CA1108743A - Method and apparatus for automatic ultrasonic flaw detection - Google Patents
Method and apparatus for automatic ultrasonic flaw detectionInfo
- Publication number
- CA1108743A CA1108743A CA282,693A CA282693A CA1108743A CA 1108743 A CA1108743 A CA 1108743A CA 282693 A CA282693 A CA 282693A CA 1108743 A CA1108743 A CA 1108743A
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- Prior art keywords
- signals
- welding
- weld zone
- flaw detection
- output signals
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
- G01N29/36—Detecting the response signal, e.g. electronic circuits specially adapted therefor
- G01N29/38—Detecting the response signal, e.g. electronic circuits specially adapted therefor by time filtering, e.g. using time gates
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
- G01N29/04—Analysing solids
- G01N29/06—Visualisation of the interior, e.g. acoustic microscopy
- G01N29/0609—Display arrangements, e.g. colour displays
- G01N29/0618—Display arrangements, e.g. colour displays synchronised with scanning, e.g. in real-time
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
- G01N29/04—Analysing solids
- G01N29/11—Analysing solids by measuring attenuation of acoustic waves
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
- G01N29/22—Details, e.g. general constructional or apparatus details
- G01N29/26—Arrangements for orientation or scanning by relative movement of the head and the sensor
- G01N29/265—Arrangements for orientation or scanning by relative movement of the head and the sensor by moving the sensor relative to a stationary material
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
- G01N29/22—Details, e.g. general constructional or apparatus details
- G01N29/30—Arrangements for calibrating or comparing, e.g. with standard objects
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/02—Indexing codes associated with the analysed material
- G01N2291/028—Material parameters
- G01N2291/02854—Length, thickness
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/04—Wave modes and trajectories
- G01N2291/044—Internal reflections (echoes), e.g. on walls or defects
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/26—Scanned objects
- G01N2291/263—Surfaces
- G01N2291/2634—Surfaces cylindrical from outside
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/26—Scanned objects
- G01N2291/267—Welds
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- Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Biochemistry (AREA)
- General Health & Medical Sciences (AREA)
- General Physics & Mathematics (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Acoustics & Sound (AREA)
- Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)
- Ultra Sonic Daignosis Equipment (AREA)
- Geophysics And Detection Of Objects (AREA)
Abstract
METHOD AND APPARATUS FOR AUTOMATIC ULTRASONIC FLAW DETECTION
Abstract of the Disclosure Method and apparatus for automatic ultrasonic flaw detection of pipe welding zones wherein the width of the weld zone is divided into a plurality of subdivisions. The ultrasonic energy received from each of the subdivisions is displayed by employing multichannel gate circuitry providing respective outputs in units of 10% of the height of the echoes in each subdivision on a cathode ray tube in synchronization with signals representative of the longitud-inal and lateral position of the probes along the pipe with respect to a reference point. The height of the defective echoes in each gate are printed together with the positions of the probe. The positions of the defects are diagrammed by a computer, thereby enabling high-speed data processing of the flaw detection information, a decrease in the time for precise flaw detection comparable to conventional manual flaw detection method and apparatus and easy determination of the flaw detection results.
Abstract of the Disclosure Method and apparatus for automatic ultrasonic flaw detection of pipe welding zones wherein the width of the weld zone is divided into a plurality of subdivisions. The ultrasonic energy received from each of the subdivisions is displayed by employing multichannel gate circuitry providing respective outputs in units of 10% of the height of the echoes in each subdivision on a cathode ray tube in synchronization with signals representative of the longitud-inal and lateral position of the probes along the pipe with respect to a reference point. The height of the defective echoes in each gate are printed together with the positions of the probe. The positions of the defects are diagrammed by a computer, thereby enabling high-speed data processing of the flaw detection information, a decrease in the time for precise flaw detection comparable to conventional manual flaw detection method and apparatus and easy determination of the flaw detection results.
Description
~31~7~3 Back~roullcl of the rnvelltio Field of the I_vention The present invention relates to automatic and accurate me-thod ancl apparatus capable of detecting rlaws mainly in circumferential weld zones of pipe lines.
Description o-f the Prior Art X-ray penetration testing has conventionally been applied for non-destructive inspective of weld zones. In conjunction with the improved performance of ultrasonic flaw detection appar~tus, the application of ultrasonic flaw detection methods and techniques have recently been required for improved detection accuracy, shortened detection time, safe operation and decreased detection costs. In particular, in the non-destructive inspection of circumferential weld zones for high-pressure pipe lines, such weld zones have been inspected by the combined use of X-ray penetration testing and ultrasonic flaw detection techniques. Ultrasonic ~.~
flaw detection has been performed mainly manually. However, manual ultrasonic flaw detection requires considerable skill and experience for the discrimination of the jamming echoes due to the weld bead, from the flaw echoes and also requires considerable technical skills. Under certain operational conditions, weld flaw detection has to be performed under severe conditions at sites such as common workshops where other operations are also being performed. Such conditions present intolerable burdens to the welding operations and inspectors.
In order to overcome sucn problems, it is desirable to automate welding flaw detection methods and techniques and also the associated necessary data processing, such as ~ .
~ - 2 -' .~ ~
recording and evaluation and the like of the detected results.
