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Ti-6Al-4V ELI在变幅载荷下的循环变形和疲劳数据。

Cyclic deformation and fatigue data for Ti-6Al-4V ELI under variable amplitude loading.

作者信息

Carrion Patricio E, Shamsaei Nima, Moser Robert D

机构信息

Laboratory for Fatigue & Additive Manufacturing Excellence (FAME), Department of Mechanical Engineering, Auburn University, Auburn, AL 36849, USA.

US Army Engineer Research and Development Center, Vicksburg, MS 39180, USA.

出版信息

Data Brief. 2017 May 19;13:180-186. doi: 10.1016/j.dib.2017.05.032. eCollection 2017 Aug.

Abstract

This article presents the strain-based experimental data for Ti-6Al-4V ELI under non-constant amplitude cyclic loading. Uniaxial strain-controlled fatigue experiments were conducted under three different loading conditions, including two-level block loading (i.e. high-low and low-high), periodic overload, and variable amplitude loading. Tests were performed under fully-reversed, and mean strain/stress conditions. For each test conducted, two sets of data were collected; the cyclic stress-strain response (i.e. hysteresis loops) in log increments, and the peak and valley values of stress and strain for each cycle. Residual fatigue lives are reported for tests with two-level block loading, while for periodic overload and variable amplitude experiments, fatigue lives are reported in terms of number of blocks to failure.

摘要

本文展示了Ti-6Al-4V ELI在非等幅循环载荷下基于应变的实验数据。在三种不同加载条件下进行了单轴应变控制疲劳实验,包括两级块加载(即高-低和低-高)、周期性过载和变幅加载。测试在完全反向以及平均应变/应力条件下进行。对于所进行的每项测试,收集了两组数据;以对数增量表示的循环应力-应变响应(即滞后回线),以及每个循环的应力和应变的峰值和谷值。报告了两级块加载测试的剩余疲劳寿命,而对于周期性过载和变幅实验,疲劳寿命以失效时的块数表示。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b820/5458061/d0f71ed8dac8/gr1.jpg

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