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Constitutive modeling and life prediction in nickel-base superalloys.

机译:镍基高温合金的本构模型和寿命预测。

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摘要

Microstructural features at different scales affect the constitutive stress-strain response and the fatigue crack initiation life in Ni-base superalloys. While numerous efforts have been made in the past to experimentally characterize the effects of these features on the stress-strain response and/or the crack initiation life, there is a significant variability in the data with sometimes contradictory conclusions, in addition to the substantial costs involved in experimental testing. Computational techniques can be useful tools to better understand these effects since they are relatively inexpensive and are not restricted by the limitations in processing techniques. This research investigated the microstructure-dependence of the stress-strain response and the fatigue crack initiation life of two Ni-base superalloys; DS GTD111, which has been developed by GE Energy for use in gas turbine blades, and IN100, developed by Pratt and Whitney, which is used in turbine discs. The focus was on developing multiscale constitutive models and computational frameworks for life prediction.; Physically-based constitutive models were formulated and implemented as user material subroutines in ABAQUS using the single crystal plasticity framework which can predict the material stress-strain response with the microstructure-dependence embedded into them. The model parameters were calibrated using experimental cyclic stress-strain histories. A computational exercise was then employed to quantify the influence of idealized microstructural variables on fatigue crack initiation life. Understanding was sought on the influence of inclusion shape, size, and spacing and the primary and neighboring grain orientations on the variability in fatigue crack incubation life in DS GTD111. A computational scheme was also formulated to predict the fatigue crack initiation life in IN100 for slip band based crack initiation and a material design framework was developed and used for the preliminary design of fatigue resistant microstructures. Lastly, it is noted that crystal plasticity models are often too computationally intensive if the objective is to model the macroscopic behavior of a textured or randomly oriented 3-D polycrystal in an engineering component. Homogenized constitutive models were formulated and implemented as user material subroutines in ABAQUS, which can capture the macroscale stress-strain response in both DS GTD111 and IN100. Even though the study was conducted on two specific Ni-base superalloys; DS GTD111 and IN100, the objective was to develop generic frameworks which should also be applicable to other alloy systems.
机译:镍基高温合金中不同尺度的微结构特征会影响本构应力-应变响应和疲劳裂纹萌生寿命。过去,人们已经进行了大量的实验来表征这些特征对应力-应变响应和/或裂纹萌生寿命的影响,但数据的可变性却很大,有时还会得出相互矛盾的结论,此外还要付出大量的成本。参与实验测试。计算技术可能是有用的工具,可以更好地理解这些效果,因为它们相对便宜并且不受制程技术的限制。本研究研究了两种镍基高温合金的应力-应变响应和疲劳裂纹萌生寿命的微观结构依赖性。 DS GTD111是由GE Energy开发的,用于燃气涡轮叶片,而IN100是由Pratt和Whitney开发的,用于涡轮盘。重点是开发用于寿命预测的多尺度本构模型和计算框架。基于物理的本构模型在ABAQUS中使用单晶可塑性框架制定并实现为用户材料子例程,该模型可以预测材料的应力-应变响应,并嵌入其中的微观结构依赖性。使用实验循环应力-应变历史来校准模型参数。然后进行计算,以量化理想化的微结构变量对疲劳裂纹萌生寿命的影响。试图了解DS GTD111中夹杂物的形状,大小和间距以及主要晶粒和邻近晶粒的取向对疲劳裂纹保温寿命变化的影响。还制定了一种计算方案来预测IN100中基于滑带的裂纹萌生的疲劳裂纹萌生寿命,并开发了材料设计框架并将其用于耐疲劳微结构的初步设计。最后,要注意的是,如果目标是在工程组件中模拟织构化或随机取向的3-D多晶的宏观行为,则晶体可塑性模型的计算量通常过大。在ABAQUS中,将均质本构模型制定并实现为用户材料子例程,该子例程可以捕获DS GTD111和IN100中的宏观应力应变响应。即使研究是针对两种特定的镍基高温合金进行的; DS GTD111和IN100,目的是开发通用框架,该框架也应适用于其他合金系统。

著录项

  • 作者

    Shenoy, Mahesh M.;

  • 作者单位

    Georgia Institute of Technology.;

  • 授予单位 Georgia Institute of Technology.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2006
  • 页码 318 p.
  • 总页数 318
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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