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A kind of preparation method of oxide/oxide ceramic matrix composite material containing elastic structure interface

A technology of oxide ceramics and elastic structure, which is applied in the field of preparation of oxide/oxide ceramic matrix composite materials, can solve the problems of low compressive strength and insufficient toughness, achieve enhanced strength, ensure effective transmission of layout and load, and improve The effect of fracture toughness

Active Publication Date: 2022-05-13
XIAN XINGUI CERAMIC COMPOSITE MATERIAL CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problems of low compressive strength and insufficient toughness of oxide / oxide ceramic matrix composites with interstitial interfaces in the prior art, the present invention provides an oxide / oxide ceramic matrix composite with elastic structure interface Material preparation method

Method used

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  • A kind of preparation method of oxide/oxide ceramic matrix composite material containing elastic structure interface

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Experimental program
Comparison scheme
Effect test

Embodiment 1

[0033] 1. Prepare a polyvinyl alcohol solution with a concentration of 2wt.%. Under the action of magnetic stirring, evenly mix SiC nanowires with a diameter of 15nm and a length <50μm into the polyvinyl alcohol solution until the SiC nanowires are in the polyvinyl alcohol solution. The concentration in the solution is 5wt.%, and then ball milled for 0.5 hours to obtain an elastic structure interface solution;

[0034] 2. Immerse the oxide fiber cloth in the elastic structure interface solution prepared in step 1 for 0.5 hours, then take it out, layer it in the mold and fix it, cure it in a vacuum furnace at 250°C and pyrolyze it at 600°C, so that A pyrolytic carbon interface containing nanowires is formed on the surface of oxide fibers;

[0035] 3. Repeat step 2 3 times to obtain an oxide fiber prefabricated body containing nanowire pyrolytic carbon with an interface thickness of 150 nm;

[0036] 4. impregnating the oxide fiber preform obtained in step 3 in an alumina sol wi...

Embodiment 2

[0042] 1. Prepare a polyvinyl alcohol solution with a concentration of 5wt.%. Under the action of magnetic stirring, evenly mix SiC nanowires with a diameter of 15nm and a length <50μm into the polyvinyl alcohol solution until the SiC nanowires are in the polyvinyl alcohol solution. The concentration in the solution is 10wt.%, and then ball milled for 1 hour to obtain an elastic structure interface solution;

[0043] 2. Immerse the oxide fiber cloth in the elastic structure interface solution prepared in step 1 for 0.5 hours, then take it out, layer it in the mold and fix it, cure it in a vacuum furnace at 300°C and pyrolyze it at 800°C, so that A pyrolytic carbon interface containing nanowires is formed on the surface of oxide fibers;

[0044] 3. Repeat step 2 for 3 times to obtain an oxide fiber prefabricated body containing nanowire pyrolytic carbon with an interface thickness of 180 nm;

[0045] 4. impregnating the oxide fiber preform obtained in step 3 in an alumina sol ...

Embodiment 3

[0051] 1. Prepare a polyvinyl alcohol solution with a concentration of 10wt.%. Under the action of magnetic stirring, evenly mix SiC nanowires with a diameter of 15nm and a length <50μm into the polyvinyl alcohol solution until the SiC nanowires are in the polyvinyl alcohol solution. The concentration in the solution is 15wt.%, and then ball milled for 1 hour to obtain an elastic structure interface solution;

[0052] 2. Immerse the oxide fiber cloth in the elastic structure interface solution prepared in step 1 for 1 hour, then take it out, layer it in the mold and fix it, cure it in a vacuum furnace at 400°C and pyrolyze it at 1000°C, so that A pyrolytic carbon interface containing nanowires is formed on the surface of oxide fibers;

[0053]3. Repeat step 2 4 times to obtain an oxide fiber preform with a nanowire pyrolytic carbon interface thickness of 200 nm;

[0054] 4. impregnating the oxide fiber preform obtained in step 3 in an alumina sol with a solid content of 25% a...

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Abstract

The invention relates to a method for preparing a ceramic matrix composite material, in particular to a method for preparing an oxide / oxide ceramic matrix composite material with an elastic structure interface, so as to solve the gap-containing interfacial oxide / oxide ceramic matrix composite material existing in the prior art. The problem of low strength and insufficient toughness of oxide ceramic matrix composites. The technical scheme adopted includes preparation of elastic structure interface solution, preparation of oxide fiber preform containing nanowire and pyrolytic carbon interface, matrix impregnation, sintering, oxidation, and finally obtaining oxide / oxide ceramic matrix composite with elastic structure interface Material. The preparation method can flexibly adjust the structure of the interstitial interface by adjusting the content of SiC nanowires and the thickness of the interstitial interface according to the needs of the components. While basically improving the fracture toughness of the material, it can effectively enhance the strength of the interstitial interface composite material and make the interstitial interface Oxide / oxide ceramic matrix composites are better used in pressure-resistant structural parts.

Description

technical field [0001] The invention relates to a preparation method of a ceramic matrix composite material, in particular to a preparation method of an oxide / oxide ceramic matrix composite material with an elastic structure interface. Background technique [0002] Both the reinforcement fiber and the matrix of the oxide / oxide ceramic matrix composite are oxides, and the oxides have a high diffusion coefficient and are easy to diffuse to form a strong interfacial bond. The interstitial interface is a commonly used interface of oxide / oxide ceramic matrix composites, which aims to leave a gap between the fiber and the matrix, realize the weak combination of the fiber and the matrix, and achieve the purpose of toughening the composite material. [0003] The preparation principle of the interstitial interface is to deposit a layer of pyrolytic carbon on the surface of the fiber by chemical vapor deposition or organic precursor impregnation pyrolysis, then impregnate and sinter t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C04B35/117C04B35/185C04B35/14C04B35/80C04B35/622C04B35/628
CPCC04B35/117C04B35/185C04B35/14C04B35/622C04B35/62863C04B35/62873C04B2235/5256C04B2235/522C04B2235/5244C04B2235/5454C04B2235/616C04B2235/6581C04B2235/656C04B2235/661C04B2235/96
Inventor 李建章张海昇王鹏马文科成来飞
Owner XIAN XINGUI CERAMIC COMPOSITE MATERIAL CO LTD