2019
DOI: 10.1111/ijac.13213
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Mechanical properties of silicon carbide—in situ zirconium carbonitride composites

Abstract: SiC-Zr 2 CN composites were fabricated by conventional hot pressing from β-SiC and ZrN powders with 2 vol% equimolar Y 2 O 3 -Sc 2 O 3 as a sintering additive. The effects of the ZrN addition on the room-temperature (RT) mechanical properties and hightemperature flexural strength of the SiC-Zr 2 CN composites were investigated. The fracture toughness gradually increased from 4.2 ± 0.3 MPa·m 1/2 for monolithic SiC to 6.3 ± 0.2 MPa·m 1/2 for a SiC-20 vol% ZrN composite, whereas the RT flexural strength (546 ± 32… Show more

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Cited by 13 publications
(9 citation statements)
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“…Preceramic polycarbosilane polymers are commonly used as precursors to make ceramic fibers 10,39 and ceramic matrix. [7][8][9]40,41 The chemical and volume changes that accompany ceramization of the polymer during pyrolysis have been documented in several studies.…”
Section: Resultsmentioning
confidence: 99%
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“…Preceramic polycarbosilane polymers are commonly used as precursors to make ceramic fibers 10,39 and ceramic matrix. [7][8][9]40,41 The chemical and volume changes that accompany ceramization of the polymer during pyrolysis have been documented in several studies.…”
Section: Resultsmentioning
confidence: 99%
“…29,30 The physics of resin under pressure is similar to the seepage pr lar approaches have been used also to mod into a mold containing fiber mats. 23,[31][32][33][34][35][36][37][38] T in these cases to determine the resin flow ing times corresponding to different infilt Preceramic polycarbosilane polymers as precursors to make ceramic fibers 10,3 trix. [7][8][9]40,41 The chemical and volume ch pany ceramization of the polymer during documented in several studies.…”
mentioning
confidence: 99%
“…The critical flaw sizes (c), calculated using K 1C = 1.35‧σ‧c 1/2, were approximately 39, 45, 68, 83, and 112 μm for SBN1, SBN2, SBN3, SBN4, and SBN5, respectively. Given that the critical flaw sizes (39-112 μm) were much larger than the average grain size (~2.3 μm), the fracture is thought to have originated from the processing defects [28]. The typical fracture origins of SBN1 and SBN5 were residual pores near the tensile surfaces in bending bars (Figure 7).…”
Section: Resultsmentioning
confidence: 99%
“…The residual thermal stresses ( σ th ) in SiC and SiO 2 can be estimated using the following equation: 20 σth=ΔαΔTE1ν,where Δα, ΔT, E , and ν denote the CTE mismatch, temperature difference (between the oxidation temperature and room temperature), elastic modulus, and Poisson's ratio, respectively. Using α α‐SiC 21 = 2.5 × 10 −6 °C −1 , α β‐SiC 21 = 1.2 × 10 −6 °C −1 , α SiO2 19 = 0.5 × 10 −6 °C −1 , E α‐SiC 21 = 409 GPa, E β‐SiC 21 = 465 GPa, E SiO2 19 = 72 GPa, ν α‐SiC 19 = 0.19, ν β‐SiC 22 = 0.19, ν SiO2 19 = 0.19, and ΔT = 600°C, the residual thermal stresses in the specimen sintered at 600°C with the β‐SiC‐SiO 2 interface were calculated to be 679 and −662 MPa for β‐SiC and SiO 2 , respectively. The corresponding residual stresses for an α‐SiC‐SiO 2 system were reduced to 212 and − 207 MPa for α‐SiC and SiO 2 , respectively.…”
Section: Resultsmentioning
confidence: 99%