航空零部件用因康奈尔718高温合金回转锻造数值模拟

A. Loyda, G. M. Hernández-Muñoz, L. Reyes-Osorio, P. Zambrano, F. Montemayor-Ibarra
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引用次数: 3

摘要

当今航空工业对其尺寸规格、力学性能和显微组织特征都有严格的质量标准。因此,所涉及的制造过程需要保持高标准。镍基高温合金存在于喷气发动机的许多部件中,其中最常见的是Inconel 718 MR高温合金,占喷气发动机的50%。这是为了抵抗高温,腐蚀和蠕变。旋锻工艺是目前航空工业中处于科技发展阶段的一种制造工艺。开发了Avrami模型与商业FEM平台(DEFORM TM 3D)相结合,以评估平均晶粒尺寸作为980°C和1000°C工作条件的函数。与以往的研究结果相比,研究结果更好地揭示了温度对旋转锻造过程中晶粒演变的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Numerical Simulation of Rotary Forging Inconel 718 Superalloy Applied to Aeronautical Components
Nowadays the aeronautical industry keeps strict quality standards in its dimensional specifications, mechanical properties and microstructural characteristics. Therefore, the involved manufacturing processes require keeping high standards. The nickel based superalloys are present in many components of the jet engines, being the Inconel 718 MR superalloy the most common, making up to 50% of the jet engine. This is designed to resist high temperatures, corrosion and creep. The process of rotary forging is a manufacturing process that is currently under scientific and technological development in the aeronautical industry. An Avrami model coupled with a commercial FEM platform (DEFORM TM 3D) was developed to evaluate the average grain size, as a function of the working conditions at 980 °C and 1000 °C. The results provide a better understanding of the influence of temperature in the grain size evolution during the rotary forging process, compared with previous reports.
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