IMR OpenIR
Microstructure evolution and work hardening behaviour during cold deformation of Haynes 214 superalloy
Liu, Jiaao1,2; Zhang, Weihong1; Mei, Feiqiang3; Xin, Xin1; Cao, Yichao4; Zhu, Chongwei5; Liu, Qingao1,2; Zhu, Xuhui5; Sun, Wenru1
通讯作者Zhang, Weihong(whzhang@imr.ac.cn) ; Sun, Wenru(wrsun@imr.ac.cn)
2023-05-01
发表期刊JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T
ISSN2238-7854
卷号24页码:5792-5804
摘要Using uniaxial compression tests, the microstructure evolution and work hardening behaviour of Haynes 214 superalloy were investigated in the strain rate range of 0.01-5 s(-1). The true strain-stress relationship was formulated based on a modified Tian model. The alloy exhibited a four-stage work hardening response similar to that previously reported for low stacking fault energy (SFE) face-centred cubic alloys. At strain lower of similar to 0.07 (stage I), the work hardening rate decreased. At stage II (strain between 0.07 and 0.16), because of dislocation cross-slip, the dislocation movement was difficult, and the rate of work hardening increased. At stage III (strain between 0.16 and 0.48), work hardening showed the second decreasing stage. This stage was attributed to the appearance of high angle boundaries (HAGBs) as well as deformation twins, which consumed dislocation, relieved stress concentration, changed the crystal orientation, and produced some slip systems in a favourable orientation. When strain was greater than 0.48 (stage IV), as the number of deformation twins increased and they crossed one another, a final, slightly consistent hardening regime was observed. In addition, work hardening behaviour was considerably influenced by the strain rate. The true stress was the highest at medium strain rate of 1 s(-1), and the second stage work-hardening rate at this strain rate was also larger than that at other rates, which was related to the generation of deformation twins at a high strain rate of 5 s(-1). (C) 2023 The Author(s). Published by Elsevier B.V. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
关键词Haynes 214 nickel-based superalloy Uniaxial compression tests Microstructure evolution Work-hardening behaviour Deformation twins
DOI10.1016/j.jmrt.2023.04.194
收录类别SCI
语种英语
WOS研究方向Materials Science ; Metallurgy & Metallurgical Engineering
WOS类目Materials Science, Multidisciplinary ; Metallurgy & Metallurgical Engineering
WOS记录号WOS:001055211300001
出版者ELSEVIER
引用统计
被引频次:5[WOS]   [WOS记录]     [WOS相关记录]
文献类型期刊论文
条目标识符http://ir.imr.ac.cn/handle/321006/179066
专题中国科学院金属研究所
通讯作者Zhang, Weihong; Sun, Wenru
作者单位1.Chinese Acad Sci, Shi Changxu Innovat Ctr Adv Mat, Inst Met Res, 72 Wenhua Rd, Shenyang 110016, Peoples R China
2.Univ Sci & Technol China, Dept Mat Sci & Engn, 96 Jinzhai Rd, Hefei 230026, Anhui, Peoples R China
3.Air Force Equipment Dept, Shenyang Area 2nd Mil Representat Room, Shenyang 110043, Peoples R China
4.AECC Shenyang Liming Aero Engine Grp Corp Ltd, Shenyang 110043, Peoples R China
5.AECC Shenyang Engine Res Inst, 1 Wanlian Rd, Shenyang 110015, Peoples R China
推荐引用方式
GB/T 7714
Liu, Jiaao,Zhang, Weihong,Mei, Feiqiang,et al. Microstructure evolution and work hardening behaviour during cold deformation of Haynes 214 superalloy[J]. JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T,2023,24:5792-5804.
APA Liu, Jiaao.,Zhang, Weihong.,Mei, Feiqiang.,Xin, Xin.,Cao, Yichao.,...&Sun, Wenru.(2023).Microstructure evolution and work hardening behaviour during cold deformation of Haynes 214 superalloy.JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T,24,5792-5804.
MLA Liu, Jiaao,et al."Microstructure evolution and work hardening behaviour during cold deformation of Haynes 214 superalloy".JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T 24(2023):5792-5804.
条目包含的文件
条目无相关文件。
个性服务
推荐该条目
保存到收藏夹
查看访问统计
导出为Endnote文件
谷歌学术
谷歌学术中相似的文章
[Liu, Jiaao]的文章
[Zhang, Weihong]的文章
[Mei, Feiqiang]的文章
百度学术
百度学术中相似的文章
[Liu, Jiaao]的文章
[Zhang, Weihong]的文章
[Mei, Feiqiang]的文章
必应学术
必应学术中相似的文章
[Liu, Jiaao]的文章
[Zhang, Weihong]的文章
[Mei, Feiqiang]的文章
相关权益政策
暂无数据
收藏/分享
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。