2015
DOI: 10.1039/c5ra07550e
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Preparation and anti-oxidation properties of Si(O)C coated carbon-bonded carbon fibre composites

Abstract: An oxidation protective Si(O)C coating was fabricated on the carbon fibres of carbon-bonded carbon fibre (CBCF) composites using sol–gel method using dimethoxydimethylsilane and methyltrimethoxysilane as precursors.

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Cited by 34 publications
(21 citation statements)
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“…However, due to the brittleness of vitreous carbon junctions, CBCF composites usually show low compression strength . Another obstacle for the practical application of CBCF composites is their poor oxidation resistance at elevated temperature …”
Section: Introductionmentioning
confidence: 99%
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“…However, due to the brittleness of vitreous carbon junctions, CBCF composites usually show low compression strength . Another obstacle for the practical application of CBCF composites is their poor oxidation resistance at elevated temperature …”
Section: Introductionmentioning
confidence: 99%
“…5,[10][11][12] Another obstacle for the practical application of CBCF composites is their poor oxidation resistance at elevated temperature. 1,[13][14][15] Fabricating inorganic material coatings (such as SiOC, SiC, ZrB 2 and their composites) on the surface of carbon fibers are thought to be an effective way to improve the oxidation resistance of CBCF composites. 5,[15][16][17][18][19][20][21][22] Because of the increased density, ceramics coated CBCF composites usually show improved mechanical properties.…”
Section: Introductionmentioning
confidence: 99%
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“…Consequently, the unique properties of CBCFs have resulted in a prominent class of lightweight materials for thermal insulation . To improve the mechanical and oxidation resistance properties of the CBCFs, intense research efforts have been conducted such as modification of CBCFs via SiOC ceramic, in‐situ grown SiC nanowire (SiC nw ), and fabrication multi‐composition anti‐oxidation layers . The oxidation resistance capability is a key property in the overall performance, which can protect the thermal protection system in an environment containing oxygen at high temperature (>400°C) .…”
Section: Introductionmentioning
confidence: 99%
“…Compared to the traditional C/C composites with densities of 1.4-1.8 g·cm -3 , 2,5 their lightweight structure, low thermal conductivity, and high temperature capability can better satisfy the development of thermal insulation for new spacecrafts. [6][7][8] However, application of the CBCF materials is significantly limited for the oxidation of carbon above 450 °C [9][10][11] .…”
Section: Introductionmentioning
confidence: 99%