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The Relationships Between Microstructure, Tensile Properties and Fatigue Life in Ti-5Al-5V-5Mo-3Cr-0.4Fe (Ti-5553).

机译:Ti-5Al-5V-5Mo-3Cr-0.4Fe(Ti-5553)的组织,拉伸性能与疲劳寿命之间的关系。

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摘要

beta-titanium alloys are being increasingly used in airframes as a way to decrease the weight of the aircraft. As a result of this movement, Ti-5Al-5V-5Mo-3Cr-0.4Fe (Timetal 555), a high-strength beta titanium alloy, is being used on the current generation of landing gear. This alloy features good combinations of strength, ductility, toughness and fatigue life in alpha+beta processed conditions, but little is known about beta-processed conditions. Recent work by the Center for the Accelerated Maturation of Materials (CAMM) research group at The Ohio State University has improved the tensile property knowledge base for beta-processed conditions in this alloy, and this thesis augments the aforementioned development with description of how microstructure affects fatigue life.;In this work, beta-processed microstructures have been produced in a Gleeble(TM) thermomechanical simulator and subsequently characterized with a combination of electron and optical microscopy techniques. Four-point bending fatigue tests have been carried out on the material to characterize fatigue life. All the microstructural conditions have been fatigue tested with the maximum test stress equal to 90% of the measured yield strength. The subsequent results from tensile tests, fatigue tests, and microstructural quantification have been analyzed using Bayesian neural networks in an attempt to predict fatigue life using microstructural and tensile inputs. Good correlation has been developed between lifetime predictions and experimental results using microstructure and tensile inputs. Trained Bayesian neural networks have also been used in a predictive fashion to explore functional dependencies between these inputs and fatigue life.;In this work, one section discusses the thermal treatments that led to the observed microstructures, and the possible sequence of precipitation that led to these microstructures. The thesis then describes the implications of microstructure on fatigue life and implications of tensile properties on fatigue life. Several additional experiments are then described that highlight possible causes for the observed dependence of microstructure on fatigue life, including fractographic evidence to provide support of microstructural dependencies.
机译:β-钛合金正越来越多地用于机身,以减轻飞机的重量。由于这种运动,目前的起落架使用了高强度β钛合金Ti-5Al-5V-5Mo-3Cr-0.4Fe(时针555)。这种合金在α+β加工条件下具有强度,延展性,韧性和疲劳寿命的良好组合,但对β加工条件知之甚少。俄亥俄州立大学材料加速成熟中心(CAMM)研究小组的最新工作改进了该合金在β处理条件下的拉伸性能知识库,并且本文通过描述微观结构如何影响来扩大上述进展。疲劳寿命。;在这项工作中,已在Gleeble(TM)热机械模拟器中制作了经过β处理的微结构,随后将其与电子和光学显微镜技术相结合进行了表征。已经对材料进行了四点弯曲疲劳测试,以表征疲劳寿命。所有的微观结构条件都经过了疲劳测试,最大测试应力等于测得的屈服强度的90%。使用贝叶斯神经网络分析了拉伸测试,疲劳测试和微观结构量化的后续结果,试图通过微观结构和拉伸输入来预测疲劳寿命。使用微观结构和拉伸输入,已经在寿命预测和实验结果之间建立了良好的相关性。经过训练的贝叶斯神经网络也已经以预测的方式用于探索这些输入和疲劳寿命之间的功能依赖性。在这项工作中,一节讨论了导致观察到的微观结构的热处理,以及导致出现沉淀的可能顺序。这些微结构。然后论文描述了微观结构对疲劳寿命的影响以及拉伸性能对疲劳寿命的影响。然后描述了几个其他的实验,这些实验突出了观察到的微观结构对疲劳寿命的依赖性的可能原因,包括提供微观结构依赖性的分形学证据。

著录项

  • 作者

    Foltz, John W., IV.;

  • 作者单位

    The Ohio State University.;

  • 授予单位 The Ohio State University.;
  • 学科 Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 2010
  • 页码 303 p.
  • 总页数 303
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:37:26

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