TY - JOUR
T1 - Coupled effects of pre-strain and heat treatment on the mechanical response and fatigue performance of Inconel 718 superalloy
AU - Zhao, Pandi
AU - Xu, Yilun
AU - Zhan, Mei
AU - Sun, Zhiyan
AU - Wang, Yuyang
AU - Xin, Hai
AU - Zheng, Zebang
N1 - Publisher Copyright:
© 2026 The Authors.
PY - 2026/5/1
Y1 - 2026/5/1
N2 - Pre-strain is a critical manufacturing variable that must be considered in the design and performance assessment of metallic components. This study examines the macro-/micro-mechanical responses and fatigue behavior of Inconel 718 superalloy at room temperature after controlled pre-straining and standard aging heat treatment. Uniaxial tensile tests show a substantial strength increase accompanied by reduced elongation as pre-strain rises, with further strengthening after heat treatment. Low-cycle fatigue (LCF) life, evaluated under a peak stress of 0.95σs for each condition, decreases markedly with increasing pre-strain and is further shortened by subsequent heat treatment. EBSD, SEM, and TEM reveal increased lattice misorientation after pre-straining, persistent subgrain boundaries, and the formation of strengthening precipitates after heat treatment. Fractography confirms a three-stage fatigue process (crack initiation, propagation, and final fracture) that is insensitive to pre-strain level or heat treatment route. Mechanistically, fatigue degradation in pre-strained specimens is dominated by planar slip and severe dislocation entanglement, whereas in pre-strained and heat-treated specimens, the cyclic softening and life reduction arise from the combined effects of γ″ shearing and residual dislocation tangles. The results, obtained for pre-strain levels of 7-35%, provide an important practical implication for material design under extreme loads: achieving a balance between strength and damage tolerance is crucial, rather than solely pursuing maximum strength.
AB - Pre-strain is a critical manufacturing variable that must be considered in the design and performance assessment of metallic components. This study examines the macro-/micro-mechanical responses and fatigue behavior of Inconel 718 superalloy at room temperature after controlled pre-straining and standard aging heat treatment. Uniaxial tensile tests show a substantial strength increase accompanied by reduced elongation as pre-strain rises, with further strengthening after heat treatment. Low-cycle fatigue (LCF) life, evaluated under a peak stress of 0.95σs for each condition, decreases markedly with increasing pre-strain and is further shortened by subsequent heat treatment. EBSD, SEM, and TEM reveal increased lattice misorientation after pre-straining, persistent subgrain boundaries, and the formation of strengthening precipitates after heat treatment. Fractography confirms a three-stage fatigue process (crack initiation, propagation, and final fracture) that is insensitive to pre-strain level or heat treatment route. Mechanistically, fatigue degradation in pre-strained specimens is dominated by planar slip and severe dislocation entanglement, whereas in pre-strained and heat-treated specimens, the cyclic softening and life reduction arise from the combined effects of γ″ shearing and residual dislocation tangles. The results, obtained for pre-strain levels of 7-35%, provide an important practical implication for material design under extreme loads: achieving a balance between strength and damage tolerance is crucial, rather than solely pursuing maximum strength.
KW - Heat treatment
KW - Low-cycle fatigue
KW - Microstructure
KW - Nickel-based superalloys
KW - Pre-strain
UR - https://www.scopus.com/pages/publications/105033072603
U2 - 10.1016/j.jmrt.2026.03.117
DO - 10.1016/j.jmrt.2026.03.117
M3 - 文章
AN - SCOPUS:105033072603
SN - 2238-7854
VL - 42
SP - 861
EP - 874
JO - Journal of Materials Research and Technology
JF - Journal of Materials Research and Technology
ER -