SU~lMARY OF THE INVENTION
It is an object oE the invention in accordance with such requirements to provide automatic ultrasonic flaw detection methods and apparatus employing a calcu-lator having an operational function to systematize the data processing of automatic ultrasonic Elaw detection.
The inventior. consists of a method for automat-ically detecting flaws in circumferentially extending pipewelding zones, comprising the steps of: moving a welding flaw detector in at least two different directions in tracking relationship to a weld zone; subdividing the width of said weld zone into a plurality of areas; trans-mitting pulsed energy to said weld zone; generating output signals from a plurality of gate circuits each respect-ively responsive to the echo signals produced by said pulsed energy from a specified one of said areas; generat-ing position signals representative of the position of said flaw detector from a reference point; and displaying said output signals and said position signals in assoc-iated relationship to indicate any welding flaws and their respective positions in each one of said plurality of areas of the weld zone.
The invention also consists of apparatus for automatically detecting flaws in circumferentially extend-ing pipe welding zones, comprising: a welding flaw de-tector movable in at least two different directions in tracking relationship to a welding zone; means for trans-mitting pulsed energy to said welding zone; means for ;~ generating output signals from a plurality of gate ~ circuits each respectively responsive to the echoes .
~ --3--produced by said pulsed ene~gy from a respective one of alike plurality of areas subdividing tlle width of said welding zone; means for generating position signals repre-sentative of the position of said flaw detector from a reference point; and means for displaying said output signals and said position signals in associated relation-ship to indicate any welding flaws and the respective position thereof in each one of said plurality of areas in the weld zone.
BRIEF DESCRIPTION OF T~E DRAWINGS
_, .
Fig. 1 is a side view of a self-propelled carrier flaw detection apparatus according to an embodiment of the invention;
Fig. 2 is a partially cut-away plan view of the self-propelled carrier of Fig. 1 on an enlarged scale;
Fig. 3 is a longitudinal sectional view taken along line III - III in Fig. 2;
Figs. 4A, 4B and 4C are illustrations showing respective scanning patterns of probes of a self-propelled carrier;
Fig. 5 is a block diagram showing data processing apparatus; and Figs. 6A, 6B (with Figs. 4A-C) show respective e~amples of printed records of deteoted flaws as obtained from such apparatus.
DETAILED DBSCRIPTION OF THE PREFERRED E~BODIMENT
The embodiment comprises the ~ollowing components. A
; weld-following mechanism enables the flaw de~ection apparatus to track the weld ~ones with weld detection probe holders.
Motors provide circum-Ferential movement and scanning o~ the probe holders and the probes carried thereby. A detector enables determination o-~ the position oF the `:
.
7~3 probes. A self-propelled carrier on which the probes are mounted detects Elaws by axial scannin~ movements of the probes while the probes are moved along the circum~er-ential weld zone at a predetermined speed (the maximum speed being about 3 m/min.). Display apparatus electri-cally displays the position of the probes and the height of the echoes. A data processing unit automatically prints the detection results.
The apparatus is characterized, in particular, by the incorporation of a data processiny unit comprising a calculator having reading and calculating functions for the high speed processing of the automatic ultrasonic flaw detector.
As shown in Fig. 1, self-propelled carrier 1 is constructed so that probe holders 4 are mounted at the center portion of trestle 2, which is driven by motor 3 for circumferential movement of the trestle. Self-propelled carrier 1 is secured to the outer periphery of pipe 5, which is to be inspected, by a pair of semi-circular holder bands 7, each of which is secured totrestle 2 at one end thereof, and includes a plurality of spaced rollers 6 for maintaining the trestle at a fixed distance from the outer periphery of pipe 6. Holder bands 7 are attached to one another by clamping units 8 attached at the opposing ends of each of the holder bands.
As shown in Figs. 2 and 3, the travelling mechanism of the carrier comprises connecting four driven magnetic rollers 9, respectively mounted at both the front and rear ends of carrier 2, to respective driving shafts 10 driven by gears 9a, 9b which are, in turn, respectively connected to a transmission shaft 11 driven by reduction gears 12, connected to a-shaft of motor 3.
.
The mechanism is thus constructed so that one motor 3 can drive concurrently fo~r magnetic rollers 9. It should be understood that such a mechanism is illustrated only as an exemplary embodiment and other suitable mechanisms can be employed, if desired.
Probe holder 4 travels on rails 16 attached to the inner walls of outer right and left frames 15 by multiple sets of roller mechanisms, each set including two rollers 14 mounted vertically with respect to one 10 another. Probe holder 4 is suspended to be movable verti-cally and in a plane perpendicular thereto with respect to weld zone 17. Probe holder 4 is suspended by connecting outer frame 15 to supporting shaft 18, attached rotatably to carrier 2 through a recess defined at the central portion thereof as illustrated in Figures 2 and 3.
Thereby, probe holder 4 is mounted on carrier 2 so as to be pivotable horizontally about supporting shaft 1~ and to be horizontally movable, at the same time, in a direction perpendicular to weld zone 17.
A rotating shaft, constructed in two independ-~ ently operable sections 20, 20' is threaded through a ;; tapped hole in block B for mounting probes T, T' and each of the shaft sections 20, 20' is driven respectively by scanning motors 19, 19' secured to holder 4 so that either one, or both, probes T, T' can be independently or con-currently moved, as desired, by actuating either motor 19 or 19'. The displacement of both probes T, T' is measured by rotary encoder 21 which measures the axial scan position and the circumferential scan position of both 30 probes T, T' in a manner known to those skilled in the art. Probes T, T' are movable because it is necessary to adjust the distance between end faces of the probes as the ::
.,,~
7~3 width of the weld bead is not constant due to the different radius o~ pipe to be inspectecl.
