2003
DOI: 10.1016/s0008-6223(02)00398-6
|View full text |Cite
|
Sign up to set email alerts
|

Effects of the interface on the graphitization of a carbon fiber/pyrolytic carbon composite

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
4
1

Citation Types

0
10
0

Year Published

2005
2005
2023
2023

Publication Types

Select...
8

Relationship

0
8

Authors

Journals

citations
Cited by 20 publications
(10 citation statements)
references
References 8 publications
0
10
0
Order By: Relevance
“…The SiC bonding layer was prepared by pack cementation at 2,073 K, and the powder compositions was as follows: 45 wt% Si (300 mesh), 40 wt% SiC (325 mesh), 6 wt% graphite (300 mesh) and 9 wt% Al 2 O 3 (325 mesh). The preparation details were reported in [9]. After the pack cementation process, hydrothermal electrophoretic deposition was conducted.…”
Section: Methodsmentioning
confidence: 99%
“…The SiC bonding layer was prepared by pack cementation at 2,073 K, and the powder compositions was as follows: 45 wt% Si (300 mesh), 40 wt% SiC (325 mesh), 6 wt% graphite (300 mesh) and 9 wt% Al 2 O 3 (325 mesh). The preparation details were reported in [9]. After the pack cementation process, hydrothermal electrophoretic deposition was conducted.…”
Section: Methodsmentioning
confidence: 99%
“…5,6 Thermal expansion mismatch between the coating and C/ C composites will result in the crazing and debonding of the coating, and induce the failure of the coating. 7 To resolve this problem, so far, some multilayer coatings have been used, such as SiC/borosilicate glass, 8 SiC/MoSi 2 -Si-B 9 and SiC/Si-W. 10 In addition, in the authors' previous work, [11][12][13] SiC whiskers have been used to minimise the size of cracks caused by the thermal expansion mismatch between the coating and C/C composites. Recently, the advanced coatings, with a functionally gradient layer to minimise the influence of the thermal expansion mismatch, are designed to be multilayer coatings.…”
Section: Introductionmentioning
confidence: 99%
“…Anti-oxidation is a key requirement for carbon/carbon (C/C) composites to be used as high-temperature structural materials in an oxygen-containing environment [1][2][3]. To prevent C/C composites from oxidation, Si-Mo-Cr alloy has been extensively used as the coating material because a compound glass layer involving SiO 2 and Cr 2 O 3 would be formed, thus effectively prevent C/C composites from oxidation due to its high resistance to both volatilization and oxygen diffusion [4,5].…”
Section: Introductionmentioning
confidence: 99%