Minor Elements and Solidification Cracking During Laser Powder-Bed Fusion of a High ?' CoNi-Base Superalloy

被引:0
|
作者
Raeker, Evan B. [1 ]
Pusch, Kira M. [1 ]
Forsik, Stephane A. J. [2 ]
Zhou, Ning [2 ]
Dicus, Austin D. [2 ]
Ren, Qing-Qiang [3 ]
Poplawsky, Jonathan D. [3 ]
Kirka, Michael M. [4 ]
Pollock, Tresa M. [1 ]
机构
[1] Univ Calif Santa Barbara, Mat Dept, Santa Barbara, CA 93106 USA
[2] Carpenter Technol Corp, R&D Dept, Reading, PA 19612 USA
[3] Oak Ridge Natl Lab, Ctr Nanophase Mat Sci, Oak Ridge, TN 37830 USA
[4] Oak Ridge Natl Lab, Mfg Sci Div, Oak Ridge, TN 37830 USA
基金
美国国家科学基金会;
关键词
NICKEL-BASED SUPERALLOY; HOT-CRACKING; MICROSTRUCTURE; BEHAVIOR;
D O I
10.1007/s11661-023-06957-6
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The cracking behavior of a high ?' volume fraction CoNi-base superalloy fabricated via laser powder bed fusion (LPBF) is studied in relation to the content of carbon and boron. Severe cracking occurred with the increase in boron content from 0.08 to 0.16 at. pct (0.015 to 0.029 wt pct), while compositions with 0.1 to 0.36 at. pct C (0.02 to 0.076 wt pct) and 0.08 at. pct B exhibited minimal cracking. Assessment of cracks in the high-boron composition shows a variation in crack density with printing parameters, and alignment of the cracks with the build direction. Scanning electron microscopy (SEM) of the crack surfaces shows evidence of a solidification cracking mode. Differential thermal analysis (DTA) reveals a decreased incipient melting temperature for the high-boron composition, and atom probe tomography (APT) is used to measure the enrichment at grain boundaries, revealing distinct boron segregation. Scheil-Gulliver solidification simulations for the different C and B levels are consistent with the incipient melting behavior observed with DTA. Evaluation of the solidification cracking susceptibility from the simulations allow for comparison of the CoNi alloy behavior to Ni-base superalloys studied for LPBF fabrication and displays how such metrics may aid in the design of new precipitation-strengthened superalloys for additive manufacturing (AM).
引用
收藏
页码:1744 / 1757
页数:14
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