Dynamic analysis and experiment investigation of a cracked dual-disc bearing-rotor system based on orbit morphological characteristics

被引:30
作者
Xiang, Ling [1 ]
Zhang, Yue [1 ]
Hu, Aijun [1 ]
Ye, Feng [1 ]
机构
[1] North China Elect Power Univ, Dept Mech Engn, Baoding 071003, Hebei, Peoples R China
基金
中国国家自然科学基金;
关键词
Bearing-rotor system; Crack; Orbit morphological characteristic; Subcritical speed; Rub-impact; Oil-film force; THEORETICAL-ANALYSIS; VIBRATION ANALYSIS; TRANSVERSE CRACK; BEHAVIOR; STABILITY; SHAFT;
D O I
10.1016/j.apm.2019.11.042
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The paper is aimed to examine dynamic behaviors of a dual-disc bearing-rotor system in multi-fault state, and the crack detection based on the orbit morphological characteristics and vibration responses is proposed. Dynamic response and vibration signal analysis are two significant studies in rotor system. Most researchers have simulated the nonlinear dynamics and analyzed the fault signal using various methods separately. However, the fault feature from vibration signal is tightly connected with the dynamic mechanism in the rotor system, especially in rotor system with coupling multi-fault. In the paper, the dynamic model of the dual-disc bearing-rotor system is established, which takes into account the effects of crack, rub-impact and nonlinear oil-film forces. The vibration responses and the effect of crack on dual-disc rotor system with multi faults are investigated. The existence of crack and the coupling effect of multi faults enrich dynamic behavior of the dual-disc bearing-rotor system, and the response near the 1/2 subcritical speed provides a criterion for crack detection. Experiment investigation is attempted for the first time, which is based on the changes of crack depth and rotation speed for multi-fault dual-disc rotor system. The analysis of the dynamic response and the orbit morphological characteristics from experiment can effectively detect the crack information. (C) 2019 Elsevier Inc. All rights reserved.
引用
收藏
页码:17 / 32
页数:16
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