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Study on the accumulative fatigue damage rules under multiaxial two-stage step spectra constructed by loadings with similar lives

机译:相似寿命载荷在多轴两步阶跃谱下的累积疲劳损伤规律研究

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摘要

In this paper, the influence on the multiaxial fatigue damage accumulation caused by loading path variation was studied. For 2024-T4 aluminium alloy, the damage evolution during the entire life was first observed. On the basis of the observation, the stage Ⅰ of fatigue damage evolution was further divided into two sub-stages, and the dominant stress parameters of these two sub-stages were proposed. Taking the dominant stress parameters into account, a phased accumulative fatigue damage model was proposed. Then, 12 multiaxial two-stage step spectra constructed by loadings with approximately identical fatigue lives were carried out on 2024-T4 aluminium alloy. The accumulative fatigue damage was calculated by the proposed model, and another five commonly used models and the calculated results were compared. According to the comparison, the newly proposed model had the most accurate results with the smallest scatter.
机译:本文研究了载荷路径变化对多轴疲劳损伤累积的影响。对于2024-T4铝合金,首先观察到其在整个寿命中的损伤演变。在观察的基础上,将疲劳损伤演化的第一阶段进一步分为两个子阶段,并提出了这两个子阶段的主应力参数。考虑到主要应力参数,提出了阶段性累积疲劳损伤模型。然后,在2024-T4铝合金上进行了十二次多轴两步阶跃谱分析,这些谱图由具有近似相同疲劳寿命的载荷构成。利用该模型计算了累积疲劳损伤,并与另外五个常用模型进行了比较。根据比较,新提出的模型具有最准确的结果,且散布最小。

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  • 作者单位

    Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

    State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

    Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

    Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

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  • 正文语种 eng
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  • 关键词

    2024-T4 aluminium alloy; accumulative damage rule; damage evolution; multiaxial fatigue; two-stage step spectrum;

    机译:2024-T4铝合金;累积损害规则;损害演变;多轴疲劳两阶段谱;

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