WO1999044366A1 - Data integration and registration method and apparatus for non-destructive evaluation of materials - Google Patents
Data integration and registration method and apparatus for non-destructive evaluation of materials Download PDFInfo
- Publication number
- WO1999044366A1 WO1999044366A1 PCT/US1999/004206 US9904206W WO9944366A1 WO 1999044366 A1 WO1999044366 A1 WO 1999044366A1 US 9904206 W US9904206 W US 9904206W WO 9944366 A1 WO9944366 A1 WO 9944366A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- sample
- image
- defect image
- defect
- referencing
- Prior art date
Links
Classifications
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
- H04N7/181—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a plurality of remote sources
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N25/00—Investigating or analyzing materials by the use of thermal means
- G01N25/72—Investigating presence of flaws
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T7/00—Image analysis
- G06T7/0002—Inspection of images, e.g. flaw detection
- G06T7/0004—Industrial image inspection
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T7/00—Image analysis
- G06T7/30—Determination of transform parameters for the alignment of images, i.e. image registration
Definitions
- the present invention is directed to a method and apparatus for non-destructive testing and evaluation of materials, and more particularly to a method and apparatus for identifying and registering defects in a sample by superimposing a defect image over a live image to locate subsurface defects in the sample.
- NDT/E non-destructive testing and evaluation
- steps thermography pulse thermography, pulse thermography, and other thermographic techniques. All of these techniques involve deliberately changing the temperature of the sample, allowing the sample to return to equilibrium temperature, and observing the temperature change of the sample via an infrared camera. Anomalous temperature changes that appear in the infrared camera image indicate subsurface defects in the sample; subsurface defects tend to impede the normal heat flow in the sample and will appear as anomalies in the image. Further, because the infrared image showing the defect is transient and may last for only a fraction of a second, the image must be captured (usually with a digital computer) and then verified with the actual sample to locate the defect.
- the actual verification process can be relatively difficult because the infrared defect image of the sample may bear little resemblance to the actual sample. For example, many subsurface defects appear only in the infrared image; to the naked eye, the sample containing the defects often appears perfectly uniform. As a result, a user must attempt to match the image of the subsurface defect with the actual, unblemished sample surface to pinpoint the location of the defect. This is further complicated by the fact that the infrared camera lens often distorts the image, causing straight lines at the periphery of the lens's field of view to appear curved in the image.
- prior art methods include using regularly spaced registration markers on the sample, calculating complex anamorphic mapping algorithms, or printing a full-size defect image and physically matching or overlaying the full-size image onto the actual sample. Because the sample may not have any distinguishing marks that appear in the defect image, precise registration of the image and the sample's surface can be difficult. In addition, these methods are time-consuming and are not particularly convenient, and at best they can only approximate the subsurface defect location due to the image distortion from the infrared camera lens. Further, measuring the depth of subsurface defects often requires some prior knowledge of the sample's dimensions or properties, such as the thickness of the sample, the depth of a known defect, the material's thermal diffusivity, etc. This information is often not available in practice, making precise depth measurements difficult with known techniques.
- NDT/E technique that allows accurate annotation, marking, and thickness measurements of specific locations on a sample, without the problems caused by differences between the image and the actual sample due to image distortion.
- the present invention is a method and apparatus for conducting
- the invention involves obtaining a defect image and a live image of the same sample and then superimposing one image on the other.
- One embodiment of the invention is directed to linking the information regarding surface defects obtained during infrared NDT/E to the actual part being inspected.
- the invention includes generating a defect image of the sample via infrared imaging or some other means.
- the defect image may have markers or other indicia locating where subsurface defects are in the sample.
- the defect image is then superimposed onto a live image of the sample.
- a user views the live image of the sample, rather than the sample itself, while transferring the marks from the defect image to the sample.
- the distorted image is used as the frame of reference for locating subsurface defects and marking the sample. This ensures that the marks in the defect image are transferred precisely from the defect image onto the sample and also eliminates the need to map the distorted image to the sample in a separate step.
