直升机旋翼
转子(电动)
非线性系统
转速
控制理论(社会学)
方位(导航)
振动
临界转速
分叉
转子动力学
刚性转子
工程类
计算机科学
物理
机械工程
人工智能
控制(管理)
量子力学
作者
Chuanbing Zhang,Hongrui Ao,Hongyuan Jiang,Yongliang Wang
标识
DOI:10.1177/10775463221135912
摘要
It is important to propose a reasonable nonlinear dynamic model of gas dynamic bearing–rotor system for the stable operation of turbocharger. This paper presents a hybrid gas journal bearing (HGJBs)–rotor system with flexible supporting structure. A fractional-order dynamic model of the symmetrical flexible HGJB–rotor system is established. A tracking–alarming method is proposed to obtain the rotational speed ratio at the bifurcation point. The stable and unstable regions of the rotational speed ratio Ω ω for both the rigid bearing–rotor system and flexible HGJB–rotor system are analyzed. The nonlinear dynamic behaviors of HGJB–rotor system versus the fractional order α d and rotational speed ratio Ω ω are studied. Results show the fractional-order dynamic model can realize the reasonable prediction of nonlinear dynamic behaviors. An increase in the rotational speed ratio Ω ω and the decrease of fractional order α d result in a growth of the vibration amplitude. The adoption of flexible supporting structure is a good strategy to increase the size of stable region.
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