DocumentCode
1881508
Title
Optical fiber bragg grating sensors applied to gas turbine engine instrumentation and monitoring
Author
Wild, G.
Author_Institution
Sch. of Aerosp., Mech., & Manuf. Eng., RMIT Univ., Melbourne, VIC, Australia
fYear
2013
fDate
19-21 Feb. 2013
Firstpage
188
Lastpage
192
Abstract
Optical fiber systems are becoming more prevalent in both commercial and military aircraft, finding applications in niche area where the properties of optical fibers are essential. However, the application of optical fibers to all aircraft systems, in particular fly-by-light, is of significant interest. In this work, an integrated engine instrumentation and monitoring system based on optical fiber Bragg grating sensors is proposed. Engine instrumentation and monitoring requires a number of different sensors, including temperature, pressure, RPM, and vibration. All four of these measurands can be monitored using FBGs, multiplexed together using the same interrogation system. Results for all of these measurands are presented, including proposed transducers for both pressure and vibration. In addition, the overall optical fiber monitoring system is proposed.
Keywords
Bragg gratings; aerospace engines; condition monitoring; fibre optic sensors; gas turbines; transducers; vibrations; RPM; aircraft systems; commercial aircraft; fly-by-light; gas turbine engine instrumentation; gas turbine engine monitoring; integrated engine instrumentation-monitoring system; interrogation system; military aircraft; optical fiber bragg grating sensors; optical fiber monitoring system; optical fiber systems; transducers; vibration; Fiber gratings; Optical fiber sensors; Strain; Temperature measurement; Temperature sensors; engine instrumentation; fiber Bragg grating; gas turbine; health and usage monitoring;
fLanguage
English
Publisher
ieee
Conference_Titel
Sensors Applications Symposium (SAS), 2013 IEEE
Conference_Location
Galveston, TX
Print_ISBN
978-1-4673-4636-8
Type
conf
DOI
10.1109/SAS.2013.6493583
Filename
6493583
Link To Document