Constitutive Model and Microstructure Evolution of Ti65 Titanium Alloy

Author:

Sun Tao1ORCID,Sun Lili1,Teng Haihao1,Liu Wenhao2,Wang Ruiqi13,Zhao Xuanjie13,Zhou Jie1

Affiliation:

1. College of Materials Science and Engineering, Chongqing University, Chongqing 400044, China

2. College of Physics, Sichuan University, Chengdu 610064, China

3. Deyang Wanhang Die Forging Co., Ltd., China National Erzhong Group Co., Deyang 618000, China

Abstract

The hot deformation behavior and mechanism of Ti65 alloy with a bimodal microstructure were investigated by isothermal compression experiments conducted on the Thermecmastor-Z simulator equipment at temperatures ranging from 950 to 1110 °C and strain rates ranging from 0.01 to 10.0 s−1. The Arrhenius constitutive model, based on strain compensation, and Grey Wolf optimization-neural network with back propagation model (GWO–BP), were both established. The differences between the experimental and predicted value of flow stress were compared and analyzed using the two models. The results show that the prediction accuracy of GWO–BP in the two-phase region is higher than that of Arrhenius model. In the single-phase region, both methods demonstrated high prediction accuracy. Compared to the single-phase region, the flow stress of Ti65 alloy shows a higher degree of softening in the two-phase region. During deformation in the two-phase region, the initial lamellar α phase transformed from a kinked and elongated morphology to a globularized topography as the strain rate decreased. Boundary-splitting was the primary mechanism leading to the spheroidization process. The degree of recrystallization increased with the increase in strain rate during the deformation in the single-phase region, while dynamic recovery and strain-induced grain boundary migration were the main deformation mechanisms at a lower strain rate. Discontinuous dynamic recrystallization may be the dominant recrystallization mechanism under a high strain rate of 10 s−1.

Funder

project of Research on the Preparation and Control Technology of Aerospace Major Alloy Forgings from Deyang Wanhang Die Forging Co., Ltd.

National Natural Science Foundation of China

Publisher

MDPI AG

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