FIFTH CANADIAN CONFERENCE ON NONDESTRUCTIVE ... - IAEA

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ROLLED JOINT CALANDRIA TUBE rs.5 - 215 - PRESSURE TUBE 6.03 H .5 MM, ROLLED JOINT FIGURE 1 FUEL CHANNEL EXHIBITINC PRESSURE TUBE SAC Pressure Tube Recei ve Coils Send Coil FIGURE 2 Send Coil THE EDDY CURRENT GAPPROBE ä 3 Receive Coils (Wound in Opposition ) > =J Pressure Calandria Tube Tube
+2.5%p Lift Off •* - 216 - +5% Wall Thickness -5% Wall Thickness -5% Wall Thickness FIGURE 3 Cap = 8 mm p = 74 \iti-cm (Zirc II) Wall Thickness = 5.0 mm COMPUTER PREDICTED COMPLEX PLANE RESP<strong>ON</strong>SE OF THE CAP PROBE -2.5%p
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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
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- 98 - characterization program bas
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- 100 - 1. Planar transducer: l.a.
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Fig. 1 1/JS - 102 - Echos observed
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- 104 - CAPABILITIES/LIMITATIONS OF
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- 106 - V = f* - 0.9 ak N [2] h. /^
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DISCUSSION - 108 - The results of t
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- 110 - FIGURE 1: Equipment Used fo
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FIGURE 4: - 112 - 5 10 IS 10 Depth
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FIGURE 6: Output of Computer Modell
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- 116 - "Events on earth consist in
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- 118 - now _n = Af (5) n where Af
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- 120 - REFERENCES 1. J.K. Feiblema
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PULSER IMMERSION TRANSDUCER WATER ^
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- 124 - 6. Ultrasonic frequency spe
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i I 1 i l - 126 - —j 10. Ultrason
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TIME RNFOSIS PLOT CRSF: - 128 - 1H.
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- 130 - THE INTRODUCTION OF REAL-TI
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5. QUALIFYING THE IMAGE - 132 - In
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- 134 - CONVENTIONAL FILM RADIOGRAP
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- 136 - 11.3 Computer Management of
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- 138 - Back end of system. The com
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- IAO - to be loaded properly into
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20. OPERATIONAL UTILIZATION - 142 -
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% -•'v/ FILM AND SCREENS ' \ INSI
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- 146 - By design, these A/E monito
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- 148 - a) enables an A/E monitor s
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- 150 - OTHER . CHANNELS CONVENTION
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DAY 2 KEYNOTE ADDRESS: Advanced Rad
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- 152 - ADVANCED RADIOGRAPHY FOR TR
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- 154 - for light weight and resist
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- 156 - available. Application exam
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- 158 - 28. V.J. Orphan, Science Ap
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CROSS SLIDE - 160 - AXIAL DRIVE : 3
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- 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,
Page 211 and 212: 2.4 Data Processing Subsystem 2.4.1
Page 213 and 214: - 200 - display parameter set could
Page 215 and 216: 5. PLAYBACK - 202 - A tape playback
Page 217 and 218: " * 0 0 MOkE* i SUN! SOW A 1 3* ~V
Page 219 and 220: SLHHT POU 422/14 - 206 - x •* F-R
Page 221 and 222: - 208 - The recent failure of a Zir
Page 223 and 224: - 210 - probe in its operating envi
Page 225 and 226: - 212 - The eddy current and wall t
Page 227: 6. SUMMARY - 214 - The failure of a
Page 231 and 232: 0 -0.2 -0.4 -0.6 -0.8 -1.0 c .1 2 o
Page 233 and 234: 0 -0.25 -0.50 -0.75 -1.00 -1.25 i 1
Page 235 and 236: - 222 - CHECKING FOR CRACKS IN GAS
Page 237 and 238: - 224 - on the fringes. (The sensit
Page 239 and 240: Figure 1 18 MW gas turbine rotor, p
Page 241 and 242: - 228 - Figure 3 Weak penetrant ind
Page 243 and 244: - 230 - Figure 7 All signals superi
Page 245 and 246: - 232 - Figure 11 Frequency respons
Page 247 and 248: - 234 - row 3 sent to 0 4 n 1Vor?d.
Page 249 and 250: 1. INTRODUCTION - 236 - In-service
Page 251 and 252: - 238 - treatment, and bending are
Page 253 and 254: - 240 - With an AC coil surrounding
Page 255 and 256: - 242 - against magnet position, tr
Page 257 and 258: 6. SUMMARY - 244 - Conventional edd
Page 259 and 260: 10 1 Centre Magnet 2 Keepers 3 End
Page 261 and 262: A - II' Concentric Groove 0.1 mm de
Page 263 and 264: - 250 ON THE RELATION BETWEEN ULTRA
Page 265 and 266: - 252 - Following a brief descripti
Page 267 and 268: CONCLUSION - 254 - In order to veri
Page 269 and 270: - 256 - 13. R.L. Smith, F.L. Rusbri
Page 271 and 272: Ultrasonic Instrumentation - 258 -
Page 273 and 274: 100 a (m" 1 ) 10 f Slope = 4 10 - 2
Page 275 and 276: - 262 - ACOUSTIC EMISSION TESTING O
Page 277 and 278: - 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
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- 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 -
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- 329 - Fig. 8: Typical Outputs of
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- 331 - ULTRASONIC ANALYSIS OF VOID
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- 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)
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- 343 - TIME (ns) Figure 9: Peak ti
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- 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
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10. EXAMPLE - 353 - The following e
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3 "/A ! - 355 - 1 I 2 I Figs. 1-4.
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INTRODUCTION - 357 - The inspection
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- 359 - A 3 by k array was construc
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INVERSION PROBLEM - 361 - The inver
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- 363 - the right of coils 1 to 6,
Page 379 and 380:
—- ••;•••• 'IM i lüi
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- 3hl 2 3 4 OISTANCE (mm) Figure h.
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- 369 - a) 0.080 X 0.010 X 0.004" 5
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- 371 - DISTANCE ;,n(m) Figure 9b
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- 373 - INTRODUCTION X-ray diffract
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and - 375 - e a -^(a + a ) + —-
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- 377 - The commercial prototype is
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- 379 - REFERENCES 1) Klug, H.P. an
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- 381 - incident x-ray beam diffrac
Page 397 and 398:
- 383 - Fig. 5(a). 200 W X-ray tube
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- 385 - Fig. 7. Head of the commerc
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- 387 - APPLICATIONS OF NEUTRON DIF
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peaks which are easily measurable.
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- 391 - directions around the circu
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I.-3 TRIPLE-AXIS NEUTRON SPECTROMET
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Ad hki£ d hkil xlO 3 - 395 - INTER
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- 397 - Fig. 5 Longitudinal, tangen
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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)
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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
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- 413 - bore axis, were scanned. Th
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- 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
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- 429 - A micrograph of the laminat
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- 431 - 2. Holography requires disp
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- 433 - 10. Green, D.R., Schneller,
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- 4 35 - Fig. 2 (a): cross-section
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10 _ 0.1 1_ 0.01 0.1 1 - 437 - TIME
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• •' '
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HEATING PULSES DETECTOR " -—FILTE
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- 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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FIFTH CANADIAN CONFERENCE ON NONDESTRUCTIVE ... - IAEA

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