Automated Damage Detection in Composite Components Using Acoustic Emission

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Abstract:

The ability of a Structural Health Monitoring (SHM) system to automatically identify damage in a composite structure is a vital requirement demanded by end-users of such systems. This paper presents the demonstration of a potential method. A composite fatigue specimen was manufactured and initially tested at 1Hz for 1000 cycles. Acoustic emission (AE) signals were recorded for complete fatigue cycles periodically in order to establish a base-line associated with undamaged specimens. The specimen was then subjected to impact damage to create barely-visible impact damage (BVID) and subjected to further fatigue cycles with acoustic emission recorded until failure. The data was subsequently analysed using a range of techniques including basic RMS signal levels and frequency-based analysis. At various stages during the test, C-scanning was used to validate the results obtained. Results demonstrated that AE is capable of detecting BVID in composite materials under fatigue loading. The proposed method has wide applicability to composite structures which are subjected to cyclic loading, such as wind turbine blades.

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Key Engineering Materials (Volumes 569-570)

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80-87

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July 2013

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© 2013 Trans Tech Publications Ltd. All Rights Reserved

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[1] American Society for Testing and Materials (ASTM), Standard practice for acoustic emission examination of fiberglass reinforced plastic resin (FRP) tanks/vessels. E1067-89. (1989).

DOI: 10.1520/e1067-07

Google Scholar

[2] S. Takeda, Y. Aoki, T. Ishikawa, N. Takeda and H. Kikukawa, Structural health monitoring of composite wing structures during durability testing, Comp. Struct. 79 (2007) 133-139.

DOI: 10.1016/j.compstruct.2005.11.057

Google Scholar

[3] W.J. Staszewski, S. Mahzan and R. Traynor, Health monitoring of aerospace composite structures – active passive approach, Comp. Sci. Tech. 69 (2009) 1678-1685.

DOI: 10.1016/j.compscitech.2008.09.034

Google Scholar

[4] D. Papasalouros, N. Tsopelas, I. Ladis, D. Kouroussis, A. Anastasopoulos, D. Lekou and F. Mouzakis, Health monitoring of a NEG-MICON 750kW wind turbine blades with acoustic emission, 30th European Conference on Acoustic Emission Testing, University of Granada, Spain, 12-15th September (2012).

DOI: 10.1201/b11837-62

Google Scholar

[5] T.P. Bradshaw, M.J. Eaton, R. Pullin, S.L. Evans and C.A. Featherston, Determination of damage levels of composite plates after low velocity impacts using acoustic emission, Advanced Materials Research 13-14 (2006) 253-258.

DOI: 10.4028/www.scientific.net/amr.13-14.253

Google Scholar

[6] M.J. Eaton, R. Pullin, M.R. Pearson, C.A. Featherston and K.M. Holford, Structural health monitoring of composite structures using embedded sensors, 15th European Conference on Composite Materials, Venice, Italy, 24-28th June (2012).

DOI: 10.1177/1475921716672206

Google Scholar

[7] R. Pullin, A. Clarke, M.J. Eaton, K.M. Holford, S.L. Evans and J.P. McCrory, Dectection of Cracking Gear Teeth Using Acoustic Emission. Applied Mechanics and Materials. 24-25 (2010) 45-50.

DOI: 10.4028/www.scientific.net/amm.24-25.45

Google Scholar

[8] R. Pullin, A. Clarke, M.J. Eaton, M.R. Pearson and K.M. Holford, Identification of the Onset of Cracking in Gear Teeth Using Acoustic Emission, Journal of Physics: Conference Series. 382 (2012).

DOI: 10.1088/1742-6596/382/1/012050

Google Scholar

[9] W.R. Broughton, G.D. Sims and M.J. Lodeiro, Overiew of DTI-funded Programme on 'Standardised Procedures for Ultrasonic Inspection of Polymer Matrix Composites. Insight – Non-Destructive Testing and Condition Monitoring 40 (1998) 8-11.

Google Scholar