In the flaw detection of weld zones, it is essential to know the distance between the center of the weld bead and the point of incidence of the ultrasonic wave from the probes T and T'. It is necessary that a mechanism for following the weld bead be used in the auto-matic flaw detection apparatus. Such following mechanisms include optical and electrical types. As such mechanisms are too complex and large to be used in situ at the sites where the pipe lines are being inspected, the apparatus adopts a system wherein four magnets 22 are attached to outer frame 15 o~ probe holder 4 to be magnetically attracted to the pipe on both sides of weld zone 17, thereby enabling probes T and T' to follow the weld zone.
Such a following or tracking mechanism is simple. Probes T, T' can be isolated from any vibration due to the close contact of magnets 22 with the outer surface of the pipe by means well known to those skilled in the art. There-; 20 fore, probes T, T' are always in contact with, or closelyadjacent to, the surface of the pipe and the tracking of the probes with respect to the bead is kept within an accuracy of 2mm, which is sufficient such that no problem is encountered in the practical use of the system.
Probes T, T' each incorporate vibrator Ta for obliquely detecting flaws, and vibrator Tb for perpendic-ularly detecting the reflected waves from the bottom of the material (see Fig. 5). To avoid cluttering the draw-ing, only the electrical connectors to vibrator Tb are shown. The electrical connections to vibrator Ta are the same as those shown for vibrator Tb. Probes T, T' each function to maintain the flaw detecting sensitivity at a constant level by receiving the reflecting waves from the bottom of the material, i.e., the pipe to be inspected, namely from the radially confronting inner sur-face of the pipe, to calibrate the re~lected waves in accordance with the change in the contacting conditions o-f the probe with the material due to the unevenness of the surface thereof. Specifically, the characteristics of the obliquely or perpendicularly incident ultrasonic energy into the material depends on the contacting conditions of the probe with the surface of the material to be inspected. The change in such contacting conditions causes fluctuation in the flaw detecting sensitivity, thereby leading to failures in the evaluation of welding defects. Therefore, it is necessary to calibrate the flaw detecting sensitivity to maintain it at a constant level.
Taking such a requirement into account, the detector employs vibrators Tb in each of probes T, T' which can calibrate - 20 the sensitivity automatically within a range of 20dB.
Such calibration is performed automatically by switching between vibrators Ta and Tb in each of probes T and T'.
Figs. 4A, 4B and 4C show the scanning patterns for only one of probes T, T', as both probes scan in the same manner. Fig. 4A shows lateral or axial scanning, ~ Fig. 4B shows longitudinal or circumferential scanning and ;~ Fig. 4C shows a scanning pattern representing the combined scanning patterns of Figs. 4A and 4B (referred to herein-after as rectangularly lateral scanning). Lateral or axial scanning performs sufficient flaw detection within a skip from 0.5 to 1.0 at a distance from the probe to the center of the bead ranging from 20 to 95mm for pipes having ~' ,~ - 8 -, "
, . ~
~ , - . .
.: .
a thickness t ranging from 8 to 15mm. The pitch for rect-angularly lateral scanning can also be adjusted to a minimum of lmm.
As shown in Fig. 5, the data processing unit for obtaining the results Erom the automatic ultrasonic ~law detector comprises position display 23 which indicates the X and Y coordinates of the position of probes T, T', namely scanning laterally in the axial direction (Y) and longitudinally, circumferentially (X) around the pipe with respect to weld zone 17. Multichannel gate circuitry 24, may for example as illustrated include the channel gates providing outputs in 10~ units of the echo amplitude from each subdivision of the weld zone, defined by subdividing the width of the weld zone into a plurality of sub-divisions. Cathode ray tube 25 displays the echo ampli-tudes from the ten channel gates in multi-channel gate circuitry 24 in synchronization with the signals indicat-ing the respective position of the probes. Printer 26 prints the echo amplitudes of any welding defects that are ~0 present, as determined by the ten channel gate output, ` together with the position of the probes.
In the operation of the automatic flaw detecting apparatus using the aforedescribed detector, self-propelled carrier 1 is mounted on pipe 5 over weld zone 17, which is to be inspected. After setting the correct distance from the welded bead to the probes T, T', carrier 1 is conveyed circumferentially in the direction X along-side the welded bead. Probes T, T' are laterally moved in the axial direction Y relative to weld zone 17 to carry 30 out the flaw detection. The positions of the probes are displayed by position display 23 and at the same time, the echo amplitudes are displayed on cathode ray tube 25.
; B~ -9-~ . .
.. . , ~ . . . . ... . .
The display of the probe signals frorn either probe T or ~r~
can be selectively displayed by a switch (not shown) in accordance with teachings well known to those skille~ in the art. The presence of echo 27 indicates a defect with-in any of the channel gates of multi-channel gate circuitry 24. The displayed echoes are always in synchronization with the lateral and longitudinal movement of the probes~
The amplitudes o-f such eclloes are digitized in 10~ units and printer 26 prints out the echo amplitudes having levels higher than a predetermined threshold value.
