基于动力学建模的太阳泰坦130燃气轮机稳定性及振动分岔分析

M. Alaoui, Abdelhamid IRATNI, Obaid S. Alshammari, A. Hafaifa, I. Colak, M. Guemana
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引用次数: 3

摘要

摘要:本文主要研究燃气轮机的振动稳定性问题,通过与杰弗科特转子的动力学模型相比较,对燃气轮机的参数进行估计,并根据实际振动测量数据建立反映燃气轮机转子特性的数学模型。几何非线性振动的加入揭示了一个超临界Hopf分岔,不稳定模态被排斥到一个小半径的稳定极限环。对安装在阿尔及利亚Djelfa气体压缩站的燃气轮机Solar TITAN 130型进行了振动测量和分析。读取振动参数时,涡轮处于工作模式。分岔监测限定了涡轮的具体工作范围,有效地提取了所研究涡轮的动态行为核心,从而为涡轮转子的有效尺寸确定提供了一种新的方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Stability and Analysis of Vibrations Bifurcation Based on Dynamic Modeling of a Solar Titan 130 Gas Turbine
Abstract This work is interested in studying the vibrations’ stability in gas turbines, compared to a dynamic model of the Jeffcott rotor, the parameters of the gas turbine will be estimated for the purpose of developing a mathematical model which points out the behavior of the turbine rotor in virtue of the data of actual vibration measurements. The addition of the geometric nonlinearities of the vibrations unveils a supercritical Hopf bifurcation, the unstable modes are repulsed towards a stable limit cycle of small radius. The vibration measurements and analyzes were performed on a gas turbine Solar TITAN 130 type mounted in a gas compression station in Djelfa, Algeria. The turbine was in the operating mode when the vibration parameters were read. Bifurcation monitoring bounds the specific operating ranges, extracts efficiently the dynamic behavior core of the studied turbine and consequently affords a new approach to efficiently dimension the turbine rotor.
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