2021
DOI: 10.1016/j.jmst.2020.06.025
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Precipitate coarsening and its effects on the hot deformation behavior of the recently developed γ'-strengthened superalloys

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Cited by 128 publications
(13 citation statements)
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“…Owing to their excellent anti-corrosion/fatigue properties and strengths, powder metallurgy (P/M) superalloys are widely applied for manufacturing the turbine disks of aero-engines [ 1 , 2 ]. However, due to the high content of alloying elements and the internal defects in P/M superalloys, hot forming processes, for example, hot-extrusion and forging processes, are fairly complex [ 3 ].…”
Section: Introductionmentioning
confidence: 99%
“…Owing to their excellent anti-corrosion/fatigue properties and strengths, powder metallurgy (P/M) superalloys are widely applied for manufacturing the turbine disks of aero-engines [ 1 , 2 ]. However, due to the high content of alloying elements and the internal defects in P/M superalloys, hot forming processes, for example, hot-extrusion and forging processes, are fairly complex [ 3 ].…”
Section: Introductionmentioning
confidence: 99%
“…That is γ′ particles tend to coarsen by consuming smaller precipitates in the thermal exposure to reduce the interface free energy [5]. When heated above the solution temperature, the coarsening behavior terminated and γ′ phases began to re-dissolve and the supersaturated solid solution re-formed.…”
Section: γ and γ′ Phasementioning
confidence: 99%
“…Many investigations have been focused on the γ′ precipitates, their evolution during heating or cooling in terms of size, shape, composition, volume fraction and lattice misfit with γ phase [5][6][7][8]. The grain boundary carbides also play an important role in the strengthening that can prevent or retard grain-boundary sliding and make the grain boundary stronger [9,10].…”
Section: Introductionmentioning
confidence: 99%
“…Bu yöntemlerin birbirlerine göre üstünlükleri vardı. Şöyle ki döküm yöntemi seri üretim için avantajlı bir üretim prosesi olmasına karşın döküm işlemindeki katılaşma çoğu zaman segregasyon ile sonuçlanır [3,4] [17]. Bu alaşımların uçaklardaki kullanım yerleri düşünüldüğünde havacılık motoru bileşenleri, gaz türbini sıcak uç bileşenleri gibi uçakların başlıca yapısal parçalarıdır [18,19].…”
Section: Introductionunclassified