The Electrostatic Sensor Applied to the Online Monitoring Experiments of Combustor Carbon Deposition Fault in Aero-Engine

被引:19
作者
Liu Pengpeng [1 ]
Zuo Hongfu [2 ]
Sun Jianzhong [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Civil Aviat, Nanjing 210016, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, RMS Ctr, Nanjing 210016, Peoples R China
基金
美国国家科学基金会;
关键词
Aero engine; combustor; carbon deposition fault; electrostatic monitoring; fault detection; SOOT PARTICLES; 2-STAGE BURNER; EXHAUST;
D O I
10.1109/JSEN.2013.2284551
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
According to the principle of gas path electrostatic monitoring in aero-engine, it has established aero-engine gas path electrostatic monitoring system that can tolerate the high-temperature and high-speed airflow. There was developing the research about the mechanism of combustor carbon deposition and online electrostatic monitoring, the fault of combustor carbon deposition in aero engine. It was chose eight stages data from the large scale data of online electrostatic monitoring experiments and being based the time of checking the combustor in aero engine, comparably analyzing rms and Kurtosis being extracted from the data as features. In order to regain the accurate charge signal and discard certain trend item, it uses least mean square to finish the transforming process that is from electrostatic voltage to electrostatic charge. The changes of exhaust gas path electrostatic level illustrate by the features, including active level, positive event rate, and negative event rate extracted from the electrostatic charge signal. It responds for the fault of combustor carbon deposition in aero-engine as well as a slight ablation fault in testing process by the features of electrostatic voltage and charge, respectively, which is being to verify the monitoring results by the report of the engine dismantled. The research of online electrostatic monitoring the fault of combustor carbon deposition in this paper would be the foundation to achieve the application of the technology in aircraft.
引用
收藏
页码:686 / 694
页数:9
相关论文
共 28 条
[1]  
[Anonymous], P GT2005 ASME TURB E
[2]  
[Anonymous], P ASME TURB EXP 2010
[3]  
[Anonymous], 2006, 2006 IEEE AER C BIG
[4]  
[Anonymous], 2006, 2006 IEEE AER C BIG
[5]   Characterization of Soot Deposition and Particle Nucleation in Exhaust Gas Recirculation Coolers [J].
Bika, Anil Singh ;
Warey, Alok ;
Long, David ;
Balestrino, Sandro ;
Szymkowicz, Patrick .
AEROSOL SCIENCE AND TECHNOLOGY, 2012, 46 (12) :1328-1336
[6]   Investigation of two-fluid methods for large eddy simulation of spray combustion in gas turbines [J].
Boileau, M. ;
Pascaud, S. ;
Riber, E. ;
Cuenot, B. ;
Gicquel, L. Y. M. ;
Poinsot, T. J. ;
Cazalens, M. .
FLOW TURBULENCE AND COMBUSTION, 2008, 80 (03) :291-321
[7]  
Chusen L., 2001, J CHIN SOC CORROSION, V21, P158
[8]   Soot Particle StudiesInstrument Inter-ComparisonProject Overview [J].
Cross, Eben S. ;
Onasch, Timothy B. ;
Ahern, Adam ;
Wrobel, William ;
Slowik, Jay G. ;
Olfert, Jason ;
Lack, Daniel A. ;
Massoli, Paola ;
Cappa, Christopher D. ;
Schwarz, Joshua P. ;
Spackman, J. Ryan ;
Fahey, David W. ;
Sedlacek, Arthur ;
Trimborn, Achim ;
Jayne, John T. ;
Freedman, Andrew ;
Williams, Leah R. ;
Ng, Nga L. ;
Mazzoleni, Claudio ;
Dubey, Manvendra ;
Brem, Benjamin ;
Kok, Greg ;
Subramanian, R. ;
Freitag, Steffen ;
Clarke, Antony ;
Thornhill, Dwight ;
Marr, Linsey C. ;
Kolb, Charles E. ;
Worsnop, Douglas R. ;
Davidovits, Paul .
AEROSOL SCIENCE AND TECHNOLOGY, 2010, 44 (08) :592-611
[9]   Burnout of soot particles in a two-stage burner with a JP-8 surrogate fuel [J].
Echavarria, Carlos A. ;
Jaramillo, Isabel C. ;
Sarofim, Adel F. ;
Lighty, JoAnn S. .
COMBUSTION AND FLAME, 2012, 159 (07) :2441-2448
[10]   Studies of soot oxidation and fragmentation in a two-stage burner under fuel-lean and fuel-rich conditions [J].
Echavarria, Carlos A. ;
Jaramillo, Isabel C. ;
Sarofim, Adel F. ;
Lighty, JoAnn S. .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2011, 33 :659-666