- Figure 1 is a flowchart illustrating an evaluation and testing method according to the present invention
- Figure 2 is a flowchart illustrating an example of the inventive method as applied to thermography
- FIGS 3a through 3f illustrate actual images taken from infrared NDT/E of an aluminum aircraft panel according to the method of the present invention.
- Figure 4 is a representative diagram of an apparatus that can be used to annotate, calibrate, and/or evaluate a sample according to the method of the present invention.
- one embodiment of the NDT/E method according to the present invention can be broken down into four steps.
- a defect image of the sample is obtained 100, digitized and displayed on a computer 102 using a computer program that has a referencing mechanism, such as drawing tool that allows the user to draw on the defect image using a mouse, touch screen, light pen, or other pointing device.
- the user can mark defects found in the defect image with the drawing tool 103.
- the defect image, including any marks made by the user, is then superimposed onto a live image 104, which is also displayed on the computer.
- the live image is preferably produced immediately thereafter and using the same lens and camera that produced the defect image to ensure a one-to-one correspondence between the live image and the defect image; using the same lens ensures that both images will have the same distortion.
- the user then marks the actual sample, using a marking pencil or similar device, while viewing the live image 106 rather than looking the sample itself. Instead of marking the part, the user may also use a point measuring device to measure characteristics of the sample, such as its thickness, and append the data to the image for annotation or calibration purposes.
- the defect image and live image can also be simply superimposed one atop the other for referencing purposes, without any user intervention.
- the defect image is subject to any lens distortion that may be present.
- inaccuracies in marking occurred because the user was attempting to map the distorted defect image onto a corresponding physical sample part, whether it was through markers on the sample or through overlaying a full-size image on the actual sample.
- the user watches the live image of the sample rather than the sample itself when referencing the sample. Because the live image and the defect image in the present invention are both distorted via the same camera lens, the defect image and the live image align perfectly with each other.
- the user will look at the live image of the marking or measurement instrument, and not the actual marking/measurement instrument itself, in real time while referencing the sample, making it possible to trace the marks from the defect image onto the sample precisely and distortion-free.
- the distorted defect image and the distorted live image both have exactly the same, albeit distorted, frame of reference.
- any marks or measurements taken while viewing the live image will correspond exactly to the marked locations in the defect image superimposed on the live image.
- the first step involves changing the sample's temperature 200 by heating or cooling the temperature through any known method. For example, heat can be applied to the sample via a flashlamp or a continuous lighting source. Defect images of the sample are then taken 202 with an infrared camera as the sample's temperature returns to equilibrium. The infrared camera preferably obtains multiple defect images from the same sample after the sample's temperature is changed, taking images at selected time intervals as the sample returns to equilibrium temperature.
- Figures 3a through 3d illustrate a time sequence of infrared images of an aluminum aircraft pane adhesively bonded to an aluminum structural frame, illustrating the transient nature of infrared NDT/E.
- Figure 3 a was taken just before heating
- Figure 3b taken 1.33 seconds after heating
- Figure 3c taken 10.67 seconds after heating
- Figure 3d taken 39.34 seconds after heating.
- the aircraft panel does not exhibit any subsurface structure before heating (Figure 3a), while just after heating, the frame can be seen in the defect image, along with a disbonded area where corrosion has occurred, in the right half of the image
- Figure 3b The frame and disbonded area are less distinct after 10.67 seconds (Figure 3c) and disappear completely after 39.34 seconds (Figure 3d).
- Figure 3d For non-destructive evaluation, the image obtained shown in Figure 3b provides the most useful information because it is the clearest image.
- the defect image is preferably displayed using a program with a "draw" mode so that the user can place marks on the defect image using a mouse, touch screen, or other pointing device.
- the area where the defects occur is then "marked” on the screen by the user 206.
