2009
DOI: 10.1016/j.corsci.2009.01.026
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Preparation and oxidation protection of CVD SiC/a-BC/SiC coatings for 3D C/SiC composites

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Cited by 65 publications
(15 citation statements)
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“…Silicon carbide (SiC) ceramics and their composites have been considered for use as structural materials for high temperature applications (e.g., parts of engines and aerospace vehicles) because they have high chemical stability, superior high-temperature strength, low thermal expansion, and high thermal shock resistance [1][2][3][4]. They also have attractive properties regarding nuclear applications, including a low neutron absorption cross-section, low induced activation, and high resistance to neutron irradiation.…”
Section: Introductionmentioning
confidence: 99%
“…Silicon carbide (SiC) ceramics and their composites have been considered for use as structural materials for high temperature applications (e.g., parts of engines and aerospace vehicles) because they have high chemical stability, superior high-temperature strength, low thermal expansion, and high thermal shock resistance [1][2][3][4]. They also have attractive properties regarding nuclear applications, including a low neutron absorption cross-section, low induced activation, and high resistance to neutron irradiation.…”
Section: Introductionmentioning
confidence: 99%
“…Anti-oxidation coatings, which may be based on carbides [7][8][9], silicides [10,11] or oxides [12][13][14], was a key technique for advanced composites.…”
Section: Introductionmentioning
confidence: 99%
“…However matrix pores exist in C/SiC composites due to the "bottom-neck effect" during CVI process, which will act as diffusion paths of oxidizing species, restricting the application of C/SiC composites in oxidation environment. Liquid silicon infiltration (LSI), slurry infiltration and their combination have been used to produce dense C/SiC composites to fill the matrix pores by Si [6,7] or self-healing components such as B 4 C, SiB 4 , and SiBC [8][9][10][11][12]. The porosity of dense C/SiC composites is effectively reduced to less than 5% but higher processing temperature (41420 1C) aggravates the mismatch between coefficient of thermal expansion (CTE) of the fiber and matrix and brings larger thermal residual stress (TRS) on the composites, resulting in the formation of intrinsic matrix micro-cracks while cooling down from the fabrication temperature to room temperature [13][14].…”
Section: Introductionmentioning
confidence: 99%