Research and Development of Impact Damage Detection System for Airframe Structures Using Optical Fiber Sensors

Tsutsui, Hiroaki; Hirano, Noriyoshi; Kimoto, Junichi; Akatsuka, Takahiko; Sashikuma, Hirofumi; Takeda, Nobuo; Tajima, Naoyuki

doi:10.1007/978-90-481-2746-7_64

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2015

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“…Since 1998 Tsutsui et al [ 136 , 137 , 138 ] have been developing an impact damage detection (IDD) system based on the use of both embedded multi-mode and single-mode small diameter optical fibres. The system detection capability relies on the optical loss due to bending of the structure and the embedded fibre after an impact event.…”

Section: Applications Of Fbg Sensorsmentioning

confidence: 99%

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

Sante

2015

Sensors

522

263

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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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Section: Applications Of Fbg Sensorsmentioning

confidence: 99%