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Introduction to the development
of NDE techniques for utilities
and refineries in Taiwan
Yung-How Wu
2009.05.08
Outlines
 Development of remote operated inspection
technique for ABWR RIP pipe welds
 Study of Ultrasonic Techniques on the Inspection
of NPP Components
 Development of Automated Electromagnetic
Techniques for Inspecting Inner Cracks of LPG
Tanks
 Reliability Assessment of Automated Eddy
Current System for Turbine Blades
 Inspection of HTHA on Reactors in CPC Refinery
Development of remote operated
inspection technique for ABWR RIP
pipe welds
Background
 The Taipower ABWR under construction was developed
by working group of GE, Nippon Tokyo Electric, Hitachi
and Toshiba. And, the vessel was constructed by Bobcock
and Hitachi K.K..
 One of major differences between ABWR and
conventional BWR is the five pairs of RIP(Reactor
Internal Pump)designed for independent cooling water
circulation. Each RIP was connected to the RPV by a
circumferential weld located in narrow gap as shown in
Fig. 1.
 Automated NDE method and scanner is required for the
inspection of RIP circumferential weld located in the
narrow gap in future ISI.
Objectives
 To develop a special scanner to carry UT, camera
or even ET probes to inspect the RIP
circumferential weld located in the narrow gap.
 To order special PA probes for narrow gap
inspection.
 To develop remote controlled inspection method
and procedures for performance demonstration in
Taiwan or EPRI before ISI.
RIP and Inspection Location
ABWR
RPV
RIP
18mm gap
RIP weld
System configuration for RIP inspection
Ultrasonic PA system to use
 Wesdyne IntraPhase 32/128
 4 probes may be used at one time
Mock up for PD
 To simulate RIP
 Reference sample installed
 To practice scanner
assembling and dissembling
 To develop remote
controlled inspection method
and practice for PD training
Study of Ultrasonic Techniques on
the Inspection of NPP Components
Objective
Using low frequency TRLPA probes to
evaluate the inspection of various nuclear
power plant components in PWR or
ABWR in Taiwan and, to determine the
detectability and testing parameters of this
TRLPA technique for dissimilar metal
welds or coarse grain materials used.
Inspection difficulties for
DMW, CSS & RIP
 Cast or forged stainless steel and nickel alloy
materials are commonly used for piping
components or jointed by Dissimilar Metal Welds
as reactor coolant system (RCS) pipings. And,
inspection difficulties arose mainly due to:
 Ultrasonic reflection from interface.
 Ultrasonic scattering of coarse grains which
reduced S/N ratio.
 Ultrasonic distortion due to velocity change in
anisotropic microstructures.
Typical construction of DMW
 Nozzle:Carbon Steel with Cladding.
 Buttering:Nickel Alloy.
 Weld:Nickel Alloy.
 Piping:Stainless Steel.
Cracks & Notches
on either sides of weld
No. 25
Macrostructure of CSS Samples
 No. 8 & No. 11:Columnar and Coarse grained structure, the max.
grain size is around 17 mm in outer region of the sample.
 No. 25:Equiaxed Grain, Average Grain Size is around 0.2 mm in
all region.
No. 8 No. 11
PA System
& TRLPA probes
 Zetec OmniScan MX
 Pulse Width:30 ~ 500 ns
 Bandwidth: 0.52~19 MHz
 Imasonic TRLPA
 Array:2D (2-3×11)
 Frequency: 1.5 MHz
PAUT Results of DMW sample
 Axial flaw A2 located in
buttering, inspected with
TRLPA probe by using
28~43 LW law.
 Circumferential flaw C1
located in pipe side. Two
components of the clustered
flaws can be clearly
distinguished.
PAUT Results of DMW sample
Flaw
No.
Type Location L
(mm)
H
(mm)
Detection (SNR) L-
6dB
(mm)
H
meas.
(mm)
ESL
(mm)
ESH
(mm)
From Pipe
(dB)
From Nozzle
(dB)
NP1 Cir.
Notch
Pipe 53.8 5.8 24 NA 60.1 6.6 6.3 0.8
NN1 Cir.
Notch
Nozzle 54.1 5.8 NA 14 62.0 4.4 7.9 -1.45
C1 Crack Pipe 50.8 7.9 13 9 62.1 8.0 11.3 0.1
C3 Crack Buttering 45.7 6.3 12 10 48.0 6.7 2.3 0.4
C5 Crack Nozzle 40.6 13.4 11 17 48.1 14.7 7.5 1.3
A2 Crack Buttering 30.5 11.9 14 18 30.0 10.8 -0.5 -1.1
 All cracks were detected from both sides.
