Experiment and simulation analysis of tribological and dynamic characteristics in aeroengine hybrid ceramic bearing
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 5 October 2023
Issue publication date: 13 November 2023
Abstract
Purpose
This paper aims to research the tribological and dynamic characteristics of aeroengine hybrid ceramic bearings through wear experiments and simulation analysis.
Design/methodology/approach
First, the authors carried out wear experiments on Si3N4–GCr15 and GCr15–GCr15 friction pairs through the ball-disc wear test rig to explore the tribological properties of their materials. Second, using ANSYS/LS-DYNA simulation software, the dynamic simulation analysis of hybrid bearings was carried out under certain working conditions, and the dynamic contact stress of all-steel bearings of the same size was simulated and compared. Finally, the change of the maximum contact stress of the main bearing under the change of load and rotation speed was studied.
Findings
The results show that the Si3N4–GCr15 pair has better tribological performance. At the same time, under the conditions of high speed and heavy load, the simulation analysis shows that the contact stress between the ceramic ball and the raceway of the ring is smaller than the steel ball. That is, hybrid bearings have better transient mechanical properties than all-steel bearings. With the speed increasing to 12,000 r/min, the maximum stress point will shift in the inner and outer rings.
Originality/value
In this study, the tribological and transient mechanical properties of Si3N4 material were comprehensively analyzed through wear experiments and dynamic simulation analysis, which provided a reference for the design of hybrid bearings for next-generation aeroengines.
Keywords
Acknowledgements
The authors acknowledge the constructive discussions with Professor Zhixiong Li of School of Engineering at Ocean University of China. The authors wish to give special thanks to Dr Jun Zhao and Professor Yijun Shi of Division of Machine Elements at Luleå University of Technology, for the fruitful discussions during this work.
Declaration of conflicting interests: The authors declared no potential conflicts of interest with respect to the research, authorship and/or publication of this article.
Funding: The authors wish to express their gratitude to the Natural Science Foundation of China (No.52072176) for supporting the research as reported in this paper.
Citation
Chen, Z., Long, W., Song, L. and Li, X. (2023), "Experiment and simulation analysis of tribological and dynamic characteristics in aeroengine hybrid ceramic bearing", Aircraft Engineering and Aerospace Technology, Vol. 95 No. 10, pp. 1694-1705. https://doi.org/10.1108/AEAT-09-2022-0244
Publisher
:Emerald Publishing Limited
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