Flight demonstration of aircraft wing monitoring using optical fiber distributed sensing system
- 5 April 2019
- journal article
- research article
- Published by IOP Publishing in Smart Materials and Structures
- Vol. 28 (5) , 055007
Abstract
We conduct flight demonstrations of aircraft monitoring by using optical fiber distributed sensing technique. We monitor a main wing of a flying test bed that is a middle-sized passenger jet. We use optical frequency domain reflectometry and long-length fiber Bragg gratings (FBGs). The sensing system measures the strain distribution profile within the FBGs with a mm order spatial resolution in real-time. Thanks to the high spatial resolution, we could observe local strain distributions due to the ribs of the wing. We also monitored strain distribution variations corresponding to various maneuvers during flight. We discussed the correlation with flight maneuvers and the interpretation of the monitoring data.Keywords
This publication has 14 references indexed in Scilit:
- Applications of Brillouin Dynamic Grating to Distributed Fiber SensorsJournal of Lightwave Technology, 2016
- [INVITED] State of the art of Brillouin fiber-optic distributed sensingOptics & Laser Technology, 2016
- Aircraft health and usage monitoring system for in-flight strain measurement of a wing structureSmart Materials and Structures, 2015
- High resolution, high sensitivity, dynamic distributed structural monitoring using optical frequency domain reflectometry2013
- Recent Progress in Distributed Fiber Optic SensorsSensors, 2012
- Proposal and experimental verification of Bragg wavelength distribution measurement within a long-length FBG by synthesis of optical coherence functionOptics Express, 2008
- Distributed Measurements with a Long Gauge FBG Sensor Using Optical Frequency Domain Reflectometry (1st Report, System Investigation Using Optical Simulation Model)Journal of Solid Mechanics and Materials Engineering, 2008
- High-spatial-resolution distributed strain measurement in optical fiber with Rayleigh scatterApplied Optics, 1998
- Fiber grating sensorsJournal of Lightwave Technology, 1997
- HIGH SPEED, IN-FLIGHT STRUCTURAL HEALTH MONITORING SYSTEM FOR MEDIUM ALTITUDE LONG ENDURANCE UNMANNED AIR VEHICLE