TY - JOUR
T1 - Tensile Behavior and Microstructural Evolution of the Polycrystalline Nickel-Based Superalloy Applied in Turbine Disk
AU - Shen, Xiuli
AU - Dong, Shaojing
AU - Chen, Zhiying
N1 - Publisher Copyright:
© 2019 Walter de Gruyter GmbH, Berlin/Boston.
PY - 2019/8/1
Y1 - 2019/8/1
N2 - In the present study, the mechanical behaviors and microstructural evolution of the nickel-based superalloy FGH97 at different temperatures and strain rates were studied. First, the tensile tests were conducted at temperatures of 20°C, 450°C and 700°C, respectively, at two specified strain rates of 0.00025 s-1 and 0.001 s-1. Second, the microscopic observations of the sections were carried out to analyze the microstructure feature. Based on the test data and the observations, it was found that the influence of strain rate on the deformation and elongation will be weakened at higher temperature. Furthermore, the phenomenon of stress serrations and the intermedia temperature brittleness were just observed at 450°C, and the reason for that was investigated.
AB - In the present study, the mechanical behaviors and microstructural evolution of the nickel-based superalloy FGH97 at different temperatures and strain rates were studied. First, the tensile tests were conducted at temperatures of 20°C, 450°C and 700°C, respectively, at two specified strain rates of 0.00025 s-1 and 0.001 s-1. Second, the microscopic observations of the sections were carried out to analyze the microstructure feature. Based on the test data and the observations, it was found that the influence of strain rate on the deformation and elongation will be weakened at higher temperature. Furthermore, the phenomenon of stress serrations and the intermedia temperature brittleness were just observed at 450°C, and the reason for that was investigated.
KW - high temperature
KW - microstructural evolution
KW - nickel-based superalloy
KW - tensile behavior
KW - uniaxial tension
UR - https://www.scopus.com/pages/publications/85073912223
U2 - 10.1515/tjj-2016-0075
DO - 10.1515/tjj-2016-0075
M3 - 文章
AN - SCOPUS:85073912223
SN - 0334-0082
VL - 36
SP - 339
EP - 346
JO - International Journal of Turbo and Jet Engines
JF - International Journal of Turbo and Jet Engines
IS - 3
ER -