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2222材料工程  2019, Vol. 47 Issue (7): 121-125    DOI: 10.11868/j.issn.1001-4381.2018.000336
  研究论文 本期目录 | 过刊浏览 | 高级检索 |
基于Normalized Cockcroft & Latham韧性损伤准则Ti600合金临界损伤值的测定
张菁丽(), 吴金平, 罗媛媛, 赵彬, 郭荻子, 赵圣泽, 杨帆
西北有色金属研究院, 西安 710016
Determination of critical damage value of Ti600 alloy based on Normalized Cockcroft & Latham ductile fracture criterion
Jing-li ZHANG(), Jin-ping WU, Yuan-yuan LUO, Bin ZHAO, Di-zi GUO, Sheng-ze ZHAO, Fan YANG
Northwest Institute for Non-ferrous Metal Research, Xi'an 710016, China
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摘要 

采用物理实验与数值模拟相结合的方法确定材料在给定条件下的临界损伤值,进行Ti600合金1010℃,0.001s-1下的拉伸实验,获得该条件下的真实应力-应变曲线。同时简化Normalized Cockcroft & Latham损伤模型,以真应变ε1代替等效应变ε,极限拉应力σUTS代替等效应力σ,计算得到高温钛合金Ti600在该条件下的临界损伤值。将此损伤值嵌入有限元软件中,对之前的拉伸过程进行数值模拟验证,以确定该临界损伤值的准确性。结果表明:Ti600合金在1010℃,0.001s-1下的临界损伤值为0.643。将其代入有限元软件模拟拉伸过程发现,试样裂纹萌生和扩展位置预测准确,最小横截面变化规律与实验基本相符。这说明基于Normalized Cockcroft & Latham模型和拉伸实验测得的Ti600临界损伤值是较准确的。

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张菁丽
吴金平
罗媛媛
赵彬
郭荻子
赵圣泽
杨帆
关键词 高温拉伸物理实验损伤预测有限元分析    
Abstract

Critical damage value of material was obtained by physical experiment combined with a finite element software. True stress-strain curve of Ti600 alloy was studied by high temperature tensile test at 1010℃ and 0.001s-1. A simplified Normalized Cockcroft & Latham ductile fracture criterion was used, in which ε and σ were substituted by ε1 and σUTS, respectively. The critical damage value of Ti600 alloy on the above experimental condition was calculated and then was embedded in a finite element software to verify its accuracy by analysing high temperature tensile process. The result shows that the critical damage value of Ti600 alloy at 1010℃ and 0.001s-1 equals 0.643. By the finite element analysis, the crack initiation and propagation are predicted well and computational variety law of minimum cross sectional area is basically agreed with the experimental law. Hence, the critical damage value of Ti600 alloy obtained by combining a Normalized Cockcroft & Latham ductile fracture criterion with a finite element software is fairly precise.

Key wordshigh temperature tension    physical experiment    damage prediction    finite element analysis
收稿日期: 2018-03-29      出版日期: 2019-07-19
中图分类号:  TG319  
基金资助:国家自然科学基金资助项目(51805442);陕西省科技统筹创新工程计划(2016KTCQ01-103)
通讯作者: 张菁丽     E-mail: jingshuishenyou@163.com
作者简介: 张菁丽(1987-), 女, 博士, 工程师, 研究方向为钛合金成形, 联系地址:陕西省西安市未央区未央路96号西北有色金属研究院(710016), E-mail:jingshuishenyou@163.com
引用本文:   
张菁丽, 吴金平, 罗媛媛, 赵彬, 郭荻子, 赵圣泽, 杨帆. 基于Normalized Cockcroft & Latham韧性损伤准则Ti600合金临界损伤值的测定[J]. 材料工程, 2019, 47(7): 121-125.
Jing-li ZHANG, Jin-ping WU, Yuan-yuan LUO, Bin ZHAO, Di-zi GUO, Sheng-ze ZHAO, Fan YANG. Determination of critical damage value of Ti600 alloy based on Normalized Cockcroft & Latham ductile fracture criterion. Journal of Materials Engineering, 2019, 47(7): 121-125.
链接本文:  
http://jme.biam.ac.cn/CN/10.11868/j.issn.1001-4381.2018.000336      或      http://jme.biam.ac.cn/CN/Y2019/V47/I7/121
Fig.1  试样尺寸示意图
Fig.2  拉伸实验简图
Fig.3  Ti600合金工程应力-应变曲线
Fig.4  Ti600合金真实应力-应变曲线
Fig.5  Ti600合金高温拉伸过程
Fig.6  试样最小横截面直径变化曲线
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