2015
DOI: 10.1016/j.msea.2015.05.035
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Effect of heat treatment on the microstructure and mechanical properties of Inconel 718 processed by selective laser melting

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Cited by 612 publications
(278 citation statements)
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“…These values are very close to nickel-based superalloys used for advanced turbine engines with YS often in the range of 900-1300 MPa and UTS of 1200-1600 MPa [18]. However, it should be noted that SLM-processed materials are characterized by a strong anisotropy and high residual stresses after fabrication which affect their mechanical behavior [9,19,20]. Consequently, further studies of high-temperature mechanical properties of Ti-Re alloys, taking into account the microstructure anisotropy and internal stresses, are needed for their comparison to Ni-based superalloys.…”
Section: Introductionsupporting
confidence: 64%
“…These values are very close to nickel-based superalloys used for advanced turbine engines with YS often in the range of 900-1300 MPa and UTS of 1200-1600 MPa [18]. However, it should be noted that SLM-processed materials are characterized by a strong anisotropy and high residual stresses after fabrication which affect their mechanical behavior [9,19,20]. Consequently, further studies of high-temperature mechanical properties of Ti-Re alloys, taking into account the microstructure anisotropy and internal stresses, are needed for their comparison to Ni-based superalloys.…”
Section: Introductionsupporting
confidence: 64%
“…Besides the microstructure characterizations, focus is also put on the building orientation dependency of mechanical properties. Though the mechanical properties largely depend on the specific process parameters, the general trends and observations are common to all SLM IN718 builds: the horizontally built samples have slightly higher tensile strength than the vertically built samples [160,164,166,194,195].…”
Section: Slm In718mentioning
confidence: 99%
“…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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