Exemplary printed records of welding defects detected by the present detector are shown in Figures 6A
and 6B, wherein Fig. 6A shows lateral scanning relative to the axial direction and Fig. 6B shows an example of rect-angularly lateral scanning at a scanning distance of lmm.
Fig. 6A shows the results of the flaw detection when the probe was positioned at a point 7~.5mm from a reference point on the circumference of the pipe, which was scanned . laterally relative to the axial direction over ten sub-divisions of the weld zone width. If an echo representing a defect is present within the ten channel gates, the echo amplitude will be digitized in 10% units so that numeral l represents 10%, numeral 2 represents 20% of the echo height, and so forth. The asterisks represent echo ampli-; tudes greater than 100%. In Fig. 6A, the higher values recorded within the portion enclosed by a solid line, namely from the third gate to the sixth gate, indicates that a number of defects are found within the third to the sixth zones of the ten subdivisions in the weld zone.
Similarly, the rectangularly lateral scanning pattern,Fig. 6B, indicates that a number of defects are present .
3~7~
within the portion enclose~ by the solid line, namely, from the second to the fifth zones, at distances 17 to 18 mm from a reference point.
In sur~ary, a weld zone is scanned by probes movable laterally with respect to the axial direction of the longitudinal movement along the weld zone of a self-propelled carrier on which the probes are mounted. The echo amplitudes of welding defects present within each gate output, associated with a subdivision oE the weld zone, is synchronized with the position coordinates of the probes on a printer so that approximate conditions of the welding defects are indicated during the flaw detection operation and the distribution of the welding defects can be observed at a glance to concurrently determine the severity of the defects to be classified. In addition, the self-propelled carrier on which the detector is mounted has a structure enabling detection oE welding defects in a constantly stable manner, so that the accuracy of the flaw detection apparatus and method is very high. Furthermore, it is possible to graphically depict the depth of welding defects, echo amplitudes, the length and severity of the welding defects incorporating a mlni-computor in a cordance with the foregoing de~cription.
. .
.~ ' .
~"~ -- 1 1 --. ~ .
Description o-f the Prior Art X-ray penetration testing has conventionally been applied for non-destructive inspective of weld zones. In conjunction with the improved performance of ultrasonic flaw detection appar~tus, the application of ultrasonic flaw detection methods and techniques have recently been required for improved detection accuracy, shortened detection time, safe operation and decreased detection costs. In particular, in the non-destructive inspection of circumferential weld zones for high-pressure pipe lines, such weld zones have been inspected by the combined use of X-ray penetration testing and ultrasonic flaw detection techniques. Ultrasonic ~.~
flaw detection has been performed mainly manually. However, manual ultrasonic flaw detection requires considerable skill and experience for the discrimination of the jamming echoes due to the weld bead, from the flaw echoes and also requires considerable technical skills. Under certain operational conditions, weld flaw detection has to be performed under severe conditions at sites such as common workshops where other operations are also being performed. Such conditions present intolerable burdens to the welding operations and inspectors.
In order to overcome sucn problems, it is desirable to automate welding flaw detection methods and techniques and also the associated necessary data processing, such as ~ .
~ - 2 -' .~ ~
recording and evaluation and the like of the detected results.
SU~lMARY OF THE INVENTION
It is an object oE the invention in accordance with such requirements to provide automatic ultrasonic flaw detection methods and apparatus employing a calcu-lator having an operational function to systematize the data processing of automatic ultrasonic Elaw detection.
The inventior. consists of a method for automat-ically detecting flaws in circumferentially extending pipewelding zones, comprising the steps of: moving a welding flaw detector in at least two different directions in tracking relationship to a weld zone; subdividing the width of said weld zone into a plurality of areas; trans-mitting pulsed energy to said weld zone; generating output signals from a plurality of gate circuits each respect-ively responsive to the echo signals produced by said pulsed energy from a specified one of said areas; generat-ing position signals representative of the position of said flaw detector from a reference point; and displaying said output signals and said position signals in assoc-iated relationship to indicate any welding flaws and their respective positions in each one of said plurality of areas of the weld zone.
The invention also consists of apparatus for automatically detecting flaws in circumferentially extend-ing pipe welding zones, comprising: a welding flaw de-tector movable in at least two different directions in tracking relationship to a welding zone; means for trans-mitting pulsed energy to said welding zone; means for ;~ generating output signals from a plurality of gate ~ circuits each respectively responsive to the echoes .
~ --3--produced by said pulsed ene~gy from a respective one of alike plurality of areas subdividing tlle width of said welding zone; means for generating position signals repre-sentative of the position of said flaw detector from a reference point; and means for displaying said output signals and said position signals in associated relation-ship to indicate any welding flaws and the respective position thereof in each one of said plurality of areas in the weld zone.
BRIEF DESCRIPTION OF T~E DRAWINGS
_, .
Fig. 1 is a side view of a self-propelled carrier flaw detection apparatus according to an embodiment of the invention;
Fig. 2 is a partially cut-away plan view of the self-propelled carrier of Fig. 1 on an enlarged scale;
Fig. 3 is a longitudinal sectional view taken along line III - III in Fig. 2;
Figs. 4A, 4B and 4C are illustrations showing respective scanning patterns of probes of a self-propelled carrier;
Fig. 5 is a block diagram showing data processing apparatus; and Figs. 6A, 6B (with Figs. 4A-C) show respective e~amples of printed records of deteoted flaws as obtained from such apparatus.
