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Development of a processing-structure-fatigue property model for single crystal superalloys.

机译:单晶高温合金加工结构疲劳性能模型的建立。

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摘要

Single crystal nickel-base superalloys have emerged as the materials of choice for high-temperature applications when significant resistance to fatigue loading is required. Although the fatigue life improvements due to a direct material substitution may be possible, additional gains are possible through advanced casting techniques in comparison to typical production processes. However, before integration in the manufacturing sector, optimization of a higher thermal gradient process for producing refined, homogeneous, single crystal components with improved fatigue properties is imperative.;In this dissertation, a higher cooling efficiency process, specifically, liquid-metal cooling (LMC) using Sn as the cooling medium, has been evaluated for potential fatigue property benefits of single crystal superalloy airfoil-sized components. A series of casting experiments were conducted using conventional radiation cooled Bridgman casting and the LMC process to compare the refinement in dendritic spacings and defect size distribution for 1.6 cm diameter rods. Casting conditions were selected to observe the trend in refinement with increasing cooling rate, as well as to identify the limit to structure refinement with the LMC process. Single-crystal Rene N5 and a modified version of the Rene N5 alloy were grown using both processes in order to evaluate the influence of segregation of alloying elements and defect occurrence with the addition of the refractory element, Ta. Newly developed statistical modeling techniques were employed to characterize the homogeneity in microstructure. Fatigue experiments were performed at 538°C (R = 0, f = 0.5 Hz), along with unique in-situ crack growth studies (R = 0.1, f = 20 kHz) to examine the influence of refinement on the fatigue life and crack propagation behavior.;The LMC process is capable of refining the dendritic spacings and maximum pore size by 60 and 65 pct, respectively. The primary initiation sites for fracture in the single crystals during low cycle fatigue (LCF) were casting pores that were located internally and near to the surface. These pores were strongly influenced the crack initiation life. An empirical-based processing-structure-fatigue property model that relates the critical aspects of processing conditions to fatigue life has been developed.
机译:当需要显着的抗疲劳载荷时,单晶镍基高温合金已经成为高温应用的选择材料。尽管可以通过直接替代材料来改善疲劳寿命,但与典型的生产工艺相比,通过先进的铸造技术可以获得更多的收益。但是,在整合到制造业之前,必须优化更高的热梯度工艺来生产具有改善的疲劳性能的精制,均匀,单晶组件。;本文中,需要采用更高的冷却效率工艺,特别是液态金属冷却(使用Sn作为冷却介质的LMC)已评估了单晶高温合金翼型尺寸组件潜在的疲劳性能优势。使用常规的辐射冷却Bridgman铸造和LMC工艺进行了一系列铸造实验,比较了直径为1.6 cm的棒材的枝晶间距和缺陷尺寸分布的细化。选择铸造条件以观察随着冷却速率增加而细化的趋势,以及确定LMC工艺对结构细化的限制。为了评估合金元素的偏析和添加难熔元素Ta引起的缺陷产生的影响,使用了两种工艺来生长单晶的Rene N5和Rene N5合金的改良版。采用最新开发的统计建模技术来表征微观结构的均匀性。疲劳实验在538°C(R = 0,f = 0.5 Hz)下进行,同时进行了独特的原位裂纹扩展研究(R = 0.1,f = 20 kHz),以检验细化对疲劳寿命和裂纹的影响LMC工艺能够将树突间距和最大孔径分别细化60和65 pct。低循环疲劳(LCF)期间,单晶断裂的主要起始点是位于内部且靠近表面的铸孔。这些孔强烈影响了裂纹的萌生寿命。已经建立了基于经验的加工结构疲劳特性模型,该模型将加工条件的关键方面与疲劳寿命相关联。

著录项

  • 作者

    Brundidge, Clinique L.;

  • 作者单位

    University of Michigan.;

  • 授予单位 University of Michigan.;
  • 学科 Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 2011
  • 页码 226 p.
  • 总页数 226
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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