Nonlinear Dynamic Behavior Analysis of Dual-Rotor-Bearing Systems with Looseness and Rub–Impact Faults

Author:

Lu Kuan1,Guo Dong1,Zhu Weidong2ORCID,Jin Yulin3ORCID,Cheng Hui1,Gu Xiaohui4,Fu Chao1

Affiliation:

1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China

2. University of Maryland, Baltimore, Maryland 21250

3. Southwest Jiaotong University, 610031 Chengdu, People’s Republic of China

4. Shijiazhuang Tiedao University, 050043 Shijiazhuang, People’s Republic of China

Abstract

The nonlinear dynamic behaviors of dual-rotor-bearing systems with looseness and rub–impact faults are discussed in this paper. The dual-rotor-bearing system with looseness and rub–impact coupling faults is established by the finite element method. The component mode synthesis (CMS) and proper orthogonal decomposition (POD) methods are introduced. The CMS and POD methods are used to reduce the original rotor system model, and the efficiency of the order reduction method is verified by comparing the dynamic behaviors of the original and reduced systems. The frequency spectrum and amplitude–frequency behaviors of rotor systems are studied. The results can provide qualitative guidance to structural design optimization of large rotating machines and prior information for looseness and rub–impact coupling faults.

Funder

Outstanding Fund of Natural Science Foundation of Shaanxi Province

State Key Laboratory of Mechanical Behavior and System Safety of Traffic Engineering Structures

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

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