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首页> 外文期刊>International Journal of Fatigue >High cycle fatigue characterization of a nickel-based superalloy based on a novel temperature-dependent regression method
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High cycle fatigue characterization of a nickel-based superalloy based on a novel temperature-dependent regression method

机译:基于新型温度依赖性回归法的镍基超合金高周疲劳表征

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摘要

High cycle fatigue (HCF) at elevated temperatures is a very significant issue for superalloys commonly used in the field of gas turbine engines. However, nearly all the existing HCF S-N regression models are established irrespective of the temperature factor, which leads to the inconvenience of their application in multi-temperature HCF issues of superalloys. This paper proposes a HCF characterization method based on a novel regression model for the testing data at multiple temperatures. With the model, the HCF failure cycles can be obtained by a continuous function of the fatigue stress levels and temperatures. In order to verify the present method, a series of complete HCF tests for a nickel-based superalloy GH4169 within its typical service temperature range are conducted and numerous S-N data at various temperatures are obtained. The regression calculation and some prediction based on the present model are then carried out. It has been demonstrated that the present temperature-dependent regression method is well suitable for characterizing the HCF properties at elevated temperatures range. Based on the present method, the accuracy of HCF strength evaluation is really good. Especially, lifetime prediction by the present model is satisfied since that nearly all the data points comparing the prediction with the testing data fall within the scatter band with the error factor of three.
机译:升高温度下的高循环疲劳(HCF)是燃气涡轮发动机领域通常用于常用的超合金的非常重要的问题。然而,几乎所有现有的HCF S-N回归模型都是不论温度因数如何建立,这导致它们在高温合金的多温HCF问题中的应用不便。本文提出了一种基于多温度测试数据的新型回归模型的HCF表征方法。利用该模型,通过疲劳应力水平和温度的连续函数可以获得HCF故障循环。为了验证本方法,在其典型的维修温度范围内的基于镍的超金属GH4169的一系列完整的HCF测试,并获得各种温度的许多S-N数据。然后执行基于本模型的回归计算和一些预测。已经证明,本温度依赖性回归方法很好,适用于在升高的温度范围内表征HCF性能。基于本方法,HCF强度评价的准确性非常好。特别地,满足本模型的寿命预测,因为与测试数据的比较预测几乎所有数据点都落在散射带内,误差因子为三。

著录项

  • 来源
    《International Journal of Fatigue 》 |2021年第1期| 105960.1-105960.13| 共13页
  • 作者单位

    Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation AECC Key Laboratory of Science Technology on Aeronautical Materials Testing and Evaluation Beijing Institute of Aeronautical Materials Beijing 100095 China;

    Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation AECC Key Laboratory of Science Technology on Aeronautical Materials Testing and Evaluation Beijing Institute of Aeronautical Materials Beijing 100095 China;

    Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation AECC Key Laboratory of Science Technology on Aeronautical Materials Testing and Evaluation Beijing Institute of Aeronautical Materials Beijing 100095 China;

    Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation AECC Key Laboratory of Science Technology on Aeronautical Materials Testing and Evaluation Beijing Institute of Aeronautical Materials Beijing 100095 China;

    Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation AECC Key Laboratory of Science Technology on Aeronautical Materials Testing and Evaluation Beijing Institute of Aeronautical Materials Beijing 100095 China;

    Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation AECC Key Laboratory of Science Technology on Aeronautical Materials Testing and Evaluation Beijing Institute of Aeronautical Materials Beijing 100095 China;

  • 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 cycle fatigue; Regression method; Nickel-based superalloy; Elevated temperature;

    机译:高周疲劳;回归方法;基于镍的超合金;高温;

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