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Full Length Article | Open Access

Cutting force prediction model considering tool-chip contact interface friction behavior in ULTVAM of Ti-6Al-4V

Junjin MAa, Yujie ZHANGa, Yujie LIa, Chenwei SHANb( ), Feng JIAOa, Guofu GAOa, Dinghua ZHANGb, Bo ZHAOa
School of Mechanical and Power Engineering, Henan Polytechnic University, Jiaozuo 454000, China
Key Laboratory of High Performance Manufacturing for Aero Engine, Ministry of Industry and Information Technology, Northwestern Polytechnical University, Xi’an 710072, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

Ti-6Al-4V is widely used in the aviation industry because of its high strength, and good heat resistance. However, severe tool wear on the rake face occurs during the milling of Ti-6Al-4V, which is caused by intense friction between the tool rake face and the chips. To investigate tool wear in the milling of Ti-6Al-4V, ultrasonic vibration is introduced, and a cutting force prediction model that considers tool-chip contact interface friction behavior in Ultrasonic Longitudinal-Torsional Vibration-Assisted Milling (ULTVAM) is proposed in this paper. First, the tool tip motion trajectory and dynamic cutting thickness under ULTVAM were analyzed calculated, and compared with those in Common Milling (CM). Subsequently, the effects of ultrasonic vibration on the shear force under the ultrasonic softening effect, the friction force, and the friction reversal force on the tool-chip contact interface were investigated. A dynamic milling force model under ULTVAM was established before and after friction force reversal caused by ultrasonic longitudinal-torsional vibration. Finally, numerous experiments were conducted to validate the proposed model, and the experimental results indicated that the calculated dynamic milling forces agreed well with the measured values, with errors in the X and Y directions of 5.51% and 10.23%, respectively. In addition, the average roughness of the workpiece surface also decreased (1.08, 0.9, 0.6, 0.7 μm under ultrasonic amplitudes of 0, 1, 2, and 3 μm) and the tool wear state improved on the rake face under ULTVAM.

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Chinese Journal of Aeronautics

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Cite this article:
MA J, ZHANG Y, LI Y, et al. Cutting force prediction model considering tool-chip contact interface friction behavior in ULTVAM of Ti-6Al-4V. Chinese Journal of Aeronautics, 2025, 38(6). https://doi.org/10.1016/j.cja.2024.08.043

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Received: 23 May 2024
Revised: 17 June 2024
Accepted: 08 August 2024
Published: 30 August 2024
© 2024 Chinese Society of Aeronautics and Astronautics

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).