TY - JOUR
T1 - Temperature Effect-Related High and Very High Cycle Fatigue Failure Analysis and Life Estimation of Forged Superalloy
AU - Lashari, M. I.
AU - Li, W.
AU - Hu, Z. F.
AU - Li, C.
AU - Cao, X. B.
AU - Jin, Y. Z.
N1 - Publisher Copyright:
© The Author(s) under exclusive licence to The Korean Institute of Metals and Materials 2025.
PY - 2025
Y1 - 2025
N2 - To analyze the temperature effect-related failure behavior and estimate the fatigue life of forged superalloy, high- and very-high-cycle fatigue experiments were performed. The microstructural characteristics, failure modes, and crack growth behavior are characterized by two- & three-dimensional microscopy techniques, along with electron-backscatter-diffraction (EBSD) analysis. The fractographic analysis demonstrated that surface failure at both 25 °C and 650 °C is attributed to surface flaws, whereas subsurface and internal failures are primarily driven by faceted cracking, often facilitated by inclusions or pores at 25 °C, and solely assisted by large grains at 650 °C. EBSD analysis revealed that crack propagation occurs in a transgranular manner, leading to the formation of facets; however, it is impeded by a complex structure comprised of high-angle grain boundaries and twin boundaries. In addition, under the influence of both temperatures, the threshold values for small as well as long cracks are elucidated. Finally, a fatigue life assessment approach that accounts for primary defects and different temperatures is established, and the prediction results demonstrate a closer alignment with the experimental data.
AB - To analyze the temperature effect-related failure behavior and estimate the fatigue life of forged superalloy, high- and very-high-cycle fatigue experiments were performed. The microstructural characteristics, failure modes, and crack growth behavior are characterized by two- & three-dimensional microscopy techniques, along with electron-backscatter-diffraction (EBSD) analysis. The fractographic analysis demonstrated that surface failure at both 25 °C and 650 °C is attributed to surface flaws, whereas subsurface and internal failures are primarily driven by faceted cracking, often facilitated by inclusions or pores at 25 °C, and solely assisted by large grains at 650 °C. EBSD analysis revealed that crack propagation occurs in a transgranular manner, leading to the formation of facets; however, it is impeded by a complex structure comprised of high-angle grain boundaries and twin boundaries. In addition, under the influence of both temperatures, the threshold values for small as well as long cracks are elucidated. Finally, a fatigue life assessment approach that accounts for primary defects and different temperatures is established, and the prediction results demonstrate a closer alignment with the experimental data.
KW - Elevated temperature
KW - Failure mechanism
KW - Fatigue crack growth
KW - Life estimation
KW - Nickel-based superalloy
UR - http://www.scopus.com/inward/record.url?scp=85217813574&partnerID=8YFLogxK
U2 - 10.1007/s12540-025-01912-z
DO - 10.1007/s12540-025-01912-z
M3 - Article
AN - SCOPUS:85217813574
SN - 1598-9623
JO - Metals and Materials International
JF - Metals and Materials International
ER -