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Open Access

An innovative constraining ring rolling process for manufacturing conical rings with thin sterna and high ribs

Duanyang TIANa,bXinghui HANa,b( )Lin HUAa,bXuan HUa,b
Hubei Key Laboratory of Advanced Technology for Automotive Components, Wuhan University of Technology, Wuhan 430070 China
School of Automotive Engineering, Wuhan University of Technology, Wuhan 430070, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Conical rings with thin sterna and high ribs (CRTSHR) are key bearing-load parts of aerospace equipment, which are required to be manufactured with high performance and efficiency. Traditional ring rolling is the most preferred method for manufacturing high-performance ring parts, but it can hardly achieve the forming of CRTSHR due to the extreme geometry of CRTSHR. To solve this difficulty, an innovative constraining ring rolling process (CRR) is proposed in this paper to manufacture CRTSHR. To evaluate the proposed CRR and reveal its deformation behaviors, a thermomechanical coupled FE model for CRR of CRTSHR is established. Then, the experiment for CRR of CRTSHR is performed on a modified ring rolling machine, which proves that CRR of CRTSHR is feasible and the established FE model is reliable. Based on the reliable FE model, the metal flow mode in deformed CRTSHR is analyzed, and the deformation characteristics such as the stress state, strain distribution and the evolution of power parameters in CRR of CRTSHR are revealed. Finally, the influences of key parameters such as the friction factor between ring and molds, the diameter of idle roll and the feed velocity of idle roll on CRR of CRTSHR are investigated by FE simulation.

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Chinese Journal of Aeronautics
Pages 324-339

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Cite this article:
TIAN D, HAN X, HUA L, et al. An innovative constraining ring rolling process for manufacturing conical rings with thin sterna and high ribs. Chinese Journal of Aeronautics, 2022, 35(8): 324-339. https://doi.org/10.1016/j.cja.2022.03.013

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Received: 11 February 2022
Revised: 19 February 2022
Accepted: 28 February 2022
Published: 28 March 2022
© 2022 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/).