scanning revolution

 

 

 

 

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In what sense then has the introduction of in-situ scanners caused a revolution in NDT?

Prior to the scanning revolution, in-situ NDT methods could be divided into two categories: spot measurements, and single-shot images. In general ultrasonic, eddy-current and mechanical impedance methods were in the spot-measurement category and X-ray and gamma radiography in the single-shot imaging category. Recent developments such as magneto-optic (eddy-current) imaging and Compton back-scattering profilimetry (X-ray spot measurements) have caused a blurring of these categories somewhat. However, it is the ability to scan a spot-measurement device over an area and build up an image that has introduced a third category, commonly referred to as C-scanning.

C-scans have been produced in the laboratory for many years, generally for ultrasonic imaging of flat specimens such as carbon-fiber composite skins, but relatively little work had been done on scanning with eddy-current or mechanical impedance devices. The revolution that has followed the widespread introduction of in-situ scanners has been due to the enhanced capabilities of this spot-measurement category of techniques.

Improved Visualization of Defects

A very good example of the revolution is in mechanical impedance methods. Whilst the method was capable of detecting variations in mechanical impedance indicative of the presence of a defect, the interpretation of the response was difficult. Inspections were often inconclusive because structural variations could cause even larger responses. Figure 1 illustrates the remarkable imaging resolution obtainable on a thin-skinned metal honeycomb structure. A spot measurement on this material would be very confusing because the signal would vary greatly within each cell of the honeycomb. However, the ability to look at a C-scan means that the disbonded area can be clearly identified. Effectively, the eye can filter out the honeycomb pattern variations by looking for changes in that pattern.

Mechanical impedance scans of honeycomb through thin skin

Figure 1. Mechanical Impedance scan of aluminum honeycomb. When Mr. Trevor Liddell of NDT Squadron (RAF Swanton Morley) first saw this scan, his comment was that “ANDSCAN has turned mechanical impedance into a usable in-service method!”

Eddy-current and ultrasonic methods also benefit from this use of the eye’s ability to filter out regular patterns, such as fasteners in a scan of a metal lap-joint(1,2) (see Figure 2 and Figure 3). Eddy-current impedance-plane instruments are notoriously difficult to interpret for complex structures because of edge effects, probe handling and changes in conductivity or thickness. Scanning can remove a lot of these interpretation problems.

Eddy-current corrosion map of KC135 

Figure 2. Single-frequency eddy-current scan of corrosion in a KC135 lap joint. The number of layers varies from 1 to 5.

Ultrasonic corrosion map of KC135

Figure 3. Ultrasonic depth scan of corrosion in a KC135 lap joint.

 

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Figure 4 illustrates how conventional ultrasonic thickness gauge measurements, with or without data logging, can be improved by using a scanning system and a conventional ultrasonic flaw detector in time-of-flight mode. The software allows the operator to move over any point on the scan and read off the measured thickness.

Map of remaining thickness

Figure 4. Ultrasonic thickness scan showing thickness remaining after blending out of corrosion.

One further example of the benefits of C-scanning rather than spot measurements is the ability to identify patterns. For example, ply stacking sequences can be determined in carbon-fiber composite skins by C-scanning methods where the fiber direction can be clearly identified at the depth of the reflected signal being monitored(2).

Other enhanced visualization methods such as cross-sectional slices, rotating pseudo-3D images and contour plots are shown in Figure 5 and Figure 6.

Impact damage in composite skin

Figure 5. Cross-section and pseudo-3D visualization of defects.

Impact damage in composite skin

Figure 6. Contour plot.

 

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Post-processing Capabilities

Simple image-processing techniques such as those used for photographic or radiographic images can be of similar benefit for C-scan images. For example, the use of scalable color palettes helps to enhance contrast in order to extract weak defect indications (see Figure 7).

 

Use of false colour

Figure 7.Ultrasonic Thickness - Simple use of color palettes

An array of different sizing and characterization methods can be employed to analyze C-scan images. The standard -6 dB defect sizing method can be employed using tools built into the software. Figure 8 and Figure 9 illustrate how several different characterization techniques can be used. The data produced can be copied into a spreadsheet using standard Windows commands.

Defect characterisation tools

Figure 8. Quantitative Analysis: Defect Sizing and Histograms with mean, max, min and standard deviation for a selected area.

 

-6 dB Width tool

Figure 9. Automated -6 dB width.

 

 
     

 

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References

 

  1. Smith R A,“Non-destructive evaluation for corrosion in ageing aircraft, Part 1. Introduction, ultrasonic and eddy-current methods,” Insight - Journal of the British Institute of NDT, Vol 37, No 10, pp 798-807, 1995.

  2. Smith R A," on-destructive evaluation for corrosion in ageing aircraft, Part 2. Radiography, mechanical impedance and alternative methods; comparison of techniques,” Insight - Journal of the British Institute of NDT, Vol 37, No 11, pp 884-891, 1995.

  3. Smith R A and Clarke B, “Ultrasonic C-scan determination of ply stacking sequence in carbon-fiber composites,” Insight - Journal of the British Institute of NDT, Vol 36, No 10, pp 741-747, 1994.

 

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Author: R A Smith.
Copyright © 2004 QinetiQ Ltd. All rights reserved.
Revised: September 27, 2009

 

 

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