 The through-wall sizing error was less than 1.5mm in all cases.
Inspection Results (CSS No. 25)
Cir Notch
Depth: 7.6 mm
SNR:32 dB
Axial Notch
Depth: 7.6 mm
SNR:35 dB
SNR: 40 dB
SNR: 37 dB
SNR: 36 dB
 SDH  4.7 mm
Inspection Results – CSS No. 11
No. 11 - Notch
Cir Notch:Length 28.4 mm, Depth 6.4 mm.
TPC 2D probe (1.5 MHz)
Inspection Results of RIP sample
PA probe:Imasonic 1.5M16×2E32-7.
Circumferential Inner Notch:LD = 50.8mm0.7mm.
Linear Scan, Refraction angle:45.
Inner Notch
Inspection Results of RIP sample
PA probe:Imasonic 1.5M16×2E32-7.
Circumferential Inner Notch:LD = 50.8mm0.7mm.
Linear Scan, Refraction angle:25.
Inner Notch
Conclusions
 The low frequency L-wave generated by 1.0 MHz dual 2D matrix array
probes allow for reliable detection of all cracks through the dissimilar
metal weld and the buttering.
 The 1.5 MHz 2D TRLPA probes are also able to detect all reflectors in
cast stainless steel and RIP samples in our cases.
 The corner trap signals of surface-breaking flaws were found more
obvious with lower refraction angle beam around 20.
 Using Imasonic 1.5M16×2E32-7 PA probe, the notches in SS weld were
detected with high S/N ratio at low incident angles around 25. The
result suggested lower angle rather 45 is more suitable for the surface
breaking crack inspection in some cases.
Development of Automated
Electromagnetic Techniques for
Inspecting Inner Cracks of LPG Tanks
Objective
To integrate an automated
ElectroMagnetic Array based system for
inspecting inner surface cracks on LPG
Tanks.
Background
 LPG tanks were frequently subjected to SCC on
inner surface during service and must be
inspected from inside regularly.
 Conventional ISI by MT or PT is toilsome and
costly.
 Extremely hot working condition inside in summer
 Scaffolding & epoxy coating removal for inspection
 EMA/ACFM has been used to detect surface
breaking cracks without removing coating on
components.
Electromagnetic Array
Techniques
V2/V1 = (2d + △) / △
∴ d =△/2((V2/V1) – 1)
V1
Span = △
V2
d
Surface
current Surface crack
Current
perturbation
Surface current
Crack tip
ACPD EMA or ACFM
Benefits of
EMA/ACFM techniques
 Capable of measuring both crack depth and length.
 Inspecting cracks without removal of surface
coating up to several millimeters and hence
reducing cost and time.
 Inspection results may be kept as digital records
for better review and monitor.
 Various signal displays are helpful in defect
discrimination.
Samples with Artificial Cracks
Notches Cracks
Block
Defect(mm)
Type
Depth
Lengt
h
Positn
Weld-6 Toe Crack ~2mm 12 30
Weld-9
Centerline
Crack
~2mm 13 38
41210
150
Plate-1
A group
B group
C group
Defect(mm)
Type/Positn Depth Length Width
Notch/A群
2 40 0.25
2 20 0.25
2 10 0.25
Characteristic Defect Signals
 A single defect may be detected by three successive EMA channels.
 Defect could be clearly identified by various displays.
Abs Abs
Corr
Imp
Probe scanning & Defect
detection
 Automatic scanner was used to move the probe with
different orientations.
 Transparencies were stacked between probe and sample to
create different lift-off .
Sample plate
with cracks
Probe
Auto scanner
Transparencies
Scanning
direction
Notch
axial
Crack
axial
Scanning
direction
Signals in Various Conditions
實驗1_Plate1_Plate2
0
1
2
3
4
5
6
0 1 2 3 4 5 6 7
實際深度(mm)
量測深度(mm)
 Weakest response at 380
 Amplitude decreased exponentially
with Lift-Off
 Measuring error could be
controlled down to ±25%
0
2
4
6
8
0 20 38 50 90
角度 o
振幅
1張
5張
15張
10mmx1mm 裂縫
0
5
10
0 10 20 30
投影片張數
振幅(Max/Min)
數列1
Automated Inspection System
 EMA System
 Lizard solo
 64 channels SDDPU
 Scanner Control Console
 PC + TFT monitor
 Motor control module
 Motion control &
monitoring package
 CCD camera and 2-axis
stage
 Scanner
 With 4 magnetic rollers
 Carrying 32-channel
probe
Control Console
EMA System
CCD Camera
Direct Cable Connection
NTSC Standard
Motor Control
Position Sense
EMA Signal
Automated Inspection Method
 Weld and Plate regions were
Inspected individually
 Weld: along the weldment
 Plate: as shown
 Scanner was moved to the top
position and then scan
automatically on each path.
