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Full Length Article | Open Access

Geometric size and forming force prediction in incremental flanging: A new analytical model

Chong TIANDawei ZHANG( )Guangcan YANGShengdun ZHAO
Xi’an Key Laboratory of Intelligent Equipment and Control, School of Mechanical Engineering, Xi’an Jiaotong University, Xi’an 710049, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

A new analytical model for geometric size and forming force prediction in incremental flanging (IF) is presented in this work. The complex deformation characteristics of IF are considered in the modeling process, which can accurately describe the strain and stress states in IF. Based on strain analysis, the model can predict the material thickness distribution and neck height after IF. By considering contact area, strain characteristics, material thickness changes, and friction, the model can predict specific moments and corresponding values of maximum axial forming force and maximum horizontal forming force during IF. In addition, an IF experiment involving different tool diameters, flanging diameters, and opening hole diameters is conducted. On the basis of the experimental strain paths, the strain characteristics of different deformation zones are studied, and the stable strain ratio is quantitatively described through two dimensionless parameters: relative tool diameter and relative hole diameter. Then, the changing of material thickness and forming force in IF, and the variation of minimum material thickness, neck height, maximum axial forming force, and maximum horizontal forming force with flanging parameters are studied, and the reliability of the analytical model is verified in this process. Finally, the influence of the horizontal forming force on the tool design and the fluctuation of the forming force are explained.

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Chinese Journal of Aeronautics

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Cite this article:
TIAN C, ZHANG D, YANG G, et al. Geometric size and forming force prediction in incremental flanging: A new analytical model. Chinese Journal of Aeronautics, 2025, 38(2). https://doi.org/10.1016/j.cja.2024.04.002

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Received: 15 January 2024
Revised: 09 February 2024
Accepted: 20 March 2024
Published: 05 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/).