Dynamic impact response and microstructural evolution of Inconel 690 superalloy at elevated temperatures

被引:46
|
作者
Lee, WS [1 ]
Liu, CY [1 ]
Sun, TN [1 ]
机构
[1] Natl Cheng Kung Univ, Dept Mech Engn, Tainan 701, Taiwan
关键词
Inconel; 690; dynamic impact; adiabatic shearing; dislocation; twinning;
D O I
10.1016/j.ijimpeng.2004.09.007
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This study employs a compressive split-Hopkinson bar to investigate the plastic deformation behaviour of Inconel 690 super alloy when subjected to high temperature and high-strain-rate loading conditions. Dynamic impact testing is performed under strain-rates ranging from 2.3 x 10(3) to 8.3 x 10(3) s(-1) at temperatures between 25 and 900 degrees C. Optical, scanning, and transmission electron microscopy techniques are used to analyze the fracture and microstructure characteristics of the deformed specimens in order to determine the relationship between the alloy's mechanical and microstructural properties. The experimental results indicate that temperature, strain and strain rate influence the material's mechanical properties. At constant temperature, the flow stress, and strain-rate sensitivity both increase with increasing strain rate, but the activation volume and work hardening coefficient decrease. Meanwhile, at a constant strain rate, the flow stress, strain-rate sensitivity and work hardening coefficient decrease with increasing temperature, but the activation volume and temperature sensitivity increase. Shear band formation is followed by fracture characterized by dimpled structures. Microscopy yields evidence of dislocation and twinning. The dislocation and twinning densities increase with increasing strain-rate and flow stress, but decrease with increasing temperature. It is shown that the Zerilli-Armstrong constitutive equation with experimentally determined specific material parameters successfully describes the flow behaviour of the Inconel 690 super alloy under the current test conditions. (c) 2004 Elsevier Ltd. All rights reserved.
引用
收藏
页码:210 / 223
页数:14
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