FIFTH CANADIAN CONFERENCE ON NONDESTRUCTIVE ... - IAEA

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d) Offshore structures (subsea pipelines, production platforms). This is not a complete list, but these applications satisfy both the criteria for large structures and continuous monitoring for either integrity or process control. Applications such as ice breaker monitoring have been considered, but will require a significant effort in acoustic emission signal processing and analysis before its feasibility can be established. 5. Summary: A continuous acoustic emission monitoring concept has been described. The theme of continuous monitoring is to provide information regarding the integrity of a structure, or provide feedback for process control, or both. The acoustic emission behavior of each structure would be determined through a study of materials, damage mechanisms, and service conditions. With this information the continuous A/E monitoring system may be configured to present results to personnel otherwise unskilled in A/E data interpretation. The system hardware has been developed to prototype form, and essentially represents a redeployment of conventional, advanced multichannel A/E instrumentation. However, the seismological resemblance discussed above is a better model of the system and its operational concept. 6. Acknowledgements: We wish to acknowledge the support of Petro-Canada Resou-ces with many aspects of this concept; and the encouragement and logistics support of Ontario Hydro Research Division, and Petro-Canada Exploration.
- 150 - OTHER . CHANNELS CONVENTIONAL Mil LTI- CHANNEL A/E MONITOR Figure 1: Hardware Deploynent of a Conventional A/E Monitor CONTINUOUS SEISMIC MONITORING • SEISMIC OBSERVATORY (77| SEISMIC ANALYSIS CENTER Figure 2: Seismic Model of A/E Monitoring /£ SIGNAL OUTPUT MINI coup.
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q 11 Atomic Energy of Canada Limite
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ATOMIC ENERGY OF CANADA LIMITED FIF
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CINQUIEME CONFERENCE CANADIENNE SUR
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iii ACKNOWLEDGEMENT A special note
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DAY 2 KEYNOTE ADDRESS: Advanced Rad
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DAY1 KEYNOTE ADDRESS: Five Years Ex
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MB Power has a total generating cap
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The fourth lesson learned was that
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STATION UNIT Coleson Cove Coleson C
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0*'? - 8 - Ä | '••• '~-!.if~
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- 10 - 7/8 inch Titanium Tube 3D i
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The facility at CFB Greenwood was c
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CONDITION MONITORING - 14 - The Con
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- 16 - REDUCING UNWANTED EFFECTS ~
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- 18 - When this happens, the instr
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- 20 - (CJUIMTTCJW ROTOR BLADE SHOW
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- 22 - Un»hl«ld«d prob* - good b
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STEEL FASTENERS EXAMINATION OF FAST
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- 26 - SKIP FINNED TUHt •< IG 5 I
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To gain primary statistical informa
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- 30 - The next step in the develop
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Each firing of the capacitor banks
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- 34 - At the Bruce we have complet
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1 GARTER SPRING IN VERTICAL POSITIO
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DIGITAL READ OUT 3.595 TOIL ELEMENT
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- 40 - EVALUATION OF ULTRASONIC MET
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III MEASUREMENTS AND RESULTS - 42 -
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C Real defects - 44 - Here we repor
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Flaw Figure 1: Schematic of experim
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0.5 E10 Q. 8 1.5 2.0 - 48 - Positio
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- 50 - Figure 6: Optical micrograph
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- 52 - specialized applications suc
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- 54 - As the probed surface is not
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- 56 - in practice the central frin
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- 53 - bipolar pulse, as it is seen
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- 60 - 18. J.-P. Monchalln and R. H
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Sample Lens Ultrasound - 62 - Detec
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CD CO c O Q. W 0 - 64 - Sin(7TfuT)
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- 66 - AUTOMATED ULTRASONIC TESTING
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- 68 - 2.1 Scanning Bridge and Imme
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- 70 - each waveform digitization t
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- 72 - Further development of the s
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TRANSDUCER SELECT/ PULSE CONTROL -
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SCAIIIIING BRIDGE COLOUR GRAPHICS D
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Figure J — Beam profile of 3.5 MH
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- 80 - an additional reverse magnet
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- 82 - reinitialise the stress depe
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BAR MAGNET IDEAL FIELDS MEASURED FI
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- 86 - Figure 4: Hysteresis loops f
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-150 H= 1.6 kA/m COMPRESSION -100 -
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- 90 - MAGNETISATION ANHYSTERETÎC
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(b) 19 mm diameter o Hard spot 19mm
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Q. I CO zL 2 (Ky) TYPICAL UNCERTAIN
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- 96 - Figure 14: Conceptual M-H be
Page 109 and 110: - 98 - characterization program bas
Page 111 and 112: - 100 - 1. Planar transducer: l.a.
