A monitoring experiment for gas path electrostatic probe-type sensor on turbojet engine

Information Technology Journal

Volumn 12, Issue 2, 2013, Pages 331-337

  Fu, Yu ^a   Zuo, Hongfu ^a   Wang, Ruiming ^a   Liu, Pengpeng ^a   Cai, Jing ^a   Wen, Zhenhua ^b  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

^b ZHENGZHOU INSTITUTE OF AERONAUTICAL INDUSTRY MANAGEMENT   (China)

Author keywords

Carbon fault; Condition based maintenance; Electrostatic signal; Exhaust monitoring; Gas path; Probe type sensor; Turbojet engine

Indexed keywords

CARBON DEPOSITION; CONDITION BASED MAINTENANCE; EARLY WARNING; ELECTROSTATIC SENSOR; EXHAUST PARTICLES; FUEL SPRAYS; GAS PATH; INITIAL FAULTS; MEASURED SIGNALS; REAL TIME MONITORING;

CARBON; ELECTROSTATIC DEVICES; ELECTROSTATICS; EXHAUST SYSTEMS (ENGINE); EXPERIMENTS; MAINTENANCE; PROBES; SENSORS; TURBOJET ENGINES;

CONDITION MONITORING;

EID: 84872180521     PISSN: 18125638     EISSN: 18125646     Source Type: Journal    
DOI: 10.3923/itj.2013.331.337     Document Type: Article

References (11)

1. Couch, R.P., 1978. Detecting abnormal turbine engine deterioration using electrostatic methods. J. Aircraft, 15: 692-695.
2. Hua, W., 2009. Sensing Analysis and Application Research of Gas Path Electrostatic Sensor. Nanjing University of Aeronautics and Astronautics Publishing House, Nanjing, China.
3. Li, Y., H. Zuo and Z. Wen, 2009. Simulated experiment of aircraft engine gas path debris monitoring technology. Acta Aeronaut. Astronaut. Sin., 30: 604-608.
4. Powrie, H. and A. Novis, 2006. Gas path debris monitoring for F-35 joint strike fighter propulsion system PHM. Proceedings of the IEEE Aerospace Conference, March 4-11, 2006, Big Sky, USA
5. Roemer, M. J., G. J. Kacprzynski and M.H. Schoeller, 2001. Improved diagnostic and prognostic assessments using health management information fusion. Proceedings of IEEE Systems Readiness Technology Conference, August 20-23, 2001, Valley Forge, PA, USA., pp: 365-377. (Pubitemid 34658124)
6. Sorokin, A. and F. Arnold, 2004. Electrically charged small soot particles in the exhaust of an aircraft gas-turbine engine combustor: Comparison of model and experiment. Atmos. Environ., 38: 2611-2618. (Pubitemid 38507377)
7. Wei, F. and Y. Chuanjun, 2005. Combustion Science. Northwestern Polytechnical University Publishing House, Xi'an, China.
8. Wen, Z., H. Zuo, D.K. Lau and M.G. Pecht, 2010. Research on electrostatic monitoring technology for aeroengine gas path. Proceedings of the Prognostics and Health Management Conference, January 12-14, 2010, Macao, pp: 1-5.
9. Wilhelm, S., H. Haverkamp, A. Sorok and F. Arnold, 2004. Detection of very large ions in aircraft gas turbine engine combustor exhaust: Charged small soot particles. Atmos. Environ., 38: 4561-4569. (Pubitemid 38942755)
10. Yan, Y., B. Byrnet, S. Woodhead and J. Coulthard, 1995. Velocity measurement of pneumatically conveyed solids using electrodynamic sensors. Measure. Sci. Technol., 6: 515-537.
11. Yangming, G., C. Xiaobin and Z. Baozhen, 2008. Review of prognostics and health management technology. Comput. Meas. Control, 16: 1213-1216.