LASER GENERATION OF FOCUSED ULTRASONIC WAVE Kyungyoung Jhang1, Hongjoon Kim2, Hyunmook Kim2, and Yob Ha2 School of Mechanical Engineering, Hanyang University, Hangdang-dong 17, Seongdong-gu, Seoul 133-791, Korea Department of Precision Mechanical Engineering, Graduated School of Hanyang University, Hangdang-dong 17, Seongdong-gu, Seoul 133-791, Korea ABSTRACT. An arc-shaped line array slit is used for the laser generation of focused laser-ultrasonic wave. The spatially expanded Nd: YAG pulse laser is illuminated through the arc-shaped line array slit on the surface of a sample to generate the ultrasonic wave of the same pattern as the slit. Then the generated ultrasonic wave is focused at the focal point of which distance from the slit position is dependent on the curvature of slit arc. The relationship between the characteristics of the generated ultrasonic wave including the focusing performance and several design parameters such like as slit width and slit interval are investigated. By using the focused wave we can upgrade the inspection ability for the small size defect with the improvement of spatial resolution. Also this method can be combined with the scanning mechanism to get image just like we can get by the scanning acoustic microscope(SAM) INTRODUCTION Lamb waves are guided elastic waves propagating in plate structures parallel to the boundary surfaces[l]. The propagation of these wave modes allows for the inspection of plates and strip materials along the length of the sample thus providing for the possibility of a considerable saving in time over a C-scan of the sample[2]. Recent years have seen considerable application of Lamb wave testing applied, for example, to defect detection in metal[3], composite plates[4,5], sheet thickness measurement[6], elastic constant evaluation[7] and bonded metal joint inspection[8]. The usual method of launching Lamb waves is to utilize a compression transducer coupled to sample plate with a matching wedge such that effective spatial matching into the desired Lamb wave mode is obtained[l]. An additional technique is to employ laser generation[9]. Attractive features of a laser-ultrasound source include its non-contact nature, reproducibility, broad bandwidth and capability to launch a variety of acoustic modes. Preliminary work on laseracoustic sources was conducted by White[10] using a pulsed ruby laser. But, in these methods, laser generated Lamb waves had wide bandwidth frequency, low directivity, and low sensitivity. Several techniques have been investigated to increase the amplitude and narrow the bandwidth of laser generated signal. One approach is temporal modulation of the laser source[ll]. Another method is controlling the shape and phase of the laser source to generate Lamb waves with narrow band and high directivity. Line array slit was used to generate narrow-band, high-directivity wave[12]. In his paper, arc-shaped line array slit was used to generate focused Lamb wave. This technique can upgrade the inspection ability of conventional line array slit for the small size defect with the improvement of 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/S20.00 305 specimen(aluminum, 2mm) specimen(aluminum, 2mm) 760 760 Nd-YAG LASER Slit Beam expander Broadband pinducer Osilloscope Osilloscope Computer Computer FIGURE FIGURE1.1.Experimental Experimental setup. setup. spatialresolution resolution and and be be combined combined with the scanning mechanism to spatial to get get image image just just like like we we canget getby byscanning scanning acoustic acoustic microscope(SAM). microscope(SAM). can EXPERIMENTAL ARRANGEMENT ARRANGEMENT EXPERIMENTAL FIGURE 11shows shows the the experimental experimental arrangement for the FIGURE the laser laser generation generation of of focused focused Lambwaves waves in inthe the sample sample plate. plate. The The source source laser was a Q-switched Nd:YAG Lamb Nd:YAG laser laser system. system. The diameter diameter of of the the laser laser beam beam was extended to about 20mm The 20mm by by aa beam beam expander. expander. Extended laser laser beam beam transmitted transmitted through an arc-shaped line array Extended array slit slit and and generated generated ultrasonic source source as