Dynamic Characteristics of a 5-kN Thrust Gas Turbine Front Bearing Composed of a Vibration Absorber Element and Deep Groove Ball Bearing

Bertolino Junio dos Santos, Damásio Sacrini, A. V. Rodrigues, Geraldo Creci, J. C. Menezes
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Abstract

Rolling bearings enable the development of high rotational speeds with a good load-bearing capacity and low frictional resistance. Therefore, rolling bearings can be used on a wide variety of rotating machines. This study investigated the dynamic stiffness and damping coefficients of the front bearing of a 5-kN thrust gas turbine. A Barden® 206(T) deep-groove ball bearing was the main part of the front bearing. Computational models were developed using MATLAB® for both the structural dynamics problem governed by Hertzian contact theory and the lubricated problem governed by elastohydrodynamic theory. In addition, the front bearing was composed of a vibration absorber element, which was also considered. Finite element analysis was performed on both the ball bearing and the vibration-absorbing element to assist in its final characterization. As the main results, the stiffness and damping dynamic coefficients of the front bearing were estimated and can be used to predict the rotordynamic behavior of the aeronautical gas turbine rotating set to avoid possible vibration problems during operation.
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由吸振元件和深沟球轴承组成的5kn推力燃气轮机前轴承动态特性
滚动轴承能够发展具有良好承载能力和低摩擦阻力的高转速。因此,滚动轴承可用于各种旋转机械上。对某5 kn推力燃气轮机前轴承的动刚度和阻尼系数进行了研究。Barden®206(T)深沟球轴承是前轴承的主要部分。利用MATLAB®开发了基于赫兹接触理论的结构动力学问题和基于弹性流体力学理论的润滑问题的计算模型。此外,还考虑了前轴承由吸振元件组成。对滚珠轴承和吸振元件进行了有限元分析,以协助其最终表征。研究结果表明,前轴承的刚度和阻尼动力系数可用于预测航空燃气轮机旋转机组的转子动力学行为,以避免在运行过程中可能出现的振动问题。
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