Research Activities >> SIGNAL AND IMAGE PROCESSING & DATA FUSION >>  
     
  SIGNAL AND IMAGE PROCESSING & DATA FUSION
  Eddy Current Data Fusion
  Directional Filter Banks for Image Processing  
  Ultrasonic Signal Parameterization
  Lamb Wave Mode Decomposition using Wavelets
  ADR for Hancock Welds
 
     
    Eddy Current Data Fusion for Aircraft NDE
 
 


    Nondestructive Evaluation of large aircraft structures involves the collection of high volume of data sets from different NDE modalities such as ultrasonics and eddy current. These data sets are obtained from field inspections using semi-automated scanning systems. The efficient analysis of these data would involve the uses of automated algorithms for the processing of the data sets and the representation of these data sets in a user friendly and information rich mode to a field operator allowing an informed assessment of the state of the aircraft structure, and consequently the inference of the remaining life from this analysis.

The Aircraft fuselage and wing are made of aluminum alloy, single or multi-layer, based on location, with rivets/fasteners in place that may be made of aluminum, titanium, or steel.  The primary motivation for these inspections is to detect corrosion (i.e. material thinning due to corrosion) or structural cracking due to fatigue.  With the variety of structural configurations, the analysis of ultrasonic or eddy current data is expected to be challenging. The large area, and therefore large volume of data, complicates the issue. The primary part of the work involves the development of advanced algorithms that would permit automated analysis of the data by an operator in the field.

The automated data processing algorithms will lead to a rapid inspection for the detection of corrosion (i.e., material thinning due to corrosion) and/or structural cracking in aging aircraft structures/components such as large fuselage areas on the underside and top of wings, and the skin on the cabin structure. The data in both forms i.e. signals and images are considered for the data processing. The process involves several stages of data processing including (a) preprocessing, (b) de-noising, (c) registration, (d) sewing, (e) fusion, and (f) subtraction, that when used effectively will lead to an improved management of the NDE data in a field environment. Through this data fusion analysis algorithm development, across different NDE modalities such as eddy current, ultrasonic, x-ray, and thermal imaging, both the reliability of the data interpretation and the speed of NDE data analysis will improve significantly. This will lead to cost savings while improving performance of the NDT techniques for detection of damage and defects in aircraft structures. The development of data processing, analysis, reduction, fusion, and reporting algorithms for NDE data obtained, for the legacy aircrafts, from ultrasonic and eddy current NDE systems finds extensive use in the aging aircraft program.

 
 
EC Data set 1 at 6 kHZ from a corrosded coupon
EC Data set 1 at 6 kHZ from a
corrosded coupon
 
EC Data set 2 at 12 kHz from the corroded coupon
EC Data set 2 at 12 kHz from the
corroded coupon
 
Fused Data using both the data sets showing the regions of corrosion.
Fused Data using both the data sets showing the regions of corrosion.
 
     

 

 

 
   
Directional Filter Banks for Image Processing
 


    NDE data that are represented in the form of images often have two important classes of information. These are (a) information about defects/anomalies that are present in the structure/component, and (b) characteristics of the materials/structure such as micro-structural features, geometrical boundaries, machining marks, etc. The relevance of either type of information is clearly application dependent. Usually, the NDE images have both information superimposed hence the interpretation and eventually the quantitative assessment of these images are detrimentally affected. Hence, there is a need for techniques that can decouple the above information, or at least reduce the influence of one on the other.

A Directional Filter Bank (DFB) can be used for the segmentation of NDE images containing directional information.  The DFB splits the frequency spectrum into fan shaped pass bands, which can then be used to extract directional features from the images.

The DFB is used to split an image into a desired number of sub-band images with each sub-band image containing features belonging only to a given angular range.  The DFB is a two-channel decomposition employing the Quincunx sampling matrix and the Diamond Half Band filter pair. The DFB is also designed to incorporate the property of perfect reconstruction or alias free reconstruction. Applications of the DFB towards segmenting C-Scan images of fiber-reinforced composites, Magnetic Flux Leakage (MFL) images of seamless tubes, IR images of Solar Cell panels and optical images for the computation of area coverage in a Shot peening process are discussed.

The application of the DFB towards segmentation of images from NDE inspection was demonstrated in the previous section. The DFB is a valuable tool for carrying out directional segmentation of images. The property of Perfect Reconstruction lends robustness to the segmentation, as no information is lost during the decomposition process. The use of DFB can lead to considerable simplification of image analysis tasks where complex two-dimensional textures are encountered.

The DFB has a vast potential for application in feature based image segmentation and in the automated analysis of NDE images for defect sizing and defect characterization. This may also have applications in the area of material characterization and other image processing applications.
 
 
Directional Filter Banks for Image Processing
FIG - 1
 
C-scan image of a composite plate with impact damage showing fiber information.
C-scan image of a composite plate with impact damage showing fiber information.
The filtered image of the C-scan without the fiber information.
The filtered image of the C-scan
without the fiber information.
G. Swamy, and K.Balasubramaniam, NDT&E International, 40  250–257 (2007)
 
 

 
    Ultrasonic Signal Parameterization
 
 


     Signals find applications in the Non-Destructive Evaluation (NDE) of metals and other materials like composites as well as in the field of Medical Imaging. Back scattered echoes generated by the reflection of ultrasonic waves contain information pertaining to the location, size and characteristics of the defects present, along with the material and the path information about the object under evaluation. The accurate detection, location and sizing of the defects and other imaging applications are limited by the ability to precisely estimate the information contained in the ultrasonic echoes. Model based signal parameter estimation is a technique, wherein an underlying model for the signal is assumed and parameters of the model are estimated

Signal parameter estimation of complex Ultrasonic RF Signals in the presence of noise as well as multiple overlapping echoes using a hybrid search algorithm will be discussed. This hybrid algorithm comprises of an evolutionary algorithm (Genetic Algorithm) and a gradient based algorithm (Levenberg-Marquardt Algorithm). This technique was found to overcome problems of earlier methods that are marked by the presence of local minima. In this paper, the hybrid algorithm is shown to demonstrate higher robustness when compared to a purely gradient based approach and faster convergence when compared to a purely evolutionary approach, for both simulated and experimental signals.