DETAILED DBSCRIPTION OF THE PREFERRED E~BODIMENT
The embodiment comprises the ~ollowing components. A
; weld-following mechanism enables the flaw de~ection apparatus to track the weld ~ones with weld detection probe holders.
Motors provide circum-Ferential movement and scanning o~ the probe holders and the probes carried thereby. A detector enables determination o-~ the position oF the `:
.
7~3 probes. A self-propelled carrier on which the probes are mounted detects Elaws by axial scannin~ movements of the probes while the probes are moved along the circum~er-ential weld zone at a predetermined speed (the maximum speed being about 3 m/min.). Display apparatus electri-cally displays the position of the probes and the height of the echoes. A data processing unit automatically prints the detection results.
The apparatus is characterized, in particular, by the incorporation of a data processiny unit comprising a calculator having reading and calculating functions for the high speed processing of the automatic ultrasonic flaw detector.
As shown in Fig. 1, self-propelled carrier 1 is constructed so that probe holders 4 are mounted at the center portion of trestle 2, which is driven by motor 3 for circumferential movement of the trestle. Self-propelled carrier 1 is secured to the outer periphery of pipe 5, which is to be inspected, by a pair of semi-circular holder bands 7, each of which is secured totrestle 2 at one end thereof, and includes a plurality of spaced rollers 6 for maintaining the trestle at a fixed distance from the outer periphery of pipe 6. Holder bands 7 are attached to one another by clamping units 8 attached at the opposing ends of each of the holder bands.
As shown in Figs. 2 and 3, the travelling mechanism of the carrier comprises connecting four driven magnetic rollers 9, respectively mounted at both the front and rear ends of carrier 2, to respective driving shafts 10 driven by gears 9a, 9b which are, in turn, respectively connected to a transmission shaft 11 driven by reduction gears 12, connected to a-shaft of motor 3.
.
The mechanism is thus constructed so that one motor 3 can drive concurrently fo~r magnetic rollers 9. It should be understood that such a mechanism is illustrated only as an exemplary embodiment and other suitable mechanisms can be employed, if desired.
Probe holder 4 travels on rails 16 attached to the inner walls of outer right and left frames 15 by multiple sets of roller mechanisms, each set including two rollers 14 mounted vertically with respect to one 10 another. Probe holder 4 is suspended to be movable verti-cally and in a plane perpendicular thereto with respect to weld zone 17. Probe holder 4 is suspended by connecting outer frame 15 to supporting shaft 18, attached rotatably to carrier 2 through a recess defined at the central portion thereof as illustrated in Figures 2 and 3.
Thereby, probe holder 4 is mounted on carrier 2 so as to be pivotable horizontally about supporting shaft 1~ and to be horizontally movable, at the same time, in a direction perpendicular to weld zone 17.
A rotating shaft, constructed in two independ-~ ently operable sections 20, 20' is threaded through a ;; tapped hole in block B for mounting probes T, T' and each of the shaft sections 20, 20' is driven respectively by scanning motors 19, 19' secured to holder 4 so that either one, or both, probes T, T' can be independently or con-currently moved, as desired, by actuating either motor 19 or 19'. The displacement of both probes T, T' is measured by rotary encoder 21 which measures the axial scan position and the circumferential scan position of both 30 probes T, T' in a manner known to those skilled in the art. Probes T, T' are movable because it is necessary to adjust the distance between end faces of the probes as the ::
.,,~
7~3 width of the weld bead is not constant due to the different radius o~ pipe to be inspectecl.
In the flaw detection of weld zones, it is essential to know the distance between the center of the weld bead and the point of incidence of the ultrasonic wave from the probes T and T'. It is necessary that a mechanism for following the weld bead be used in the auto-matic flaw detection apparatus. Such following mechanisms include optical and electrical types. As such mechanisms are too complex and large to be used in situ at the sites where the pipe lines are being inspected, the apparatus adopts a system wherein four magnets 22 are attached to outer frame 15 o~ probe holder 4 to be magnetically attracted to the pipe on both sides of weld zone 17, thereby enabling probes T and T' to follow the weld zone.
Such a following or tracking mechanism is simple. Probes T, T' can be isolated from any vibration due to the close contact of magnets 22 with the outer surface of the pipe by means well known to those skilled in the art. There-; 20 fore, probes T, T' are always in contact with, or closelyadjacent to, the surface of the pipe and the tracking of the probes with respect to the bead is kept within an accuracy of 2mm, which is sufficient such that no problem is encountered in the practical use of the system.
Probes T, T' each incorporate vibrator Ta for obliquely detecting flaws, and vibrator Tb for perpendic-ularly detecting the reflected waves from the bottom of the material (see Fig. 5). To avoid cluttering the draw-ing, only the electrical connectors to vibrator Tb are shown. The electrical connections to vibrator Ta are the same as those shown for vibrator Tb. Probes T, T' each function to maintain the flaw detecting sensitivity at a constant level by receiving the reflecting waves from the bottom of the material, i.e., the pipe to be inspected, namely from the radially confronting inner sur-face of the pipe, to calibrate the re~lected waves in accordance with the change in the contacting conditions o-f the probe with the material due to the unevenness of the surface thereof. Specifically, the characteristics of the obliquely or perpendicularly incident ultrasonic energy into the material depends on the contacting conditions of the probe with the surface of the material to be inspected. The change in such contacting conditions causes fluctuation in the flaw detecting sensitivity, thereby leading to failures in the evaluation of welding defects. Therefore, it is necessary to calibrate the flaw detecting sensitivity to maintain it at a constant level.
