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Fretting fatigue of AISI 9310 case-hardened steel.

机译:AISI 9310表面硬化钢的微动疲劳。

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This document details the fretting fatigue of AISI 9310 case-hardened steel. The research involved two main parts: experiments were performed in order to determine the fretting fatigue life of the material under certain operating conditions, and semi- analytical methods were used to determine contact stresses and crack growth during the experiments. Fractographic analyses were performed in support of this research to observe characteristics of the fretting process. The results from the experiments and subsequent analysis were compared with failure characteristics observed in gears made of the same material in an effort to identify similarities present.;Twelve fretting fatigue experiments were performed at room temperature with case hardened steel specimens and pads. These twelve experiments are divided into two sets, one in which a re-cast layer was present on the pads and one in which there was no re-cast layer.;Post-experimental fractography of the specimen and pad allowed for study of the contacting surfaces and resultant crack formation. Of the twelve experiments, four interrupted tests were performed to determine crack growth behavior, five tests to failure were performed to determine life, and three tests were performed to determine the coefficient of friction due to the contact during the other nine experiments. Of the tests to failure, the tests with re-cast layer removed from the pads failed in fewer cycles than the tests with the re-cast layer present.;The contact tractions and stresses for the experiments were obtained using computer code that utilizes Singular Integral Equations and FFT, which is well suited for the problem provided certain assumptions. The results from the SIE calculations compare well with FEM analyses. The Paris model was used to predict crack growth and experiment life, and the results were compared with the experiments. The modeled remaining life compared well when the experiment was stopped after the fretting cracks had formed into one crack, but the model underestimated the expected life when the experiment was stopped while multiple separate fretting cracks were present.
机译:该文档详细介绍了AISI 9310表面硬化钢的微动疲劳。该研究涉及两个主要部分:进行实验以确定材料在特定操作条件下的微动疲劳寿命,并使用半分析方法确定实验过程中的接触应力和裂纹扩展。分形分析进行了支持这项研究,以观察微动过程的特征。将实验结果和随后的分析结果与相同材料制成的齿轮中观察到的破坏特性进行比较,以找出存在的相似之处。在室温下对表面硬化的钢试样和垫块进行了十二次微动疲劳实验。这十二个实验分为两组,一组在焊盘上存在重铸层,而另一组不存在重铸层。试样和焊盘的实验后分形法用于研究接触表面和形成的裂纹。在这十二个实验中,执行了四个中断测试以确定裂纹扩展行为,执行了五个破坏测试以确定寿命,并执行了三个测试以确定在其他九个实验期间由于接触而产生的摩擦系数。在失败测试中,从焊盘上去除重铸层的测试比在有重铸层的测试中以更少的周期失败。;使用奇异积分的计算机代码获得了实验的接触牵引力和应力方程和FFT非常适合该问题,提供了某些假设。 SIE计算的结果与FEM分析相比较很好。使用巴黎模型预测裂纹扩展和实验寿命,并将结果与​​实验进行比较。当微动裂纹形成一个裂纹后停止实验时,该模型的剩余寿命进行了比较,但是当存在多个单独的微动裂纹时,该模型低估了实验停止时的预期寿命。

著录项

  • 作者

    Robinson, Lucas A. K.;

  • 作者单位

    Purdue University.;

  • 授予单位 Purdue University.;
  • 学科 Engineering Aerospace.
  • 学位 M.S.A.A.
  • 年度 2010
  • 页码 79 p.
  • 总页数 79
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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