Page 113 and 114: Fig. 1 1/JS - 102 - Echos observed
Page 115 and 116: - 104 - CAPABILITIES/LIMITATIONS OF
Page 117 and 118: - 106 - V = f* - 0.9 ak N [2] h. /^
Page 119 and 120: DISCUSSION - 108 - The results of t
Page 121 and 122: - 110 - FIGURE 1: Equipment Used fo
Page 123 and 124: FIGURE 4: - 112 - 5 10 IS 10 Depth
Page 125 and 126: FIGURE 6: Output of Computer Modell
Page 127 and 128: - 116 - "Events on earth consist in
Page 129 and 130: - 118 - now _n = Af (5) n where Af
Page 131 and 132: - 120 - REFERENCES 1. J.K. Feiblema
Page 133 and 134: PULSER IMMERSION TRANSDUCER WATER ^
Page 135 and 136: - 124 - 6. Ultrasonic frequency spe
Page 137 and 138: i I 1 i l - 126 - —j 10. Ultrason
Page 139 and 140: TIME RNFOSIS PLOT CRSF: - 128 - 1H.
Page 141 and 142: - 130 - THE INTRODUCTION OF REAL-TI
Page 143 and 144: 5. QUALIFYING THE IMAGE - 132 - In
Page 145 and 146: - 134 - CONVENTIONAL FILM RADIOGRAP
Page 147 and 148: - 136 - 11.3 Computer Management of
Page 149 and 150: - 138 - Back end of system. The com
Page 151 and 152: - IAO - to be loaded properly into
Page 153 and 154: 20. OPERATIONAL UTILIZATION - 142 -
Page 155 and 156: % -•'v/ FILM AND SCREENS ' \ INSI
Page 157 and 158: - 146 - By design, these A/E monito
Page 159: - 148 - a) enables an A/E monitor s
Page 163 and 164: DAY 2 KEYNOTE ADDRESS: Advanced Rad
Page 165 and 166: - 152 - ADVANCED RADIOGRAPHY FOR TR
Page 167 and 168: - 154 - for light weight and resist
Page 169 and 170: - 156 - available. Application exam
Page 171 and 172: - 158 - 28. V.J. Orphan, Science Ap
Page 173 and 174: CROSS SLIDE - 160 - AXIAL DRIVE : 3
Page 175 and 176: - 162 - Fig. 4. Two neutron radiogr
Page 177 and 178: INTRODUCTION (Continued) - 164 - Pr
Page 179 and 180: - 166 - SENSITOMETRIC QUALITY CONTR
Page 181 and 182: - 168 - MAKING THE TRANSITION TO AU
Page 183 and 184: (Continued) - 170 - The primary mec
Page 185 and 186: UJNXKAST o Indicated: o Calculated:
Page 187 and 188: - 174 - F»LM_i5=l£B_ DATE22=22=ß
Page 189 and 190: - 176 - RECENT MICROFUCUS X~RAY IMA
Page 191 and 192: ABSTRACT - 178 - WET CHANNEL INSPEC
Page 193 and 194: - 180 - 5) an eddy current probe to
Page 195 and 196: - 182 - tube, say 0.5-1.0 metre, so
Page 197 and 198: ACKNOWLEDGEMENTS - 184 - Many peopl
Page 199 and 200: - 186 - TABLE 3 Operational Objecti
Page 201 and 202: Pressure Tube Fuel -Carter Spring S
Page 203 and 204: «AC UUSU«O«HII INCUMKTM - 190 -
Page 205 and 206: Inlet or Outlet £nd Outlet 2m - 19
Page 207 and 208: - 194 - AN ADVANCED HEAT EXCHANGER
Page 209 and 210: - 196 - storage terminal. However,
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2.4 Data Processing Subsystem 2.4.1
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- 200 - display parameter set could
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5. PLAYBACK - 202 - A tape playback
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" * 0 0 MOkE* i SUN! SOW A 1 3* ~V
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SLHHT POU 422/14 - 206 - x •* F-R
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- 208 - The recent failure of a Zir
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- 210 - probe in its operating envi
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- 212 - The eddy current and wall t
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6. SUMMARY - 214 - The failure of a
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+2.5%p Lift Off •* - 216 - +5% Wa
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0 -0.2 -0.4 -0.6 -0.8 -1.0 c .1 2 o
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0 -0.25 -0.50 -0.75 -1.00 -1.25 i 1
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- 222 - CHECKING FOR CRACKS IN GAS
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- 224 - on the fringes. (The sensit
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Figure 1 18 MW gas turbine rotor, p
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- 228 - Figure 3 Weak penetrant ind
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- 230 - Figure 7 All signals superi
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- 232 - Figure 11 Frequency respons
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- 234 - row 3 sent to 0 4 n 1Vor?d.
