Nonlinear Modeling and Vibration Response Analysis of a Dual-Rotor System with an Inter-Shaft Graphite Seal

Author:

Xiao Sen1,Yu Pingchao2,Jiang Zihan2,Wang Cun3,Chen Jiayu2,Zhang Qicheng4ORCID

Affiliation:

1. Chengdu Aircraft Industry (Group) Co., Ltd., Chengdu 610037, China

2. College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China

3. Beijing Institute of Power Machinery, Beijing 100074, China

4. Bristol Composites Institute, University of Bristol, University Walk, Bristol BS8 1TR, UK

Abstract

The inter-shaft graphite seal is a common structure in the dual-rotor system, and may generate nonlinear lateral excitation when there is large relative angular motion at the seal position. This paper represents the first attempt to study the nonlinear behaviors of a dual-rotor system with inter-shaft graphite seal excitations. First, an excitation model of the inter-shaft graphite seal is proposed by the analytical method. This model is then introduced into the beam finite element model of a dual rotor system, and the dynamic equations of the whole system are finally obtained. The vibration responses under the effect of the inter-shaft seal are clarified by analyzing 3D waterfall plots, rotor orbits, and time and frequency domain waveforms. The results show that the inter-shaft seal can lead to vibration coupling between HP and LP rotors. The axial spring stiffness and contact end face friction coefficient of the graphite seal have a significant effect on rotor vibration. When those two parameters are small, only coupling vibration phenomena can be observed, i.e., the rotation frequency of one rotor can be observed in another rotor vibration. With the increase in axial spring stiffness or contact end face friction coefficient, multiple modes of LP and HP rotors are excited, which dominates the vibration behaviors of the dual rotor system.

Funder

National Natural Science Foundation of China

Jiangsu Province Natural Science Foundation

Aeronautical Science Foundation of China

Postdoctoral Science Foundation Project

Publisher

MDPI AG

Reference28 articles.

1. Huang, Q. (2001). Aero Engine Design Manual Volume 10, Aviation Industry Press. Engine Design Manual, Editor in Chief of the Editorial Committee.

2. Dynamic modeling and nonlinear analysis for lateral–torsional coupling vibration in an unbalanced rotor system;Yu;Appl. Math. Model.,2024

3. Research on the Application of Aeroengine Sealing Technology;Hu;Aeroengine,2012

4. Hao, M., Li, Z., Ren, B., and Wang, X. (2014). Mechanical Sealing Technology and Applications, China Petrochemical Press. [2nd ed.].

5. Huang, W., Li, Y., and Wang, Y. (2016). Principles and Design of Mechanical Seals, Mechanical Industry Press.

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3