Zobrazeno 1 - 10
of 91
pro vyhledávání: '"C. Argyrakis"'
Publikováno v:
The Minerals, Metals & Materials Series ISBN: 9783031274466
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29d03bbe3cc9e521c883dc7d66bdc539
https://doi.org/10.1007/978-3-031-27447-3_3
https://doi.org/10.1007/978-3-031-27447-3_3
Autor:
F. Schulz, Yu Lu, Paul Bowen, Magnus Anderson, C. Argyrakis, Hector Basoalto, Hiroto Kitaguchi
Publikováno v:
Acta Materialia. 191:81-100
The precipitation kinetics of gamma prime in the nickel based superalloy RR1000 has been characterised after solid-solution heat treatments and isothermal aging conditions relevant to service conditions. Multi-modal precipitate dispersions are formed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c2df60c32e137f42074732ad78ee4d4b
https://doi.org/10.1016/j.actamat.2020.03.058
https://doi.org/10.1016/j.actamat.2020.03.058
Autor:
Mark Hardy, J.A. Hawk, Paul D. Jablonski, Sammy Tin, Hiroto Kitaguchi, V. Saraf, R. C. Buckingham, Martin Detrois, E. T. McDevitt, C. Argyrakis
Publikováno v:
Metallurgical and Materials Transactions A. 51:2626-2650
This paper reviews the status of technology in design and manufacture of new wrought polycrystalline Ni-base superalloys for critical engineering applications. There is a strong motivation to develop new alloys that are capable of operating at higher
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::46d9189dd8ef9a71effc8886efdbb7dc
https://doi.org/10.1007/s11661-020-05773-6
https://doi.org/10.1007/s11661-020-05773-6
Autor:
M. C. Hardy, R. C. Buckingham, K. Severs, B. Cockings, J. McCarley, K. Ho, C. Argyrakis, S. Tin
Publikováno v:
Metallurgical and Materials Transactions A. 54:2127-2127
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5a1dc13d8c878480281221763d10b486
https://doi.org/10.1007/s11661-023-06971-8
https://doi.org/10.1007/s11661-023-06971-8
Autor:
C. M. F. Rae, Suyang Yu, C. Papadaki, Paul Bowen, R. C. Buckingham, Mark Hardy, P. M. Mignanelli, Alexander Evans, C. Argyrakis, S. C. H. Llewelyn, Howard J. Stone, C. Jackson, Hangyue Li, Alison Wilson, Hiroto Kitaguchi, Nick Jones, Ed Pickering, K. Severs, D.J. Child, KA Christofidou
Publikováno v:
Superalloys 2020 ISBN: 9783030518332
Two new alloy compositions for possible disk rotor applications have been examined. Both were intended to have higher \( \gamma ^{{\prime }} \) content than the existing alloy, RR1000, and be produced using powder metallurgy and isothermal forging to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5b4db02d3edf11fc9588920a44c104be
https://doi.org/10.1007/978-3-030-51834-9_2
https://doi.org/10.1007/978-3-030-51834-9_2
Publikováno v:
Reliability Engineering & System Safety. 164:110-123
A microstructure and deformation mechanism based fatigue crack initiation and life prediction model, which links microstructure variability of a polycrystalline material to the scatter in fatigue life, is validated using an uncertainty quantification
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a920b5cfd694bacd3c0bf0813ff5e104
https://doi.org/10.1016/j.ress.2017.03.006
https://doi.org/10.1016/j.ress.2017.03.006
The microstructural evolution following compression and subsequent sub-solvus and super-solvus heat treatment was studied in the Ni-based superalloy, RR1000, typically used for rotor disc applications in aero-engines. For a low strain rate of 0.1 s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5b9f7f7c9d28e79d082cc4244050a709
http://wrap.warwick.ac.uk/121425/4/WRAP-on-evolution-primary-gamma-high-strain-heat-treatment-Slater-2019.pdf
http://wrap.warwick.ac.uk/121425/4/WRAP-on-evolution-primary-gamma-high-strain-heat-treatment-Slater-2019.pdf
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Publikováno v:
The Minerals, Metals & Materials Series ISBN: 9783319894799
ATI 718Plus® is a polycrystalline multi-phase strengthened Ni-base superalloy suitable for turbine disc applications in aero engines. A typical turbine disc experiences temperatures in the rim up to 650–700 \(^{\circ }\)C and stresses as high as 1
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9c062ea835e5f8098261df8f31421bb0
https://doi.org/10.1007/978-3-319-89480-5_25
https://doi.org/10.1007/978-3-319-89480-5_25