热-流-固耦合作用下多层气体箔型推力轴承的热弹流动力分析

IF 5.3 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Qihong GAO, Wenjing SUN, Jingzhou ZHANG
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引用次数: 0

摘要

在超高速和小型化叶轮机械中,气膜轴承面临着严重而复杂的热-流-固耦合问题。本研究采用三维热-流-固耦合方法,对特定多层气膜推力轴承在稳定转速下的连续加载过程进行了热-等效流体动力学(TEHD)数值分析。结果表明,多层气膜的整体刚度呈非线性,其中推力底部气膜是主要的弹性变形结构,而推力顶部气膜在加载过程中保持了清晰的空气动力学形状,这有助于减少摩擦损伤并获得足够的加载能力。在低负载情况下,气膜的波动极为敏感,随着负载的增加,气膜的波动急剧减弱。在快速增长后,粘热和摩擦扭矩与轴承载荷的增加呈线性关系。根据多层气膜的确切堆叠顺序和接触位置,重叠配置可通过热传导有效传递最小气膜处积累的粘剪切热,同时提供弹性支撑。由于粘性热量在不同载荷下具有很强的不均匀性,顶箔表面的温度分布呈现出明显的变化,而推力板和顶箔表面的峰值温度和平均温度之间的差异会随着载荷的增加而大幅扩大。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Thermo-elasto-hydrodynamic analysis of a specific multi-layer gas foil thrust bearing under thermal-fluid–solid coupling

Gas foil bearing faces severe and complex thermal-fluid–solid coupling issues when in ultra-high speed and miniaturized impeller machineries. In this study, a Thermo-Elasto-Hydrodynamic (TEHD) analysis of a specific multi-layer gas foil thrust bearing on the continuous loading process within a steady rotational speed is numerically investigated by a three-dimensional thermal-fluid–solid coupling method. Results indicate that the multi-layer foil exhibits nonlinear overall stiffness, with the thrust bottom foil serving as the primary elastic deformation structure, while the thrust top foil maintains a well-defined aerodynamic shape during a loading process, which helps reduce frictional damage and achieve an adequate loading capacity. For low loads, the fluctuation of the gas film is extremely sensitive, and it weakens dramatically as the load increases. The viscous heating and friction torque exhibit a linear relationship with an increasing bearing load after a rapid growth. Depending on the exact stacking sequence and contact position of the multi-layer gas foil, the overlapping configuration allows for efficient transfer of viscous-shearing heat accumulated at the smallest air film through thermal conduction while providing elastic support. Due to the strong inhomogeneity of the viscous heat under varying loads, the temperature distribution on the top foil surface shows pronounced variations, while the difference between the peak and average temperatures of the thrust plate and top foil surfaces widens substantially with an increasing load.

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来源期刊
Chinese Journal of Aeronautics
Chinese Journal of Aeronautics 工程技术-工程:宇航
CiteScore
10.00
自引率
17.50%
发文量
3080
审稿时长
55 days
期刊介绍: Chinese Journal of Aeronautics (CJA) is an open access, peer-reviewed international journal covering all aspects of aerospace engineering. The Journal reports the scientific and technological achievements and frontiers in aeronautic engineering and astronautic engineering, in both theory and practice, such as theoretical research articles, experiment ones, research notes, comprehensive reviews, technological briefs and other reports on the latest developments and everything related to the fields of aeronautics and astronautics, as well as those ground equipment concerned.
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