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Multi-component composite zirconium boride-based ceramic material and preparation method thereof

A multi-component composite and ceramic material technology, applied in the field of ceramic materials, can solve problems such as ZrB2, and achieve the effects of low cost, excellent performance and simple process

Active Publication Date: 2019-03-01
CHANGSHU INSTITUTE OF TECHNOLOGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Aiming at the defects of the prior art, the present invention provides a multi-component composite zirconium boride-based ceramic material, which solves the problem of ZrB 2 The problem of insufficient mechanical properties, and can improve its anti-oxidation performance

Method used

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  • Multi-component composite zirconium boride-based ceramic material and preparation method thereof
  • Multi-component composite zirconium boride-based ceramic material and preparation method thereof
  • Multi-component composite zirconium boride-based ceramic material and preparation method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0024] According to the molar ratio of zirconium hydride: boron carbide: silicon: aluminum: graphite = 8.4: 4.0: 4.2: 0.8: 1.2, weigh the raw material zirconium hydride powder (purity ≥ 99.9%, particle size ≤ 37 microns), boron carbide powder (purity ≥ 99 %, particle size ≤ 10 microns), silicon powder (purity ≥ 99.9%, particle size ≤ 48 microns), aluminum powder (purity ≥ 99.9%, particle size ≤ 48 microns) and graphite powder (purity ≥ 99.9%, particle size ≤ 12 microns) , placed in a ball mill and mixed evenly, then placed in a graphite mold sprayed with boron nitride on the surface, cold-pressed for molding, hot-pressed and sintered in an argon atmosphere, and heated to 1750 °C at a rate of 15 °C / min to reach the sintering temperature point Finally, the pressure was gradually increased to 30MPa, kept for 1.5h, then cooled at a rate of 15°C / min, annealed at 1450°C and kept at a pressure of 30MPa for 40min, and finally turned off and cooled in the furnace to obtain the composite...

Embodiment 2

[0026] According to the molar ratio of zirconium hydride: boron carbide: silicon: aluminum: graphite = 8.0: 3.6: 3.8: 1.4: 2.7, weigh the raw material zirconium hydride powder (purity ≥ 99.9%, particle size ≤ 37 microns), boron carbide powder (purity ≥ 99 %, particle size ≤ 10 microns), silicon powder (purity ≥ 99.9%, particle size ≤ 48 microns), aluminum powder (purity ≥ 99.9%, particle size ≤ 48 microns) and graphite powder (purity ≥ 99.9%, particle size ≤ 12 microns) , placed in a ball mill and mixed evenly, then placed in a graphite mold sprayed with boron nitride on the surface, cold-pressed for molding, hot-pressed and sintered in an argon atmosphere, and heated to 1850°C at a rate of 20°C / min. After reaching the sintering temperature , the pressure was gradually increased to 25MPa, and kept for 1.2h, then cooled at a rate of 20°C / min, annealed at 1550°C, 25MPa pressure and kept for 30min, and finally turned off the power and cooled with the furnace. Obtain the composite...

Embodiment 3

[0028]According to the molar ratio of zirconium hydride: boron carbide: silicon: aluminum: graphite = 7.6: 3.2: 3.4: 2.0: 4.2, weigh the raw material zirconium hydride powder (purity ≥ 99.9%, particle size ≤ 37 microns), boron carbide powder (purity ≥ 99 %, particle size ≤ 10 microns), silicon powder (purity ≥ 99.9%, particle size ≤ 48 microns), aluminum powder (purity ≥ 99.9%, particle size ≤ 48 microns) and graphite powder (purity ≥ 99.9%, particle size ≤ 12 microns) , placed in a ball mill and mixed evenly, then placed in a graphite mold sprayed with boron nitride on the surface, cold-pressed for molding, hot-pressed and sintered in an argon atmosphere, and heated to 1950°C at a rate of 30°C / min. After reaching the sintering temperature , the pressure was gradually increased to 20MPa, kept for 1h, then cooled at a rate of 30°C / min, annealed at 1650°C, 20MPa pressure and kept for 20min, and finally turned off the power and cooled with the furnace. Obtain the composite materi...

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Abstract

The invention discloses a multi-component composite zirconium boride-based ceramic material, which is prepared from ZrB2 matrix, a Zr2[Al(Si)]4C5 tough phase and a SiC tough phase. The ZrB2 matrix accounts for 53-67% of the total volume of the multi-component composite zirconium boride-based ceramic material, and the SiC tough phase accounts for 18-22% of the total volume of the ultra-high temperature ceramic. The invention also discloses a method for preparing the multi-component composite zirconium boride-based ceramic material by one step by using zirconium hydride powder, boron carbide powder, silicon powder, aluminum powder and graphite powder as raw materials. The multi-component composite zirconium boride-based ceramic material provided by the invention has better mechanical properties and oxidation resistance, the preparation method is simple, the raw materials are easy to obtain, and the cost is low.

Description

technical field [0001] The invention relates to a ceramic material and a preparation method thereof, in particular to a multi-component composite zirconium boride-based ceramic material, which belongs to the technical field of ceramic materials. Background technique [0002] Ultra-High Temperature Ceramics (UHTCs) is a class of advanced structural ceramics with a melting point higher than 3000°C and expected to be applied above 1800°C. UHTCs mainly include binary carbides and borides of group IVB and VB transition metals. In the UHTCs family, ZrB 2 It has a low theoretical density, which has a huge advantage in the aerospace field oriented to lightweight structure design. In order to further improve ZrB 2 performance, generally in ZrB 2 Introduce SiC with lower density. However, a strong and tough phase is used, and the reinforcing and toughening structure is single, and the modification effect is limited. Therefore, the existing technology has prepared ZrB by introduc...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C04B35/58C04B35/622
CPCC04B35/58078C04B35/622C04B2235/38C04B2235/3821C04B2235/402C04B2235/425C04B2235/428
Inventor 余磊刘辉王旭红纪网金张建浩王哲飞殷仕龙姚霞喜
Owner CHANGSHU INSTITUTE OF TECHNOLOGY