A NEW EDDY CURRENT SURFACE PROBE FOR SHORT FLAWS WITH MINIMAL LIFT-OFF NOISE H. Hoshikawa, K. Koyama, and M. Maeda Nihon University, Izumicho Narashino Chiba 275-8575, Japan ABSTRACT. The authors have devised a new eddy current surface probe that generates minimal lift-off noise and provides phase information on depth of flaws. The probe comprises a tangential exciting coil and two tangential detecting coils. The authors expect that the new probe will make eddy current testing more reliable in detecting flaws and more quantitative in evaluating depth of flaws than the conventional probes. INTRODUCTION Conventional eddy current probes detect flaws in the material by detecting the variation of the exciting coil impedance or of the eddy current circulating along the exciting coil. However, the eddy current circulating along the exciting coil changes not only by flaws but also by the variation of the probe lift-off from the test material. The large lift-off noise makes a shambles of the signal phase and prevents eddy current testing from utilizing the phase. Thus the signal phase can hardly have been utilized to evaluate flaws. As a result, only the amplitude of flaw signals has been used to evaluate flaws for the conventional surface probes. Since the signal amplitude changes not only by the depth of flaws but also by the length and width, eddy current testing has not been considered as a quantitative method of evaluating depth of surface flaws. The authors already devised a couple of eddy current surface probes with minimal lift-off noise [1-3]. However, @ probe reported last year [3] has a problem in evaluating short flaws. Demand for more reliable eddy current testing requires more diverse probes. Thus the authors have devised yet another eddy current surface probe combining a tangential exciting coil and two tangential detecting coils. The experimental results have indicated that the new probe can detect shorter surface flaws with minimal lift-off noise. The new probe generates a figure-eight-like signal pattern as it scans over a flaw. The phase of the signal changes according to depth of flaws with little influence from the length, width, and direction of flaws. The probe makes it possible to evaluate depth of flaws based on the signal phase, which makes eddy current testing more reliable and quantitative than the conventional method. Thus the eddy current testing using the new probe provides the phase information on depth of flaws just like the inner bobbin coil probe used for the eddy current inspection of tubing. CP657, Review of Quantitative Nondestructive Evaluation Vol. 22, ed. by D. O. Thompson and D. E. Chimenti © 2003 American Institute of Physics 0-7354-0117-9/03/S20.00 413 A NEW PROBE COMBINING TANGENTIAL COILS Conventional eddy current probes suffer from large lift-off noise because they detect the eddy current induced in the test material by the exciting coil or the perpendicular magnetic flux to the test material surface. Since the eddy current changes drastically by the probe lift-off from the test material, it is inevitable for conventional probes to suffer from large noise. The authors have conceived the following idea of a new lift-off noise free eddy current probe. A probe can be lift-off noise free if it detects the eddy current generated by a flaw and not directly by the exciting coil. Such a probe can be realized by arranging a tangential exciting coil perpendicular to tangential detecting coils that detect only the magnetic flux parallel to the material surface and perpendicular to them or only the eddy current parallel to them. FIGURE 1 shows a newly developed eddy current probe combining a tangential exciting coil and two tangential detecting coils arranged perpendicularly to on both sides of the exciting coil. The tangential exciting coil induces eddy current parallel to itself. Two tangential detecting coils connected additively in series detect only the magnetic flux parallel to the material surface and perpendicular to them or only the eddy current component circulating parallel to them. The probe is named Plus Probe since it looks like a plus sign when seen from its top. FIGURE 2 shows the schematic eddy current circulation at the surface of the test material. When there is no flaw in the material, the eddy current induced by the tangential exciting coil circulates only perpendicular to the tangential detecting coils as shown in Figure 2(a). Thus the detecting coils generate no signal because they only pick up the eddy current component circulating parallel to them. The detecting coils generate no signal by the variation of the probe lift-off from the test material that causes the eddy current to change in amplitude and not in the circulating direction. On the other hand, if the test material has a flaw parallel to the detecting coils as shown Figure 2(b), some of the eddy current circulates along the flaw and causes the detecting coils to generate a signal. Thus Plus Probe can pick up flaws with no lift-off noise in principle. Plus Probe can also eliminate the troublesome bridge balance procedure from eddy current testing because it generates no signal as long as there is no flaw in the test material. /Test material Detecting coils FIGURE 1. A new eddy current surface probe with minimal lift off noise that comprises tangential coils. 