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

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 °C) to elevated temperatures (up to 760 °C). The fatigue crack initiation behavior was governed by persistent slip bands (PSBs) at lower temperatures (−195 °C to 427 °C) in contrast to temperatures above 427 °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 °C to 427 °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 °C, the absence of PSBs was equally damaging for both processes. • Cryogenic to high temperature fatigue behavior of AM Hastelloy-X (HX) was studied. • LP-DED HX had marginally longer fatigue lives than L-PBF at higher strain amplitudes. • Initial cyclic hardening at room/elevated temperatures occurred for both processes. • Fatigue resistance for both processes decreased with rising temperatures above 427 °C. • Microstructural features instead of volumetric defects governed crack initiation.

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Publication Details

Journal
Journal of Manufacturing Processes
Published
2025-01-27
DOI
https://doi.org/10.1016/j.jmapro.2025.01.068
Citations
5
Primary Topic
Additive Manufacturing Materials and Processes
Type
article
Field-Weighted Citation Impact
3.57

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article

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

Muztahid Muhammad, Donald A. Godfrey, Paul Gradl, Anita Schöbel et al.
5 citations
Journal of Manufacturing Processes
Additive Manufacturing Materials and Processes
3.57
article

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

Muztahid Muhammad, Donald A. Godfrey, Paul Gradl, Anita Schöbel, Shuai Shao, Reza Ghiaasiaan, Nima Shamsaei
article en
5 citations

Abstract

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 °C) to elevated temperatures (up to 760 °C). The fatigue crack initiation behavior was governed by persistent slip bands (PSBs) at lower temperatures (−195 °C to 427 °C) in contrast to temperatures above 427 °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 °C to 427 °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 °C, the absence of PSBs was equally damaging for both processes. • Cryogenic to high temperature fatigue behavior of AM Hastelloy-X (HX) was studied. • LP-DED HX had marginally longer fatigue lives than L-PBF at higher strain amplitudes. • Initial cyclic hardening at room/elevated temperatures occurred for both processes. • Fatigue resistance for both processes decreased with rising temperatures above 427 °C. • Microstructural features instead of volumetric defects governed crack initiation.

Journal of Manufacturing ProcessesVol. 136
Nikon (United States) (US), Marshall Space Flight Center (US), Auburn University (US)
National Science Foundation, Marshall Space Flight Center
Openalex Percentile: Top 8%
Additive Manufacturing Materials and Processes
3.57
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