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Full Length Article | Open Access

Drilling process of indexable drill bit based on Coupled Eulerian-Lagrangian method: A simulation study

Desheng HUa, Caixu YUEa( ), Xianli LIUa, Zhipeng JIANGa, Yongshi XUa, Junhui LUa, Steven Y. LIANGb
Key Laboratory of Advanced Manufacturing and Intelligent Technology, Ministry of Education, Harbin University of Science and Technology, Harbin 150080, China
George W. Woodruff School of Mechanical Engineering, Georgia Institute of Technology, Atlanta 30332, USA

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

42CrMo steel has the characteristics of high strength, high wear resistance, high impact resistance, and fatigue resistance. Therefore, drilling 42CrMo steel has always been a challenging task. The indexable drill bit has the advantages of high processing efficiency and low processing cost and has been widely used in the field of aerospace hole processing. To better understand the machining mechanism of the indexable drill bit, this paper uses the Coupled Eulerian-Lagrangian method (CEL) to simulate the three-dimensional drilling model for the first time. The simulation results of the drilling force obtained by the CEL method and Lagrangian method are compared with the experimental results. It is verified that the CEL method is easy to converge and can avoid the problem of program interruption caused by mesh distortion, and the CEL simulation value is more consistent with the actual value. Secondly, the simulation results of cutting force and blade cutting edge node temperature under different process parameters are extracted. The variation of time domain cutting force, frequency domain cutting force and tool temperature with process parameters are obtained. This study provides a new method for the prediction of cutting performance and the optimization of process parameters of indexable drills.

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Chinese Journal of Aeronautics
Pages 477-492

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Cite this article:
HU D, YUE C, LIU X, et al. Drilling process of indexable drill bit based on Coupled Eulerian-Lagrangian method: A simulation study. Chinese Journal of Aeronautics, 2024, 37(11): 477-492. https://doi.org/10.1016/j.cja.2024.03.046

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Received: 28 November 2023
Revised: 24 December 2023
Accepted: 02 February 2024
Published: 03 April 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/).