磁悬浮流体机械喘振控制研究
DOI:
CSTR:
作者:
作者单位:

1.常州大学;2.南京航空航天大学

作者简介:

通讯作者:

中图分类号:

基金项目:

国家自然科学基金项目(面上项目,重点项目,重大项目);


Surge control of magnetic suspension fluid machinery
Author:
Affiliation:

1.Changzhou University;2.Nanjing University of Aeronautics and Astronautics

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    针对磁悬浮流体机械喘振问题,依据流体机械系统喘振状态时质量流量和压升的波动,采用基于质量流量的喘振控制策略。具体来说,利用喘振控制器求出叶轮轴向调节间隙值,并作为悬浮位置参考信号输入到轴向磁悬浮轴承闭环控制系统中,从而在轴向磁悬浮轴承系统作动下改变磁悬浮流体机械转子轴向位置,即改变叶轮叶尖间隙,以实现喘振的主动控制。仿真结果表明,当施加喘振控制时,可以扩展流体机械的稳定运行范围,由未控制下的15.5%节流阀开度扩展至喘振控制下的14%。通过模拟激振的方式辨识了喘振频率,并研究了PID控制器中控制参数对喘振控制性能的影响规律。该方法具有控制简单、无需外加硬件、无效率损失等优点。

    Abstract:

    Aiming at the surge problem of magnetic suspension fluid machinery, according to the fluctuation of mass flow and pressure rise in the surge State of fluid machinery system, a surge control strategy based on mass flow is adopted. The surge controller obtains the axial adjustment clearance value of the impeller and inputs it into the closed-loop control system of the axial magnetic bearing as the suspension position reference signal, so as to change the axial position of the magnetic levitation fluid machinery rotor under the action of the axial magnetic bearing system, that is, change the blade tip clearance of the impeller, so as to realize the active control of surge. The simulation results show that when surge control is applied, the stable operation range of fluid machinery can be extended from 15.5% throttle opening under uncontrolled to 14% under surge control. The surge frequency is identified by simulating the excitation, and the influence of the control parameters in the PID controller on the surge control performance is studied. This method has the advantages of simple control, no additional hardware and no efficiency loss.

    参考文献
    相似文献
    引证文献
引用本文
分享
相关视频

文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2021-09-24
  • 最后修改日期:2022-03-07
  • 录用日期:2022-03-08
  • 在线发布日期:
  • 出版日期:
文章二维码
您是第位访问者
振动工程学报 ® 2026 版权所有
技术支持:北京勤云科技发展有限公司