 Scanning route was
monitored by CCD camera
and full coverage was assured.
CCD Camera
NTSC Standard
Position Sense
Frame GrabberCard
LPG Tank Steel Plate
Field of View
Real Scan Path
Ideal Trajectory
Field Trials
 Scanning is controlled and
monitored through CCD camera
by inspector operating below the
LPG tank.
Conclusions
Laboratory and preliminary field trials proved
the method satisfactory in detecting real
cracks down to 10mm in length and 1mm in
depth in both regions. However, minor
improvement on the scanner manipulation is
required before practical application.
Reliability Assessment of
Automated Eddy Current System for
Turbine Blades
Objective
 to develop an automated eddy current
method assisted by a self-aligned
manipulator scanning along the disk rim of
Westinghouse turbine. The light-weighted
manipulator was mainly designed for
inspecting blade on L-2 stage disk where
root cracks were most frequently found
during ISI.
Background
 Blades and disk rim of turbine were
frequently subjected to fatigue cracking and
resulted in unscheduled shutdown and even
more a total failure of turbines. Hence,
reliable routine inspection is crucial to
operation safety and efficiency of turbines
operation.
Westinghouse turbine blade &
scanner designed for inspection
Airfoil-trail Edge
Airfoil-lead Edge
Scanning method with EC probe
Reliability Accessment
Definition of defect size vs signal
amplitude
Flowchart of POD analysis
Data collection and analysis
Conclusions
The signal response analysis was used to establish
the practical reliability analysis method for this
automated eddy current inspection system. The
probability of detection curve was shown as a unit
step function which indicated the quality of the
system was good enough. When defect length was
greater than 0.5mm the POD was almost 100%,
However, the result was obtained from a mock up
in a well-controlled experimental environment
then further test should be carried out in the field.
Inspection of HTHA on Reactors
in CPC Refinery
Reactors and surface condition
HTHA inspection areas
HTHA inspection in the field
HTHA problem and inspection method
TOFD results to identify and
measure HYHA crack
Results

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Introduction to NDE automation1.pdf

  • 1. Introduction to the development of NDE techniques for utilities and refineries in Taiwan Yung-How Wu 2009.05.08
  • 2. Outlines  Development of remote operated inspection technique for ABWR RIP pipe welds  Study of Ultrasonic Techniques on the Inspection of NPP Components  Development of Automated Electromagnetic Techniques for Inspecting Inner Cracks of LPG Tanks  Reliability Assessment of Automated Eddy Current System for Turbine Blades  Inspection of HTHA on Reactors in CPC Refinery
  • 3. Development of remote operated inspection technique for ABWR RIP pipe welds
  • 4. Background  The Taipower ABWR under construction was developed by working group of GE, Nippon Tokyo Electric, Hitachi and Toshiba. And, the vessel was constructed by Bobcock and Hitachi K.K..  One of major differences between ABWR and conventional BWR is the five pairs of RIP(Reactor Internal Pump)designed for independent cooling water circulation. Each RIP was connected to the RPV by a circumferential weld located in narrow gap as shown in Fig. 1.  Automated NDE method and scanner is required for the inspection of RIP circumferential weld located in the narrow gap in future ISI.
  • 5. Objectives  To develop a special scanner to carry UT, camera or even ET probes to inspect the RIP circumferential weld located in the narrow gap.  To order special PA probes for narrow gap inspection.  To develop remote controlled inspection method and procedures for performance demonstration in Taiwan or EPRI before ISI.
  • 6. RIP and Inspection Location ABWR RPV RIP 18mm gap RIP weld
  • 7. System configuration for RIP inspection
  • 8. Ultrasonic PA system to use  Wesdyne IntraPhase 32/128  4 probes may be used at one time
  • 9. Mock up for PD  To simulate RIP  Reference sample installed  To practice scanner assembling and dissembling  To develop remote controlled inspection method and practice for PD training
  • 10. Study of Ultrasonic Techniques on the Inspection of NPP Components
  • 11. Objective Using low frequency TRLPA probes to evaluate the inspection of various nuclear power plant components in PWR or ABWR in Taiwan and, to determine the detectability and testing parameters of this TRLPA technique for dissimilar metal welds or coarse grain materials used.
