材料工程2024,Vol.52Issue(12) :179-187.DOI:10.11868/j.issn.1001-4381.2022.001033

纳米晶AlCoCrFeNi的动态结构演化及失效机理研究

Dynamic structure evolution and failure mechanism of nanocrystalline AlCo-CrFeNi

张荣 祁文军
材料工程2024,Vol.52Issue(12) :179-187.DOI:10.11868/j.issn.1001-4381.2022.001033

纳米晶AlCoCrFeNi的动态结构演化及失效机理研究

Dynamic structure evolution and failure mechanism of nanocrystalline AlCo-CrFeNi

张荣 1祁文军1
扫码查看

作者信息

  • 1. 新疆大学 机械工程学院,乌鲁木齐 830017
  • 折叠

摘要

采用分子动力学方法模拟温度300 K和应变速率1×109 s-1下Y方向单轴拉伸纳米晶(单晶、多晶)AlCoCrFeNi高熵合金的微结构动态演化、位错及孔洞运动特性,揭示失效机理.模拟结果显示:纳米多晶AlCoCrFeNi高熵合金的最大承载荷、纵向模量和延展性均低于纳米单晶体,屈服前纳米多晶相比纳米单晶应变降幅为25%,应力峰值降幅为23.8%.拉伸过程中两种晶体的相变、位错、孔洞、失效机理均有差异.纳米单晶在拉伸过程中,主要发生FCC结构向非晶态结构转变,相变后原子位置发生变化,伴随大量Shorkly位错产生,并随非晶态结构增长方向移动,进而非晶态结构区孔洞形核、长大、贯穿到失效断裂,呈现非晶化穿孔断裂为主.纳米多晶在拉伸过程中,主要发生FCC结构向HCP结构和非晶态结构转变,相变后原子位置发生变化,伴随大量 1/6<112>(Shorkly)位错和少量 1/6<110>(Stair-rod)位错、1/3<100>(Hirth)位错及其他位错的不断产生和湮灭,材料发生一定的塑性变形,晶界非晶态结构区孔洞形核、沿晶长大并扩展、沿晶贯穿到失效断裂,呈现沿晶断裂为主.

Abstract

The molecular dynamics method was used to simulate the microstructure dynamic evolution,dislocation,and pore motion characteristics of AlCoCrFeNi high-entropy alloy at temperature 300 K and strain rate of 1×109 s-1,and the failure mechanism was revealed.The simulation results show that the maximum load-bearing,longitudinal modulus,and ductility of the nano-polycrystalline AlCoCrFeNi high-entropy alloy are lower than those of nano-monocrystalline.The strain reduction and peak stress reduction of nano-polycrystalline before yield are 25%and the peak stress reduction is 23.8%.The phase transition,dislocation,hole,and failure mechanism of the two nanocrystallines are different during the stretching process.During the stretching process of nano-monocrystals,the FCC structure is mainly transformed into a non-crystalline structure.The atomic position changes after the phase change,accompanied by a large number of Shorkly dislocations,and moves with the growth direction of the non-crystalline structure.The hole nucleation,growth,penetration,and failure fracture of non-crystalline structure area are mainly amorphous perforation fault.During the stretching process of nano-polycrystalline,the FCC structure mainly transforms to HCP structure and non-crystalline structure,and the atomic position changes after the phase change,accompanied by a large number of 1/6<112>(Shortly)dislocations and a small number of 1/6<110>(Stair-rod)dislocations,1/3<100>(Hirth)dislocations,and other dislocations continue to be generated and annihilated.The material undergoes certain plastic deformation,with nucleation of pores in the non-crystalline structure area of the grain boundary,growth and expansion along the grain boundary,and penetration through the grain boundary until failure fracture,showing mainly intergranular fracture.

关键词

分子动力学/AlCoCrFeNi/高熵合金/结构演化/纳米晶

Key words

molecular dynamics/AlCoCrFeNi/high-entropy alloy/structural evolution/nanocrystalline

引用本文复制引用

出版年

2024
材料工程
中国航发北京航空材料研究院

材料工程

CSTPCDCSCD北大核心
影响因子:0.78
ISSN:1001-4381
段落导航相关论文