3POWRIE H E G, MCNICHOLAS K. Gas path cognition monitoring during accelerated mission testing of a demon- strator engine [ R ]. A1AA-1997-2904,1997.
4POWRIE H E G, FISHER C E. Engine health monitoring: towards total prognostics [ C ]. IEEE Aerospace Conference Proceedings, 1999,3 : 11-20.
5CHUPP R E, GHASRIPOOR F, MOORE C D, et al. Ap-plying abradable seals to industrial gas turbines [ C ]. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, USA ,2002,7:7-10.
6ZHAO H, BARBER G C, LIU J. Friction and wear in high speed sliding with and without electrical current [ J ]. Wear,2001,249(5-6 ) :409-414.
7NOVIS A,POWR1E H E G. PHM sensors implementation in the real world-a status report [ C ]. IEEE Aerospace Conference Proceeding, 2006.
8MORRIS S,WOOD R J K,HARVEY T J,et al. Use of electrostatic charge monitoring for early detection of adhe- sive wear in oil lubricated contacts[J]. Journal of Tribal- ogy, 2002,124 ( 2 ) : 288-296.
9WEN ZH H,ZUO H F,PECHT M G. Electrostatic moni- toring of gas path debris for aero-engine [ J ]. IEEE Trans- action on reliability ,2011,60( 1 ) :33-40.
10WILCOX M, RANSOM D. Engine distress detection in gas turbines with electrostatic: sensors [ C ]. Proceedings of ASME Turbo Expo 2010: Power for land, sea and Air. GT2010, Glasgow, UK, 2010.