The hybrid algorithm, when applied for signal parameter estimation problems in the ultrasonic NDE context combines the advantages of a gradient based approach and an evolutionary approach, providing higher robustness than the gradient based methods and higher speed when compared to the genetic algorithm. Robustness is needed especially in cases where an inspection of the estimated parameters does not reveal their optimality like in the case of overlapping echoes. In this paper the improvement in the range of the initial guess allowed was shown to be more than 500% when compared to the Gauss-Newton method. Similarly, the reduction in the computation time was observed to be about 90% when compared to the Genetic algorithm used alone.

It is additionally shown that the hybrid-GA improves the signal to noise ratio and correct for under-sampling of data. The defect sizes as estimated by the hybrid GA based signal parameterization technique was observed to be within ± 4 % of the actual defect sizes.
 
 
 

Experimental Setup
Experimental Setup
 
Thermo gram of wall thickness loss
Thermo gram of wall thickness loss
 

Actual Defect Size
(mm)

Estimated Defect Size Using GA
(mm)

Percentage Error
%

3.5

3.43

+1.14

2.5

2.52

-0.80

1.5

1.56

-2.40

The universal plot for the TT mode for diffusivity measurement.
 

 
    ADR for Hancock Welds
 
 


    Radiographic Testing using X-rays is  commonly used NDT method for detecting internal welding flaws. It is based on the ability of X-rays  to pass through metal and other materials opaque to ordinary light, and produce photographic records by the transmitted radiant energy. Because different materials absorb either X-ray  to different extent, penetrated rays show variations in intensity on the receiving films. That provides a means to examine the internal structure of a weld. Traditionally, experienced workers are required to evaluate the weld quality based on radiographic images. Therefore, the results very much depend upon the capability and experience of the operator. Unfortunately, the manual interpretation process is time-consuming and the results could be very subjective, inconsistent, and sometimes biased. Therefore, it is desirable to develop a computer based automated defect recognition (ADR) system to increase the objectivity, consistency, accuracy, and efficiency of RT inspection.

Digital image processing techniques are employed to lessen the noise effects and to improve the contrast, so that the principal objects in the image can be more apparent than the background. Feature extraction is necessary to obtain a set of features that can describe the characteristics of welding defects. These features should be small in number and high in discriminatory power. Pattern classification methods are needed to analyze feature data and make a prediction of the defect type. Pattern classification algorithms might differ in efficiency and accuracy. Therefore, two renowned supervised algorithms: Artificial Neural Network (ANN) and Support Vector Machine (SVM) were investigated.

The approach is listed as follows:

  • Segmentation
  • Pre-Processing
  • Identification of defect
          - Image Contouring and Texture Extraction of suspected regions
          - Morphologically single the defect
  • Feeding obtained data to ANN
  • Training of ANN with large number of datasets

  •  
     
     

    Digitized Image of  the hancock value.
    Digitized Image of  the hancock value.
     
    The registered, segmented, and equalized image.
    The registered, segmented, and
    equalized image.
     
    The thresholed middle region with the automated detected weld defect (circled)
    The thresholed middle region with the automated detected weld defect (circled)
     

     
        Wavelet Based Lamb Wave Mode Decomposition
     
     


        The multiple mode and dispersive nature of ultrasonic Lamb waves complicate their signal interpretation. Others have shown that it is possible to obtain a plate’s dispersion relationship by using the two dimensional Fourier Transform to operate on multiple, equally spaced waveforms. Unfortunately, the need for exact, spatially sampled data restricts the practicality of the 2D-FFT for inspection applications. In contrast, Time-Frequency Representations (TFR) requires only a single RF signal for analysis.

    This work explores the use of Wavelet Transform combined with theoretical dispersion relationship to automatically identify modes (without source position known a-priori) by exploiting their dispersive nature, a widely considered unfavorable property,  of the ultrasonic Lamb waves. Four different methods to identify modes are discussed and an efficient algorithm is presented. The algorithm also identifies the possible source location of the modes.

    It was found that the techniques using adaptive template generation prove effective for the interpretation of complex Lamb wave signals. The technique requires the material properties and geometry of the sample as inputs for analytically deriving the templates for individual modes using the dispersion curves. This technique was found to work well for cases where the multiple modes were separated in the dispersion curve. However, difficulties were encountered in regions where modes intersected.

    The Wavelet based technique for mode decompositeion from composite Lamb wave signals.
    The Wavelet based technique for mode decompositeion
    from composite Lamb wave signals.
     

    Experimental setup for Lamb mode generation.
    Experimental setup for Lamb
    mode generation..
     
    Typical A0 mode template.
    The registered, segmented, and
    equalized image.
     
    The template matched WT of the A0 signal with dispersion curve.
    The template matched WT of the A0
    signal with dispersion curve.
     
     
     
     







































































































































































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