华南理工大学学报(自然科学版) ›› 2025, Vol. 53 ›› Issue (9): 98-105.doi: 10.12141/j.issn.1000-565X.240305

• 机械工程 • 上一篇    下一篇

气体轴承-转子系统双向流固耦合特性分析及等效气膜厚度的建立与验证

马文琦  马海龙 秦雨彬  黄大利   

  1. 大连海事大学 船舶与海洋工程学院,辽宁 大连 116026

  • 出版日期:2025-09-25 发布日期:2025-01-17

Analysis of Bidirectional Fluid-Structure Interaction Characteristics of Gas Bearing-Rotor Systems and the Establishment and Verification of Equivalent Air Film Thickness

MA Wenqi  MA Hailong  QIN Yubin  HUANG Dali   

  1. Naval Architecture and Ocean Engineering College, Dalian Maritime University, Dalian 116026, Liaoning, China
  • Online:2025-09-25 Published:2025-01-17

摘要:

采用计算流体动力学(CFD)方法对气体轴承-转子系统进行流场特性仿真时,气膜厚度是至关重要的结构参数之一,但由于零件加工过程中产生的形状、尺寸误差以及系统装配造成的偏差等原因,导致实际气膜与理想设计气膜在空间形貌及尺度上都存在一定的偏差,进而影响数值解算结果的可靠性及准确性。本论文提出流场有效气膜厚度的概念,通过双向流固耦合数值仿真模拟与实验结果对比分析及修正,最终确定合理的等效气膜厚度。研究结果表明:采用双向流固耦合数值模拟方法可揭示气膜流场瞬态特性及转子姿态的变化规律,并对气体轴承-转子系统是否能够安全运行进行预判和评估,节省了实验测试成本;采用转子倾斜角作为对比分析特征,为数值仿真结果和实验测试结果二者之间的系统性能偏差分析提供了直观的参考依据;等效气膜厚度的建立可最大程度上简化数值仿真模型,提高数值仿真效率,同时其结果又具有一定的可靠性;以供气压力0.6MPa,单边稳态加载力80N为例,通过误差分析和逼近,循环建立和修正流固耦合仿真模型中预估的等效气膜厚度,最终实现了将系统倾斜角相对误差控制5%以内,极大提高了数值模拟仿真结果与实际工程系统性能的一致性,进而为气体轴承-转子仿真系统在结构设计、性能预测及评估中的应用提供了可靠方法及依据。

关键词: 气体轴承-转子系统, 双向流固耦合, 等效气膜厚度, 稳态加载

Abstract:

When computational fluid dynamics (CFD) is used to simulate the flow field characteristics of a gas bearing-rotor system, the thickness of the gas film is one of the crucial structural parameters. However, due to the shape and size errors generated during the machining of parts and the deviation caused by the system assembly, there are certain deviations in the spatial morphology and scale between the actual gas film and the ideal design gas film. Then the reliability and accuracy of the numerical solution are affected. In this paper, the concept of effective gas film thickness of flow field is proposed, and the reasonable equivalent gas film thickness is determined by the comparison and analysis of the bidirectional fluid-structure coupling numerical simulation and experimental results. The results show that the bidirectional fluid-structure coupling numerical simulation method can reveal the transient characteristics of the gas film flow field and the changing law of the rotor attitude, and predict and evaluate whether the gas bearing-rotor system can operate safely, saving the test cost. The rotor inclination Angle is used as the comparative analysis feature, which provides a direct reference for the analysis of the system performance deviation between the numerical simulation results and the experimental test results. The establishment of equivalent gas film thickness can simplify the numerical simulation model to the greatest extent, improve the efficiency of numerical simulation, and the results have a certain reliability. Taking the gas supply pressure of 0.6MPa and the unilateral steady-state loading force of 80N as examples, the equivalent gas film thickness predicted in the fluid-to-solid coupling simulation model was established and corrected through error analysis and approximation, and the relative error of the system inclination Angle was controlled within 5% in the end, which greatly improved the consistency between the numerical simulation results and the actual engineering system performance. It provides a reliable method and basis for the application of gas bearing rotor simulation system in structural design, performance prediction and evaluation.

Key words: gas bearing-rotor system, two-way fluid-structure coupling, equivalent gas film thickness, model modification