High-temperature deformation and processing maps of Zr-4 metal matrix with dispersed coated surrogate nuclear fuel particles

被引:15
作者
Chen, Jing [1 ]
Liu, Huiqun [1 ]
Zhang, Ruiqian [2 ,3 ]
Li, Gang [2 ,3 ]
Yi, Danqing [1 ]
Lin, Gaoyong [1 ]
Guo, Zhen [2 ,3 ]
Liu, Shaoqiang [2 ,3 ]
机构
[1] Cent S Univ, Sch Mat Sci & Engn, Changsha 410083, Hunan, Peoples R China
[2] Nucl Power Inst China, Chengdu 610213, Sichuan, Peoples R China
[3] Sci & Technol Reactor Fuel & Mat Lab, Chengdu 610213, Sichuan, Peoples R China
关键词
Zr-4 metal matrix; Coated surrogate nuclear fuel particles; High-temperature deformation; Processing map; Microstructure; HOT DEFORMATION; ACTIVATION-ENERGY; MICROSTRUCTURE EVOLUTION; MICROENCAPSULATED FUELS; COATING LAYER; BEHAVIOR; COMPOSITE; ALLOY; STEEL; FABRICATION;
D O I
10.1016/j.rinp.2018.04.025
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
High-temperature compression deformation of a Zr-4 metal matrix with dispersed coated surrogate nuclear fuel particles was investigated at 750 degrees C-950 degrees C with a strain rate of 0.01-1.0 s(-1) and height reduction of 20%. Scanning electron microscopy was utilized to investigate the influence of the deformation conditions on the microstructure of the composite and damage to the coated surrogate fuel particles. The results indicated that the flow stress of the composite increased with increasing strain rate and decreasing temperature. The true stress-strain curves showed obvious serrated oscillation characteristics. There were stable deformation ranges at the initial deformation stage with low true strain at strain rate 0.01 s(-1) for all measured temperatures. Additionally, the coating on the surface of the surrogate nuclear fuel particles was damaged when the Zr-4 matrix was deformed at conditions of high strain rate and low temperature. The deformation stability was obtained from the processing maps and microstructural characterization. The high-temperature deformation activation energy was 354.22, 407.68, and 433.81 kJ/mol at true strains of 0.02, 0.08, and 0.15, respectively. The optimum deformation parameters for the composite were 900-950 degrees C and 0.01 s(-1). These results are expected to provide guidance for subsequent determination of possible hot working processes for this composite.
引用
收藏
页码:1057 / 1066
页数:10
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