Damage assessment and monitoring of composite ship joints
Source abstract
Abstract
This paper describes the research activities associated with the damage assessment of maritime structures, conducted within the Cooperative Research Centre for Advanced Composite Structures, which aims to develop the capability to predict the criticality of typical damage in a ship joint and to develop and test techniques for its structural health monitoring (SHM). The research is focused on modelling and testing of a typical monolithic glass fibre reinforced polymer composite T-joint, which is subjected to disbonds at various interfaces. Methods for determining critical disbond sizes and two semi empirical methods have been evaluated. Embedded optical fibre Bragg grating sensors have been assessed for SHM. Issues have been addresses, involving embedding optical fibres into the joint interface and a technique has been developed for successful embedding and positioning of sensors. The performance of embedded Bragg grating sensors in such joints has been shown to be satisfactory and the effects of artificially induced disbonds on the strain distribution have been determined via finite element modelling and have been experimentally verified. The use of the random decrement signature of the structural response to turbulence has been assessed for SHM. Models and experiments involving typical joints with artificially induced disbonds have indicated that this technique could be successfully used to detect and characterise damage.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Advanced Fiber Optic Sensors · Structural Health Monitoring Techniques · Optical measurement and interference techniques
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (21)
Show source-provided references
1. Composites Fabrication Association, www.cfa-hq.com
2. Geometry and damage effects in a composite marine T-joint, Presented at ICCS 12, Monash Uni, Melbourne, November 200310.1016/j.compstruct.2004.04.036 ↗
3. Davidson BD. A predictive methodology for delamination growth in laminated composites Part II, US Dept of Transportation, FAA, Office of Aviation Research DOT/FAA/AR-97/87, October 2001
4. The analysis of skin to stiffener debonding in composite aerospace structures10.1016/S0263-8223(02)00110-1 ↗
5. Ship hull structure monitoring using fibre optic sensors10.1088/0964-1726/10/3/308 ↗
6. Damage detection and assessment in fibre-reinforced composite structures with embedded fibre optic sensors—review10.1088/0964-1726/11/6/314 ↗
7. Anastasi RF, Lopatin C. Application of a fiber optic distributed strain sensor system to woven E-glass composite. TM-2001-211051. NASA. 2001
8. Galea SC, Rajic N, Powlesland IG, Moss S, Konak MJ, Van der Velden S, et al. Overview of DSTO smart structures activities related to structural health monitoring. DSTO International Conference on Health and Usage Monitoring 2001, Melbourne, Australia, 2001
9. Galea SC, Rajic N, Moss S, McKenzie I, Koh YL, Chiu WK. In situ health monitoring of composite bonded repairs. Third International Workshop on Structural Health Monitoring, Stanford University, CA, USA, 2001
10. Li HCH, Herszberg I, Mouritz AP. Damage monitoring in large composite joints using smart sensors—a research overview. CRC-ACS TM03013. April 2003
11. Li HCH, Davis CE, Herszberg I, Mouritz AP, Galea S, Thomson RS. Application of fibre optic strain sensors for the health monitoring of adhesive bonded composite ship joints. Proceedings of the Fourth International Conference on Structural Health Monitoring, Stanford University, 15–17 September, 2003
12. Sensitivity of embedded fibre optic bragg grating sensors to disbonds in bonded composite ship joints. Presented at ICCS 12, Monash Uni, Melbourne, November 200310.1016/j.compstruct.2004.04.045 ↗
13. Damage detection in a fibre reinforced composite beam using random decrement signatures. Presented at ICCS 12, Monash Uni, Melbourne, November 200310.1016/j.compstruct.2004.04.033 ↗
14. Simpson JO, Wise SA, Bryant RG, Cano RJ, Gates TS, Hinkley JA, et al. Innovative materials for aircraft morphing, SPIE’S Fifth Annual International Symposium on Smart Structures and Materials, San Diego, CA, USA. 1998
15. Dakin · 1988
16. Brown T, Wood K, Childers B, Cano R, Jensen B, Rogowski R. Fiber optic sensors for health monitoring of morphing aircraft. SPIE Sixth Annual International Symposium on Smart Structures and Materials, Newport Beach, California, USA. 199910.1117/12.351590 ↗
17. Kalamkarov AL, MacDonald DO. Fabrication and testing of smart FRP reinforcements. Eleventh International Conference on Composite Materials, Gold Coast, Queensland, Australia. 1997
18. Jones M, Chiu WK. SHM Systems for maritime applications: alternative methods for damage diagnosis. CRC-ACS TM04010. April 2004
19. Jones M, Chiu WK, Herszberg I. Developments towards an in situ technique for delamination detection in thick glass-reinforced plastic composite structures, ACAM 2005, Melbourne, Australia. 2005
20. Cole Jr HA. On-line Failure Detection and Damping Measurement of Aerospace Structures by Random Decrement Signatures, NASA CR-2205. 1973
21. Damage identification in a ship’s structure using neural networks10.1016/S0029-8018(01)00077-4 ↗