2018
DOI: 10.1007/s11661-018-4745-6
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Rejuvenation of Single-Crystal Ni-Base Superalloy Turbine Blades: Unlimited Service Life?

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Cited by 25 publications
(18 citation statements)
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“…Therefore, this degraded microstructure will deteriorate the creep property of K465 alloy. Similar results were also previously reported on a single crystal Ni-base superalloy [32]. However, it is still not clear why the creep property of a sample with high accumulated strain cannot be fully rejuvenated by performing RHT.…”
Section: Effect Of Rht On the Creep Behavior Of K465 Alloysupporting
confidence: 86%
“…Therefore, this degraded microstructure will deteriorate the creep property of K465 alloy. Similar results were also previously reported on a single crystal Ni-base superalloy [32]. However, it is still not clear why the creep property of a sample with high accumulated strain cannot be fully rejuvenated by performing RHT.…”
Section: Effect Of Rht On the Creep Behavior Of K465 Alloysupporting
confidence: 86%
“…The limitations of these approaches are that they are much more time consuming and they require the knowledge of the initial distribution of elements in the as-cast state. The same applies regarding the optimization of the precipitate size during aging heat treatments using phase-field approaches [113][114][115][116][117] at the expanse of very simple and efficient mean-field Lifshitz-Slyozov-Wagner (LSW) models [118,119].…”
Section: 22) Optimizationsmentioning
confidence: 99%
“…No exception to this "rule of thumbs" can be noticed in the open literature for ~ <001> oriented components (the usual crystallographic orientation along the profile of blades) while it is known that the optimal precipitate edge length in terms of creep resistance for ~ <111> oriented SX specimens is around 200 nm [64]. This optimal precipitate size and regularity is also one of the targets to be reached for serviced components using rejuvenation procedures involving a ST and/or HIPping procedure after several hours of use [114,[120][121][122].…”
Section: ) Mechanical Properties Sensitivity To the Processing Parameters 41) Creep And Tensile Propertiesmentioning
confidence: 99%
“…At present, two methods have been proposed to extend the lives of crept superalloys, which are hot isostatic pressing [7,8] and rejuvenation heat treatment [9][10][11]. Hot isostatic pressing shows great advantages in closing up the creep holes, while rejuvenation heat treatment, which employs much less complex equipment and auxiliaries, is more suitable to superalloy single crystal components after a certain period of service without many creep holes generated.…”
Section: Introductionmentioning
confidence: 99%