Temperature-dependent fatigue behavior of additively manufactured Hastelloy-X: The effect of manufacturing process

被引:0
|
作者
Muhammad, Muztahid [1 ,2 ]
Ghiaasiaan, Reza [1 ,2 ]
Gradl, Paul R. [3 ]
Schobel, Andre [4 ]
Godfrey, Donald [5 ]
Shao, Shuai [1 ,2 ]
Shamsaei, Nima [1 ,2 ]
机构
[1] Auburn Univ, Natl Ctr Addit Mfg Excellence NCAME, Auburn, AL 36849 USA
[2] Auburn Univ, Dept Mech Engn, Auburn, AL 36849 USA
[3] NASA Marshall Space Flight Ctr, Prop Dept, Huntsville, AL 35812 USA
[4] Nikon SLM Solut Grp AG, Lubeck, Germany
[5] Nikon SLM Solut NA Inc, Wixom, MI 48393 USA
基金
美国国家航空航天局; 美国国家科学基金会;
关键词
Additive manufacturing; Hastelloy-X; Fatigue; Cryogenic; High temperatures; MECHANISMS; ALLOYS;
D O I
10.1016/j.jmapro.2025.01.068
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This study examined the strain-controlled, fully-reversed fatigue behavior of Hastelloy-X produced by two distinct additive manufacturing techniques, laser powder bed fusion (L-PBF) and laser powder directed energy deposition (LP-DED), across a temperature range from cryogenic conditions (-195 degrees C) to elevated temperatures (up to 760 degrees C). The fatigue crack initiation behavior was governed by persistent slip bands (PSBs) at lower temperatures (-195 degrees C to 427 degrees C) in contrast to temperatures above 427 degrees C where PSBs were absent. At elevated temperatures, in the absence of PSBs, the accumulation of fatigue damage appeared to be more rapid, leading to shorter fatigue lives. The room temperature fatigue lives at lower strain amplitudes were governed by fatigue crack initiation and were shorter for the LP-DED material that permitted easier slip. At-195 degrees C to 427 degrees C, fatigue lives of LP-DED material at higher strain amplitudes were governed by crack growth and were prolonged by the more plasticity-induced crack closure as compared to the L-PBF material. Above 427 degrees C, the absence of PSBs was equally damaging for both processes.
引用
收藏
页码:123 / 136
页数:14
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