The Proceedings of the Symposium on the Motion and Vibration Control
Online ISSN : 2424-3000
2010
Session ID : 3C14
Conference information
3C14 Damage detection in aircraft composite materials using a built-in broadband ultrasonic propagation system
Yoji OkabeKeiji FujibayashiMamoru ShimazakiHideki Soejima
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CONFERENCE PROCEEDINGS FREE ACCESS

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Abstract
As one of structural health monitoring systems, the authors developed a broadband ultrasonic propagation system using macro fiber composite (MFC) actuators and fiber Bragg grating (FBG) sensors. This system can send and receive broadband Lamb waves efficiently in a specific direction, and the MFCs and FBGs can be integrated into composite laminates because of their flexibility and high fracture strain. In this research, this system was applied to detect an interlaminar delamination in carbon fiber reinforced plastic (CFRP) laminates. One MFC and one FBG were bonded on each surface of the CFRP laminate to generate and receive the symmetric modes and the anti-symmetric modes separately for identification of the multiple modes of Lamb waves in the laminate. Then we investigated the mode conversion of Lamb waves at both tips of a delamination in the middle of the thickness of the lamimate, through an experiment and finite element analysis (FEA). On the basis of the knowledge about the mode conversion, an index to evaluate the delamination length was proposed using velocity changes by the mode conversions. From the results of experiments and FEA for the laminates with an artificial delamination, this new index was found to be effective to evaluate the delamination progress in the laminate quantitatively.
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© 2010 The Japan Society of Mechanical Engineers
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