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Open AccessJournal ArticleDOI

Fibre Optic Sensors for Structural Health Monitoring of Aircraft Composite Structures: Recent Advances and Applications.

Raffaella Di Sante
- 30 Jul 2015 - 
- Vol. 15, Iss: 8, pp 18666-18713
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TLDR
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.
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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Citations
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Fibre Bragg Grating Based Strain Sensors: Review of Technology and Applications.

TL;DR: Some advanced applications and key sectors of the global fibre-optic strain sensors market are envisaged, as well as the main market players acting in this field.
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Piezoelectric Transducer-Based Structural Health Monitoring for Aircraft Applications.

TL;DR: The requirements for practical implementation and use of structural health monitoring systems in aircraft application, state-of-the-art techniques for solving some practical issues, such as sensor network integration, scalability to large structures, reliability and effect of environmental conditions, robust damage detection and quantification are discussed.
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TL;DR: An overview of the different types of FOS used for strain/temperature sensing in composite materials and their compatibility with and suitability for embedding inside a composite material is presented.
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A review on optical fiber sensors for environmental monitoring

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Recent development of fiber-optic chemical sensors and biosensors: Mechanisms, materials, micro/nano-fabrications and applications

TL;DR: In this paper, the authors present the foundations of fiber-optic chemical sensing or biosensing, including the sensing mechanisms of various fiberoptic sensors, sensing materials and the novel techniques for sensing materials deposition.
References
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Journal ArticleDOI

Interferometric Fiber Optic Sensors

TL;DR: Each type of interferometric sensor is reviewed in terms of operating principles, fabrication methods, and application fields and some specific examples of recently reported interferometeric sensor technologies are presented in detail to show their large potential in practical applications.
Journal ArticleDOI

Structural health monitoring techniques for aircraft composite structures

TL;DR: A review of currently used inspection methods is presented and some examples are described where Lamb wave based scanning techniques have been used to identify internal damage in multi-layered composite structures in this article.
Journal ArticleDOI

Recent progress in Brillouin scattering based fiber sensors.

TL;DR: The progress on improving sensing performance parameters like spatial resolution, sensing length limitation and simultaneous temperature and strain measurement is reviewed.
Book

Composite Materials For Aircraft Structures

TL;DR: In this paper, the differences between composites and metals, structural design procedures and in-service performance of those materials are discussed, as well as their applications in aeronautical design and structure.
Journal ArticleDOI

Fiber optics strain gauge.

TL;DR: A fiber optics strain gauge measuring strains of <0.4 × 10.2 × 10 m 1 is demonstrated, utilizing the change in optical pathlength caused by strain in a fiber.
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