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兵工学报 ›› 2020, Vol. 41 ›› Issue (7): 1401-1407.doi: 10.3969/j.issn.1000-1093.2020.07.018

• 论文 • 上一篇    下一篇

Ti6321钛合金在Taylor杆冲击下的动态断裂微观组织观测

徐雪峰1, 王琳1,2,3, 程兴旺1,2, 刘安晋1, Tayyeb Ali1, 周哲1, 宁子轩1, 张斌斌4, 赵登辉5   

  1. (1.北京理工大学 材料学院, 北京 100081; 2.北京理工大学 冲击环境材料技术国家级重点实验室, 北京 100081;3.北京理工大学 爆炸科学与技术国家重点实验室, 北京 100081; 4.洛阳船舶材料研究所, 河南 洛阳 471023;5.中国兵器工业标准化研究所, 北京 100089)
  • 收稿日期:2019-05-13 修回日期:2019-05-13 上线日期:2020-09-23
  • 作者简介:徐雪峰(1995—), 男, 硕士研究生。 E-mail: bit_xfx@163.com
  • 基金资助:
    爆炸科学与技术国家重点实验室基金项目(YBKT-17-06)

Dynamic Observation of Fracture Microstructure of Ti6321 Titanium Alloy in TaylorBar Impact Test

XU Xuefeng1, WANG Lin1,2,3, CHENG Xingwang1,2, LIU Anjin1, TAYYEB Ali1, ZHOU Zhe1, NING Zixuan1, ZHANG Binbin4, ZHAO Denghui5   

  1. (1.School of Materials Science and Engineering, Beijing Institute of Technology, Beijing 100081, China; 2.National Key Laboratory of Science and Technology on Materials under Shock and Impact, Beijing Institute of Technology, Beijing 100081, China; 3.State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing 100081, China; 4.Luoyang Ship Materials Research Institute, Luoyang 471023, Henan, China; 5.China Ordnance Industrial Standardization Research Institute, Beijing 100089, China)
  • Received:2019-05-13 Revised:2019-05-13 Online:2020-09-23

摘要: 通过固溶处理获得近α型Ti6321钛合金的双态和魏氏组织,研究不同组织对材料在Taylor杆冲击条件下动态损伤和断裂行为的影响。利用Taylor杆对材料进行动态加载,弹体的撞击速度范围为146~228 m/s,结合光学显微镜、扫描电子显微镜和定量金相表征方法对其微观组织演化进行观察分析。结果表明:双态组织的Ti6321合金具有更好的抗冲击性能;双态组织和魏氏组织试样在加载后的显微组织均发生了明显变化,随着冲击加载速度的增加,双态组织的初生α晶粒尺寸由25.3 μm减小至16.7 μm,次生α相和β相在载荷作用下变形、碎化;对于魏氏组织钛合金,次生α相沿受力方向显著拉长;观察断口可以发现,两种组织试样的断口均可以分为光滑熔融区和韧窝区,两个区域之间的界限并不明显;两种组织试样均发生了绝热剪切破坏,相比于魏氏组织,双态组织Ti6321合金具有较低的绝热剪切敏感性。

关键词: 钛合金, 动态断裂行为, Taylor杆冲击实验, 绝热剪切带

Abstract: The duplex and lamellar structures were obtained by heat treatment of near α-Ti6321 alloy. The influences of different microstructures on the dynamic damage and fracture behavior of material are investigated under Taylor bar impact test. The Taylor bar is used to test the cylindrical samples under dynamic compression loading, with impact velocity ranging from 146 m/s to 228 m/s. The microstructure evolution is observed and analyzed by using optical microscope, scanning electronic microscopy and quantitative metallography. The experimental results show that Ti6321 alloy with duplex structure exhibits better impact resistance property. All samples deform significantly after dynamic compression loading. With increase in impact velocity, the primary α grain size of the duplex structure decreases from 25.3 μm to 16.7 μm, and the secondary α phase and β phase are deformed and crushed under dynamic loading. The secondary α phase of lamellar structure samples is significantly elongated along the direction of the loading. The smooth melting areas and dimple areas can be observed from the impact fracture morphologies, and the boundary between two areas is not obvious. The failure mode of titanium alloy with both the structures is adiabatic shear banding. Compared to lamellar structure samples, Ti6321 alloy with duplex structure exhibits a better capability to resist an adiabatic shear damage. Key

Key words: titaniumalloy, dynamicfracturebehavior, Taylorbarimpacttest, adiabaticshearbanding

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