基于十字坐标系子结构建模方法的角度不对中故障转子的模态和响应特性

IF 1 4区 工程技术 Q3 ENGINEERING, AEROSPACE
Yu Liu, Diwen Zhao, Zhi Wang, Yanting Ai
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引用次数: 0

摘要

有限元模型被广泛应用于不对中转子的动态分析中,但目前的有限元转子模型无法模拟角度不对中转子的轴特性,而角度不对中转子与无不对中转子的轴特性是一致的。为实现角度不对中转子的精确建模,引入了一种新的建模方法--交叉坐标子结构建模法,以建立不对中转子的模型,其中转子的不同部分围绕不同的轴旋转。基于这种建模方法,在 ANSYS 的帮助下建立了角度不对中转子的三维实体模型,并通过模态分析和谐波响应分析获得了不对中转子的模态特性和临界转速。通过基于 Newmark 方法的数值模拟和实验测试,获得了转子模型在不平衡力和不对中载荷共同作用下的响应特性。结果表明,当转子发生角度不对中时,会出现 "转子旋转 "模态,并且在谐波响应分析中会产生更多的响应峰值。角度不对中转子的典型故障特征在频谱和轨道图上与数值模拟和实验测试结果基本一致。研究成果可为旋转机械系统不对中故障的模拟和识别提供理论依据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modal and response characteristics of rotor with angle misalignment fault based on cross-coordinate system substructure modeling method
Finite element models are widely used in dynamic analysis of misalignment rotor, but present finite element rotor models cannot simulate the axis characteristics of angle misalignment rotor, which consistent with the one with no misalignment. For achieving the precisely modeling of angle misalignment rotor, a novel modeling method called cross-coordinate substructure modeling method is introduced to establish the model of misalignment rotor, in which different parts of rotor rotate around different axis. Based on this modeling method, the 3D solid models of angle misalignment rotor are established with the help of ANSYS, and the modal characteristics and critical speeds of the misalignment rotor are achieved through modal analysis and harmonic response analysis. The numerical simulation based on Newmark method and experiment tests is carried out to obtain the response characteristics of the rotor model under the combined action of unbalanced force and misalignment load. The results show that the modal “rotation of rotor” appears, and the more amounts of response peaks can be aroused in harmonic response analysis when the rotor occurs angle misalignment. The typical fault characteristics of angle misalignment rotor in the spectrums and orbit diagrams are generally consistent both in the numerical simulation and experiment test. The research results can provide a theoretical basis for simulation and identification of the misalignment fault in rotating machinery system.
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来源期刊
CiteScore
2.40
自引率
18.20%
发文量
212
审稿时长
5.7 months
期刊介绍: The Journal of Aerospace Engineering is dedicated to the publication of high quality research in all branches of applied sciences and technology dealing with aircraft and spacecraft, and their support systems. "Our authorship is truly international and all efforts are made to ensure that each paper is presented in the best possible way and reaches a wide audience. "The Editorial Board is composed of recognized experts representing the technical communities of fifteen countries. The Board Members work in close cooperation with the editors, reviewers, and authors to achieve a consistent standard of well written and presented papers."Professor Rodrigo Martinez-Val, Universidad Politécnica de Madrid, Spain This journal is a member of the Committee on Publication Ethics (COPE).
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