2022
DOI: 10.1016/j.xcrp.2022.100991
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Creep strength of refractory high-entropy alloy TiZrHfNbTa and comparison with Ni-base superalloy CMSX-4

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Cited by 14 publications
(5 citation statements)
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“…An AgieCharmilles Cut 200 SP wire-cut electrical discharge machine is used to slice the ingots into ~1 mm thick sheets. The second specimen type, called rolled state, is TiZrNbHfTa derived through cold-rolling an arc-melted ingot after 48 h of homogenization at 1200 °C under vacuum, as described by Gadelmeier et al [23]. A final sheet thickness of ~1 mm is obtained after a ~90 % thickness reduction during the rolling process.…”
Section: Materials Synthesismentioning
confidence: 99%
“…An AgieCharmilles Cut 200 SP wire-cut electrical discharge machine is used to slice the ingots into ~1 mm thick sheets. The second specimen type, called rolled state, is TiZrNbHfTa derived through cold-rolling an arc-melted ingot after 48 h of homogenization at 1200 °C under vacuum, as described by Gadelmeier et al [23]. A final sheet thickness of ~1 mm is obtained after a ~90 % thickness reduction during the rolling process.…”
Section: Materials Synthesismentioning
confidence: 99%
“…One such class comprises the RHEAs which, because of their high melting points, have been proposed as candidates for ultrahigh-temperature applications 3 6 . However, a single-phase RHEA, TiZrHfNbTa, was recently shown to be significantly weaker in creep than CMSX-4 despite the former’s higher melting point 7 . The weakness was ascribed to two factors: faster diffusion in the BCC matrix of the RHEA relative to the FCC matrix of CMSX-4 and a lack of precipitates.…”
Section: Introductionmentioning
confidence: 99%
“…Meanwhile, RHEAs with higher melting points must also be investigated since diffusion will be slower in such materials. One such RHEA is VNbMoTaW 8 , whose melting point is ~500 °C higher than TiZrHfNbTa 7 , 9 , 10 . However, it has a major disadvantage: lack of ductility at room temperature even in compression 8 .…”
Section: Introductionmentioning
confidence: 99%
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“…This research was mainly driven by the need for more heat-resistant materials in aircraft engine turbosuperchargers. It has been paced in the 1940s by the increasing demands of the gas turbine engine technology, and in the early 1950s by space based nuclear reactor programs (Fawley et al, 1972;Philips et al, 2020). Ni-based superalloys with their unique combination of mechanical and physical properties at temperatures up to 1,150 °C (Rame et al, 2020) have since been the staple structural material of high temperature applications.…”
Section: Introductionmentioning
confidence: 99%