Impact Localization on Composite Wing Using a Single FBG Sensor and Error Outlier Based Impact Localization Algorithm

##plugins.themes.bootstrap3.article.main##

##plugins.themes.bootstrap3.article.sidebar##

Published Jul 14, 2017
Pratik Shrestha Yurim Park Hyunseok Kwon Chun-Gon Kim

Abstract

Low velocity impact on composite structure can result in occurrence of barely visible impact damage (BVID) which are difficult to detect. Aircraft structures are vulnerable to such BVID because of low velocity impact due to runway debris, bird strike, tool drop, etc. Therefore, low velocity impact monitoring of composite structure is highly desirable for impact detection and localization. Additionally, SHM of large-scale structures with fewer numbers of sensors is desirable to reduce the complexity involved with the dataacquisition and processing. In this paper, feasibility of localizing low velocity impact on composite structure using a single sensor was investigated. Three FBG sensors were attached on the surface of the full-scale  composite wing and the signal from each of the FBG sensor was processed using the error outlier based impact localization algorithm to predict the location of the impact. The localization results demonstrated the feasibility of localizing impact on composite structure using a single FBG sensor; overall, the impacts were localized with average error of about 26.6 mm.

Abstract 29 | PDF Downloads 26

##plugins.themes.bootstrap3.article.details##

Keywords

PHM

References
Baker, A., Dutton, S., & Kelly, D. (1986). Composite Materials for Aircraft Structures. AIAA.
Kim, J.-H., Park, Y., Kim, Y.-Y., Shrestha, P., & Kim, C.- G. (2015). Aircraft health and usage monitoring system for in-flight strain measurement of a wing
structure. Smart Materials and Structures, 24(10), 1– 12. http://doi.org/10.1088/0964-1726/24/10/105003
Kim, Y. Y., Kim, J. H., Park, Y., Shrestha, P., Kwon, H. J. and, & Kim, C. G. (2016). Low-speed impact localization on a stiffened composite structure using
reference data method. Composites Research, 29(1), 1–6.
Measures, R. M. (2001). Structural Monitoring with Fiber Optic Technology. San Diego, Calif.: Academic Press.
Roeseler, W. G., Sarh, B., & Kismarton, M. U. (2007). Composite structures: The first 100 years. In 16th International Conference on Composite Materials (pp.1–10).
Shrestha, P., Kim, J. H., Park, Y., & Kim, C. G. (2015). Impact localization on composite wing using 1D array FBG sensor and RMS/correlation based reference database algorithm. Composite Structures, 125, 159–169. http://doi.org/10.1016/j.compstruct.2015.01.029
Shrestha, P., Kim, J. H., Park, Y., & Kim, C. G. (2016). Impact localization on composite structure using FBG sensors and novel impact localization technique based on error outliers. Composite Structures, 142, 263–271. http://doi.org/10.1016/j.compstruct.2016.01.088
Shrestha, P., Park, Y., & Kim, C.-G. (2017). Low velocity impact localization on composite wing structure using error outlier based algorithm and FBG sensors. Composites Part B: Engineering, 116C, 310–324. http://doi.org/http://dx.doi.org/10.1016/j.compositesb.2016.10.068
Section
Special Session Papers