Fibre Optic Sensors for Structural Health Monitoring of Aircraft Composite Structures: Recent Advances and Applications
In-service structural health monitoring of composite aircraft structures plays a key role in the assessment of their performance and integrity. In recent years, Fibre Optic Sensors (FOS) have proved to be a potentially excellent technique for real-time in-situ monitoring of these structures due to t...
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| Veröffentlicht in: | Sensors (Basel, Switzerland) Jg. 15; H. 8; S. 18666 - 18713 |
|---|---|
| 1. Verfasser: | |
| Format: | Journal Article |
| Sprache: | Englisch |
| Veröffentlicht: |
Switzerland
MDPI
30.07.2015
MDPI AG |
| Schlagworte: | |
| ISSN: | 1424-8220, 1424-8220 |
| Online-Zugang: | Volltext |
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| Abstract | In-service structural health monitoring of composite aircraft structures plays a key role in the assessment of their performance and integrity. In recent years, Fibre Optic Sensors (FOS) have proved to be a potentially excellent technique for real-time in-situ monitoring of these structures due to their numerous advantages, such as immunity to electromagnetic interference, small size, light weight, durability, and high bandwidth, which allows a great number of sensors to operate in the same system, and the possibility to be integrated within the material. However, more effort is still needed to bring the technology to a fully mature readiness level. In this paper, recent research and applications in structural health monitoring of composite aircraft structures using FOS have been critically reviewed, considering both the multi-point and distributed sensing techniques. |
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| AbstractList | In-service structural health monitoring of composite aircraft structures plays a key role in the assessment of their performance and integrity. In recent years, Fibre Optic Sensors (FOS) have proved to be a potentially excellent technique for real-time in-situ monitoring of these structures due to their numerous advantages, such as immunity to electromagnetic interference, small size, light weight, durability, and high bandwidth, which allows a great number of sensors to operate in the same system, and the possibility to be integrated within the material. However, more effort is still needed to bring the technology to a fully mature readiness level. In this paper, recent research and applications in structural health monitoring of composite aircraft structures using FOS have been critically reviewed, considering both the multi-point and distributed sensing techniques. |
| Author | Di Sante, Raffaella |
| AuthorAffiliation | Department of Industrial Engineering—DIN, University of Bologna, Forlì 47121, Italy; E-Mail: raffaella.disante@unibo.it ; Tel.: +39-54-337-4458 |
| AuthorAffiliation_xml | – name: Department of Industrial Engineering—DIN, University of Bologna, Forlì 47121, Italy; E-Mail: raffaella.disante@unibo.it ; Tel.: +39-54-337-4458 |
| Author_xml | – sequence: 1 givenname: Raffaella surname: Di Sante fullname: Di Sante, Raffaella |
| BackLink | https://www.ncbi.nlm.nih.gov/pubmed/26263987$$D View this record in MEDLINE/PubMed |
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| Title | Fibre Optic Sensors for Structural Health Monitoring of Aircraft Composite Structures: Recent Advances and Applications |
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