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首页> 外文期刊>International journal of impact engineering >Dynamic response and failure mechanism of Ti-6AL-4V hi-lock bolts under combined tensile-shear loading
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Dynamic response and failure mechanism of Ti-6AL-4V hi-lock bolts under combined tensile-shear loading

机译:Ti-6AL-4V高强度锁紧螺栓在组合剪切载荷作用下的动力响应及破坏机理

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摘要

This paper is focused on the dynamic mechanical behavior and failure characteristics of Ti-6AL-4V hi-lock bolt (HLB) under combined tensile-shear loading. Firstly, the dynamic mechanical properties of Ti-6AL-4V alloy under the quasi-static, intermediate strain rate and high strain rate are investigated by using an electronic universal testing machine, a high velocity hydraulic servo-testing machine and Split Hopkinson Pressure Bar (SHPB). A Johnson-Cook model is established to describe the dynamic constitutive relationship of Ti-6AL-4V alloy on the basis of the experimental results. A novel experimental fixture and a new collision-type loading method are proposed to investigate the dynamic failure characteristics of HLB. The dynamic pure tensile, 30 degrees tensile-shear coupling, 45 degrees tensile-shear coupling, 60 degrees tensile-shear coupling, pure shear experiments of HLB are conducted at the velocities of 0.01 m/s, 0.1 m/s and 1 m/s, respectively. Furthermore, a finite element model is established to validate the experimental results, and good agreement is obtained between the experimental and the simulation results. The experimental results show that the failure mode and the failure load of the HLB are greatly affected by the loading condition but less by the loading speed.
机译:本文主要研究Ti-6AL-4V锁紧螺栓(HLB)在组合拉伸剪切载荷下的动态力学行为和破坏特性。首先,使用电子万能试验机,高速液压伺服试验机和斯普利特霍普金森压力棒(Tiping AL-6V)研究了Ti-6AL-4V合金在准静态,中等应变率和高应变率下的动态力学性能。 SHPB)。建立了Johnson-Cook模型,根据实验结果描述了Ti-6AL-4V合金的动态本构关系。提出了一种新型的实验夹具和一种新的碰撞式加载方法来研究HLB的动态失效特性。在0.01 m / s,0.1 m / s和1 m / s的速度下进行了HLB的动态纯拉伸,30度拉伸-剪切耦合,45度拉伸-剪切耦合,60度拉伸-剪切耦合,纯剪切实验。分别。此外,建立了一个有限元模型来验证实验结果,并且在实验和仿真结果之间取得了良好的一致性。实验结果表明,HLB的失效模式和失效载荷受载荷条件的影响较大,而载荷速度的影响较小。

著录项

  • 来源
    《International journal of impact engineering 》 |2019年第9期| 140-151| 共12页
  • 作者单位

    Aircraft Strength Res Inst China, Aviat Key Lab Sci & Technol Struct Impact Dynam, Xian 710065, Shaanxi, Peoples R China;

    Aircraft Strength Res Inst China, Aviat Key Lab Sci & Technol Struct Impact Dynam, Xian 710065, Shaanxi, Peoples R China;

    Aircraft Strength Res Inst China, Aviat Key Lab Sci & Technol Struct Impact Dynam, Xian 710065, Shaanxi, Peoples R China;

    Beihang Univ, Inst Solid Mech, Beijing 100191, Peoples R China;

    Beihang Univ, Inst Solid Mech, Beijing 100191, Peoples R China|Univ Manchester, Sch Mech Aerosp & Civil Engn, Manchester M13 9PL, Lancs, England;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    High-lock bolts; Combined tensile-shear loading; Dynamic test; Failure mode;

    机译:高锁紧螺栓;组合拉伸剪切载荷;动态测试;故障模式;

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