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航空发动机尾气静电信号基线模型分析及应用

孙见忠 左洪福 刘鹏鹏 余有锋 陈志雄

孙见忠, 左洪福, 刘鹏鹏, 余有锋, 陈志雄. 航空发动机尾气静电信号基线模型分析及应用[J]. 航空动力学报, 2013, 28(3): 531-540.
引用本文: 孙见忠, 左洪福, 刘鹏鹏, 余有锋, 陈志雄. 航空发动机尾气静电信号基线模型分析及应用[J]. 航空动力学报, 2013, 28(3): 531-540.
SUN Jian-zhong, ZUO Hong-fu, LIU Peng-peng, YU You-feng, CHEN Zhi-xiong. Analysis and application of baseline model of aero-engine exhaust gas electrostatic monitoring signals[J]. Journal of Aerospace Power, 2013, 28(3): 531-540.
Citation: SUN Jian-zhong, ZUO Hong-fu, LIU Peng-peng, YU You-feng, CHEN Zhi-xiong. Analysis and application of baseline model of aero-engine exhaust gas electrostatic monitoring signals[J]. Journal of Aerospace Power, 2013, 28(3): 531-540.

航空发动机尾气静电信号基线模型分析及应用

基金项目: 国家自然科学基金与中国民航联合基金重点项目(60939003);江苏省普通高校研究生科研创新计划(CXLX12_0164)

Analysis and application of baseline model of aero-engine exhaust gas electrostatic monitoring signals

  • 摘要: 开展了基于尾气静电信号的航空发动机气路监控技术的应用研究,把尾气静电监测信号EGEMS作为一种新的气路状态参数并建立其基线模型,通过监控尾气静电信号RMS(root mean square)值的偏差值实现对气路部件的实时监控.首先从尾气静电监测的角度总结了尾气碳烟颗粒物的排放特性,分析了尾气静电信号的基线成分、主要影响因素及典型故障静电信号特征,在此基础上分别提出了基于燃油流量单参数的尾气静电信号基线模型(参数化模型)和基于多元状态估计技术的多参数基线模型(非参数化模型)挖掘技术.通过对某型涡轴发动机尾气静电信号的分析表明:所建立的基线模型能够准确反映发动机不同工况下的尾气静电信号的基本特征,有效地监测到气路的异常状态,验证了所提方法的可行性和有效性.

     

  • [1] 陈卫,程礼,李全通,等.航空发动机监控技术[M].北京:国防工业出版社,2011.
    [2] Honor P,Novis A.Gas path debris monitoring for F-35 Joint Strike Fighter propulsion system PHM[R].Big Sky,MT:IEEE Aerospace Conference Proceedings,2006.
    [3] Couch R P,Rossback D R,Burgess R W,et al.Sensing incipient engine failure with electrostatic probes[C]//Instrumentation for Airbreathing Propulsion,Proceeding of the Symposium.Seattle WA,USA:AIAA,1972:519-529.
    [4] Powrie H E G,Mcnicholas K.Gas path condition monitoring during accelerated mission testing of a demonstrator engine[R].AIAA-97-2904,1997.
    [5] Fisher C E.Gas turbine condition monitoring systems:an integrated approach[R].Big Sky,MT IEEE Aerospace Conference Proceedings,2000.
    [6] Fisher C E.Gas path debris monitoring:a 21st century PHM tool[R].Big Sky,MT IEEE Aerospace Conference Proceedings,2000.
    [7] 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)
    [8] 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)
    [9] 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. LI Yaohua, ZUO Hongfu, LIU Pengpeng. Gas path electrostatic monitoring of turbo-shaft engine: an exploratory experiment[J].Acta Aeronautica et Astronautica Sinica,2010,31(11):2174-2181. (in Chinese)
    [10] 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 experiments[J].Acta Aeronautica et Astronautica Sinica, 2010,31(6):1156-1163. (in Chinese)
    [11] 孙见忠,左洪福,詹志娟,等.涡轴发动机尾气静电信号影响因素分析[J].航空学报,2012,33(3):412-420. SUN Jianzhong, ZUO Hongfu, ZHAN Zhijuan, et al. Analysis of the influencing factors on the exhaust gas electrostatic monitoring signal of a turbo-shaft engine[J].Acta Aeronautica et Astronautica Sinica, 2012, 33(3):412-420. (in Chinese)
    [12] 金如山.航空燃气轮机燃烧室[M].北京:宇航出版社,1988.
    [13] Lefebvre A H.Gas turbine combustion[M].Washington: Hemisphere Pub.Corp.,1983.
    [14] Wey C C,Anderson B E,Hudgins C,et al.Aircraft particle emissions experiment (APEX)[R].NASA/TM-2006-214382,2006.
    [15] Kinsey J S.Characterization of emissions from commercial aircraft engines during the aircraft particle emissions experiment (APEX) 1 to 3[R].EPA-600/R-091/130,2009.
    [16] Kinsey J,Dong Y,Williams D C,et al.Physical characterization of the aircraft particle emissions from commercial aircraft engines during the [JP+1]aircraft particle emissions experiment (APEX) 1-3[J].Atmospheric Environment,2010,44(7):2147-2156.
    [17] 陈锐,周彤,顾铭企.某型发动机主燃烧室积炭的排除[J].航空发动机,1996(3):16-20. CHEN Rui,ZHOU Tong,GU Mingqi.Remove of the carbon deposit in the combustion chamber of some aeroengine[J].Aeroengine,1996(3):16-20. (in Chinese)
    [18] 姚四伟,张力先,霍岩.发动机燃烧室部件故障的分析与预防[J].西安航空技术高等专科学校学报,2008,26(1):18-20. YAO Siwei,ZHANG Lixian,HUO Yan.Analysis and prevention on malfunctions of engine combustion chamber parts[J].Journal of Xian Aerotechnical College,2008,26(1):18-20.(in Chinese)
    [19] Hines J W,Garvey D,Seibert R,et al.Technical review of on-line monitoring techniques for performance assessment:Volume 2 theoretical issues[R].Washington DC,US:Nuclear Regulatory Commission,NUREG/CR-6895,2007.
    [20] Hines J W,Usynin A.MSET performance optimization through regularization[J].Nuclear Engineering and Technology,2005,38(2):356-362.
    [21] Hines J W,Garvey D.Traditional and robust vector selection methods for use with similarity based models[R].Albuquerque,MN:5th International Topical Meeting on Nuclear Plant Instrumentation,Control and Human-Machine Interface Technologies,2006.
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出版历程
  • 收稿日期:  2012-03-25
  • 刊出日期:  2013-03-28

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