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Numerical analysis on the deformation characteristics and microstructure behaviors of forged IN718 aeroengine drum

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Abstract

This work is motivated by the fact that the microstructures of nickel-based alloy forged parts influenced by hot deformation have a great impact on the mechanical properties of their final parts. In this paper, a simplified 2D half-symmetry FE model embedded with the JMAK model is developed to predict the deformation characteristics and microstructure behaviors of an IN718 aeroengine drum in hot forging procedure and then verified by experiments. Moreover, based on two evaluation indexes, the distribution uniformities and general levels of effective strain, strain rate, temperature, dynamic recrystallization, and grain size within the forged IN718 alloy drum are analyzed quantitatively. The results suggest that unlike strain rate and grain size, the maximum values of effective strain, temperature, and dynamic recrystallization volume fraction are located at the internal wall of the forged drum, and their distribution uniformities become worse with the increment of forging strokes. Besides, the Xavg and davg show an opposite evolution trend as increasing forging strokes, which are mainly related to the increments of εavg and Tavg as well as the grain refinement of dynamic recrystallization.

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Data are available from the corresponding author on request.

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Funding

This work was supported by the Hubei Provincial Natural Science Foundation of China (Grant nos. 2020CFB115 and 2020CFB112).

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Shiyuan Luo: conceptualization, methodology, software, and writing—original draft. Kai Yan: investigation, validation, and writing—original draft. Jia Li: validation and writing—original draft. Guangming Zou: data curation and writing—review and editing. Po Zhang: data curation and writing—review and editing. Liangcai Zeng: supervision and writing—review and editing.

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Correspondence to Shiyuan Luo.

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Luo, S., Yan, K., Li, J. et al. Numerical analysis on the deformation characteristics and microstructure behaviors of forged IN718 aeroengine drum. Int J Adv Manuf Technol 126, 3749–3764 (2023). https://doi.org/10.1007/s00170-023-11392-3

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