期刊文献+

基于STFT的缝翼滑轨故障静电监测技术的研究 被引量:3

Study on electrostatic monitoring of slat rail based on STFT
下载PDF
导出
摘要 针对飞机缝翼运动机构需要实时监测的要求,提出了一种新的能够提前预警故障的方法,即基于静电感应的状态监测方法。分析了静电监测的原理,并通过模拟实验对该方法进行了初步的研究。实验结果表明:静电传感器能够有效地监测到故障的静电荷水平变化,验证了此传感器用于缝翼滑轨模拟试验件监测的有效性。介绍了短时傅里叶变换(STFT)时频分析原理,利用STFT对数据进行处理,分析其特性,为进一步研究机载化缝翼滑轨的静电监测设备提供了一定的依据。 Aiming at the demend for real time monitoring of aircraft slat rail, a new method which based on electrostatic induction of condition monitoring method of early warning of fault is proposed. The foundational principle of electrostatic monitoring method is analyzed, the preliminary experiment research on electrostatic monitoring method is carried out. The result of the experiment shows that the electrostatic sensor can effectively detect changes in the electrostatic charge level due to fault, indicating availability of the application of electrostatic in the model of slat rail. The theory of short-time Fourier transform(STFT) is introduced. STFT is used to process the data, and its characteristics is analyzed. It provides a further research of airborne slat rail monitoring equipment.
出处 《传感器与微系统》 CSCD 北大核心 2011年第9期15-17,共3页 Transducer and Microsystem Technologies
基金 国家自然科学基金与中国民航总局联合资助基金重点项目(60939003)
关键词 缝翼滑轨 静电传感器 短时傅里叶变换 slat rail electrostatic sensor short-time Fourier transform(STFF)
  • 相关文献

参考文献2

二级参考文献22

  • 1YAN Yong. Mass flow measurement of bulk solids in pneumatic pipeline [J]. Measurement Science and Technology, 1996, 7(12): 1687-1706.
  • 2MA J, YAN Yong. Design and evaluation of electrostatic sensors for the measurement of velocity of pneumatically conveyed solids [J]. Flow Measurement and Instrumentation, 2000, 11(3): 195-204.
  • 3SOROKIN A, ARNOLD F. Electrically charged small soot particles in the exhaust of an aircraft gas-turbine engine combustor: comparison of model and experiment[J]. Atmospheric Environment, 2004, 38(17): 2611-2618.
  • 4WILHELM S, HAVERKAMP H, SOROKIN A, ARNOLD F. Detection of very large ions in aircraft gas turbine engine combustor exhaust: charged small soot particles? [J]. Atmospheric Environment, 2004,38(27): 4561-4569.
  • 5HAVERKAMP H, WILHELM S, SOROKIN A, ARNOLD F. Positive and negative ion measurements in jet aircraft engine exhaust: concentrations, sizes and implications for aerosol formation [J]. Atmospheric Environment, 2004, 38(18): 2879-2884.
  • 6POWRIE H E G, MCNICHOLAS K. Gas path condition monitoring during accelerated mission testing of a demonstrator engine[C]// The 33rd AIAA/ASME / SAE/ASEE Joint Propulsion Conference and Exhibit Seattle. WA, USA: AIAA, 1997: 2904-2914.
  • 7FISHER C E. Gas path debris monitoring-a 21st century PHM tool [C]// Aerospace Conference Proceedings, 2000 IEEE, Montana, USA, 2000, 6: 441-448.
  • 8POWRIE H, NOVIS A. Gas path debris monitoring for F-35 joint strike fighter propulsion system PHM[C]// Aerospace Conference Proceedings, 2006 IEEE Montana, USA, 2006, 11: 1-8.
  • 9N E Huang, Z Shen, S R Long, et al. The empirical mode decomposition and the Hilbert spectrum for nonlinear and non-stationary time series analysis, Proc Roy Soc , London A,1998, 454, 903-995.
  • 10B Boashash, Estimating and interpreting the instantaneous frequency of a signal, Part Ⅰ: Fundamentals, Proc IEEE, 1992, 80(4), 520-538.

共引文献34

同被引文献11

引证文献3

二级引证文献4

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部