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Effects of static and imbalance loads on nonlinear response of rigid rotor supported on gas foil bearings

机译:静电和不平衡负荷对燃气箔轴承支撑刚性转子非线性响应的影响

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摘要

This paper presents an experimental and numerical investigation into the effects of static and imbalance loads on the nonlinear rotordynamic performance of a rigid rotor supported on gas foil bearings (GFBs). The interesting phenomenon that static loads can lead to high sub-synchronous motions in rotor-GFB systems is reported for the first time in this paper. The effects of static and imbalance loads on coast-down tests, synchronous response amplitudes, peak response frequency, appearance of sub-synchronous vibrations and time extent of coast-down responses are measured and discussed. A rotordynamic model based on FEM and unsteady Reynolds equation is derived to predict the nonlinear response of the system. The foil structure and gas film in-series are considered to derive the unsteady bearing force. The predictions are consistent with the test data. The relationships between static or imbalance loads and nonlinear response, especially the vibrations in sub-synchronous frequencies, are discussed. In the numerical simulations, as the static and imbalance loads increase, the vibration component changes from mainly synchronous to sub-synchronous and then back to synchronous vibrations. When the static and imbalance loads change, the natural frequency of the rotor-GFB system could be shifted into or away from the threshold of the whirl vibration with a typical factor, A. = 0.5, and lead to serious sub-synchronous vibrations. The experimental data and theoretical predictions help with the engineering design and implementation of GFBs in high-performance micro turbomachineries.
机译:本文介绍了静态和不平衡载荷对燃气箔轴承(GFBS)支撑的刚性转子的非线性旋转动力性能的实验和数值研究。本文首次报道了静电载荷可以导致转子-GFB系统中高副同步运动的有趣现象。测量并讨论了静止和不平衡负荷对海岸下降测试,同步响应幅度,峰值响应频率,外观的外观振动和海岸向下响应时间范围的影响。导出基于有限元和非稳态雷诺等式的圈动力学模型来预测系统的非线性响应。箔结构和气膜串联被认为是导出不稳定的轴承力。预测与测试数据一致。讨论了静态或不平衡负载和非线性响应之间的关系,尤其是副同步频率的振动。在数值模拟中,随着静态和不平衡负荷的增加,振动分量主要从主要同步变化,然后返回同步振动。当静态和不平衡负载变化时,转子-GFB系统的固有频率可以与典型因子,A. = 0.5的旋转振动的阈值转移或远离旋转振动的阈值,并导致严重的子同步振动。实验数据和理论预测有助于高性能微型涡轮机的工程设计和实现GFBS。

著录项

  • 来源
    《Mechanical systems and signal processing》 |2019年第1期|106271.1-106271.22|共22页
  • 作者单位

    College of Pecroleum and Engineering Yangtze University Wuhan 430072 PR China The State Key Laboratory of Advanced Design and Manufacturing for Vehicle Body Hunan University Changsha 410082 PR China;

    The State Key Laboratory of Advanced Design and Manufacturing for Vehicle Body Hunan University Changsha 410082 PR China;

    The State Key Laboratory of Advanced Design and Manufacturing for Vehicle Body Hunan University Changsha 410082 PR China;

    The State Key Laboratory of Advanced Design and Manufacturing for Vehicle Body Hunan University Changsha 410082 PR China;

    College of Pecroleum and Engineering Yangtze University Wuhan 430072 PR China;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Gas foil bearings; Nonlinear rotordynamics; Static and imbalance loads; Sub-synchronous vibrations;

    机译:燃气箔轴承;非线性旋转性能;静态和不平衡负荷;子同步振动;

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