2015
DOI: 10.1016/j.ceramint.2014.08.051
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Brazing of ZrB2–SiC–C ceramic and GH99 superalloy to form reticular seam with low residual stress

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Cited by 63 publications
(16 citation statements)
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“…But when the holding is longer, the thick interface between ZS and filler has rather big residual stress due to mismatches of the Young's modulus and the coefficients of thermal expansions between the two materials. These residual stresses induce micro-crack in the interface and deteriorate the mechanical properties [33]. On the other hand, longer holding time leads to larger amount and size of brittle intermetallics (e.g.…”
Section: Resultsmentioning
confidence: 99%
“…But when the holding is longer, the thick interface between ZS and filler has rather big residual stress due to mismatches of the Young's modulus and the coefficients of thermal expansions between the two materials. These residual stresses induce micro-crack in the interface and deteriorate the mechanical properties [33]. On the other hand, longer holding time leads to larger amount and size of brittle intermetallics (e.g.…”
Section: Resultsmentioning
confidence: 99%
“…3). The total evolutions of strain field and cracking of C/SiC composites were monitored by DIC 8 under different sizes, which would be beneficial to provide more information to reveal the fracture characteristics of C/SiC composites.…”
Section: R-curve Experimentalmentioning
confidence: 99%
“…Thermo-mechanical properties of C/SiC composites; for instance, fracture toughness, fracture strength, residual stresses, crack extension resistance curves (R-curve), hardness, thermal and oxidation resistance play an important role in predicting their performance and disabilities. In recent years, different experimental methods such as tension [2][3][4], indentation [5][6][7], shear [6,[8][9][10][11] and bending tests [12][13][14][15][16] have been developed to analyze those key properties of ceramic matrix composites [17,18]. Mei MPa, which was affected by loading rate during tensions [4,19].…”
mentioning
confidence: 99%
“…Much work has been done to join ceramics and ceramic matrix composites, including brazing [3][4], diffusion welding [5] and precursor infiltration [6], however, the joining strength is still not enough to satisfy the requirement in aerospace application. The mechanical joining by the introduction of bolts can satisfy the joining strength at moderately high temperature, but most researches focused on metal joints [7][8][9], whose heat insulation properties are quite poor, and rare studies have been done on heat shorts blocking joints.…”
Section: Introductionmentioning
confidence: 99%