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Zone-based reliability analysis on fatigue life of GH720Li turbine disk concerning uncertainty quantification

机译:基于不确定度量化的GH720Li涡轮盘疲劳寿命的基于区域可靠性分析

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摘要

Probabilistic-based design for turbine disk can quantify risk and thus improve the reliability of the component. This paper presents a zone-based reliability framework in combination with uncertainty quantification for low cycle fatigue (LCF) life prediction of a turbine disk. In this investigation, a zone based modeling methodology is proposed instead of the traditional hot spot method, which accounts for all of the potential regions influencing the turbine disk's failure probability. The LCF life reliability of the whole turbine disk is achieved by jointing failure probability at each zone. The reliability framework developed involves the uncertainties from physical inputs and model parameters, in which geometry and model parameters are quantified using statistical method and Bayesian inference respectively, while the discretization error induced by finite element analysis is corrected using Richardson extrapolation method. Finally, the reliability analysis on the LCF life of a GH720Li turbine disk is performed considering the uncertainty quantification. It is demonstrated that the proposed zone-based reliability method in this paper is more accurate compared with the traditional hot spot method. (C) 2017 Elsevier Masson SAS. All rights reserved.
机译:基于概率的涡轮盘设计可以量化风险,从而提高组件的可靠性。本文提出了一种基于区域的可靠性框架,并结合了不确定性量化来预测涡轮盘的低周疲劳(LCF)寿命。在这项研究中,提出了一种基于区域的建模方法,而不是传统的热点方法,该方法解决了影响涡轮盘故障概率的所有潜在区域。整个涡轮盘的LCF寿命可靠性是通过每个区域的接合失效概率来实现的。建立的可靠性框架涉及来自物理输入和模型参数的不确定性,其中几何和模型参数分别使用统计方法和贝叶斯推断进行量化,而有限元分析引起的离散化误差则使用Richardson外推法进行校正。最后,考虑了不确定性量化,对GH720Li涡轮盘的LCF寿命进行了可靠性分析。结果表明,与传统的热点算法相比,本文提出的基于区域的可靠性方法更加准确。 (C)2017 Elsevier Masson SAS。版权所有。

著录项

  • 来源
    《Aerospace science and technology》 |2017年第11期|300-309|共10页
  • 作者单位

    Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China|Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China|Beijing Key Lab Aeroengine Struct & Strength, Beijing 100191, Peoples R China;

    Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China;

    Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China|Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China|Beijing Key Lab Aeroengine Struct & Strength, Beijing 100191, Peoples R China;

    McGill Univ, Min & Mat Engn, Montreal, PQ H3A 0C5, Canada;

    Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China;

    Case Western Reserve Univ, Dept Mech & Aerospace Engn, Cleveland, OH 44106 USA;

  • 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

    Uncertainty quantification; Low cycle fatigue; Turbine disk; Reliability analysis; GH720Li superalloy;

    机译:不确定度量化低周疲劳涡轮盘可靠性分析GH720Li高温合金;

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