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Application of continuum damage mechanics to vibration fatigue life prediction

机译:连续损伤力学在振动疲劳寿命预测中的应用

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摘要

It is pivotal to predict the multiaxial vibration fatigue life during mechanical structural dynamics design. An algorithm of the finite element method implementation for multiaxial high cycle fatigue life evaluation is proposed, on the basis of elastic evolution model of continuum damage mechanics. By considering structural dynamic characteristics, namely, resonant frequencies and mode shapes, this algorithm includes a modal analysis and harmonic analysis, which makes this different from existing fatigue life prediction methods. A 10% decrease in the resonant frequency is regarded as the failure criterion. A critical damage value was obtained, which indicates mesocrack initiation fulfilment. To validate the effectiveness of the algorithm, auto-phase sine resonance track-and-dwell experiments were conducted on notched cantilever beams made of Ti-6A1-4V alloy. The life predictions are conservative and in good agreements with the experimental results, which are mainly distributed within a scatter band of 2. This investigation could provide technical support for structural dynamics design and the analysis of reusable spacecraft.
机译:预测机械结构动力学设计过程中的多轴振动疲劳寿命至关重要。在连续损伤力学的弹性演化模型的基础上,提出了一种用于多轴高周疲劳寿命评估的有限元算法实现算法。通过考虑结构动力学特性,即共振频率和模态形状,该算法包括模态分析和谐波分析,这使其不同于现有的疲劳寿命预测方法。谐振频率降低10%被视为失效标准。获得了临界损伤值,其表明中裂纹起始完成。为了验证该算法的有效性,在由Ti-6A1-4V合金制成的缺口悬臂梁上进行了自动相位正弦共振跟踪和驻留实验。寿命预测是保守的,并且与实验结果吻合良好,实验结果主要分布在2的分散带内。该研究可以为结构动力学设计和可重复使用航天器的分析提供技术支持。

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  • 作者单位

    Structural Dynamics Laboratory of Aerospace Propulsion, School of Astronautics, Beihang University, Beijing, China;

    Structural Dynamics Laboratory of Aerospace Propulsion, School of Astronautics, Beihang University, Beijing, China;

    Structural Dynamics Laboratory of Aerospace Propulsion, School of Astronautics, Beihang University, Beijing, China;

    Structural Dynamics Laboratory of Aerospace Propulsion, School of Astronautics, Beihang University, Beijing, China;

    Structural Dynamics Laboratory of Aerospace Propulsion, School of Astronautics, Beihang University, Beijing, China;

    Structural Dynamics Laboratory of Aerospace Propulsion, School of Astronautics, Beihang University, Beijing, China;

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

    auto-phase SRTD vibration; continuum damage mechanics; vibration fatigue;

    机译:自相SRTD振动;连续损伤力学;振动疲劳;

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