Vibration performance of dual rotor systems considering elastohydrodynamic lubrication of intershaft bearings

被引:0
|
作者
Li J. [1 ,2 ,3 ]
Cao S. [1 ,2 ,3 ]
Guo H. [1 ,2 ,3 ]
Nie R. [1 ,2 ,3 ]
Hou Y. [1 ,2 ,3 ]
机构
[1] School of Mechanical Engineering, Tianjin University, Tianjin
[2] Tianjin Key Laboratory of Nonlinear Dynamics and Control (Tianjin University), Tianjin
[3] National Demonstration Center for Experimental Mechanics Education, Tianjin University, Tianjin
关键词
Dual rotor system; Dynamic characteristics; Elastohydrodynamic lubrication; Experimental research; Intershaft bearing;
D O I
10.11918/201909168
中图分类号
学科分类号
摘要
To study the nonlinear vibration characteristics of dual rotor systems considering the elastohydrodynamic lubrication (EHL) of intershaft bearings, an intershaft bearing contact model and an intershaft bearing-dual rotor system model for aero-engine were established based on the EHL theory and the rotor dynamics theory. The dynamic characteristics of the system were obtained by numerical simulation. The amplitude-frequency response of the dual rotor system was analyzed under the conditions with or without EHL. The influences of Hertz contact stiffness, radial clearance, and viscosity of lubricating oil of intershaft bearing on the system characteristics were compared. Results show that EHL had little effect on the vibration amplitude and the position of the resonant peak of the high pressure rotor and low pressure rotor at the first order resonant peak, while it had great effect on the resonant peak in the high speed range, which made the resonant peak move to the right and decreased its amplitude. With varying Hertz contact stiffness and radial clearance of intershaft bearing, the variation of amplitude at the first order resonant peak was less than 5% when considering EHL, and that at the second order resonant peak was between 4% and 9%. The position of the first order resonant peak was not offset, while that of the second order resonant peak moved about 2%-8% to the high-frequency direction. The influence on the vibration amplitude of the low pressure rotor and high pressure rotor was less than 1% when the viscosity of lubricating oil was changed. Finally, simulation results were validated by gas-driven dual rotor experimental facility. Copyright ©2021 Journal of Harbin Institute of Technology.All rights reserved.
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页码:138 / 147
页数:9
相关论文
共 23 条
  • [1] FERRARIS G, MAISONNEUVE V, LALANNE M., Prediction of the dynamic behavior of non-symmetrical coaxial co-or counter-rotating rotors, Journal of Sound and Vibration, 195, 4, (1996)
  • [2] CHEN Guo, Vibration modelling and verifications for whole aero-engine, Journal of Sound and Vibration, 349, (2015)
  • [3] HU Qinghua, DENG Sier, TENG Hongfei, A 5-DOF model for aeroengine spindle dual-rotor system analysis, Chinese Journal of Aeronautics, 24, 2, (2011)
  • [4] BAI Xuechuan, Research on dynamical characteristics of counter-rotating dual-rotor system of aero-engines, (2013)
  • [5] ZHANG Tiancheng, CAO Shuqian, LI Liqing, Et al., Analysis and experiment of coupled bending and torsional vibration of a rub-impact dual-rotor system, Journal of Aerospace Power, 34, 3, (2019)
  • [6] WANG Nanfei, JIANG Dongxiang, XU Hongzhi, Dynamic characteristics analysis of a dual-rotor system with inter-shaft bearing, Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering, 233, 3, (2017)
  • [7] GAO Peng, HOU Lei, YANG Rui, Et al., Local defect modelling and nonlinear dynamic analysis for the inter-shaft bearing in a dual-rotor system, Applied mathematical Modeling, 68, (2019)
  • [8] SUN Chuanzong, CHEN Yushu, HOU Lei, Steady-state response characteristics of a dual-rotor system induced by rub-impact, Nonlinear Dynamics, 86, 1, (2016)
  • [9] HOU Lei, CHEN Yushu, FU Yiqiang, Et al., Application of the HB-AFT method to the primary resonance analysis of a dual-rotor system, Nonlinear Dynamics, 88, 4, (2017)
  • [10] ZHAO Lianchun, Research on vibration of ball bearings, (2003)