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Combined high and low cycle fatigue life prediction model based on damage mechanics and its application in determining the aluminized location of turbine blade

机译:基于损伤力学的高低周疲劳组合寿命预测模型及其在确定叶片渗铝位置中的应用

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摘要

A new combined high and low cycle fatigue (CCF) life prediction model based on the damage mechanics theory is proposed in this paper. The model parameters are fitted based on the material data and blade data respectively. Verification tests are carried out to evaluate predicted results in combination with the experimental data. Results illustrate that the new model based on the blade data can predict the blade life with relatively higher accuracy (within 2.2 times of scatter band), which is much better than that based on the material data (within 178.2 times of scatter band). Afterward, in comparison with typical existing models, the newly proposed model can predict the turbine blade life more accurately. What's more, based on the newly proposed model, a novel determination method for permitted aluminized location in the turbine blade is put forward. Then, combined with aluminized blade tests, correlated model parameters are determined and the permitted aluminized location distribution is given by using the novel method. The presented life model and the determination method may have a great value for potential engineering applications.
机译:提出了一种基于损伤力学理论的高,低周疲劳组合寿命预测模型。分别基于材料数据和叶片数据拟合模型参数。进行验证测试以结合实验数据评估预测结果。结果表明,基于叶片数据的新模型可以相对较高的精度(在散射带的2.2倍之内)预测叶片寿命,这比基于材料数据(在散射带的178.2倍之内)要好得多。之后,与典型的现有模型相比,新提出的模型可以更准确地预测涡轮叶片的寿命。此外,基于新提出的模型,提出了一种确定涡轮叶片中渗铝位置的新方法。然后,结合镀铝刀片测试,确定相关的模型参数,并使用新方法给出允许的镀铝位置分布。提出的寿命模型和确定方法可能对潜在的工程应用具有重要的价值。

著录项

  • 来源
    《International Journal of Fatigue》 |2019年第10期|120-130|共11页
  • 作者单位

    Beihang Univ, Sch Energy & Power Engn, 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|Natl Key Lab Sci & Technol Aeroengine Aerothermod, Beijing 100191, Peoples R China|Beijing Key Lab Aeroengine Struct & Strength, Beijing 100191, Peoples R China;

    AVIC CAPDI Integrat Equipment Co Ltd, Beijing 100120, Peoples R China;

    Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China|Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China|Natl Key Lab Sci & Technol Aeroengine Aerothermod, 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;

  • 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

    CCF test; Life prediction model; Damage mechanics; Nonlinear interaction; Aluminizing treatment;

    机译:CCF测试;寿命预测模型;损伤力学;非线性相互作用;铝化处理;

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