- An example of such a display is shown in Figure 3e, where the image from Figure 3b is taken as the defect image.
- the area where the plate defect appears has been circled by the user, using the "draw" mode in the computer program generating the defect image, to highlight the area at which the subsurface defect is located.
- the defect image is marked 206, it is superimposed onto a digitized live image 208, which is also displayed on the computer monitor.
- a digitized live image 208 which is also displayed on the computer monitor.
- both the defect image and the live image are obtained using the same infrared camera lens and because the camera is not moved after the defect image is obtained, both the defect image and the live image exhibit the same amount of lens distortion and have a one-to-one correspondence with each other; the defect image and live image do not have any distortion with respect to each other.
- the defect image is superimposed on the live image, the user can transfer the reference marks from the defect image to the sample 210 exactly and distortion-free. As shown in Figure 3f, the user does this by viewing his hand (or the marking instrument) on the sample via the live image, not by directly watching the physical sample.
- the marks are made on the actual sample precisely correspond to the location of the defect.
- the user may also contact the sample with a point measuring probe, such as an ultrasonic thickness gauge or thermocouple, to measure the local properties of the sample. Because the probe will appear in the live image, the user can mark the position of the probe on the defect image and then read the probe measurement through a serial data connection. The information can be appended to the image for annotation or calibration purposes.
- FIG. 4 illustrates one apparatus that can be used to carry out the inventive method with respect to thermography.
- the apparatus includes a reflective hood 400 that focuses light from heating lamps 402 onto a sample 404.
- the heating lamps 402 can be flashlamps (e.g. xenon lamps) or continuous lamps (e.g. halogen lamps). Regardless of the type of lamp used, reflectors 403 or some other means should be used to distribute light uniformly over the sample 404 surface at the opinion of the hood 400 so that the sample heats evenly.
- the front end of the hood 400 is open and is placed on or near the sample 404.
- the back portion of the hood 400 is designed to accommodate a lens 406 of an infrared camera 408.
- the hood 400 also preferably has an access door 410 to allow the user to reach inside the hood 400 and mark the sample, if desired.
- the apparatus shown in Figure 4 also includes a display 412 for displaying the defect image and the live image generated by the infrared camera 408.
- the apparatus also includes a microcontroller or personal computer 414, which may be located in the infrared camera 408 itself, attached to the thermography apparatus in some other way, or located remotely and accessed via 2-way serial or parallel data communication.
- a measuring instrument 416 such as an ultrasonic thickness gauge, can also be provided to conduct thickness measurements or other measurements.
- a user interface 418 such as an operator keypad or touch screen, is provided on the apparatus to allow marking of the defect image and manipulation of the images on the display 412.
- the invention uses a distorted live image and a distorted defect image to locate subsurface defects, the one-to-one correspondence between the two distorted images creates a new frame of reference from which to pinpoint the defect locations, greatly increasing the accuracy and speed at which subsurface defects can be located and marked.
- the invention also allows complementary NDT/E methods to be used in conjunction with the defect image so that the defect image can be annotated or can be calibrated so thickness measurements can be obtained directly from the image, without requiring prior information from a reference sample or any other source. Further, the invention can be used with any infrared NDT/E method, independently of how the method changes the sample's temperature, generates the defect image, or processes the data.