Taking such a requirement into account, the detector employs vibrators Tb in each of probes T, T' which can calibrate - 20 the sensitivity automatically within a range of 20dB.
Such calibration is performed automatically by switching between vibrators Ta and Tb in each of probes T and T'.
Figs. 4A, 4B and 4C show the scanning patterns for only one of probes T, T', as both probes scan in the same manner. Fig. 4A shows lateral or axial scanning, ~ Fig. 4B shows longitudinal or circumferential scanning and ;~ Fig. 4C shows a scanning pattern representing the combined scanning patterns of Figs. 4A and 4B (referred to herein-after as rectangularly lateral scanning). Lateral or axial scanning performs sufficient flaw detection within a skip from 0.5 to 1.0 at a distance from the probe to the center of the bead ranging from 20 to 95mm for pipes having ~' ,~ - 8 -, "
, . ~
~ , - . .
.: .
a thickness t ranging from 8 to 15mm. The pitch for rect-angularly lateral scanning can also be adjusted to a minimum of lmm.
As shown in Fig. 5, the data processing unit for obtaining the results Erom the automatic ultrasonic ~law detector comprises position display 23 which indicates the X and Y coordinates of the position of probes T, T', namely scanning laterally in the axial direction (Y) and longitudinally, circumferentially (X) around the pipe with respect to weld zone 17. Multichannel gate circuitry 24, may for example as illustrated include the channel gates providing outputs in 10~ units of the echo amplitude from each subdivision of the weld zone, defined by subdividing the width of the weld zone into a plurality of sub-divisions. Cathode ray tube 25 displays the echo ampli-tudes from the ten channel gates in multi-channel gate circuitry 24 in synchronization with the signals indicat-ing the respective position of the probes. Printer 26 prints the echo amplitudes of any welding defects that are ~0 present, as determined by the ten channel gate output, ` together with the position of the probes.
In the operation of the automatic flaw detecting apparatus using the aforedescribed detector, self-propelled carrier 1 is mounted on pipe 5 over weld zone 17, which is to be inspected. After setting the correct distance from the welded bead to the probes T, T', carrier 1 is conveyed circumferentially in the direction X along-side the welded bead. Probes T, T' are laterally moved in the axial direction Y relative to weld zone 17 to carry 30 out the flaw detection. The positions of the probes are displayed by position display 23 and at the same time, the echo amplitudes are displayed on cathode ray tube 25.
; B~ -9-~ . .
.. . , ~ . . . . ... . .
The display of the probe signals frorn either probe T or ~r~
can be selectively displayed by a switch (not shown) in accordance with teachings well known to those skille~ in the art. The presence of echo 27 indicates a defect with-in any of the channel gates of multi-channel gate circuitry 24. The displayed echoes are always in synchronization with the lateral and longitudinal movement of the probes~
The amplitudes o-f such eclloes are digitized in 10~ units and printer 26 prints out the echo amplitudes having levels higher than a predetermined threshold value.
Exemplary printed records of welding defects detected by the present detector are shown in Figures 6A
and 6B, wherein Fig. 6A shows lateral scanning relative to the axial direction and Fig. 6B shows an example of rect-angularly lateral scanning at a scanning distance of lmm.
Fig. 6A shows the results of the flaw detection when the probe was positioned at a point 7~.5mm from a reference point on the circumference of the pipe, which was scanned . laterally relative to the axial direction over ten sub-divisions of the weld zone width. If an echo representing a defect is present within the ten channel gates, the echo amplitude will be digitized in 10% units so that numeral l represents 10%, numeral 2 represents 20% of the echo height, and so forth. The asterisks represent echo ampli-; tudes greater than 100%. In Fig. 6A, the higher values recorded within the portion enclosed by a solid line, namely from the third gate to the sixth gate, indicates that a number of defects are found within the third to the sixth zones of the ten subdivisions in the weld zone.
Similarly, the rectangularly lateral scanning pattern,Fig. 6B, indicates that a number of defects are present .
3~7~
within the portion enclose~ by the solid line, namely, from the second to the fifth zones, at distances 17 to 18 mm from a reference point.
In sur~ary, a weld zone is scanned by probes movable laterally with respect to the axial direction of the longitudinal movement along the weld zone of a self-propelled carrier on which the probes are mounted. The echo amplitudes of welding defects present within each gate output, associated with a subdivision oE the weld zone, is synchronized with the position coordinates of the probes on a printer so that approximate conditions of the welding defects are indicated during the flaw detection operation and the distribution of the welding defects can be observed at a glance to concurrently determine the severity of the defects to be classified. In addition, the self-propelled carrier on which the detector is mounted has a structure enabling detection oE welding defects in a constantly stable manner, so that the accuracy of the flaw detection apparatus and method is very high. Furthermore, it is possible to graphically depict the depth of welding defects, echo amplitudes, the length and severity of the welding defects incorporating a mlni-computor in a cordance with the foregoing de~cription.
. .
.~ ' .
