Laser Powder Bed Fusion (LPBF) M789 is a recently developed alloy for fatigue‑critical tooling applications, yet its fatigue behaviour in the presence of intrinsic and extrinsic discontinuities remains largely uncharacterised. This study evaluates the discontinuity‑controlled fatigue response of the alloy using polished, as‑printed, and corrosion‑pitted specimens, fatigue tested and complemented by non‑destructive characterisation, fractography, and extreme value analysis. A Kitagawa–Takahashi diagram incorporating the experimentally measured long‑crack threshold was employed to assess the applicability of LEFM, El‑Haddad, and Murakami models. The experiments highlighted that failure initiated at discontinuities with contributions from the microstructure. Fatigue strength ranged from 93 to 282 MPa depending on surface condition, making the idealised peak fatigue strength unattainable. Process‑induced discontinuities exhibited crack‑like behaviour accurately captured by LEFM and El‑Haddad models, whereas corrosion pits have a notch‑controlled behaviour driven by geometry, with minimal interaction effect between neighbouring discontinuities. The geometric effects account for deviations from fatigue‑strength predictions and demonstrate that discontinuity size alone is insufficient to rank severity when morphologies differ. Overall, the study establishes a discontinuity‑informed basis for predicting the fatigue behaviour of LPBF M789 and supports the development of reliable design methodologies for fatigue‑critical tooling components manufactured from the alloy. .

Discontinuity-controlled fatigue performance and model assessment for LPBF-M789 maraging stainless steel with different surface conditions

Patriarca, L.;
2026-01-01

Abstract

Laser Powder Bed Fusion (LPBF) M789 is a recently developed alloy for fatigue‑critical tooling applications, yet its fatigue behaviour in the presence of intrinsic and extrinsic discontinuities remains largely uncharacterised. This study evaluates the discontinuity‑controlled fatigue response of the alloy using polished, as‑printed, and corrosion‑pitted specimens, fatigue tested and complemented by non‑destructive characterisation, fractography, and extreme value analysis. A Kitagawa–Takahashi diagram incorporating the experimentally measured long‑crack threshold was employed to assess the applicability of LEFM, El‑Haddad, and Murakami models. The experiments highlighted that failure initiated at discontinuities with contributions from the microstructure. Fatigue strength ranged from 93 to 282 MPa depending on surface condition, making the idealised peak fatigue strength unattainable. Process‑induced discontinuities exhibited crack‑like behaviour accurately captured by LEFM and El‑Haddad models, whereas corrosion pits have a notch‑controlled behaviour driven by geometry, with minimal interaction effect between neighbouring discontinuities. The geometric effects account for deviations from fatigue‑strength predictions and demonstrate that discontinuity size alone is insufficient to rank severity when morphologies differ. Overall, the study establishes a discontinuity‑informed basis for predicting the fatigue behaviour of LPBF M789 and supports the development of reliable design methodologies for fatigue‑critical tooling components manufactured from the alloy. .
2026
Cracks; Discontinuity; El-Haddad; KT diagram; M789 alloy; Murakmi; Pits;
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/1311728
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