is 250rpm, and the ball milling time is 100h;...

Embodiment 2

[0060] This embodiment provides a BN nanotube interface phase toughened carbon fiber reinforced ceramic matrix composite material, the specific preparation steps are as follows:

[0061] Degumming treatment: Arrange the carbon fiber weaving in a vacuum sintering furnace, and under the protection of argon, heat it up to 900℃ at a heating rate of 15°C / min. After the fiber is degummed, it is cooled to room temperature with the furnace to obtain a degummed carbon fiber woven cloth ;

[0062] S1. Preparation of impregnation solution: Boron oxide powder, boric acid powder, magnesium oxide powder and FeCl 3 The powder is mixed according to the ratio of 25:60:5:10 by mass, and placed in a zirconia ceramic ball mill jar filled with isopropanol for ball milling to obtain an impregnation solution; wherein: the mass ratio of isopropanol to the mixed powder is 200: 10. The mass ratio of ball to material is 120:1, the ball milling speed is 250rpm, and the ball milling time is 100h;

[006...

Embodiment 3

[0068] This embodiment provides a BN nanotube interface phase toughened carbon fiber reinforced ceramic matrix composite material, the specific preparation steps are as follows:

[0069] Degumming treatment: Arrange the carbon fiber weaving in a vacuum sintering furnace, and under the protection of argon, heat it up to 900℃ at a heating rate of 15°C / min. After the fiber is degummed, it is cooled to room temperature with the furnace to obtain a degummed carbon fiber woven cloth ;

[0070] S1. Preparation of impregnation solution: Boron oxide powder, boric acid powder, magnesium oxide powder and FeCl 3 The powder is mixed according to the ratio of 40:45:5:10 by mass, and placed in a zirconia ceramic ball mill jar filled with isopropanol for ball milling to obtain an impregnation solution; wherein: the mass ratio of isopropanol to the mixed powder is 200: 10. The mass ratio of ball to material is 120:1, the ball milling speed is 250rpm, and the ball milling time is 100h;

[007...

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Abstract

The invention relates to a BN nanotube interface phase strengthening and toughening carbon fiber reinforced ceramic matrix composite material. The following components are included in terms of mass percentage: h-BN is less than 0.5 wt.%, SiC is 10-30 wt.%, elemental Si is less than 10 wt.% and carbon balance. The preparation method is as follows: using carbon fiber woven cloth or felt body as a raw material, and sequentially performing degumming treatment, precursor impregnation-drying-high temperature heat treatment, matrix carbon densification and molten silicon infiltration process, to obtain BN nanotube interface phase strengthening and toughening carbon fiber Reinforced ceramic matrix composites. The invention makes full use of the good physical and chemical compatibility of BN with carbon fiber and matrix carbon, but does not react with liquid silicon and has the characteristics of poor wettability, and creatively grows BN nanotubes with high strength and large specific surface area protection in the carbon fiber in situ. The carbon fibers that play the main load-bearing function in the C / C-SiC composite material realize the strengthening and toughening of the C / C-SiC composite material prepared by the molten silicon infiltration process, and improve the mechanical properties of the C / C-SiC composite material; at the same time, The invention also improves the fatigue resistance of the C / C-SiC composite material.

Description

technical field [0001] The invention belongs to the technical field of composite materials, and more specifically relates to a BN nanotube interfacial phase reinforced carbon fiber reinforced ceramic matrix composite material and a preparation method thereof. Background technique [0002] Carbon fiber reinforced carbon-silicon carbide double matrix (C / C-SiC) composite material has light weight, high specific strength, high specific modulus, oxidation resistance, corrosion resistance, high friction coefficient, good thermal conductivity, high density and low preparation cost Relatively low and a series of advantages, it is a very competitive new generation of ceramic matrix composite materials, and has broad application prospects in the fields of friction materials, high-temperature thermal structures, and aerospace. [0003] At present, the molten silicon infiltration method (LSI) is mainly used at home and abroad to produce low-cost and high-density C / C-SiC composite materi...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C04B35/80C04B35/52C04B35/573
CPCC04B35/806C04B35/52C04B35/573C04B2235/3826C04B2235/422C04B2235/428C04B2235/6567C04B2235/658C04B2235/6562C04B2235/656C04B2235/524C04B2235/5248C04B2235/96C04B2235/77
Inventor 李杨肖鹏
Owner CENT SOUTH UNIV
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