材料科学
高温合金
剪切(物理)
微观结构
极限抗拉强度
位错
材料的强化机理
冶金
变形机理
合金
单晶
延展性(地球科学)
复合材料
打滑(空气动力学)
结晶学
蠕动
热力学
化学
物理
作者
Zihao Tan,X.G. Wang,Yao Du,Tao-Tao Duan,Yanhong Yang,J.L. Liu,J.D. Liu,Lin Yang,J.G. Li,Yu Zhou,Xiaofeng Sun
标识
DOI:10.1016/j.msea.2020.138997
摘要
The affordability has become a key element in the development of the modern aero-engines thus the design and research of low-cost single crystal superalloys are in great demand. A kind of novel Nickel-based single crystal superalloy with cost reduction was designed in this work and the temperature dependence on the microstructure modification as well as corresponding deformation mechanisms during tensile tests were systematically investigated. The experimental alloy exhibited a remarkable yield strength of 912 MPa but relatively poor ductility at 760 °C. At higher temperatures, an overt strain softening occurred before the tensile rupture and the fracture features were identified as dimples induced by the accumulated micro-pores. The stacking faults shearing mechanism prevailed at room temperature and there presented two types of stacking faults in the γ′ precipitates. Both decomposition and cross-slip of the a/2 <101> superdislocation were observed at 760 °C while the deformation mechanism was controlled by APB-coupled dislocation pairs shearing the γ′ phase at 980 °C. With temperature increasing to 1100 °C and 1120 °C, the amount of shearing dislocation pairs decreased dramatically, besides, the interfacial dislocation networks and rafted γ/γ′ structures were formed. The degradation of mechanical properties was considerably slight from 1100 °C to 1120 °C, however, three primary microstructure modifications were emphasized.
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