TY - JOUR
T1 - Microstructure of nickel-base superalloy MAR-M247 additively manufactured through scanning laser epitaxy (SLE)
AU - Basak, Amrita
AU - Das, Suman
N1 - Publisher Copyright:
© 2017 Elsevier B.V.
PY - 2017
Y1 - 2017
N2 - Scanning laser epitaxy (SLE) is a laser powder bed fusion (LPBF) based additive manufacturing (AM) process developed for the repair and manufacture of gas turbine hot-section components made of nickel-base superalloys. In the present study, the single-pass fabrication of more than 1500 μm thick deposits of MAR-M247, a non-weldable superalloy atop similar chemistry substrates using a high-power laser beam is demonstrated. Metallurgical continuity is achieved across the entire deposit-substrate interface and the samples show little or no warpage across a broad range of processing parameters. In order to relieve the residual stresses and enable precipitation of the strengthening phases, the SLE-deposited MAR-M247 samples are subjected to a commercially available heat treatment process. Microstructures of the as-deposited and the heat-treated MAR-M247 samples are investigated using optical microscopy (OM), scanning electron microscopy (SEM), energy dispersive X-ray spectroscopy (EDS), X-ray diffraction (XRD), and Vickers microhardness measurements. The crack-free deposits obtained here for MAR-M247 represent one of the first few successes reported for a non-weldable alloy of its kind. The results demonstrate that the SLE process has significant potential for the AM-based repair of existing and fabrication of entirely new gas turbine hot-section components utilizing feedstocks of high γ′ content nickel-base superalloy powders. The results also establish that MAR-M247 is an attractive material for the LPBF-based AM processes.
AB - Scanning laser epitaxy (SLE) is a laser powder bed fusion (LPBF) based additive manufacturing (AM) process developed for the repair and manufacture of gas turbine hot-section components made of nickel-base superalloys. In the present study, the single-pass fabrication of more than 1500 μm thick deposits of MAR-M247, a non-weldable superalloy atop similar chemistry substrates using a high-power laser beam is demonstrated. Metallurgical continuity is achieved across the entire deposit-substrate interface and the samples show little or no warpage across a broad range of processing parameters. In order to relieve the residual stresses and enable precipitation of the strengthening phases, the SLE-deposited MAR-M247 samples are subjected to a commercially available heat treatment process. Microstructures of the as-deposited and the heat-treated MAR-M247 samples are investigated using optical microscopy (OM), scanning electron microscopy (SEM), energy dispersive X-ray spectroscopy (EDS), X-ray diffraction (XRD), and Vickers microhardness measurements. The crack-free deposits obtained here for MAR-M247 represent one of the first few successes reported for a non-weldable alloy of its kind. The results demonstrate that the SLE process has significant potential for the AM-based repair of existing and fabrication of entirely new gas turbine hot-section components utilizing feedstocks of high γ′ content nickel-base superalloy powders. The results also establish that MAR-M247 is an attractive material for the LPBF-based AM processes.
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U2 - 10.1016/j.jallcom.2017.02.013
DO - 10.1016/j.jallcom.2017.02.013
M3 - Article
AN - SCOPUS:85013885226
SN - 0925-8388
VL - 705
SP - 806
EP - 816
JO - Journal of Alloys and Compounds
JF - Journal of Alloys and Compounds
ER -