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1. INTRODUCTION - 236 - In-service
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- 238 - treatment, and bending are
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- 240 - With an AC coil surrounding
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- 242 - against magnet position, tr
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6. SUMMARY - 244 - Conventional edd
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10 1 Centre Magnet 2 Keepers 3 End
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A - II' Concentric Groove 0.1 mm de
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- 250 ON THE RELATION BETWEEN ULTRA
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- 252 - Following a brief descripti
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CONCLUSION - 254 - In order to veri
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- 256 - 13. R.L. Smith, F.L. Rusbri
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Ultrasonic Instrumentation - 258 -
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100 a (m" 1 ) 10 f Slope = 4 10 - 2
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- 262 - ACOUSTIC EMISSION TESTING O
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- 264 - Metal components with class
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- 266 - Any recognizable fibre dama
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- 268 - FIGURE 1 EXPULSION OF FIBRE
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100 95 LU LU 5 S 90 ^"-85 K H H 80
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- 272 - FIGURE 6 SENSORS AND PREAMP
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900 800 700 i/> 600 H Z O 500 U 400
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- 276 - ACOUSTIC SORTING OF GRINDER
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- 278 - 6e P = Po c - St or p = p0
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- 280 - (9) for hardened steel. All
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- 282 - but not reseted, so the com
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- 284 - GOOD CRACKED 0 2 4 6 8 0 2
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0 - 286 - Figure 5: Resonance frequ
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- 288 - GOOD 0 .8 1.6 2.4 3.2 Level
Page 303 and 304:
- 290 - THE BENEFITS OF NDT TRAININ
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- 292 - C.S.N.D.T. Chapters continu
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- 294 - The groundwork is in place.
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- 296 - The graduates of these prog
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- 298 - CERTIFICATION OF NONDESTRUC
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- 300 - (e) A differing but persist
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250 200 150 100 50 Magnetic Particl
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LOOKING INTO THE FUTURE R.S. Sh.an.
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- 305 - Another 'near future 1 need
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- 307 - NDE OF STRUCTURAL CERAMICS
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- 309 - The system described in thi
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and - 311 - S = a 2j for XR>a (2) S
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TRANSCEIVER digital signal display
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m "O -30 z o Ul -40 u. Ul ce o o Ü
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- 317 - deep penetration in same fo
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- 319 - the density by »w3 to 7%.
