固溶温度对TB6钛合金动态力学性能和微观组织的影响

张昭 郭保桥 冉春 陈稳 陈鹏万

张昭, 郭保桥, 冉春, 陈稳, 陈鹏万. 固溶温度对TB6钛合金动态力学性能和微观组织的影响[J]. 高压物理学报, 2021, 35(6): 064104. doi: 10.11858/gywlxb.20210762
引用本文: 张昭, 郭保桥, 冉春, 陈稳, 陈鹏万. 固溶温度对TB6钛合金动态力学性能和微观组织的影响[J]. 高压物理学报, 2021, 35(6): 064104. doi: 10.11858/gywlxb.20210762
ZHANG Zhao, GUO Baoqiao, RAN Chun, CHEN Wen, CHEN Pengwan. Effect of Solution Temperature on Dynamic Mechanical Properties and Microstructure of TB6 Titanium Alloy[J]. Chinese Journal of High Pressure Physics, 2021, 35(6): 064104. doi: 10.11858/gywlxb.20210762
Citation: ZHANG Zhao, GUO Baoqiao, RAN Chun, CHEN Wen, CHEN Pengwan. Effect of Solution Temperature on Dynamic Mechanical Properties and Microstructure of TB6 Titanium Alloy[J]. Chinese Journal of High Pressure Physics, 2021, 35(6): 064104. doi: 10.11858/gywlxb.20210762

固溶温度对TB6钛合金动态力学性能和微观组织的影响

doi: 10.11858/gywlxb.20210762
基金项目: 国家自然科学基金(12072038)
详细信息
    作者简介:

    张 昭(1977-),男,硕士研究生,主要从事钛合金动态力学行为研究. E-mail:bitzhangzhao@163.com

    通讯作者:

    郭保桥(1976-),男,博士,副教授,主要从事实验力学、冲击动力学研究. E-mail:baoqiao_guo@bit.edu.cn

  • 中图分类号: O347.3

Effect of Solution Temperature on Dynamic Mechanical Properties and Microstructure of TB6 Titanium Alloy

  • 摘要: 研究了固溶温度对近β相TB6钛合金动态力学性能和微观组织的影响。以分离式霍普金森压杆为加载手段,对固溶处理前后的TB6钛合金进行了动态压缩试验。结果表明:固溶处理前后TB6钛合金都具有应变率强化效应,压缩破坏形式为典型的剪切破坏;TB6钛合金由应变硬化效应转变为应变软化效应的固溶温度为700~750 ℃。光学显微镜观测、X射线衍射和扫描电镜表征结果表明:700 ℃固溶处理后,TB6钛合金中的初生α相部分溶解,强度下降;750 ℃及以上固溶处理后,初生α相全部转化为β相,β晶粒长大,强度提升,但塑性显著降低。

     

  • 图  固溶处理工艺流程

    Figure  1.  Flow chart of solution process

    图  SHPB压杆装置示意图

    Figure  2.  Schematic of a SHPB set-up

    图  动态压缩试样宏观形貌

    Figure  3.  Typical macro-morphologies after dynamic compression

    图  不同应变率下的真应力-真应变曲线(固溶温度为700 ℃)

    Figure  4.  True stress versus true strain at different strain rates (at 700 ℃ solution)

    图  不同处理后的试样第一次剪切破环时的真应力-塑性应变曲线

    Figure  5.  True stress versus plastic strain for the first shear fracture of the specimens treated at different temperatures

    图  不同固溶温度处理后试样的屈服应力-应变率曲线

    Figure  6.  Yield stress versus strain rate of specimens treated at different solution temperatures

    图  1100 s−1时不同固溶温度处理后的真应力-真应变曲线

    Figure  7.  True stress versus true strain of specimens treated at different temperatures loading at 1100 s−1 strain rate

    图  不同固溶温度条件下材料的显微组织

    Figure  8.  Microstructures of specimens treated at different solution temperatures

    图  不同固溶温度条件下试样的XRD谱

    Figure  9.  XRD patterns of specimens treated at different solution temperatures

    图  10  不同温度固溶处理后试样的断面形貌

    Figure  10.  Cross-section morphologies of specimens treated at different solution temperatures

    表  1  TB6钛合金的化学成分(质量分数)[19]

    Table  1.   Chemical compositions of TB6 alloy (mass fraction)[19] % 

    HONFeAlVTi
    0.010.030.031.932.9310.13Rest
    下载: 导出CSV

    表  2  试样第一次破坏时的力学性能指标

    Table  2.   Mechanical performance of specimens for the first shear fracture

    Temperature/℃Maximum plastic strain Yield stress
    Value Ratio/% Value/MPa Ratio/%
    Untreated0.18171115
    7000.1660 −8.641010−9.42
    7500.0621−65.82127514.35
    8000.0254−86.02132318.65
    下载: 导出CSV
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  • 收稿日期:  2021-03-30
  • 修回日期:  2021-04-09

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