as same same shape shape of of the slit slit on the sample plate. The ultrasonic The sample sample was was an an aluminum plate plate with with 2mm 2mm thickness. thickness. The The ultrasonic ultrasonic waves aluminum waves generated generated by by the the laser laser source source was detected detected by by aa pinducer, pinducer, and and the the wave wave signal signal was was was monitored monitored by by oscilloscope. oscilloscope. AA standard GPIB GPIB data data interface interface allowed allowed signals signals to standard to be be transferred transferred from from the the oscilloscope oscilloscope toto aa personalcomputer computer for for subsequent subsequent data data processing personal processing and and storage. storage. DESIGNOF OFARC-SHAPED ARC-SHAPED SLITS SLITS DESIGN Three parameters parameters of of arc-shaped arc-shaped slits slits were were determined. determined. The Three The prarmeters prarmeters are are slit slit space, space, slit number, and focusing length of arc. In first step, we determined slit space. In this slit number, and focusing length of arc. In first step, we determined slit space. In this step, step, taking the the sensitivity sensitivity of of detector detector into into consideration, consideration, we taking we determined determined the the frequency frequency of of ultrasonic wave wave generated generated by by slit. slit. From From the the frequency, frequency, we ultrasonic we determined determined the the wave wave length length with dispersion dispersion curve curve (FIGURE (FIGURE 2). 2). Generally, Generally, AO with A0 mode mode is is generated generated dominantly dominantly so so that that we have tried to generate AO mode, and its wavelength was determined from we have tried to generate A0 mode, and its wavelength was determined from the the relationshipbetween between the the frequency frequency and and wavelength relationship wavelength which which is is given givenby by V = (λ / d ) × ( f × d ) 306 (1) (1) 10 A4 9 S2 S4 P has e veloc ity (k m /s ) 8 « to £ S1 7 A3 A2 S3 6 S0 5 A1 44 33 22 A0 11 00 0 22 44 6 8 6 8 FFre r eqquueennccyy --TThhi icckknneessss pprroodduucctt ((MMHHzz**mmm m )) 10 FIGURE 2. Lamb wave phase velocities velocities in in an an aluminum aluminumplate. plate. Where, Where, V V is is phase phase velocity velocity of of the the wave, wave, λA is is wavelength, wavelength, dd isis thickness thickness of of the the plate, plate, ff isis frequency frequency of of the the wave. wave. As As frequency frequency is is selected selected and and the the thickness thickness of of the the plate plate isis determined when we select the plate, from the dispersion curve curve at FIGURE FIGURE 1, 1, we we can can find find the thickness of the plate plate is the velocity velocity of of the the wave. wave. In In here, here, the the thickness of the is 2mm, 2mm, frequency frequency is is 1.75MHz. 1.75MHz. At At the the dispersion dispersion curve, curve, phase phase velocity velocity of of the the A0 AOmode mode Lamb Lamb wave wave is is about about 2.8km/s. 2.8km/s. By By substitute substitute velocity, velocity, and and frequency frequency in in equation equation (1), (1), the the wavelength wavelength was was determined determined as as 1.5mm 1.5mm and and this this become become space space between between slits. slits. In In the the next next step, step, number number of of slits slits was was determined. determined. Many Many slits slits make make frequencyfrequencybandwidth bandwidth narrow, narrow, but but laser laser spot spot diameter diameter was was limited limited as as 10~20mm. 10~20mm. So, So, too too many many slits slits were were not not needed. needed. Generally, Generally, the the number number of of slits slits N N is is N = Ds / λ + 2 , (2) (2) where, where, D Dss is is laser laser spot spot size size on on the the slit slit array. array, because because the the wavelength wavelength was was determined determined in in the the former former step, step, we we can can determine determine the the number number of of slits slits by by the the equation equation (2). (2). Lastly, Lastly, The The focal focal length length of of the the slits slits was was determined determined from from radius radius of of