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Experimental investigation of grain size effect on fatigue crack growth rate in turbine disc superalloy GH4169 under different temperatures

机译:GH4169涡轮盘合金在不同温度下晶粒尺寸对疲劳裂纹扩展速率影响的实验研究

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摘要

Systematic experiments for fatigue crack growth (FCG) rate on compact tension (CT) specimens have been conducted in nickel-based superalloy GH4169 at a broad range of temperatures with a frequency of 10 Hz and a stress ratio of 0.1. In order to investigate the crack closure behavior, FCG experiments at stress ratio of 0.5 were also performed by comparing with the results at stress ration of 0.1. CT specimens were cut from three typical locations of an actual forged turbine disc to investigate the effect of grain size on the FCG behaviors. The grain size distribution, precipitates and fracture surface characteristics at different locations of the turbine disc were examined through optical microscope, transmission electron microscope (TEM) and scanning electronic microscope (SEM) analyses. Digital image correlation (DIC), optical interferometry and oxide film measurements were carried out to investigate the presence and inducement of the crack closure. Then a modified FCG model, with a distribution factor that evaluates the scattering in the FCG rate, was formulated to describe the dependence of FCG rate on grain size. Finally, the possible microscopic mechanisms to explain the grain size effect on the FCG behaviors based on crack deflection and blockage, and the crack closure inducements involving plasticity and oxide were discussed in this study.
机译:已经在频率为10 Hz且应力比为0.1的宽温度范围内的镍基高温合金GH4169中进行了紧凑张力(CT)样品上疲劳裂纹扩展(FCG)速率的系统实验。为了研究裂纹闭合行为,通过与应力比为0.1的结果进行比较,还进行了应力比为0.5的FCG实验。从实际的锻造涡轮盘的三个典型位置切割出CT标本,以研究晶粒尺寸对FCG行为的影响。通过光学显微镜,透射电子显微镜(TEM)和扫描电子显微镜(SEM)分析检查了涡轮盘不同位置的晶粒尺寸分布,析出物和断裂表面特性。进行了数字图像相关性(DIC),光学干涉测量和氧化膜测量,以研究裂纹闭合的存在和诱因。然后,建立了一个修正的FCG模型,该模型具有评估FCG速率中的散射的分布因子,以描述FCG速率对晶粒尺寸的依赖性。最后,本研究探讨了可能的微观机理,以解释晶粒尺寸对基于裂纹偏转和阻塞的FCG行为的影响,以及涉及塑性和氧化物的裂纹闭合诱发因素。

著录项

  • 来源
    《Materials Science and Engineering》 |2016年第4期|318-331|共14页
  • 作者单位

    School of Energy and Power Engineering, Beihang University, Beijing 100191, China ,Collaborative Innovation Center of Advanced Aero-Engine, Beijing 100191, China ,Beijing Key Laboratory of Aero-Engine Structure and Strength, Beijing 100191, China;

    School of Energy and Power Engineering, Beihang University, Beijing 100191, China;

    Mining and Materials Engineering, McGill University, Montreal QC, Canada H3A 0C5;

    Mining and Materials Engineering, McGill University, Montreal QC, Canada H3A 0C5;

    China Aviation Powerplant Research Institute, Zhuzhou 412002, China;

    School of Energy and Power Engineering, Beihang University, Beijing 100191, China ,Collaborative Innovation Center of Advanced Aero-Engine, Beijing 100191, China ,Beijing Key Laboratory of Aero-Engine Structure and Strength, Beijing 100191, China;

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

    Experimental investigation; Fatigue crack growth rate; Grain size; Crack closure inducement;

    机译:实验研究;疲劳裂纹增长率晶粒大小;裂纹闭合诱发;

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