Carbon fiber-enhanced ZrB2-ZrN composite ceramic-based composite material and preparation method thereof

A technology of composite ceramics and composite materials, which is applied in the field of ultra-high temperature thermal protection structures, can solve the problems of uncontrollable material components and distribution, inability to shape components with complex shapes, and limit the application range of material engineering, so as to achieve high component content, The effect of high temperature resistance and high volume content of ceramic phase

Active Publication Date: 2016-01-13
NAT UNIV OF DEFENSE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, the disadvantage of the slurry method is that the uneven distribution of ceramic powder leads to uncontrollable material composition and distribution in the later stage, and the inability to form components with complex shapes limits the scope of engineering applications of materials.

Method used

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  • Carbon fiber-enhanced ZrB2-ZrN composite ceramic-based composite material and preparation method thereof
  • Carbon fiber-enhanced ZrB2-ZrN composite ceramic-based composite material and preparation method thereof
  • Carbon fiber-enhanced ZrB2-ZrN composite ceramic-based composite material and preparation method thereof

Examples

Experimental program
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Effect test

Embodiment 1

[0035] A carbon fiber reinforced ZrB 2 -ZrN multiphase ceramic matrix composites, with ZrB 2 -ZrN composite phase ceramics as the matrix, and carbon fiber braids as the reinforcing phase. Among them, carbon fiber reinforced ZrB 2 -The volume fraction of carbon fiber in the ZrN multiphase ceramic matrix composite is 51%, ZrB 2 -The volume fraction of ZrN composite ceramics is 28.5%, while ZrB 2 -ZrB in ZrN composite ceramics 2 The volume fraction of ZrN is 9.5%, and the volume fraction of ZrN is 19%.

[0036] The carbon fiber reinforced ZrB of the present embodiment 2 -The preparation method of ZrN composite material, comprises the following steps:

[0037] S1. Preforming of fiber reinforcement: 200g of carbon fiber is three-dimensionally braided by a three-dimensional braiding machine to form a braided piece to obtain a carbon fiber reinforcement.

[0038] S2. Preparation of fiber protective coating: using propylene as the precursor, the carbon fiber reinforced body obt...

Embodiment 2

[0046] A carbon fiber reinforced ZrB 2 -ZrN multiphase ceramic matrix composites, with ZrB 2 -ZrN composite phase ceramics as the matrix, and the three-dimensional needle-punched felt of carbon fiber as the reinforcing phase. Among them, the volume fraction of carbon fiber in the carbon fiber reinforced ZrB2-ZrN composite ceramic matrix composite is 20%, and the ZrB 2 The volume fraction of -ZrN composite ceramics is 57%. while ZrB 2 -ZrB in ZrN composite ceramics 2 The volume fraction of ZrN is 19%, and the volume fraction of ZrN is 38%.

[0047] The carbon fiber reinforced ZrB of the present embodiment 2 -The preparation method of ZrN composite material, comprises the following steps:

[0048] S1. Preforming of fiber reinforcement: 80g of non-weft cloth and 20g of mesh tire are laminated and then needle punched with a needle punching machine to form a three-dimensional needle-punched felt to obtain a three-dimensional needle-punched carbon fiber reinforcement.

[0049...

Embodiment 3

[0056] A carbon fiber reinforced ZrB 2 -ZrN multiphase ceramic matrix composites, with ZrB 2 -ZrN composite ceramics as the matrix, with carbon cloth laminated puncture as the reinforcement phase, in which carbon fiber reinforced ZrB 2 -The carbon fiber volume fraction in the ZrN multiphase ceramic matrix composite is 20%, and the ZrB 2 -The volume fraction of ZrN composite ceramics is 31%, while ZrB 2 -ZrB in ZrN composite ceramics 2 The volume fraction is 10%, and the volume fraction of ZrN is 21%.

[0057] The carbon fiber reinforced ZrB of the present embodiment 2 -The preparation method of ZrN composite material, comprises the following steps:

[0058] S1. Preforming of fiber reinforcement: use two-dimensional carbon cloth as the carbon fiber reinforcement phase, laminate 30 layers of two-dimensional carbon cloth and perform Z-direction puncture to make carbon cloth laminated puncture to obtain carbon fiber reinforcement.

[0059] S2. Preparation of fiber protective...

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Abstract

The invention discloses a carbon fiber-enhanced ZrB2-ZrN composite-ceramic-based composite material and a preparation method thereof. In the composite material, carbon fibers are employed as an enhancement body and ZrB2-ZrN composite ceramic is employed as a base body. The preparation method includes the following steps: with propylene as a precursor, depositing a carbon coating layer on surface of the carbon fiber enhancement body through a chemical vapor deposition process to obtain the carbon fiber enhancement body of which the surface is deposited by the carbon coating layer; compacting the carbon fiber enhancement body of which the surface is deposited by the carbon coating layer to obtain a porous C / BN prefabricate; and performing fusion infiltration to the porous C / BN prefabricate with zirconium metal or zirconium alloy to obtain the carbon fiber-enhanced ZrB2-ZrN composite-ceramic-based composite material. The preparation method is simple, is low in cost and is short in period. The composite material is high in compactness degree, is high in ceramic phase volume percentage and is homogeneous in distribution.

Description

technical field [0001] The invention belongs to the technical field of ultra-high-temperature thermal protection structures, and in particular relates to a ceramic-based composite material with a boride-nitride composite ultra-high-temperature ceramic as a matrix and a preparation method thereof. Background technique [0002] Hypersonic vehicles have become the main development direction of new hypersonic weapon systems and aerospace, and will play an important role in future national security and development. With the increase of the flight speed of hypersonic vehicles, the demand for ultra-high temperature resistant and ablation-resistant materials is becoming more and more urgent. The existing materials can no longer meet the needs of the development of thermal protection systems and propulsion systems of hypersonic vehicles. It is necessary to develop a new generation of resistant materials. Ultra-high temperature, anti-ablation, anti-thermal shock, high reliability new ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C04B35/80C04B35/58C04B41/88
Inventor 陈思安胡海峰张玉娣张长瑞李勇马新吴金泰
Owner NAT UNIV OF DEFENSE TECH
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