arc. arc. LAMB LAMB WAVE WAVE SIGNAL SIGNAL GENERATED GENERATED BY BY ARC-SHAPED ARC-SHAPEDSLIT SLIT Typical Typical signals signals recorded recorded at at the the focusing focusing point point are are shown shown in in FIGURE FIGURE 33 with with STFT STFT contour contour plot. plot. Peak Peak frequency frequency of of signal signal generated generated by by slit slit space space 1.5mm 1.5mm was was about about 1.75MHz, 1.75MHz, and and itit was was about about 600kHz 600kHz when when the the slit slit space space was was 4mm. 4mm. ItIt shows shows that that frequency frequency of of the the Lamb Lamb wave wave generated generated by by the the arc-shaped arc-shaped slit slit array array was was determined determined by by slit slit space space as as we we designed. designed. From From the the contour contour plot plot of of STFT, STFT, we we can can find find that that A0 AOmode mode Lamb Lamb waves waves were were dominantly dominantly generated. generated. More More intensive intensive ultrasound ultrasound was was generated generated from from the the slit slit array array which which have than 1.5mm have 4mm 4mm slit-space slit-space than 1.5mm slit-space. slit-space. To To verify verify that that the the arc-shaped arc-shaped line line array array slits slits were were generating generating focused focused wave wave in in aa satisfactory satisfactory manner, manner, experiments experiments were were performed performed on on an an aluminum aluminum test test plates plates of of 2mm 2mm thickness. thickness. A A 1.75MHz 1.75MHz pinducer pinducer was was moved moved from from point point to to point point as as seen seen in in FIGURE FIGURE 44 to to detect detect the the Lamb Lamb wave wave signals signals and and peak peak to to peak peak value value of of the the signal signal was was measured measured at at each each points. points. Simulation Simulation using using simple simple scalar scalar diffraction diffraction theory theory was was performed performed to to compare compare with with this this experiment. experiment. FIGURE FIGURE 55 shows shows the the result. result. The The experimental experimental result result and and simultation simulation 307 Timef micro-seel 2 Frequency-Thickness Product (MHz*mm) 3 4 5 6 7 8 Frequency-Thickness Product (MHz*mm) Slit space 1.5mm Slit Slit space space 1.5mm 1.5mm Slit space 1.5mm Slit space4mm 4mm Slit Slit space Slitspace space4mm 4mm FIGURE 3.3.Lamb wave signal and its plot of of Short Short Time TimeFourier Fourier transform.The The focusinglength length of FIGURE FIGURE 3. 3. Lamb Lamb wave wave signal transform. focusing ofof FIGURE Lamb wave signal and its contour contour plot plot of of Short Short Time Time Fourier Fouriertransform. transform. The Thefocusing focusing length lengthof the arc was 35mm, the thickness of aluminum sample plate was was2mm. 2mm. the arc was 35mm, the thickness sample plate thearc arcwas was35mm, 35mm,the thethickness thicknessof ofaluminum aluminumsample sampleplate platewas was2mm. 2mm. the 5mm 5mm 5mm 5mm „«* <> ••j > o <> o (> <) (> *• \ < > - © center © back © Front Front Front Front center center back back FIGURE 4. Lamb wave detection points generating focused wave. FIGURE to verify generating focused wave.The Thepinducer pinducerlocated locatedon onthese these FIGURE4.4. 4.Lamb Lambwave wavedetection detection points points to to verify focused wave. The pinducer located on these FIGURE Lamb wave detection points to verify generating focused wave. The pinducer located on these points and amplitudes of the Lamb wave signals were measured. The spaces between the points were 5mm. points and amplitudes of the Lamb wave signals were measured. The spaces between the points were 5mm. points and amplitudes of the Lamb wave signals measured. The spaces between the points were 5mm. points and amplitudes of the Lamb wave signals were measured. The spaces between the points were 5mm. 999 0.05 0.05 0.05 1 U.U& 0. 045 888 0. 0.045 045 7 0.045iB<-x 0.04x^^^v \ 77 0.04 0.04 U M4 "<v 6 0. 035 0. 035 66 0. 035 ^,ua&^ 0.03 55 t-— -2S 0.03 0.03 5 0. 025 *X.Jk % 4 0. 025 0. 025 434 Z^* U.Uk!t» 0.02 Bv ' 0.02 0.02 ———— Jl * ," 0. 015 U.U2 323 T*~>x!^.^ ^^ 0. 015 0. 015 g;* U.U1& 0.01 js^>^ ^ *->NX 212 0.01 1 0.01 U.U1 0. 