TY - JOUR
T1 - Temperature Effects on the Deformation Mechanisms in a Ni-Co-Based Superalloys
AU - Hu, Rui
AU - Zhao, Jiaheng
AU - Yang, Cheng
AU - Du, Jinhui
AU - Luo, Xian
AU - Bi, Zhongnan
AU - Gan, Bin
N1 - Publisher Copyright:
© 2022 by the authors.
PY - 2022/10
Y1 - 2022/10
N2 - The tensile properties of a Ni-Co-based superalloy were investigated from room temperature to 900 °C. From 25 to 650 °C, the yield strength and tensile strength of the alloy decreased slightly, while the elongation decreased sharply. From 760 °C to 900 °C, the yield strength and tensile strength were greatly reduced, while the elongation also had a low value. With the increase in temperature, the deformation mechanism transformed from anti-phase boundary shearing to stacking fault shearing, and then from deformation twinning to Orowan bypassing, respectively. Deformation twins were generated in the deformed alloy with high-density stacking faults and they can contribute to the high strength. The alloy in this study has good mechanical properties and hot working characteristics below 760 °C and can be used as a turbine disk, turbine blade, combustion chamber, and other aircraft structural parts.
AB - The tensile properties of a Ni-Co-based superalloy were investigated from room temperature to 900 °C. From 25 to 650 °C, the yield strength and tensile strength of the alloy decreased slightly, while the elongation decreased sharply. From 760 °C to 900 °C, the yield strength and tensile strength were greatly reduced, while the elongation also had a low value. With the increase in temperature, the deformation mechanism transformed from anti-phase boundary shearing to stacking fault shearing, and then from deformation twinning to Orowan bypassing, respectively. Deformation twins were generated in the deformed alloy with high-density stacking faults and they can contribute to the high strength. The alloy in this study has good mechanical properties and hot working characteristics below 760 °C and can be used as a turbine disk, turbine blade, combustion chamber, and other aircraft structural parts.
KW - deformation mechanism
KW - intermediate-temperature brittleness
KW - microstructure
KW - nickel-based superalloy
UR - http://www.scopus.com/inward/record.url?scp=85140760713&partnerID=8YFLogxK
U2 - 10.3390/cryst12101409
DO - 10.3390/cryst12101409
M3 - 文章
AN - SCOPUS:85140760713
SN - 2073-4352
VL - 12
JO - Crystals
JF - Crystals
IS - 10
M1 - 1409
ER -