4.7 Article

Impact imaging of aircraft composite structure based on a model-independent spatial-wavenumber filter

期刊

ULTRASONICS
卷 64, 期 -, 页码 10-24

出版社

ELSEVIER SCIENCE BV
DOI: 10.1016/j.ultras.2015.07.006

关键词

Composite structure; Impact imaging; Lamb wave; Spatial-wavenumber filter; Linear piezoelectric sensor array

资金

  1. National Science Fund for Distinguished Young Scholars [51225502]
  2. Natural Science Foundation of China [51205189]
  3. Chinese Foundation of Postdoctoral Science [2012M510134]
  4. Research Funds for the Doctoral Program of Higher Educations in China [20123218120007]
  5. State Key Laboratory of Mechanics and Control of Mechanical Structures (Nanjing University of Aeronautics and Astronautics) [MCMS-0513K01, 0515Y01]
  6. Priority Academic Program Development of Jiangsu Higher Education Institutions
  7. Qing Lan Project
  8. Hong Kong Scholars Program

向作者/读者索取更多资源

The spatial-wave number filtering technique is an effective approach to distinguish the propagating direction and wave mode of Lamb wave in spatial-wave number domain. Therefore, it has been gradually studied for damage evaluation in recent years. But for on-line impact monitoring in practical application, the main problem is how to realize the spatial-wave number filtering of impact signal when the wave number of high spatial resolution cannot be measured or the accurate wave number curve cannot be modeled. In this paper, a new model-independent spatial-wave number filter based impact imaging method is proposed. In this method, a 2D cross-shaped array constructed by two linear piezoelectric (PZT) sensor arrays is used to acquire impact signal on-line. The continuous complex Shannon wavelet transform is adopted to extract the frequency narrow band signals from the frequency wideband impact response signals of the PZT sensors. A model-independent spatial-wave number filter is designed based on the spatial-wave number filtering technique. Based on the designed filter, a wave number searching and best match mechanism is proposed to implement the spatial-wave number filtering of the frequency narrow band signals without modeling, which can be used to obtain a wave number-time image of the impact relative to a linear PZT sensor array. By using the two wave number-time images of the 2D cross-shaped array, the impact direction can be estimated without blind angle. The impact distance relative to the 2D cross-shaped array can be calculated by using the difference of time-of-flight between the frequency narrow band signals of two different central frequencies and the corresponding group velocities. The validations performed on a carbon fiber composite laminate plate and an aircraft composite oil tank show a good impact localization accuracy of the model-independent spatial-wave number filter based impact imaging method. (C)2015 Elsevier B.V. All rights reserved.

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