005 r ------* 101 0. 005 i 0. 005 U.UU5 00 1 0 0 -10 -8 -6 -4 -2 0 2 4 6 8 10 u0 0 -10 -8 -6 -4 -2 0 2 4 6 8 10 10 5 5 10 -10 --55 00 55 1010 -10 -8- 8-6- 6-4 - -24 -0 2 20 24 4 66 8 10 10 -- 10 10 1 0 - 5 0 5 1 Simulation Experiment Simulation Experiment Simulation Experiment Simulation Experiment FIGURE intensity lines. ( dashed :: front, solid :: center, FIGURE5.5. 5. Wave Waveintensity intensity distribution distribution measured measured at at 55 5 points points along along three three FIGURE three lines. lines.(((dashed dashed ::front, front,solid solid ::center, center, FIGURE 5.Wave Wave distribution measured measured at at 5 points points along along three lines. dashed front, solid center, dashdot :: back )) intensity distribution dashdot back dashdot : back ) y/^U^)3 dashdot: back) 308 1 2 3 1 4 Time(|j,sec) 2 3 Time (jisec) ..J............J...........J............J............J... i.............i.............i.............. i.. |....« 1 1 Freq. (kHz) Freq. (kHz) Single slit(Slit width 2mm) Slit array(Slit space 4mm, 5 slits) FIGURE 6. Variation of frequency bandwidth as slit numbers. result are similar in crossing points between the intensity distribution lines and side lobes. It shows that focused waves could be generated by the arc-shaped line array slits effectivly. FIGURE 6 illustrates Lamb wave signal which was generated by arc-shaped single slit to compare with waves generated by arc-shaped slit array. The wave generated by slit array have relatively narrow bandwidth and low frequency area was eliminated which represented in wave signals generated by single slit. CONCLUSION Arc-shaped slits were designed for generating the focused ultrasound. Intensity of ultrasound increases around the designed focusing point and it shows that the focused Lamb wave can be generated by arc-shaped array slits. It is expected that the focused Lamb wave generated by arc-shaped slit will be more effective to detect small size defect than conventional linear line array slit. ACKNOWLEDGEMENTS This work was supported by Domestic Co-work Program of the New Technology Development and Research Center of Laser Application (RRC). REFERENCES 1. Vikotorov, LA. "Rayleigh and Lamb waves physical theory and applications"(Plenum Press, New York, 1967), Chapter 2, pp. 67-121 2. Karautkramer, J. and Karautkramer, H., "Ultrasonic testing of materials"(Springer Verlag, 1977,2nd edn), Chapter 22, pp.399-426 3. Alleyne, D.N. and Cawley, P., "The interaction of lamb waves with defects", IEEE Trans. Ultrason. Ferroelectr. Freq. Control., 1992, 39, (3), pp. 381-397 4. Guo, N. and Cawley., P., "Lamb wave reflection for the quick non-destructive evaluation of large composite laminates", Mater. Eval. 1994, 52, (3), pp. 404-411 5. Pierce, S.G Staszevski, W. J. Gachagan, A. James, I.R. Philp, W.R.Worden, K. Culshaw, B. Mcnab, A. Tomlinson, G.R. and Hayard, G., "Ultrasonic condition 309 monitoring of composite structures using a low profile acoustic source and an embedded optical fibre sensor", Proc. SPIE Int. Opt. Eng., 1997, 3041, pp. 437-448 6. Dewhurst, RJ. Noui,I. and Shan, Q., "Polymer film thickness measurement using laser-ultrasound techniques", Rev. Sci. Instrum., 1990,61,(6), pp. 1736-1742 7. Rogers, W.P., "Elastic property measurement using Rayleigh Lamb waves", Res. Nondestru. Eval., 1995, 6, pp. 185-208 8. Bork, U. and Challis, R.E., "Nondestructive evaluation of the adhesive fillet size in a tpeel joint using ultrasonic lamb waves and a linear-network for data discrimination", Meas. Sci. Technol., 1995, 6, (1), pp. 72-84 9. Scruby, C.B. and Drain, L. E., "Laser ultrasonics: technique and applications" (Adam Hilger, 1990) Chapter 5, pp. 223-324 10. Hite, R. M., "Generation of transient elastic waves by transient surface heating", J. Appl. Phys., 1963, 34, (12), pp.3559-3567 11. Pierce, R. Ume, C. and Jarzynski, J., "Temporal Generation of a laser source for the generation of ultrasonic waves", Ultrasonics, 1995, 33, (2) pp. 133-137 12. Cerniglia, D. Jhang, K. Y. and Djordjevic, B. B." Non-Contact Ultrasonic testing of Aircraft Lap Joint", Proceedings of 15th World Conference on Non-Destructive Testing, edited by G. Nardoni et al., Italian Society for NDE, 2000, 161st in CD title 310
© Copyright 2025 Paperzz