  • 12. Inspection difficulties for DMW, CSS & RIP  Cast or forged stainless steel and nickel alloy materials are commonly used for piping components or jointed by Dissimilar Metal Welds as reactor coolant system (RCS) pipings. And, inspection difficulties arose mainly due to:  Ultrasonic reflection from interface.  Ultrasonic scattering of coarse grains which reduced S/N ratio.  Ultrasonic distortion due to velocity change in anisotropic microstructures.
  • 13. Typical construction of DMW  Nozzle:Carbon Steel with Cladding.  Buttering:Nickel Alloy.  Weld:Nickel Alloy.  Piping:Stainless Steel.
  • 14. Cracks & Notches on either sides of weld
  • 15. No. 25 Macrostructure of CSS Samples  No. 8 & No. 11:Columnar and Coarse grained structure, the max. grain size is around 17 mm in outer region of the sample.  No. 25:Equiaxed Grain, Average Grain Size is around 0.2 mm in all region. No. 8 No. 11
  • 16. PA System & TRLPA probes  Zetec OmniScan MX  Pulse Width:30 ~ 500 ns  Bandwidth: 0.52~19 MHz  Imasonic TRLPA  Array:2D (2-3×11)  Frequency: 1.5 MHz
  • 17. PAUT Results of DMW sample  Axial flaw A2 located in buttering, inspected with TRLPA probe by using 28~43 LW law.  Circumferential flaw C1 located in pipe side. Two components of the clustered flaws can be clearly distinguished.
  • 18. PAUT Results of DMW sample Flaw No. Type Location L (mm) H (mm) Detection (SNR) L- 6dB (mm) H meas. (mm) ESL (mm) ESH (mm) From Pipe (dB) From Nozzle (dB) NP1 Cir. Notch Pipe 53.8 5.8 24 NA 60.1 6.6 6.3 0.8 NN1 Cir. Notch Nozzle 54.1 5.8 NA 14 62.0 4.4 7.9 -1.45 C1 Crack Pipe 50.8 7.9 13 9 62.1 8.0 11.3 0.1 C3 Crack Buttering 45.7 6.3 12 10 48.0 6.7 2.3 0.4 C5 Crack Nozzle 40.6 13.4 11 17 48.1 14.7 7.5 1.3 A2 Crack Buttering 30.5 11.9 14 18 30.0 10.8 -0.5 -1.1  All cracks were detected from both sides.  The through-wall sizing error was less than 1.5mm in all cases.
  • 19. Inspection Results (CSS No. 25) Cir Notch Depth: 7.6 mm SNR:32 dB Axial Notch Depth: 7.6 mm SNR:35 dB SNR: 40 dB SNR: 37 dB SNR: 36 dB  SDH  4.7 mm
  • 20. Inspection Results – CSS No. 11 No. 11 - Notch Cir Notch:Length 28.4 mm, Depth 6.4 mm. TPC 2D probe (1.5 MHz)
  • 21. Inspection Results of RIP sample PA probe:Imasonic 1.5M16×2E32-7. Circumferential Inner Notch:LD = 50.8mm0.7mm. Linear Scan, Refraction angle:45. Inner Notch
  • 22. Inspection Results of RIP sample PA probe:Imasonic 1.5M16×2E32-7. Circumferential Inner Notch:LD = 50.8mm0.7mm. Linear Scan, Refraction angle:25. Inner Notch
  • 23. Conclusions  The low frequency L-wave generated by 1.0 MHz dual 2D matrix array probes allow for reliable detection of all cracks through the dissimilar metal weld and the buttering.  The 1.5 MHz 2D TRLPA probes are also able to detect all reflectors in cast stainless steel and RIP samples in our cases.  The corner trap signals of surface-breaking flaws were found more obvious with lower refraction angle beam around 20.  Using Imasonic 1.5M16×2E32-7 PA probe, the notches in SS weld were detected with high S/N ratio at low incident angles around 25. The result suggested lower angle rather 45 is more suitable for the surface breaking crack inspection in some cases.
  • 24. Development of Automated Electromagnetic Techniques for Inspecting Inner Cracks of LPG Tanks
  • 25. Objective To integrate an automated ElectroMagnetic Array based system for inspecting inner surface cracks on LPG Tanks.
  • 26. Background  LPG tanks were frequently subjected to SCC on inner surface during service and must be inspected from inside regularly.  Conventional ISI by MT or PT is toilsome and costly.  Extremely hot working condition inside in summer  Scaffolding & epoxy coating removal for inspection  EMA/ACFM has been used to detect surface breaking cracks without removing coating on components.
