2010
DOI: 10.1016/j.scriptamat.2010.06.045
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ZrC–ZrB2 matrix composites with enhanced toughness prepared by reactive hot pressing

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Cited by 27 publications
(13 citation statements)
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“…Nevertheless, an undesirably exaggerated grain growth occurs with the addition of Zr. Other authors demonstrate an improvement of ZrC sinterability by addition of ZrB 2 and SiC [7][8][9][10]. An alternative sintering method, which enables high densification of ZrC material, is spark plasma sintering (SPS).…”
Section: Introductionmentioning
confidence: 99%
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“…Nevertheless, an undesirably exaggerated grain growth occurs with the addition of Zr. Other authors demonstrate an improvement of ZrC sinterability by addition of ZrB 2 and SiC [7][8][9][10]. An alternative sintering method, which enables high densification of ZrC material, is spark plasma sintering (SPS).…”
Section: Introductionmentioning
confidence: 99%
“…Basic investigations were conducted with regard to sub-stoichiometry or incorporation of oxygen for ZrC (meaning ZrC x O y with x < 1, y  1) powder processing and promotion of ZrC sintering by additives [4,5,9,[15][16][17]. These papers discuss specific effects of ZrC x O y composition in relation to sintering behavior.…”
Section: Introductionmentioning
confidence: 99%
“…Owing to the promising properties such as high melting temperature, hardness and modulus, excellent chemical stability, good electrical and thermal conductivity, and similar coefficient of thermal expansion (CTE) to Zr 3 [Al(Si)] 4 C 6 , both ZrB 2 and ZrC are ideal reinforcements for Zr 3 [Al(Si)] 4 C 6 matrix. Furthermore, ZrB 2 -ZrC composites show improved properties than either individual component [11,12]. As a result, Zr 3 [Al(Si)] 4 C 6 matrix composites reinforced by ZrB 2 and ZrC have been developed in our previous work, in which Zr 3 [Al(Si)] 4 C 6 matrix was toughened and strengthened significantly by the in situ incorporation of ZrB 2 and ZrC [13].…”
Section: Introductionmentioning
confidence: 92%
“…Due to its high melting point, high hardness, solid-state phase stability, and good thermomechanical and thermochemical properties, zirconium carbide (ZrC) is considered to be a high potential ultra-high temperature ceramic (UHTC) material that can be used for structural components in next-generation rocket engines and hypersonic spacecrafts, which require the ability to tolerate extreme conditions [1][2][3][4][5][6]. However, poor sinterability and low oxidation resistance in air limit its wide applications in extreme conditions [4,[7][8][9][10].…”
Section: Introductionmentioning
confidence: 99%