2016
DOI: 10.1016/j.jeurceramsoc.2016.02.009
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Sintering behaviour, solid solution formation and characterisation of TaC, HfC and TaC–HfC fabricated by spark plasma sintering

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Cited by 207 publications
(147 citation statements)
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“…The most common bond coats are those based on metallic MCrAlY alloys (where M=Co, Ni or Ni-Co mixtures) 34 and the basic rule to avoid cracks or delamination between the thermal protective coating on top and the bond coat is the matching of the coefficients of thermal expansion (CTE) of both materials. It has been recently found that the CTE of binary and ternary alloys for the Ta-Hf-C system varies from 7.08 to 7.66·10 −6 /K in the range from 25 to 2000 °C 35 , which match the CTE values for some common MCrAlY alloys in the range of 500 to 700 °C 34 , which is a similar temperature range as the used in this work to study the corrosion behavior of the Ta-Hf-C samples. In addition, the high thermal conductivities reported for TaC 36 and Ta-Hf-C 35 carbides ensure an enhanced heat dissipation for applications that requires working at high temperatures such as turbine blades or hypersonic flights 35 .…”
Section: Resultssupporting
confidence: 72%
“…The most common bond coats are those based on metallic MCrAlY alloys (where M=Co, Ni or Ni-Co mixtures) 34 and the basic rule to avoid cracks or delamination between the thermal protective coating on top and the bond coat is the matching of the coefficients of thermal expansion (CTE) of both materials. It has been recently found that the CTE of binary and ternary alloys for the Ta-Hf-C system varies from 7.08 to 7.66·10 −6 /K in the range from 25 to 2000 °C 35 , which match the CTE values for some common MCrAlY alloys in the range of 500 to 700 °C 34 , which is a similar temperature range as the used in this work to study the corrosion behavior of the Ta-Hf-C samples. In addition, the high thermal conductivities reported for TaC 36 and Ta-Hf-C 35 carbides ensure an enhanced heat dissipation for applications that requires working at high temperatures such as turbine blades or hypersonic flights 35 .…”
Section: Resultssupporting
confidence: 72%
“…Melting of HfC 0.98 samples was also achieved with intermediate and short pulses. The lower thermal diffusivity24 of HfC compared to TaC produces higher heat concentration in the sample surface, producing higher temperatures at lower applied power. Furthermore, much less vaporisation was observed in pure hafnium carbide compared with all of the other compositions, judging from the size of the vapour plume traces visible on the sample holder above the sample after the melting experiments.…”
Section: Resultsmentioning
confidence: 99%
“…Diffractions of Cu were barely observable, while ZrC phase was absent in the consolidated ceramic. The dominant XRD peaks from the consolidated ceramic were indexed by TaC with significant broadening and shift towards lower 2 positions, indicating formation of a (Ta, Zr)C ss [18,19]. SEM of the polished-and-thermally etched surface (not shown) revealed uniform equiaxed grains having an average diameter from ∼0.9 to 6.4 m.…”
Section: General Observationmentioning
confidence: 99%