Microstructure, mechanical properties and oxidation resistance of C/C-SIC-ZRB2 composites

Wenbo Han; Changling Zhou; Chonghai Wang; Yumin Zhang; Huayu Zhang; Zhuju Wang

Microstructure, mechanical properties and oxidation resistance of C/C-SIC-ZRB2 composites

Wenbo Han^*
, Changling Zhou
, Chonghai Wang
, Yumin Zhang
, Huayu Zhang
, Zhuju Wang

^*Corresponding author for this work

School of Astronautics

Ltd
Harbin Institute of Technology Shenzhen

Research output: Contribution to conference › Paper › peer-review

Abstract

To overcome the poor oxidation resistance of C/C composites, anti-oxidation SiC and ZrB2-SiC ceramics were introduced into C/C composites by chemical vapor infiltration (CVI) and precursor infiltration-pyrolysis (PIP). The microstructure, mechanical properties and oxidation resistance of C/C-SiC-ZrB2 composites were investigated. The ZrB2-SiC ceramic exhibits uniform dispersion and distribution in C/C composite. The C/C-SiC-ZrB2 composites pyrolyzed at 1500°C has the highest flexural strength (315 MPa) and fracture toughness (10.87 MPam^1/2). The flexural strength, tensile strength and compressive strength increased with temperature. The C/C-SiC-ZrB2 composites exhibited low ablation characteristics in plasma ablation experiments, and the linear ablation rate was 3.67×10^-3 mm/s. The composite material, which exhibited synergistic effect between toughening and oxidation resistance, has potential application in the field of hypersonic vehicle.

Original language	English
State	Published - 2019
Event	22nd International Conference on Composite Materials, ICCM 2019 - Melbourne, Australia Duration: 11 Aug 2019 → 16 Aug 2019

Conference

Conference	22nd International Conference on Composite Materials, ICCM 2019
Country/Territory	Australia
City	Melbourne
Period	11/08/19 → 16/08/19

Keywords

Mechanical properties
Microstructure
Oxidation resistance
ZrB2

Cite this

@conference{80ebbec369ab40358346958b72a15f45,

title = "Microstructure, mechanical properties and oxidation resistance of C/C-SIC-ZRB2 composites",

abstract = "To overcome the poor oxidation resistance of C/C composites, anti-oxidation SiC and ZrB2-SiC ceramics were introduced into C/C composites by chemical vapor infiltration (CVI) and precursor infiltration-pyrolysis (PIP). The microstructure, mechanical properties and oxidation resistance of C/C-SiC-ZrB2 composites were investigated. The ZrB2-SiC ceramic exhibits uniform dispersion and distribution in C/C composite. The C/C-SiC-ZrB2 composites pyrolyzed at 1500°C has the highest flexural strength (315 MPa) and fracture toughness (10.87 MPam1/2). The flexural strength, tensile strength and compressive strength increased with temperature. The C/C-SiC-ZrB2 composites exhibited low ablation characteristics in plasma ablation experiments, and the linear ablation rate was 3.67×10-3 mm/s. The composite material, which exhibited synergistic effect between toughening and oxidation resistance, has potential application in the field of hypersonic vehicle.",

keywords = "Mechanical properties, Microstructure, Oxidation resistance, ZrB2",

author = "Wenbo Han and Changling Zhou and Chonghai Wang and Yumin Zhang and Huayu Zhang and Zhuju Wang",

note = "Publisher Copyright: {\textcopyright} 2019 International Committee on Composite Materials. All rights reserved.; 22nd International Conference on Composite Materials, ICCM 2019 ; Conference date: 11-08-2019 Through 16-08-2019",

year = "2019",

language = "英语",

}

TY - CONF

T1 - Microstructure, mechanical properties and oxidation resistance of C/C-SIC-ZRB2 composites

AU - Han, Wenbo

AU - Zhou, Changling

AU - Wang, Chonghai

AU - Zhang, Yumin

AU - Zhang, Huayu

AU - Wang, Zhuju

PY - 2019

Y1 - 2019

N2 - To overcome the poor oxidation resistance of C/C composites, anti-oxidation SiC and ZrB2-SiC ceramics were introduced into C/C composites by chemical vapor infiltration (CVI) and precursor infiltration-pyrolysis (PIP). The microstructure, mechanical properties and oxidation resistance of C/C-SiC-ZrB2 composites were investigated. The ZrB2-SiC ceramic exhibits uniform dispersion and distribution in C/C composite. The C/C-SiC-ZrB2 composites pyrolyzed at 1500°C has the highest flexural strength (315 MPa) and fracture toughness (10.87 MPam1/2). The flexural strength, tensile strength and compressive strength increased with temperature. The C/C-SiC-ZrB2 composites exhibited low ablation characteristics in plasma ablation experiments, and the linear ablation rate was 3.67×10-3 mm/s. The composite material, which exhibited synergistic effect between toughening and oxidation resistance, has potential application in the field of hypersonic vehicle.

AB - To overcome the poor oxidation resistance of C/C composites, anti-oxidation SiC and ZrB2-SiC ceramics were introduced into C/C composites by chemical vapor infiltration (CVI) and precursor infiltration-pyrolysis (PIP). The microstructure, mechanical properties and oxidation resistance of C/C-SiC-ZrB2 composites were investigated. The ZrB2-SiC ceramic exhibits uniform dispersion and distribution in C/C composite. The C/C-SiC-ZrB2 composites pyrolyzed at 1500°C has the highest flexural strength (315 MPa) and fracture toughness (10.87 MPam1/2). The flexural strength, tensile strength and compressive strength increased with temperature. The C/C-SiC-ZrB2 composites exhibited low ablation characteristics in plasma ablation experiments, and the linear ablation rate was 3.67×10-3 mm/s. The composite material, which exhibited synergistic effect between toughening and oxidation resistance, has potential application in the field of hypersonic vehicle.

KW - Mechanical properties

KW - Microstructure

KW - Oxidation resistance

KW - ZrB2

UR - https://www.scopus.com/pages/publications/85097339387

M3 - 论文

AN - SCOPUS:85097339387

T2 - 22nd International Conference on Composite Materials, ICCM 2019

Y2 - 11 August 2019 through 16 August 2019

ER -

Microstructure, mechanical properties and oxidation resistance of C/C-SIC-ZRB2 composites

Abstract

Conference

Keywords

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