2015
DOI: 10.1016/j.msea.2015.06.021
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Effect of standard heat treatment on the microstructure and mechanical properties of selective laser melting manufactured Inconel 718 superalloy

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Cited by 572 publications
(229 citation statements)
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“…EDS analysis showed that the atomic ratio of Fe:Nb in the white plate-like phase observed in homogenized specimens (Spot 5 in Figure 6) is 2.5:1. Although the plate-like phase could not be detected by X-ray diffraction due to a relatively small amount of precipitates, its morphology and composition are comparable with the Laves phase reported in the literature [3,19]. Qi et al [3] reported the partial dissolution of the Laves phase during solution treatment at 980 °C of laser net shape manufactured specimens.…”
Section: Phase Analysis Of Heat-treated Inconel 718supporting
confidence: 62%
“…EDS analysis showed that the atomic ratio of Fe:Nb in the white plate-like phase observed in homogenized specimens (Spot 5 in Figure 6) is 2.5:1. Although the plate-like phase could not be detected by X-ray diffraction due to a relatively small amount of precipitates, its morphology and composition are comparable with the Laves phase reported in the literature [3,19]. Qi et al [3] reported the partial dissolution of the Laves phase during solution treatment at 980 °C of laser net shape manufactured specimens.…”
Section: Phase Analysis Of Heat-treated Inconel 718supporting
confidence: 62%
“…Differently, the subsequently published TEM work by Zhang et al [163] and Choi et al [192] showed that the asmanufactured SLM IN718 has very few γ ′ /γ ′′ precipitated in matrix due to the high temperature gradient and rapid solidification rate, but instead large amount of fine Laves phases and carbides can be found as well as dislocation sub-grain structures.…”
Section: Slm In718mentioning
confidence: 96%
“…As that for titanium alloys, employing SLM or EBM to manufacture Ni-base superalloys would depend on the specific case or application, since each process has its pros and cons. So far, the Ni-base superalloys applied to SLM are mainly the weldable ones, i.e., IN718 [113,[160][161][162][163][164][165][166][167], IN625 [79,80,168,169], Hastelloy X [170][171][172][173][174], Nimonic 263 [110], which have low additions of both Ti and Al and are less susceptible to strain age cracking. Expansion to the less-weldable Ni-base superalloys has also been attempted, such as IN939 [175], IN100 [176], IN738LC [177][178][179][180][181], CM247LC [114,[182][183][184] and Rene 142 [81].…”
Section: Materials Manufactured With Slmmentioning
confidence: 99%
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