~"~ -- 1 1 --. ~ .
Claims (12)
1. A method for automatically detecting flaws in circumferentially extending pipe welding zones, comprising the steps of:
moving a welding flaw detector in at least two different directions in tracking relationship to a weld zone;
subdividing the width of said weld zone into a plurality of areas;
transmitting pulsed energy to said weld zone;
generating output signals -from a plurality of gate circuits each respectively responsive to the echo signals produced by said pulsed energy from a specified one of said areas;
generating position signals representative of the position of said flaw detector from a reference point; and displaying said output signals and said position signals in associated relationship to indicate any welding flaws and their respective positions in each one of said plurality of areas of the weld zone.
moving a welding flaw detector in at least two different directions in tracking relationship to a weld zone;
subdividing the width of said weld zone into a plurality of areas;
transmitting pulsed energy to said weld zone;
generating output signals -from a plurality of gate circuits each respectively responsive to the echo signals produced by said pulsed energy from a specified one of said areas;
generating position signals representative of the position of said flaw detector from a reference point; and displaying said output signals and said position signals in associated relationship to indicate any welding flaws and their respective positions in each one of said plurality of areas of the weld zone.
2. A method as in Claim 1, further comprising the step of recording said output signals and said position signals in associated relationship to indicate any welding flaws and their respective positions in the weld zone.
3. A method as in Claim 2 wherein said step of generating output signals includes the step of limiting the amplitude of those output signals representing echoes exceed-ing a given threshold value to a percentage of their normal amplitude and further comprising the steps of digitizing said reduced amplitude signals and said position signals prior to said step of displaying.
4. A method as in Claim 3, wherein the flaw detector is movably mouthed in a self-propelled carrier and said step of moving includes the steps of propelling said carrier circumferentially in tracking relationship to said weld zone and moving said flaw detector transversely with respect to the movement of said carrier.
5. A method as in Claim 4, wherein said step of digitizing said position signals includes the step of generating digital signals representative of the position of said Claw detector in both the circumferential and transverse directions of movement thereof.
6. A method as in Claim 5, wherein said steps of displaying and recording include the respective display and recording of said digital position signals in relation to the associated amplitude levels for each of said subdivided areas.
7. Apparatus for automatically detecting flaws in circumferentially extending pipe welding zones, comprising:
a welding flaw detector movable in at least two different directions in tracking relationship to a welding zone;
means for transmitting pulsed energy to said welding zone;
means for generating output signals from a plurality of gate circuits each respectively responsive to the echoes produced by said pulsed energy from a respective one of a like plurality of areas subdividing the width of said welding zone;
means for generating position signals representative of the position of said flaw detector from a reference point; and means for displaying said output signals and said position signals in associated relationship to indicate any welding flaws and the respective position thereof in each one of said plurality of areas in the weld zone.
a welding flaw detector movable in at least two different directions in tracking relationship to a welding zone;
means for transmitting pulsed energy to said welding zone;
means for generating output signals from a plurality of gate circuits each respectively responsive to the echoes produced by said pulsed energy from a respective one of a like plurality of areas subdividing the width of said welding zone;
means for generating position signals representative of the position of said flaw detector from a reference point; and means for displaying said output signals and said position signals in associated relationship to indicate any welding flaws and the respective position thereof in each one of said plurality of areas in the weld zone.
8. Apparatus as in Claim 7 further comprising means for recording said output signals and said position signals in associated relationship to indicate any welding flaw and the respective position thereof in the weld zone.
9. Apparatus as in Claim 8 wherein said means for generating output signals includes means for limiting the amplitude of those output signals representing echoes exceed-ing a threshold value to a percentage of their normal amplitude; and further comprising means for digitizing the reduced amplitude signals and said position signals.
10. Apparatus as in Claim 9 further comprising a self-propelled carrier for mounting said flaw detector and including means for propelling said carrier circumferentially in tracking relationship to said weld zone and moving said flaw detector transversely with respect to the movement of said carrier.
11. Apparatus as in claim 10 wherein said means for digitizing said position signals includes means for goner-ating digital signals representative of the position of said flaw detector in both the circumferential and transverse directions thereof.
