DocumentCode :
2340038
Title :
Optical semiconductor blade vibration monitoring system for gas turbine engine
Author :
Kawasima, T. ; Iinuma, H. ; Minagawa, N.
Author_Institution :
Engine Design Dept., Ishikawajima-Harima Heavy Ind. Co. Ltd., Tokyo, Japan
fYear :
1994
fDate :
10-12 May 1994
Firstpage :
601
Abstract :
A low-cost optical blade vibration monitoring system was designed to measure the deflection of vibrating gas turbine rotor blade tips under engine running conditions. The basic principle of the new system is the use of low-cost semiconductors and shorter optical fiber bundles. This approach yields a simple and inexpensive system with much less hardware than required for former systems. The results of basic tests show that the new semiconductor system performs at the same level of accuracy and a better S/N level. The system has been applied on development engines to monitor fan blade, compressor blade, and also turbine blade vibration and proved its capability. The system is about one third cost of the former system and has better performance
Keywords :
fibre optic sensors; gas turbines; laser beam applications; semiconductor lasers; vibration measurement; blade vibration monitoring; compressor blade; cost; deflection; fan blade; gas turbine engine; low-cost semiconductors; optical fiber bundles; performance; turbine blade vibration; Blades; Condition monitoring; Engines; Hardware; Optical design; Optical fibers; Semiconductor device testing; System testing; Turbines; Vibration measurement;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation and Measurement Technology Conference, 1994. IMTC/94. Conference Proceedings. 10th Anniversary. Advanced Technologies in I & M., 1994 IEEE
Conference_Location :
Hamamatsu
Print_ISBN :
0-7803-1880-3
Type :
conf
DOI :
10.1109/IMTC.1994.352026
Filename :
352026
Link To Document :
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