  • 27. Electromagnetic Array Techniques V2/V1 = (2d + △) / △ ∴ d =△/2((V2/V1) – 1) V1 Span = △ V2 d Surface current Surface crack Current perturbation Surface current Crack tip ACPD EMA or ACFM
  • 28. Benefits of EMA/ACFM techniques  Capable of measuring both crack depth and length.  Inspecting cracks without removal of surface coating up to several millimeters and hence reducing cost and time.  Inspection results may be kept as digital records for better review and monitor.  Various signal displays are helpful in defect discrimination.
  • 29. Samples with Artificial Cracks Notches Cracks Block Defect(mm) Type Depth Lengt h Positn Weld-6 Toe Crack ~2mm 12 30 Weld-9 Centerline Crack ~2mm 13 38 41210 150 Plate-1 A group B group C group Defect(mm) Type/Positn Depth Length Width Notch/A群 2 40 0.25 2 20 0.25 2 10 0.25
  • 30. Characteristic Defect Signals  A single defect may be detected by three successive EMA channels.  Defect could be clearly identified by various displays. Abs Abs Corr Imp
  • 31. Probe scanning & Defect detection  Automatic scanner was used to move the probe with different orientations.  Transparencies were stacked between probe and sample to create different lift-off . Sample plate with cracks Probe Auto scanner Transparencies Scanning direction Notch axial Crack axial Scanning direction
  • 32. Signals in Various Conditions 實驗1_Plate1_Plate2 0 1 2 3 4 5 6 0 1 2 3 4 5 6 7 實際深度(mm) 量測深度(mm)  Weakest response at 380  Amplitude decreased exponentially with Lift-Off  Measuring error could be controlled down to ±25% 0 2 4 6 8 0 20 38 50 90 角度 o 振幅 1張 5張 15張 10mmx1mm 裂縫 0 5 10 0 10 20 30 投影片張數 振幅(Max/Min) 數列1
  • 33. Automated Inspection System  EMA System  Lizard solo  64 channels SDDPU  Scanner Control Console  PC + TFT monitor  Motor control module  Motion control & monitoring package  CCD camera and 2-axis stage  Scanner  With 4 magnetic rollers  Carrying 32-channel probe Control Console EMA System CCD Camera Direct Cable Connection NTSC Standard Motor Control Position Sense EMA Signal
  • 34. Automated Inspection Method  Weld and Plate regions were Inspected individually  Weld: along the weldment  Plate: as shown  Scanner was moved to the top position and then scan automatically on each path.  Scanning route was monitored by CCD camera and full coverage was assured. CCD Camera NTSC Standard Position Sense Frame GrabberCard LPG Tank Steel Plate Field of View Real Scan Path Ideal Trajectory
  • 35. Field Trials  Scanning is controlled and monitored through CCD camera by inspector operating below the LPG tank.
  • 36. Conclusions Laboratory and preliminary field trials proved the method satisfactory in detecting real cracks down to 10mm in length and 1mm in depth in both regions. However, minor improvement on the scanner manipulation is required before practical application.
  • 37. Reliability Assessment of Automated Eddy Current System for Turbine Blades
  • 38. Objective  to develop an automated eddy current method assisted by a self-aligned manipulator scanning along the disk rim of Westinghouse turbine. The light-weighted manipulator was mainly designed for inspecting blade on L-2 stage disk where root cracks were most frequently found during ISI.
  • 39. Background  Blades and disk rim of turbine were frequently subjected to fatigue cracking and resulted in unscheduled shutdown and even more a total failure of turbines. Hence, reliable routine inspection is crucial to operation safety and efficiency of turbines operation.
  • 40. Westinghouse turbine blade & scanner designed for inspection Airfoil-trail Edge Airfoil-lead Edge
  • 43. Definition of defect size vs signal amplitude
  • 44. Flowchart of POD analysis
  • 46. Conclusions The signal response analysis was used to establish the practical reliability analysis method for this automated eddy current inspection system. The probability of detection curve was shown as a unit step function which indicated the quality of the system was good enough. When defect length was greater than 0.5mm the POD was almost 100%, However, the result was obtained from a mock up in a well-controlled experimental environment then further test should be carried out in the field.
  • 47. Inspection of HTHA on Reactors in CPC Refinery
  • 48. Reactors and surface condition
  • 50. HTHA inspection in the field
  • 51. HTHA problem and inspection method
  • 52. TOFD results to identify and measure HYHA crack