SHM with FBGs on a Full-scale Composite Aircraft Part

Leonardo P. Salvini; Daniel R. Louzada; Paula M. P. Gouvêa; Paulo Anchieta da Silva; Fernando Dotta; Laudier Jacques de Moraes da Costa; L. C. Guedes Valente; Arthur M. B. Braga

doi:10.1364/ACOFT.2016.JM6A.29

Photonics and Fiber Technology 2016 (ACOFT, BGPP, NP)
OSA Technical Digest (online) (Optica Publishing Group, 2016),
paper JM6A.29
•https://doi.org/10.1364/ACOFT.2016.JM6A.29

SHM with FBGs on a Full-scale Composite Aircraft Part

Leonardo P. Salvini, Daniel R. Louzada, Paula M. P. Gouvêa, Paulo Anchieta da Silva, Fernando Dotta, Laudier Jacques de Moraes da Costa, L. C. Guedes Valente, and Arthur M. B. Braga

Australian Conference on Optical Fibre Technology 2016

Sydney Australia
5–8 September 2016
ISBN: 978-1-943580-17-0

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Joint Poster Session I (JM6A)

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L. P. Salvini, D. R. Louzada, P. M. P. Gouvêa, P. A. d. Silva, F. Dotta, L. J. de Moraes da Costa, L. C. Guedes Valente, and A. M. B. Braga, "SHM with FBGs on a Full-scale Composite Aircraft Part," in Photonics and Fiber Technology 2016 (ACOFT, BGPP, NP), OSA Technical Digest (online) (Optica Publishing Group, 2016), paper JM6A.29.

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Abstract

This paper discusses results obtained in a Structural Health Monitoring (SHM) test of a full-scale composite aircraft part using Fibre Bragg gratings (FBGs). The FBGs were bonded to the surface of the aircraft part to monitor the part before and after localized damage was created.

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