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density 10 3 kg/m 3 dissipation fac
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(0 60 g40 «MM "5. 3 O ü Cö §20
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60 PZT7 Vp " - 325 - o A —polariz
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- 327 -
Page 343 and 344:
- 329 - Fig. 8: Typical Outputs of
Page 345 and 346:
- 331 - ULTRASONIC ANALYSIS OF VOID
Page 347 and 348:
- 333 - function is approximated by
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PULSER/RECEIVER OSCILLOSCOPE SPECTR
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to •a I a. a Ê £ < IS i-o 00 -
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Figure 5: Frequency spectra from: (
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- 341 - 100 150 Void Diameter (jjm)
Page 357 and 358:
- 343 - TIME (ns) Figure 9: Peak ti
Page 359 and 360:
- 345 - COMPUTER SIMULATION OF ULTR
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pu = T XX + T Xy tt x y pV = T Xy +
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- 349 - linear system of equations
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- 351 - These boundary conditions a
Page 367 and 368:
10. EXAMPLE - 353 - The following e
Page 369 and 370:
3 "/A ! - 355 - 1 I 2 I Figs. 1-4.
Page 371 and 372:
INTRODUCTION - 357 - The inspection
Page 373 and 374:
- 359 - A 3 by k array was construc
Page 375 and 376:
INVERSION PROBLEM - 361 - The inver
Page 377 and 378:
- 363 - the right of coils 1 to 6,
Page 379 and 380:
—- ••;•••• 'IM i lüi
Page 381 and 382:
- 3hl 2 3 4 OISTANCE (mm) Figure h.
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- 369 - a) 0.080 X 0.010 X 0.004" 5
Page 385 and 386:
- 371 - DISTANCE ;,n(m) Figure 9b
Page 387 and 388:
- 373 - INTRODUCTION X-ray diffract
Page 389 and 390:
and - 375 - e a -^(a + a ) + —-
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- 377 - The commercial prototype is
Page 393 and 394:
- 379 - REFERENCES 1) Klug, H.P. an
Page 395 and 396:
- 381 - incident x-ray beam diffrac
Page 397 and 398:
- 383 - Fig. 5(a). 200 W X-ray tube
Page 399 and 400:
- 385 - Fig. 7. Head of the commerc
Page 401 and 402:
- 387 - APPLICATIONS OF NEUTRON DIF
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peaks which are easily measurable.
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- 391 - directions around the circu
Page 407 and 408:
I.-3 TRIPLE-AXIS NEUTRON SPECTROMET
Page 409 and 410:
Ad hki£ d hkil xlO 3 - 395 - INTER
Page 411 and 412:
- 397 - Fig. 5 Longitudinal, tangen
Page 413 and 414:
I - INTRODUCTION - 399 - Polyethyle
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- 401 - This together with the expr
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- 403 - (5v/v)fit must be considere
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Transducer Signal - 405 - P.E.(p.v)
Page 421 and 422:
ü .CO ü m O o CÖ g •4—> Q 2.
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- 409 - The present study was carri
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- 411 - Since tomographlc Images ar
Page 427 and 428:
- 413 - bore axis, were scanned. Th
Page 429 and 430:
- 415 - normally measured with a sh
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(a) L (b) ic) 1 - 417 - •HwK- |3A
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Figure A : Orientation of the casti
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- 421 - APPENDIX A Determination of
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ÜJ I/) 1 ce TO PE/ a. 100 90 - 80
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- 425 - This paper will concentrate
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- 427 - Ultrasonic and radiographie
Page 443 and 444:
- 429 - A micrograph of the laminat
Page 445 and 446:
- 431 - 2. Holography requires disp
Page 447 and 448:
- 433 - 10. Green, D.R., Schneller,
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- 4 35 - Fig. 2 (a): cross-section
Page 451 and 452:
10 _ 0.1 1_ 0.01 0.1 1 - 437 - TIME
Page 453 and 454:
• •' '
Page 455 and 456:
HEATING PULSES DETECTOR " -—FILTE
Page 457 and 458:
- 443 - 5 10 POSITION (mm) Fig. 10
Page 459 and 460:
- 445 - MATERIALS EFFECTS ON ACOUST
Page 461 and 462:
- 447 - orientation of these specim
Page 463 and 464:
- 449 - determined experimentally f
Page 465 and 466:
STRUCTURE •^ TRANSDUCER (S) - 451
Page 467 and 468:
- 453 - 500 PRESSURE (KPO) LEAK DIA
Page 469 and 470:
Caron, V. Energy Mines & Resources
Page 471 and 472:
Mclntyre, Dent Babcock & Wilcox Can
Page 473:
ISSN 0067-0367 To identify individu
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