Study on the thermal fatigue behavior of SiC coated carbon/carbon composites

Qian Gang Fu; He Jun Li; Ke Zhi Li; Xiao Hong Shi; Min Huang; Guo Dong Sun; Yu Lei Zhang

doi:10.1016/j.msea.2006.07.031

Study on the thermal fatigue behavior of SiC coated carbon/carbon composites

Qian Gang Fu, He Jun Li, Ke Zhi Li, Xiao Hong Shi, Min Huang, Guo Dong Sun, Yu Lei Zhang

School of Materials Sience and Engineering

Northwestern Polytechnical University Xian

Research output: Contribution to journal › Article › peer-review

16 Scopus citations

Abstract

A SiC coating was prepared on carbon/carbon (C/C) composites surface by pack cementation and the thermal fatigue behavior of the SiC coated C/C composites was studied. During thermal cycle between 1873 K air and 373 K boiling water, the weight of the SiC coated sample decreased lightly, while the flexural strength was reduced obviously. After thermal cycle for 50 times, the weight loss of the SiC coated sample was 2.76% and the percentage of remaining strength was 74.5%. The decrease of the flexural strength during the thermal cycle was primarily due to the debonding of the fiber-matrix interfaces and the oxidation of the coated samples by oxygen or vapor.

Original language	English
Pages (from-to)	335-338
Number of pages	4
Journal	Materials Science and Engineering: A
Volume	434
Issue number	1-2
DOIs	https://doi.org/10.1016/j.msea.2006.07.031
State	Published - 25 Oct 2006

Keywords

Carbon/carbon composites
Coating
Fracture

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10.1016/j.msea.2006.07.031

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title = "Study on the thermal fatigue behavior of SiC coated carbon/carbon composites",

abstract = "A SiC coating was prepared on carbon/carbon (C/C) composites surface by pack cementation and the thermal fatigue behavior of the SiC coated C/C composites was studied. During thermal cycle between 1873 K air and 373 K boiling water, the weight of the SiC coated sample decreased lightly, while the flexural strength was reduced obviously. After thermal cycle for 50 times, the weight loss of the SiC coated sample was 2.76% and the percentage of remaining strength was 74.5%. The decrease of the flexural strength during the thermal cycle was primarily due to the debonding of the fiber-matrix interfaces and the oxidation of the coated samples by oxygen or vapor.",

keywords = "Carbon/carbon composites, Coating, Fracture",

author = "Fu, {Qian Gang} and Li, {He Jun} and Li, {Ke Zhi} and Shi, {Xiao Hong} and Min Huang and Sun, {Guo Dong} and Zhang, {Yu Lei}",

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T1 - Study on the thermal fatigue behavior of SiC coated carbon/carbon composites

AU - Fu, Qian Gang

AU - Li, He Jun

AU - Li, Ke Zhi

AU - Shi, Xiao Hong

AU - Huang, Min

AU - Sun, Guo Dong

AU - Zhang, Yu Lei

PY - 2006/10/25

Y1 - 2006/10/25

N2 - A SiC coating was prepared on carbon/carbon (C/C) composites surface by pack cementation and the thermal fatigue behavior of the SiC coated C/C composites was studied. During thermal cycle between 1873 K air and 373 K boiling water, the weight of the SiC coated sample decreased lightly, while the flexural strength was reduced obviously. After thermal cycle for 50 times, the weight loss of the SiC coated sample was 2.76% and the percentage of remaining strength was 74.5%. The decrease of the flexural strength during the thermal cycle was primarily due to the debonding of the fiber-matrix interfaces and the oxidation of the coated samples by oxygen or vapor.

AB - A SiC coating was prepared on carbon/carbon (C/C) composites surface by pack cementation and the thermal fatigue behavior of the SiC coated C/C composites was studied. During thermal cycle between 1873 K air and 373 K boiling water, the weight of the SiC coated sample decreased lightly, while the flexural strength was reduced obviously. After thermal cycle for 50 times, the weight loss of the SiC coated sample was 2.76% and the percentage of remaining strength was 74.5%. The decrease of the flexural strength during the thermal cycle was primarily due to the debonding of the fiber-matrix interfaces and the oxidation of the coated samples by oxygen or vapor.

KW - Carbon/carbon composites

KW - Coating

KW - Fracture

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U2 - 10.1016/j.msea.2006.07.031

DO - 10.1016/j.msea.2006.07.031

M3 - 文章

AN - SCOPUS:33748051737

SN - 0921-5093

VL - 434

SP - 335

EP - 338

JO - Materials Science and Engineering: A

JF - Materials Science and Engineering: A

IS - 1-2

ER -

Study on the thermal fatigue behavior of SiC coated carbon/carbon composites

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Keywords

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