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An Improved Empirical Constitutive Model for γ'-Strengthened Nickel-Based Superalloys

机译:γ'强化镍高超合金的改进的经验构成模型

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Advanced superalloys were developed for high performance systems such as jet engines, internal combustion engines and gas turbines. Nickel-based superalloys are strengthened by the γ'-phase, through various mechanisms, such as lattice parameter mismatch, coherent strain, or anti-phase boundary. Due to the changing of lattice parameters of γ-phase and γ'-phase at various temperatures, the deformation mechanisms perform anomalously. The objective of this paper is to develop a constitutive model for nickel-based superalloys, which could be further implemented in finite element analysis. In order to derive an accurate constitutive model, strain hardening function, thermal sensitivity function, and flow softening function were determined. Also, piecewise method was applied as a function of the temperature ranges. The novel constitutive model proposed for superalloys was compared with material testing data (flow stress) and a good agreement was found for a temperature range from 294K to 1144K.
机译:高级超合金用于高性能系统,如喷射发动机,内燃机和燃气轮机。镍基超合金通过γ'-阶段加强,通过各种机制,例如晶格参数失配,相干菌株或抗相边界。由于γ相的晶格参数和各种温度下的γ'-阶段的变化,变形机制大致执行。本文的目的是开发一种基于镍的超合金的本构体模型,可以在有限元分析中进一步实施。为了得出精确的本构体模型,测定应变硬化功能,热敏功能和流动软化功能。此外,作为温度范围的函数施加分段方法。将用于超合金的新型本构模型与材料测试数据(流量应力)进行比较,并且发现良好的一致性范围为294K至1144K。

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