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Analysis of a pulsating fatigue process on carbon steel with different carbide shapes

机译:不同碳化物形状的碳钢的脉动疲劳过程分析

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摘要

In the pulsating fatigue process, the relationship between cyclic softening (hardening) and ratcheting should be clarified from the perspective of the practical use of the mechanical parts. However, most previous reports have been limited to predicting of ratcheting curves using constitutive equations. Consequently, there are few qualitative discussions regarding the relationship between cyclic softening (hardening) and ratcheting for changes in the number of cycles. In this study, the plastic strain amplitude, which represents the fatigue damage, is plotted on the X axis and the ratcheting strain rate is plotted on the Y axis, cycle by cycle, to investigate the fatigue and ratcheting damage simultaneously. This figure is known as the SH curve after Dr. Susumu Horibe. As an example, the pulsating fatigue processes of JIS S25C (AISI 1025) with three different carbide shape types are analyzed under the conditions that the engineering stress amplitudes are over their lower yield points. Using SH curves it is shown that regardless of the shape of the carbide, the fatigue behavior should be divided into five stages. Stage 1 corresponds to the un-pinning of dislocations from the Cottrell atmosphere. Stage II corresponds to the propagation of the Luders band. Stage III corresponds to an increase in short range dislocation movement during the formation of cellular structures due to multiple slip locations. Stage IV corresponds to the fracture of the cellular structure due to an increase in the true stress. Stage V corresponds to crack initiation and propagation. The plastic strain amplitude increases with the number of cycles, while the ratcheting strain rate decreases, especially in stage III; this phenomenon has never been reported previously. At this stage, the microstructure was observed by TEM. It is also determined that in this case, the maximum stress is over the lower yield point, and the ratcheting strain rate is dominant over the fatigue life.
机译:在脉动疲劳过程中,应从机械零件的实际使用角度阐明循环软化(硬化)与棘轮之间的关系。但是,大多数以前的报告仅限于使用本构方程预测棘轮曲线。因此,很少有关于循环软化(硬化)和棘轮变化之间的关系的定性讨论。在这项研究中,代表疲劳损伤的塑性应变幅度绘制在X轴上,棘轮应变率绘制在Y轴上,逐周期绘制,以同时研究疲劳和棘轮损伤。此图在Susumu Horibe博士之后被称为SH曲线。例如,在工程应力振幅超过其较低屈服点的条件下,分析了具有三种不同碳化物形状类型的JIS S25C(AISI 1025)的脉动疲劳过程。使用SH曲线表明,不管碳化物的形状如何,疲劳行为都应分为五个阶段。第1阶段对应于解除Cottrell大气中的位错。第二阶段对应于Luders频带的传播。阶段III对应于由于多个滑动位置而在细胞结构形成期间短程位错运动的增加。 IV期对应于由于真实应力的增加而引起的细胞结构的破裂。第五阶段对应于裂纹的萌生和扩展。塑性应变幅度随着循环次数的增加而增加,而棘轮应变率降低,特别是在阶段III中。这种现象以前从未报道过。在这一阶段,通过TEM观察了微观结构。还确定在这种情况下,最大应力在较低的屈服点以上,并且棘轮应变率在疲劳寿命中占主导地位。

著录项

  • 来源
    《Materials Science and Engineering》 |2014年第10期|218-223|共6页
  • 作者单位

    Department of Modern Mechanical Engineering, Graduate School of Waseda University, 3-4-1 Shinjyuku-ku Okubo, Tokyo 169-8555, Japan;

    Department of Modern Mechanical Engineering, Graduate School of Waseda University, 3-4-1 Shinjyuku-ku Okubo, Tokyo 169-8555, Japan,Japan Society for the Promotion of Science, 5-3-1, Chiyoda-ku Kojimachi, Tokyo 102-0083, Japan,Japan Aerospace Exploration Agency, 3-1-1, Cyuou-ku Yoshinodai, Sagamihara, Kanagawa 252-5210, Japan;

    Department of Modern Mechanical Engineering, Graduate School of Waseda University, 3-4-1 Shinjyuku-ku Okubo, Tokyo 169-8555, Japan,Kagami Memorial Research Institute for Materials Science and Technology, Waseda University, 2-8-26, Nishi-Waseda, Shinjyuku-ku, Tokyo 169-0051, Japan;

    Department of Modern Mechanical Engineering, Graduate School of Waseda University, 3-4-1 Shinjyuku-ku Okubo, Tokyo 169-8555, Japan;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Fatigue; Plastic strain amplitude; Ratcheting strain rate; Carbon steel;

    机译:疲劳;塑性应变幅度;棘轮应变率;碳素钢;

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