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高应变率载荷下纯钛的非连续冲击疲劳失效模型及其微观机理

惠煜中 徐浩嘉 郝宏炜 沈将华

爆炸与冲击2024,Vol.44Issue(1):77-85,9.
爆炸与冲击2024,Vol.44Issue(1):77-85,9.DOI:10.11883/bzycj-2023-0073

高应变率载荷下纯钛的非连续冲击疲劳失效模型及其微观机理

Discontinuous impact fatigue failure model and microscopic mechanism of pure titanium under high strain-rate loading

惠煜中 1徐浩嘉 1郝宏炜 1沈将华2

作者信息

  • 1. 西北工业大学航空学院,陕西西安 710072
  • 2. 西北工业大学航空学院,陕西西安 710072||陕西省冲击动力学及工程应用重点实验室,陕西西安 710072
  • 折叠

摘要

Abstract

The fatigue failure behavior of structural materials under repeated impact loads has always attracted much attention.Mastering its damage accumulation process and evolution mechanism at the micro-scale is the fundamental way to understand the impact fatigue failure mechanism.Due to the complexity of the impact fatigue load itself and the limitations of the current experimental equipment,there are still major problems in the study of impact fatigue failure of materials.Therefore,pure titanium was used as the research object and a strain-controlled impact fatigue life test was designed based on the traditional split Hopkinson tension bar system.The strain-controlled impact fatigue life test was achieved by changing the length of the striker,and the amplitude of the incident wave needed to be kept at the same level when using different striker tests.The relationship between strain amplitude and impact fatigue life was analyzed.The impact fatigue interruption experiments of 5 times,10 times and 20 times were carried out with 100 mm bullets.The microstructure of the samples after different impact times were characterized by electron backscatter diffraction(EBSD)and then the quasi-static mechanical properties were tested.The fracture morphology after impact fatigue failure was observed by scanning electron microscope(SEM).The cyclic hardening/softening law and its microscopic evolution mechanism of pure titanium during impact fatigue failure were studied.The results show that the strain-controlled impact fatigue life test can be realized by changing the striker length.The Manson-Coffin fatigue life model can better reflect the relationship between impact fatigue life and strain amplitude of pure titanium.Moreover,pure titanium exhibits cyclic hardening during impact fatigue failure,which is mainly due to the combined effect of fine grain strengthening caused by twin deformation and strain hardening caused by plastic deformation during fatigue.Finally,the impact fatigue damage of pure titanium is mainly manifested as the loss of deformation ability.

关键词

冲击疲劳/纯钦/Manson-Coffin模型/微观组织

Key words

impact fatigue/pure titanium/Manson-Coffin model/microstructure

分类

数理科学

引用本文复制引用

惠煜中,徐浩嘉,郝宏炜,沈将华..高应变率载荷下纯钛的非连续冲击疲劳失效模型及其微观机理[J].爆炸与冲击,2024,44(1):77-85,9.

基金项目

国家自然科学基金(11802247) (11802247)

爆炸与冲击

OA北大核心CSTPCD

1001-1455

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