期刊文献+

涡轴发动机尾气静电监测信号影响因素分析 被引量:18

Analysis of Factors Influencing the Exhaust Gas Electrostatic Monitoring Signals of a Turbo-shaft Engine
原文传递
导出
摘要 针对某型航空涡轴发动机试车台实验所获得的尾气静电监测信号,结合发动机台架试车状态和性能数据,分别在两个时间尺度上展开分析研究。研究发现发动机的工作状态和健康状态均对尾气静电信号产生重要影响。在小时间尺度上的分析发现,无故障情况下影响尾气静电信号变化的主要因素为燃油供给量,尾气静电信号能量随燃油供给量的增加近似按指数规律上升;而在大时间尺度上的分析发现,在一定的燃油供给和恒定的自由涡轮转速条件下,尾气静电信号能量随着发动机性能的缓慢衰退而逐渐上升。实测尾气静电信号所反映的趋势与初步的理论分析结果相一致,为建立涡轴发动机尾气静电信号的健康"基线",进而用于气路状态监测及故障识别提供了初步的依据。研究还发现,静电监测技术不仅能够为突发性故障提供预警信息,而且能够反映发动机整机性能衰退,进一步拓展了静电传感器的监测能力及其在航空发动机健康管理中的应用。 Based on the exhaust gas electrostatic monitoring signals of a turbo-shaft engine,an analytical study is carried out in combination with other engine operating parameters on two time scales.The results presented in this study show that both the engine operating condition and health status have a significant effect on the monitored exhaust gas electrostatic signal.On the small time scale,for an engine without fault the major factor that may cause change in the electrostatic signal is fuel delivery,and the energy of the signal will increase almost exponentially with more fuel feed.On the large time scale,given a constant fuel delivery and power shaft speed,the energy of the exhaust gas electrostatic signal will increase as the engine deteriorates gradually.The trend extracted from the monitored signal is in agreement with the theoretical analysis,which may serve as an initial basis for the establishment of a base line in the electrostatic signal,and in turn facilitate further application,such as to gas path component condition monitoring and fault identification.The research also demonstrates that the electrostatic monitoring technique can not only provide a precursor for the impending fault,but also track the gradual performance degradation for a turbo-shaft engine,and this may mean an extension of the capacity and application of the electrostatic monitoring sensor in engine health management.
出处 《航空学报》 EI CAS CSCD 北大核心 2012年第3期412-420,共9页 Acta Aeronautica et Astronautica Sinica
基金 国家自然科学基金与中国民航联合资助基金重点项目(60939003)~~
关键词 静电 监测 性能衰退 发动机健康管理 气路分析 涡轴发动机 electrostatics monitoring performance deterioration engine health management gas path analysis turbo-shaft engine
  • 相关文献

参考文献11

  • 1Couch R P,Rossback D R,Burgess R W,et al.Sensingincipient engine failure with electrostatic probes.Instru-mentation for Airbreathing Propulsion,Proceeding of theSymposium.1972:519-529.
  • 2Cartwright R A,Fisher C.Marine gas turbine conditionmonitoring by gas path electrostatic detection techniques.International Gas Turbine and Aero-engine Congress andExposition.1991.
  • 3Powrie H E G,Mcnicholas K.Gas path condition monito-ring during accelerated mission testing of a demonstratorengine.AIAA-1997-2904,1997.
  • 4Powrie H E G,Novis A.Gas path debris monitoring forF-35joint strike fighter propulsion system PHM.IEEEAerospace Conference Proceedings.2006.
  • 5文振华,左洪福,李耀华.气路颗粒静电监测技术及实验[J].航空动力学报,2008,23(12):2321-2326. 被引量:32
  • 6李耀华,左洪福,文振华.航空发动机气路颗粒静电监测技术模拟实验[J].航空学报,2009,30(4):604-608. 被引量:25
  • 7李耀华,左洪福,刘鹏鹏.某型航空涡轮轴发动机尾气静电监测探索性实验[J].航空学报,2010,31(11):2174-2181. 被引量:20
  • 8Sorokin A,Arnold F.Electrically charged small soot par-ticles in the exhaust of an air craft gas turbine engine com-bustor:comparison of model and experiment.Atmosphe-ric Environment,2004,38(17):2611-2618.
  • 9Lefebvre A H.Gas turbine combustion.Washington D.C.:Hemisphere Publishing Corporation,1983.
  • 10Dopelheuer A,Lecht M.Influence of engine performance on emissions characteristics.Symposium of the Applied Vehicle Technology Pane-gas Turbine Engine Combus-tion,Emissions and Alternative Fuels.1998.

二级参考文献30

  • 1牛培峰,张君.小波分析技术在汽轮机故障诊断中的应用[J].动力工程,2007,27(1):76-80. 被引量:21
  • 2Powrie H E G,Mcnicholas K. Gas path condition monito ring 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
  • 3Powrie H E G, Fisher C E. Engine health monitoring: towards total prognostics[C]// IEEE Aerospace Applications Conference Proceedings. CA, USA: IEEE, 1999 (3) : 11-20.
  • 4Fisher C E. Gas path debris monitoring-A 21st century PHM tool [C]//IEEE Aerospace Conference Proceedings. Montana, USA : IEEE , 2000,6 : 441-448.
  • 5Powrie H , Novis A. Gas path debris monitoring for F-35 joint strike fighter propulsion system PHM[C]//Proceedings of IEEE Aerospace Conference. Montana, USA: IEEE ,2006(2) : 1-8.
  • 6Novis A, Powrie H. PHM sensor implementation in the real world-a status report[C]//Proceedings of IEEE Aerospace Conference. Montana,USA,IEEE, 2006(3) t 1-9.
  • 7Sorokin 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) : 2611-2618.
  • 8徐长发,李国宽.实用小波分析方法[M].武汉:华中科技大学出版社,2005.
  • 9Couch R P, Rossback D R, Burgess R W, et al. Sensing incipient engine failure with electrostatic probes[C]//Instrumentation for Airbreathing Propulsion, Proceedings of the Symposium. 1972:515 529.
  • 10Couch R P. Detecting abnormal turbine engine deterioration using electrostatic methods[J]. Journal of Aircraft, 1978, 15(10):692 -696.

共引文献47

同被引文献209

引证文献18

二级引证文献91

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