12. Apparatus as in Claim 11 wherein said means for displaying and said means for recording respectively include means for displaying and means for recording said digital positions signals in relation to the associated amplitude levels of each of said subdivided areas.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP145480/76 | 1976-12-02 | ||
JP14548076A JPS5369691A (en) | 1976-12-02 | 1976-12-02 | Method and apparatus for automatic supersonic crack detection |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1108743A true CA1108743A (en) | 1981-09-08 |
Family
ID=15386218
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA282,693A Expired CA1108743A (en) | 1976-12-02 | 1977-07-14 | Method and apparatus for automatic ultrasonic flaw detection |
Country Status (6)
Country | Link |
---|---|
JP (1) | JPS5369691A (en) |
CA (1) | CA1108743A (en) |
DE (1) | DE2753635C2 (en) |
FR (1) | FR2373058A1 (en) |
GB (1) | GB1559469A (en) |
NO (1) | NO148972C (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8146430B2 (en) | 2006-05-10 | 2012-04-03 | Jireh Industries Ltd. | Method and apparatus for conveying an ultrasonic sensor about an outer peripheral surface of a tube |
Families Citing this family (20)
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US4204434A (en) * | 1978-12-18 | 1980-05-27 | The Budd Company | Ultrasonic testing of welds in wheels |
NL7904973A (en) * | 1979-06-26 | 1980-12-30 | Roentgen Tech Dienst Bv | SYSTEM FOR EXAMINING WELDED CONNECTIONS IN PIPES WITH ULTRASONIC WAVES. |
FR2469754A1 (en) * | 1979-11-16 | 1981-05-22 | Sumitomo Metal Ind | AUTOMATIC ULTRA-SOUND CONTROL APPARATUS |
JPS6329243Y2 (en) * | 1980-12-27 | 1988-08-05 | ||
JPS5896249A (en) * | 1981-12-04 | 1983-06-08 | Hitachi Ltd | Inspection mechanism guide positioning device |
JPS5960257A (en) * | 1982-09-29 | 1984-04-06 | Hitachi Ltd | Trackless pipe scanning device for pipe inspection |
FR2547923B3 (en) * | 1983-06-22 | 1985-06-07 | Siderurgie Fse Inst Rech | METHOD AND DEVICE FOR DETERMINING THE MACROINCLUSIONARY CLEANLINESS OF A METAL, IN PARTICULAR OF A STEEL |
DE3337635A1 (en) * | 1983-10-15 | 1985-04-25 | M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 8500 Nürnberg | Manipulator for checking circular and longitudinal seams of bends in nuclear power stations |
DE3410954A1 (en) * | 1984-03-24 | 1984-09-20 | Hermann 8000 München Schimkat | Device for operating an ultrasonic test head |
FR2570502B1 (en) * | 1984-09-14 | 1988-01-15 | Dassault Avions | INSTALLATION FOR ULTRASONIC CHECKING OF WORKPIECES, AND DEVICE FOR SCANNING A SURFACE OF THE WORKPIECE TO BE TESTED |
FR2578647B1 (en) * | 1985-03-06 | 1987-03-06 | Alsthom Atlantique | DEVICE FOR CONTROLLING FAULTS OF ROTORS OF ELECTRIC MACHINES |
DE3603153A1 (en) * | 1986-02-01 | 1987-08-06 | Nukem Gmbh | ARRANGEMENT FOR DESTRUCTION-FREE TESTING OF CYLINDER-SHAPED WORKPIECES |
TW241410B (en) * | 1992-01-28 | 1995-02-21 | Westinghouse Electric Corp | |
JP2005315843A (en) * | 2004-03-31 | 2005-11-10 | Tokyo Electric Power Co Inc:The | Ultrasonic inspection method and device |
JP2006200906A (en) * | 2005-01-18 | 2006-08-03 | Tokyo Electric Power Co Inc:The | Scanning flaw inspection device and method |
US8590383B2 (en) | 2008-06-24 | 2013-11-26 | Alstom Technology Ltd | Ultrasonic inspection probe carrier system for performing non-destructive testing |
US9019364B2 (en) | 2012-07-17 | 2015-04-28 | Alstom Technology Ltd | Remote visual inspection system |
DE102016221730A1 (en) * | 2016-11-07 | 2018-05-09 | Robert Bosch Gmbh | Method for the detection of material inhomogeneities |
US20230142556A1 (en) * | 2020-04-22 | 2023-05-11 | Simply Aut Ltd. | Magnetic ultrasound testing system |
CN114856266B (en) * | 2022-06-11 | 2024-06-14 | 安徽中合水务发展有限公司 | Environment-friendly water supply and drainage standardized pump house construction process |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1147089A (en) * | 1966-11-22 | 1969-04-02 | Nat Res Dev | Ultrasonic inspection system for materials |
US3575042A (en) * | 1968-08-28 | 1971-04-13 | Gen Dynamics Corp | Automatic digital recording weld defect detector |
US3844165A (en) * | 1973-10-03 | 1974-10-29 | Amf Inc | End area inspection tool for automated nondestructive inspection |
JPS5346112B2 (en) * | 1973-12-25 | 1978-12-11 | ||
US3921440A (en) * | 1975-01-02 | 1975-11-25 | Air Prod & Chem | Ultrasonic pipe testing system |
-
1976
- 1976-12-02 JP JP14548076A patent/JPS5369691A/en active Pending
-
1977
- 1977-07-13 NO NO772496A patent/NO148972C/en unknown
- 1977-07-14 GB GB29650/77A patent/GB1559469A/en not_active Expired
- 1977-07-14 CA CA282,693A patent/CA1108743A/en not_active Expired
- 1977-07-18 FR FR7721884A patent/FR2373058A1/en active Granted
- 1977-12-01 DE DE2753635A patent/DE2753635C2/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8146430B2 (en) | 2006-05-10 | 2012-04-03 | Jireh Industries Ltd. | Method and apparatus for conveying an ultrasonic sensor about an outer peripheral surface of a tube |
Also Published As
Publication number | Publication date |
---|---|
NO148972C (en) | 1984-02-01 |
DE2753635C2 (en) | 1984-07-26 |
GB1559469A (en) | 1980-01-16 |
FR2373058A1 (en) | 1978-06-30 |
DE2753635A1 (en) | 1978-06-08 |
JPS5369691A (en) | 1978-06-21 |
NO148972B (en) | 1983-10-10 |
NO772496L (en) | 1978-06-05 |
FR2373058B1 (en) | 1981-08-28 |
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