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Real-time Monitoring System of Composite Aircraft Wings Utilizing Fibre Bragg Grating Sensor

Embedment of Fibre Bragg Grating (FBG) sensor in composite aircraft wings leads to the advancement of structural condition monitoring. The monitored aircraft wings have the capability to give real-time response under critical loading circumstances. The main objective of this paper is to develop a re...

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Main Authors: Vorathin, E., Z. M., Hafizi, S. A., Che Ghani, K. S., Lim
Format: Conference or Workshop Item
Language:English
Published: IOP Publishing 2016
Subjects:
TJ Mechanical engineering and machinery
Online Access:http://umpir.ump.edu.my/id/eprint/15339/1/fkm-2016-vorathin-Real-time%20monitoring%20system%20of%20composite%20aircraft.pdf
http://umpir.ump.edu.my/id/eprint/15339/
http://dx.doi.org/10.1088/1757-899X/152/1/012024
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spelling my.ump.umpir.153392018-10-16T07:45:25Z http://umpir.ump.edu.my/id/eprint/15339/ Real-time Monitoring System of Composite Aircraft Wings Utilizing Fibre Bragg Grating Sensor Vorathin, E. Z. M., Hafizi S. A., Che Ghani K. S., Lim TJ Mechanical engineering and machinery Embedment of Fibre Bragg Grating (FBG) sensor in composite aircraft wings leads to the advancement of structural condition monitoring. The monitored aircraft wings have the capability to give real-time response under critical loading circumstances. The main objective of this paper is to develop a real-time FBG monitoring system for composite aircraft wings to view real-time changes when the structure undergoes some static loadings and dynamic impact. The implementation of matched edge filter FBG interrogation system to convert wavelength variations to strain readings shows that the structure is able to response instantly in real-time when undergoing few loadings and dynamic impact. This smart monitoring system is capable of updating the changes instantly in real-time and shows the weight induced on the composite aircraft wings instantly without any error. It also has a good agreement with acoustic emission (AE) sensor in the dynamic test. IOP Publishing 2016 Conference or Workshop Item PeerReviewed application/pdf en cc_by http://umpir.ump.edu.my/id/eprint/15339/1/fkm-2016-vorathin-Real-time%20monitoring%20system%20of%20composite%20aircraft.pdf Vorathin, E. and Z. M., Hafizi and S. A., Che Ghani and K. S., Lim (2016) Real-time Monitoring System of Composite Aircraft Wings Utilizing Fibre Bragg Grating Sensor. In: IOP Conference Series: Materials Science and Engineering, AEROTECH VI - Innovation in Aerospace Engineering and Technology, 8–9 November 2016 , Kuala Lumpur, Malaysia. pp. 1-9., 152 (012024). ISSN 1757-8981 (Print), 1757-899X (Online) http://dx.doi.org/10.1088/1757-899X/152/1/012024
institution Universiti Malaysia Pahang
building UMP Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Malaysia Pahang
content_source UMP Institutional Repository
url_provider http://umpir.ump.edu.my/
language English
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Vorathin, E.
Z. M., Hafizi
S. A., Che Ghani
K. S., Lim
Real-time Monitoring System of Composite Aircraft Wings Utilizing Fibre Bragg Grating Sensor
description Embedment of Fibre Bragg Grating (FBG) sensor in composite aircraft wings leads to the advancement of structural condition monitoring. The monitored aircraft wings have the capability to give real-time response under critical loading circumstances. The main objective of this paper is to develop a real-time FBG monitoring system for composite aircraft wings to view real-time changes when the structure undergoes some static loadings and dynamic impact. The implementation of matched edge filter FBG interrogation system to convert wavelength variations to strain readings shows that the structure is able to response instantly in real-time when undergoing few loadings and dynamic impact. This smart monitoring system is capable of updating the changes instantly in real-time and shows the weight induced on the composite aircraft wings instantly without any error. It also has a good agreement with acoustic emission (AE) sensor in the dynamic test.
format Conference or Workshop Item
author Vorathin, E.
Z. M., Hafizi
S. A., Che Ghani
K. S., Lim
author_facet Vorathin, E.
Z. M., Hafizi
S. A., Che Ghani
K. S., Lim
author_sort Vorathin, E.
title Real-time Monitoring System of Composite Aircraft Wings Utilizing Fibre Bragg Grating Sensor
title_short Real-time Monitoring System of Composite Aircraft Wings Utilizing Fibre Bragg Grating Sensor
title_full Real-time Monitoring System of Composite Aircraft Wings Utilizing Fibre Bragg Grating Sensor
title_fullStr Real-time Monitoring System of Composite Aircraft Wings Utilizing Fibre Bragg Grating Sensor
title_full_unstemmed Real-time Monitoring System of Composite Aircraft Wings Utilizing Fibre Bragg Grating Sensor
title_sort real-time monitoring system of composite aircraft wings utilizing fibre bragg grating sensor
publisher IOP Publishing
publishDate 2016
url http://umpir.ump.edu.my/id/eprint/15339/1/fkm-2016-vorathin-Real-time%20monitoring%20system%20of%20composite%20aircraft.pdf
http://umpir.ump.edu.my/id/eprint/15339/
http://dx.doi.org/10.1088/1757-899X/152/1/012024
_version_ 1643667647722684416
score 13.211869

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