Microstructural evolution of an aged Ni-based superalloy under two-stage hot compression with different strain rates

被引:29
作者
Li, Kuo-Kuo [1 ,2 ]
Chen, Ming-Song [1 ,2 ]
Lin, Y. C. [1 ,2 ,3 ]
Yuan, Wu-Quan [1 ,2 ]
机构
[1] Cent S Univ, Sch Mech & Elect Engn, Changsha 410083, Hunan, Peoples R China
[2] State Key Lab High Performance Complex Mfg, Changsha 410083, Hunan, Peoples R China
[3] Cent S Univ, Light Alloy Res Inst, Changsha 410083, Hunan, Peoples R China
基金
中国国家自然科学基金;
关键词
Hot deformation; Alloy; Dynamic recrystallization; Microstructural evolution; NICKEL-BASED SUPERALLOY; DYNAMIC RECRYSTALLIZATION BEHAVIOR; STRENGTH ARMOR STEEL; DEFORMATION-BEHAVIOR; CONSTITUTIVE MODEL; PROCESSING MAP; TEMPERATURE DEFORMATION; CRYOGENIC TEMPERATURE; FLOW BEHAVIOR; GRAIN-SIZE;
D O I
10.1016/j.matdes.2016.09.007
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The microstructural evolution of an aged Ni-based superalloy under two-stage hot compressive deformation with different strain rates is investigated. In terms of strain rate, the hot compressive tests include two types: constant and stepped strain rates. For the first type, the strain rate remains constant during thewhole hot compression, while for the second type, the hot compression process consists of two stages: I and II. Moreover, the strain rate of stage I (0.01, 0.1, and 1 s(-1)) is larger than that of stage II (0.001 s(-1)). It is found that the strain rate and strain of stage I greatly affect the microstructural evolution for the hot compressive deformation with stepped strain rates. In the tested strain rate and strain, both the dissolution rate of delta phase and the dynamic recrystallization (DRX) volume fraction increase with the decrease of strain rate or the increase of strain in stage I. Compared with the constant strain rate hot deformation, the stepped strain rates can obviously promote DRX behaviors and the dissolution of d phase if the appropriate strain rate and strain of stage I are chosen. These findings can be directly applied in the practical industrial production of superalloy components. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:344 / 352
页数:9
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