414 Eddy Eddy current current Eddy Eddycurrent current Flaw Flaw \ \ / Detecting Detecting Detectingcoils coils Detecting coils coils (a) (b) (a)with withnonoflaw flaw (b)with withaaflaw flaw by the the tangential tangentialexciting excitingcoil. coil. FIGURE FIGURE2.2. Schematic Schematiccirculation circulationofofeddy eddycurrent currentatatthe the surface surface of of the the test test material material by Test Testfrequency frequency: :20kHz 20kHz 0.2 Flaw Flaw ::width width 0.5mm 0.5mm 0.2 In-phase in phasecomponent component 0.1 0.1 In-phase in phasecomponent component 0.1 o 0 -0.1 -0.1 -0.1 0 -028 -0.2 20 10 0 -10 -20 20 10 0 -10 -20 -0.2 -20 -10 0 10 20 -20 -10 0 10 20 (a) (b) (a)Θ0 probe probe (b) Plus Probe FIGURE depth. FIGURE3.3. Signals Signalsobtained obtainedby by Θ 0 probe probeand andPlus PlusProbe Probe for foraa surface surface slit slit flaw of 5mm 5mm length and 80% depth. Figure2(b) 2(b)also alsoindicates indicatesthe the flaw flaw signal signal pattern pattern by by Plus Plus Probe Probe as as itit scans scans over over aa flaw. flaw. Figure Sincethe theeddy eddycurrent currentcirculates circulatesininopposite oppositedirections directionsabove above and and below below the the flaw, flaw, the tangential Since detectingcoils coilsgenerate generateaaplus plusororminus minus signal signal depending depending on on their their position position with with respect respect to to the the detecting flaw.When Whenthe thedetecting detectingcoils coilsare areright right over over the the flaw, flaw, they they do do not not generate generate any any signal signal because flaw. theeddy eddycurrents currentscirculate circulateininthe theopposite oppositedirections directions atat both both sides sides of of the the flaw flaw and and cancel out the the detectingcoil coilsignal. signal.Thus ThusPlus PlusProbe Probegenerates generatesaafigure figure eight eightlike likesignal signal pattern pattern as as itit scans scans over over detecting a flaw. Since the probe generates practically minimal lift-off noise and the probe lift-off a flaw. Since the probe generates practically minimal lift-off noise and the probe lift-off influenceslittle littleon onthe thephase phaseofofflaw flawsignals, signals,the thesignal signalphase phasecan canbe be used used for for evaluating evaluating depth of influences flaws. flaws. EXPERIMENTALRESULTS RESULTS EXPERIMENTAL Experimentswere wereconducted conductedfor forPlus Plus Probe Probe that that consists consists of of aa tangential tangential exciting exciting coil coil of Experiments 19x19mm22and andtangential tangential detecting detecting coils coils of of 7x9mm 7x9mm22.. Each Each coil coil was was wound wound with with 1mm 1mm22 cross cross 19x19mm section.Test Testmaterials materials were were brass brass plates plates ofof 1.5mm 1.5mm thickness. thickness. Each Each test test plate plate has has an an electric electric section. discharge machined machined slit slit flaw flaw and and each each flaw flaw isis different different inin depth, depth, length, length, and and width. width. Test Test discharge frequencyofof20 20kHz kHzwas waschosen chosentoto make make 1.5 1.5ofofthe the ratio ratio of of the the plate plate thickness thickness to to the the standard standard frequency penetrationdepth depthfor forthe thebrass brassplate. plate. penetration Figure33shows showsin-phase in-phasecomponent componentofofsignals signalsobtained obtainedby by Θ@ probe probe[3] [3]and andPlus Plus Probe Probe Figure theyscan scanover overaasurface surface flaw flaw ofof5mm 5mm length length and and 80% 80% depth. depth. The The figure figure indicates indicates that that Plus Plus asasthey Probegenerates generatessimpler simplerflaw flaw signal signalthan than Θ @ probe. probe. Probe 415 Test frequency : 20kHz Flaw : length 15mm, width 0.5mm, depth 0~80% flaw signal lift-off noise 3 1 s a §0.5 §0.5 lift-offnoise = 0.08~0.59mm 0 0.5 1 In-phase component 0 0.5 1 In-phase component (a) 0 probe FIGURE 4. Flaw signals and lift-off noises in the voltage plane. Test frequency ' 20kHz (b) Plus Probe Flaw ' length 15mm, width 0.5mm 0.07 £0.1 - t» \ \ \ \ aa <-^^^-> 1 ~od t - flaw depth — — 80% -•-60% -0.1 -----40% —— 20% i . X 'f . flaw depth — — 80% -•-60% —-40% l . ^V N \ \ \ \ \ v^ ) i -0.1 0 0.1 In-phase component [V] 07 0 In-phase component [V] (a) front surface flaws (b) back surface flaws FIGURE 5. Signal patterns by Plus Probe for flaws with different depths. Experiments on lift-off noise were conducted by inserting thin papers of different thickness between the probe and the test material. Figure 4 indicates that both @ probe and Plus Probe generate far larger flaw signals than lift-off noise. Thus the new probe can detect flaws with far higher signal-to-noise ratio than conventional probes. Figure 5 shows signal patterns obtained by Plus Probe for front surface flaws and back surface flaws with different depths. Figure 5(a) indicates that the signal phase advances forward as the depth of front surface flaws increases. On the other hand, the phase lags behind as the depth of back surface flaws increases as shown in Figure 5(b). Figure 5 also indicates that the signal phase is quite stable against the fluctuation of the probe lift-off. Figure 6 shows flaw signal patterns obtained by @ probe and by Plus Probe for flaws with different lengths. Figure 6(a) indicates that the amplitude of flaw signals by @ probe changes a lot as the flaw length decreases. On the other hand, the amplitude of flaw signals by Plus Probe does not change much as shown in Figure 6(b). Figure 6 also shows that the signal phase does not change much by the flaw length. Experimental results have also indicated that the width of flaws and the angle of flaws with respect to the detecting coils change the amplitude of flaw signals a lot but keep the phase almost constant. 416 Test frequency: 20kHz Flaw : depth 80%, width 0.5mm r o.i 0.1 I a a o 3 -0.1 -0.1 -0.1 _L 0 _L 0.1 flaw length — •— 15mm —--10mm ——— 5mm -0.1 0 0.1 In-phase component [V] In-phase component [V] (a) 0 probe (b) Plus Probe FIGURE 6. Signal patterns by & probe and by Plus Probe for different flaw lengths. Test frequency: 20kHz Flaw ' length 15mm, width 0.5mm 0.5,————,——— 3 0 Uft-ofllmm) —---0 —— 0.08 —— 0.16 —— 0.59 ———1.05 { -O.i -0.1 0 0.1 In-phase component ) 0 0.5 In-phase component [V] (a) 0 probe (b) Plus Probe FIGURE?. Signal patterns by 0 probe and by Plus Probe for different lift-offs. Figure 7 shows signal patterns for a flaw of 100% depth by @ probe and by Plus Probe when the lift-off of the probes changes from 0 to 1.05mm. The lift-off causes the amplitude to change much while it causes the phase less. Figure 8 shows variation of the signal phase for a 100% depth flaw vs. probe lift-off. The figures indicate that the phase variation is only couple of degrees if the variation of the lift-off is kept within 0.2mm. Thus Plus Probe provides eddy current testing a method of evaluating flaw depth by utilizing the signal phase without much influence from the probe lift-off variation. The authors have derived the flaw depth evaluation curve for the brass plate based on the phase of flaw signals as shown in Figure 9. Thus the depth of flaws in the brass plate can be evaluated by applying the phase of flaw signals to the curve in the figure without much influence from the variations of flaw length and width. The relation between signal phase and flaw depth is just the same as the one known for the tubing inspection by the inner bobbin coils probe. The authors expect that the flaw depth evaluation method based on the signal phase will improve the accuracy of flaw depth evaluation in eddy current testing. 417 Test frequency ' 20kHz Flaw ' length 15mm, width 0.5mm bfl -8 - Plus probe - ©probe -20, 0 0.5 1 lift-off[mm] 1.5 FIGURE 8. Phase variations of the signal for a 100% depth flaw by lift-off. Test frequency ' 20kHz Flaw ' length 15mm, width 0.5mm lOOr -100 -50 0 50 Flaw signal phase[deg] FIGURE 9. Flaw depth evaluation curve based on signal phase. CONCLUSION The experimental results have indicated that Plus Probe generates only minimal lift-off noise and provides a way to evaluate flaw depth based on signal phase without much influence from the length and width. The authors expect that the new probe utilizing both amplitude and phase of the flaw signal will make the eddy current testing more reliable in detecting flaws and more quantitative in evaluating flaws than the conventional probes utilizing only the flaw signal amplitude. REFERENCES 1. 2. 3. Hoshikawa, H. and Koyama, K., "A New Eddy Current Probe Using Uniform Rotating Eddy Current," Materials Evaluation, 56,1, 85-89 (1998). Hoshikawa, H., Koyama, K. and Karasawa, H., "A New ECT without Lift-off Noise and Phase Information on Flaw Depth," Review in Progress Quantitative NDE, 20A, 969-976 (2001). Hoshikawa, H., Koyama, K. and Maeda, M., "Signal Phase Indication of Flaw Depth by a Lift-off Noise Free Eddy Current Probe," Review in Progress Quantitative NDE, 21A, 430-437 (2002). 418
© Copyright 2025 Paperzz