Imaging defects in laminate composite plates using focused shear waves generated by air-coupled transducer

Abstract This research develops a nondestructive evaluation (NDE) technique to obtain images of two types of defects, delamination and debonding, in a thick laminate composite plate as a laboratory material system for wind turbine blades. The technique uses focused shear waves which are generated and detected by a set of noncontact, air-coupled ultrasonic transducers. The noncontact nature of the air-coupled method facilitates rapid scanning/inspection of large composite structures. Ray-tracing simulations are performed which visualize the focusing behavior of the focused shear waves in the specimen, from which the experimental parameters are determined. The proposed focused shear wave technique is compared with a Lamb-wave based technique, showing that the present technique is more appropriate for direct imaging of these defects. The obtained images of delamination and debonding defects agree well with the estimated defect locations and dimensions. This demonstrates the feasibility of further developing the present technique for specific field applications in wind turbine blades.

[1]  C. Fiorini,et al.  Vibration-based delamination diagnosis and modelling for composite laminate plates , 2015 .

[2]  K. Balasubramaniam,et al.  Interaction of the primary anti-symmetric Lamb mode (Ao) with symmetric delaminations: numerical and experimental studies , 2009 .

[3]  Zhongqing Su,et al.  A quantitative identification approach for delamination in laminated composite beams using digital damage fingerprints (DDFs) , 2006 .

[4]  Peter Cawley,et al.  Single Sided Inspection of Composite Materials Using Air Coupled Ultrasound , 1998 .

[5]  P. Cawley,et al.  The generation, propagation, and detection of Lamb waves in plates using air‐coupled ultrasonic transducers , 1996 .

[6]  G. Georgeson,et al.  EVALUATION OF AIR COUPLED ULTRASOUND FOR COMPOSITE AEROSPACE STRUCTURE , 2009 .

[7]  Sylvain Chatillon,et al.  Optimization of ultrasonic arrays design and setting using a differential evolution , 2011 .

[8]  A. G. Beattie,et al.  Acoustic emission monitoring of a wind turbine blade during a fatigue test , 1997 .

[9]  K. Balasubramaniam,et al.  Characterisation of rectangular type delaminations in composite laminates through B- and D-scan images generated using Lamb waves , 2011 .

[10]  Reimondas Sliteris,et al.  The review of non-destructive testing techniques suitable for inspection of the wind turbine blades , 2008 .

[11]  Krishnan Balasubramaniam,et al.  Interaction of guided Lamb waves with an asymmetrically located delamination in a laminated composite plate , 2010 .

[12]  Paul D. Wilcox,et al.  A probabilistic approach for the optimisation of ultrasonic array inspection techniques , 2014 .

[13]  Reimondas Sliteris,et al.  NDT of wind turbine blades using adapted ultrasonic and radiographic techniques , 2009 .

[14]  W. Ke,et al.  3D finite element simulations of an air-coupled ultrasonic NDT system , 2009 .

[15]  V. Giurgiutiu Tuned Lamb Wave Excitation and Detection with Piezoelectric Wafer Active Sensors for Structural Health Monitoring , 2005 .

[16]  David K. Hsu,et al.  Air‐Coupled Ultrasonic Measurements in Composites , 2004 .

[17]  S. Rokhlin,et al.  Double through‐transmission bulk wave method for ultrasonic phase velocity measurement and determination of elastic constants of composite materials , 1992 .

[18]  David K. Hsu,et al.  Inspecting Composites with Airborne Ultrasound: Through Thick and Thin , 2006 .

[19]  R Kazys,et al.  Air-coupled ultrasonic investigation of multi-layered composite materials. , 2006, Ultrasonics.