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CREEP OF γ-TIAL BASED ALLOYS - EXPERIMENTS AND COMPUTATIONAL MODELING

机译:γ-TiA1合金的蠕变 - 实验和计算建模

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Internietallic γ-TiAl based materials are qualified to become an important material for advanced applications especially in aeroengine and aerospace industries (Kim, 1994). Research and development have progressed significantly within the last few years and led to comprehensive understanding of fundamental correlations between alloy composition and microstructure, processing behavior and mechanical properties. It is well known that the mechanical properties of γ-TiAl alloys depend strongly on microstructure, which in turn is influenced by the alloy chemistry and the applied heat treatments. A designed fully lamellar (DFL) microstructure which consists of colonies of parallel γ-TiAl (tetragonal face centered L1_0 structure) and α_2-Ti_3Al (ordered hexagonal DO_(19) structure) laths with a colony size in the range of 150-200μm possesses superior creep resistance. Recent studies (Parthasarathy et al. 1998, Crofts et al. 1996, Maruyama et al. 1997) have shown that interface spacing has a major influence on the creep behavior. This may allow the conclusion that the interfaces γ/γ and α_2/γ must play a role in limiting creep flow or providing creep strength. In this paper differently spaced DFL microstructures were adjusted in order to investigate their influence on creep. Fine grained sheet material exhibiting a nominal composition of Ti-46.5at%Al-4at%(Cr,Nb,Ta,B) was used and short term creep tests were carried out in air at 700°C and 800°C under a load stress of 175MPa constant in time. The interface spacing was varied in the range of 1.2μm to 0.14 μm by altering the cooling rates from 1 K/min to 200K/min. A first approach in modeling the steady state creep deformation of the fully lamellar material in question is presented. A power law description for diffusion controlled dislocation creep is proposed and a structure factor is introduced which depends on the lamellar orientation with respect to the loading axis as well as on the mean lamellar interface spacing.
机译:基于Internietallicγ-Tial基材料被称为适用于尤其是在Aeroengine和Aerospace Industries(Kim,1994)中的先进应用的重要材料。在过去几年中,研究和开发显着进展,并导致了对合金组成和微观结构,加工行为和机械性能之间的基本相关性的全面了解。众所周知,γ-Tial合金的机械性能强烈地依赖于微观结构,这反过来受合金化学和施加的热处理的影响。由平行γ-Tial(四方面为中心L1_0结构)和α_2-Ti_3AL的菌落组成的设计的完全层状(DFL)微结构,其菌落尺寸在150-200μm的范围内耐高采烈的抗蠕变性。最近的研究(Parthasarathy等,1998,Crofts等人1996,Maruyama等,1997)表明,界面间距对蠕变行为产生了重大影响。这可能允许结论是γ/γ和α_2/γ必须在限制蠕变流或提供蠕变强度时发挥作用的作用。在本文中,调整了不同间隔的DFL微观结构,以便研究它们对蠕变的影响。使用具有Ti-46.5At%的标称组成的细粒片材使用,并且在负载下在700℃和800℃下在空气中进行短期蠕变试验。应激175MPa恒定的时间。通过将冷却速率从1 k / min改变为200k / min,界面间距在1.2μm至0.14μm的范围内变化。提出了一种在质量上建模的稳态蠕变变形的第一方法。提出了一种用于扩散控制位错蠕变的动力法描述,并引入结构因子,其取决于相对于装载轴的层状取向以及平均层状界面间距。

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