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某型航空涡扇发动机静电传感器机载化监测实验

殷逸冰 左洪福 付宇 刘宸宁 冒慧杰

殷逸冰, 左洪福, 付宇, 刘宸宁, 冒慧杰. 某型航空涡扇发动机静电传感器机载化监测实验[J]. 航空动力学报, 2016, 31(12): 3054-3063. doi: 10.13224/j.cnki.jasp.2016.12.030
引用本文: 殷逸冰, 左洪福, 付宇, 刘宸宁, 冒慧杰. 某型航空涡扇发动机静电传感器机载化监测实验[J]. 航空动力学报, 2016, 31(12): 3054-3063. doi: 10.13224/j.cnki.jasp.2016.12.030
YIN Yi-bing, ZUO Hong-fu, FU Yu, LIU Chen-ning, MAO Hui-jie. Experiment on electrostatic sensors airborne monitoring of a turbofan aero-engine[J]. Journal of Aerospace Power, 2016, 31(12): 3054-3063. doi: 10.13224/j.cnki.jasp.2016.12.030
Citation: YIN Yi-bing, ZUO Hong-fu, FU Yu, LIU Chen-ning, MAO Hui-jie. Experiment on electrostatic sensors airborne monitoring of a turbofan aero-engine[J]. Journal of Aerospace Power, 2016, 31(12): 3054-3063. doi: 10.13224/j.cnki.jasp.2016.12.030

某型航空涡扇发动机静电传感器机载化监测实验

doi: 10.13224/j.cnki.jasp.2016.12.030
基金项目: 

国家自然科学基金与中国民航联合资助基金重点项目(60939003);国家自然科学基金(61179056);航空科学基金(2013ZB52029)

详细信息
    作者简介:

    殷逸冰(1992-),男,安徽宣城人,博士生,主要从事航空发动机状态监控及故障诊断方面的研究.

  • 中图分类号: V231.25

Experiment on electrostatic sensors airborne monitoring of a turbofan aero-engine

  • 摘要: 计了一种特定尺寸的静电传感器,并将其装配在涡扇发动机低压涡轮出口附近的尾喷管管壁,以民用涡扇发动机为静电传感器载体及监测对象开展静电监测实验.以一个完整性能试车过程为周期,采集周期内的尾气静电信号.进一步对静电信号和发动机性能参数进行数据对比分析,同时对测试过程中异常状态下活动率水平(AL)和负事件率(NER)进行计算.实验验证了航空发动机静电监测技术具备机载化的可行性,实验结果表明:正常状态下静电信号电压幅值大小约为5mV,静电水平跟随运行功率变化并呈正相关性;静电传感器对尾气中存在的异常颗粒具有良好的监测效果,在发动机富油状态下静电信号的活动率水平和负事件率分别达到14pC及8%.

     

  • [1] Powrie H E G,Mcnicholas K.Gas path condition moni-toring during accelerated mission testing of a demonstrator engine[R].Seattle,WA:The 33rd AIAA/ ASME / SAE/ASEE Joint Propulsion Conference and Exhibit,1997.
    [2] Powrie H E G,Fisher C E.Monitoring of foreign objects ingested into the intake of a gas turbine aero-engine[R].Swansea,UK:International Conference on Condition Monitoring,1999.
    [3] Navarra K,Lawton R,Hearrell N.An enterprise strategy for implementing conditioned-based maintenance plus (CBM+) research in the USAF[R].Big Sky,MT:IEEE Aerospace Conference,1997.
    [4] Sangha M S,Yu D L,Gomm J B.On-board monitoring and diagnosis for spark ignition engine air path via adaptive neural networks[J].Journal of Automobile Engineering,2006,220(11):1641-1655.
    [5] Powrie H E G,Fisher C E.Engine health monitoring:towards total prognostics[R].Big Sky,MT:IEEE Aerospace Conference,1999.
    [6] Powrie H E G,Fisher C E.Monitoring of foreign objects into the intake of a gas turbine aero-engine[R].Big Sky,MT:IEEE Aerospace Conference,1999.
    [7] Fisher C E.Gas path debris monitoring:a 21st century PHM tool[R].Big Sky,MT:IEEE Aerospace Conference,2000.
    [8] Fisher C E.Gas turbine condition monitoring systems:an integrated approach[R].Big Sky,MT:IEEE Aerospace Conference,2000.
    [9] Fisher C E.Data and information fusion for gas path debris monitoring[R].Big Sky,MT:IEEE Aerospace Conference,2001.
    [10] Novis A,Powrie H E G.PHM Sensor implementation in the real world:a status report[R].Big Sky,MT:IEEE Aerospace Conference,2001.
    [11] Powrie H E G,Novis A.Gas path debris monitoring for F-35 joint strike fighter propulsion system PHM[R].Big Sky,MT:IEEE Aerospace Conference,2006.
    [12] 文振华,左洪福,李耀华,等.一种新的航空发动机气路监测方法[J].南京航空航天大学学报,2009,41(2):248-252. WEN Zhenhua,ZUO Hongfu,LI Yaohua,et al.New method for aero engine gas path monitoring[J].Journal of Nanjing University of Aeronautics and Astronautics,2009,41(2):248-252.(in Chinese)
    [13] 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. WEN Zhenhua,ZUO Hongfu,LI Yaohua.Gas path debris electrostatic monitoring technology and experiment[J].Journal of Aerospace Power,2008,23(12):2321-2326.(in Chinese)
    [14] 文振华.基于静电感应的航空发动机气路监测技术研究[D].南京:南京航空航天大学,2009. WEN Zhenhua.Aero-engine gas path monitoring technology based on electrostatic induction[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2009.(in Chinese)
    [15] 刘鹏鹏,左洪福,付宇,等.涡喷发动机尾气静电监测及气路故障特征[J].航空动力学报,2013,28(2):473-480. LIU Pengpeng,ZUO Hongfu,FU Yu,et al.Exhaust gas electrostatic monitoring and gas path fault feature for turbojet engine[J].Journal of Aerospace Power,2013,28(2):473-480.(in Chinese)
    [16] 李耀华,左洪福,文振华,等.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. LI Yaohua,ZUO Hongfu,WEN Zhenhua,et al.Simulated experiment of aircraft engine gas path debris monitoring technology[J].Acta Aeronautica et Astronautica Sinica,2009,30(4):604-608.(in Chinese)
    [17] 李耀华,左洪福.碰摩故障静电监测方法及模拟实验[J].航空学报,2010,31(6):1156-1163. LI Yaohua,ZUO Hongfu.Method for rub fault detection based on electrostatic technique:model and simulated experiment[J].Acta Aeronautica et Astronautica Sinica,2010,31(6):1156-1163.(in Chinese)
    [18] Fu Y,Zuo H F.Recognition for change-point of aero-engine components based on projective transformation[J].Information Technology Journal,2014,13(2):347-352.
    [19] Fu Y,Zuo H F.Mean change-point model for aero-engine component faults[J].Journal of Vibroengineering,2013,15(4):1627-1633.
    [20] 文振华,左洪福,王华,等.航空发动机气路静电监测传感器特性[J].传感器与微系统,2008,27(11):28-31. WEN Zhenhua,ZUO Hongfu,WANG Hua,et al.Characters of sensor for aero-engine gas path electrostatic monitoring[J].Transducer and Microsystem Technologies,2008,27(11):28-31.(in Chinese)
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出版历程
  • 收稿日期:  2015-03-12
  • 刊出日期:  2016-12-28

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