网站首页期刊简介编委会过刊目录投稿指南广告合作征订与发行联系我们English
TC2管材超塑性变形行为
英文标题:Study on superplastic behavior of TC2 extrusion tube
作者:刘宝胜 吴为 曾元松 韩秀全 
单位:北京航空制造工程研究所 
关键词:TC2 超塑性 m值 激活能 K值 
分类号:
出版年,卷(期):页码:2014,39(4):122-125
摘要:

 采用TC2管材纵向剖条试样,在880及920 ℃、初始应变速率分别为1.0×10-4,5.0×10-4,8.0×10-4,2.0×10-3和5.0×10-3 s-1条件下进行了超塑性拉伸试验。样本数据显示,TC2管材在880 ℃及应变速率1.0×10-4 s-1条件下获得最大伸长率为240%。基于等应变原则,结合Backofen超塑性本构方程,采用多试样法获得了不同温度下的m值。采用Arrhenius简化本构方程计算了TC2管激活能Q。最后,以斜率法和截距法计算了880及920 ℃时的K值,结果显示,2种方法计算结果接近。

 The superplastic behavior of longitudinal cutting sample for TC2 extrusion tube was investigated at the temperatures of 880 and 920 ℃ and at the strain rates of 1.0×10-4,5.0×10-4,8.0×10-4,2.0×10-3 and 5.0×10-3s-1. According to the sample data, the maximum elongation of 240% was obtained at the condition of 880 ℃ and strain rate 1.0×10-4s-1. Based on equal strain principle and Backofen superplastic constitutive equation, the approach of multiple samples was applied to test the m value. The activation energy Q was also calculated by using Arrhenius equation. Finally, K values at 880 and 920 ℃ were calculated by using slope method and intercept method, and the results of which were close. 

基金项目:
航空基金资助项目(201211250001)
作者简介:
刘宝胜(1979-),男,博士,工程师
参考文献:

[1]《中国航空材料手册》编辑委员会. 中国航空材料手册: 第四卷. 钛合金 铜合金[M]. 北京: 中国标准出版社, 2001.


 

“China Aviation Materials Handbook” Editorial Board of China Aeronautical Materials Manual: Volume IV. Titanium Copper Alloy[M]. Beijing: Standards Press of China, 2001.

 

[2]王洋, 尤逢海, 朱景川, 等.TA15 合金热变形行为研究[J]. 机械工程材料, 2006, 30(11): 63-65. 

 

Wang Yang, You Fenghai, Zhu Jingchuan, et al. Hot study on deformation behavior of TA15 alloy [J]. Materials for Mechanical Engineering, 2006, 30 (11): 63-65.

 

[3]邵宗科, 张文明, 黄重国, 等. TC4钛合金负角度零件超塑成形及性能研究[J]. 稀有金属, 2012, 36(4): 511-516.

 

Shao Zongke, Zhang Wenming, Huang Zhongguo, et al. Superplastic forming and mechanical properties for TC4 alloy negative-angle part[J]. Rare Metals, 2012, 36(4): 511-516.

 

[4]Li Miaoquan, Xiong Aiming, Cheng Shenghui, et al. Effects of process parameters on the microstructure during the hot compression of a TC6 titanium alloy[J].Rare Metals, 2004, 23(3): 263-268.

 

[5]赵建国, 张士宏, 程明, 等. TC21合金的高温变形行为及其组织演变[J]. 稀有金属, 2009, 33(2):153-158. 

 

Zhao Jianguo, Zhang Shihong, Cheng Ming, et al. Deformation behaviors and microstructure evolution of TC21 alloy in hot working[J]. Rare Metal Materials and Engineering, 2009, 33(2):153-158. 

 

[6]周伟, 葛鹏, 赵永庆, 等. Ti-5553合金高温变形时动态再结晶行为[J]. 稀有金属材料与工程, 2012, 41(8): 1381-1384.

 

Zhou Wei, Ge Peng, Zhao Yongqing, et al. The dynamic recrystallization behavior of Ti-5553 titanium alloy during hot deformation[J]. Rare Metal Materials and Engineering,2012, 41(8): 1381-1384.

 

[7]刘彬, 黄旭, 黄利军, 等. TB6钛合金多重固溶时效热处理工艺研究[J]. 稀有金属, 2009, 33(4): 489-493.

 

Liu Bin, Huang Xu, Huang Lijun, et al. Effect of multiple solution and aging treatment on microstructure and mechanical property of TB6 titanium alloy[J]. Chinese Journal of Rare Metals, 2009, 33(4): 489-493.

 

[8]GB/T 24172-2009. 金属超塑性材料拉伸性能测定方法[S]. 

 

GB/T 24172-2009. Determination of tensile properties of metallic superplastic materials method [S]. 

 

[9]吴诗惇. 金属超塑性变形理论[M]. 北京: 国防工业出版社, 1997.

 

Wu Shidun. Metal Superplastic Deformation Theory [M]. Beijing: National Defense Industry Press, 1997.

 

[10]张凯峰, 王国峰. 先进材料超塑成形技术[M]. 北京: 科学出版社, 2012. 

 

Zhang Kaifeng, Wang Guofeng. Advanced Materials Superplastic Forming Technology [M]. Beijing: Science Press, 2012.

 

[11]Sellars C M, Tegart W J. Hot workability[J]. International Metallurgical Reviews,1972, 17(1):1-24.
服务与反馈:
文章下载】【加入收藏
《锻压技术》编辑部版权所有

中国机械工业联合会主管  中国机械总院集团北京机电研究所有限公司 中国机械工程学会主办
联系地址:北京市海淀区学清路18号 邮编:100083
电话:+86-010-82415085 传真:+86-010-62920652
E-mail: fst@263.net(稿件) dyjsjournal@163.com(广告)
京ICP备07007000号-9