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- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Physics & Mathematics (AREA)
- Theoretical Computer Science (AREA)
- Computer Vision & Pattern Recognition (AREA)
- Analytical Chemistry (AREA)
- Life Sciences & Earth Sciences (AREA)
- Biochemistry (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Chemical & Material Sciences (AREA)
- Quality & Reliability (AREA)
- General Health & Medical Sciences (AREA)
- Health & Medical Sciences (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Investigating Or Analyzing Materials Using Thermal Means (AREA)
- Investigating Materials By The Use Of Optical Means Adapted For Particular Applications (AREA)
- Closed-Circuit Television Systems (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU29748/99A AU2974899A (en) | 1998-02-25 | 1999-02-25 | Data integration and registration method and apparatus for non-destructive evaluation of materials |
EP99911002A EP1064789A4 (en) | 1998-02-25 | 1999-02-25 | Data integration and registration method and apparatus for non-destructive evaluation of materials |
JP2000534006A JP2002505436A (en) | 1998-02-25 | 1999-02-25 | Data integration and registration method for non-destructive evaluation of substances |
US09/623,071 US6795784B1 (en) | 1998-02-25 | 1999-02-25 | Data integration and registration method and apparatus for non-destructive evaluation of materials |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US7592098P | 1998-02-25 | 1998-02-25 | |
US60/075,920 | 1998-02-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1999044366A1 true WO1999044366A1 (en) | 1999-09-02 |
Family
ID=22128762
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1999/004206 WO1999044366A1 (en) | 1998-02-25 | 1999-02-25 | Data integration and registration method and apparatus for non-destructive evaluation of materials |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP1064789A4 (en) |
JP (1) | JP2002505436A (en) |
AU (1) | AU2974899A (en) |
WO (1) | WO1999044366A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001266125A (en) * | 2000-03-15 | 2001-09-28 | Olympus Optical Co Ltd | Substrate inspecting device |
CN107192759A (en) * | 2017-06-09 | 2017-09-22 | 湖南大学 | A kind of photovoltaic cell lossless detection method and system based on sensing optical heat radiation |
US10242439B1 (en) | 2016-08-17 | 2019-03-26 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Contrast based imaging and analysis computer-implemented method to analyze pulse thermography data for nondestructive evaluation |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102010014744B4 (en) * | 2010-04-13 | 2013-07-11 | Siemens Aktiengesellschaft | Apparatus and method for projecting information onto an object in thermographic surveys |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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US5351307A (en) * | 1991-11-15 | 1994-09-27 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Process and apparatus for the acquisition and processing of screen images |
US5444241A (en) * | 1993-10-01 | 1995-08-22 | The Regents Of The University Of California | Emissivity corrected infrared method for imaging anomalous structural heat flows |
US5774568A (en) * | 1995-01-27 | 1998-06-30 | Gec Alsthom Systemes Et Services Sa | Method of testing a surface non-destructively in particular in a hostile environment |
Family Cites Families (4)
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US4751571A (en) * | 1987-07-29 | 1988-06-14 | General Electric Company | Composite visible/thermal-infrared imaging apparatus |
US4755874A (en) * | 1987-08-31 | 1988-07-05 | Kla Instruments Corporation | Emission microscopy system |
JPH01296785A (en) * | 1988-05-24 | 1989-11-30 | Fujitsu Ltd | Picture superimposing device |
US5637871A (en) * | 1993-06-07 | 1997-06-10 | Computational Systems, Inc. | Portable digital infrared thermography system |
-
1999
- 1999-02-25 AU AU29748/99A patent/AU2974899A/en not_active Abandoned
- 1999-02-25 WO PCT/US1999/004206 patent/WO1999044366A1/en active Application Filing
- 1999-02-25 EP EP99911002A patent/EP1064789A4/en not_active Withdrawn
- 1999-02-25 JP JP2000534006A patent/JP2002505436A/en active Pending
Patent Citations (3)
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US5351307A (en) * | 1991-11-15 | 1994-09-27 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Process and apparatus for the acquisition and processing of screen images |
US5444241A (en) * | 1993-10-01 | 1995-08-22 | The Regents Of The University Of California | Emissivity corrected infrared method for imaging anomalous structural heat flows |
US5774568A (en) * | 1995-01-27 | 1998-06-30 | Gec Alsthom Systemes Et Services Sa | Method of testing a surface non-destructively in particular in a hostile environment |
Non-Patent Citations (3)
Title |
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DESURVIRE E.: "ERBIUM DOPED FIBER AMPLIFIERS. PRINCIPLES AND APPLICATIONS.", 1 January 1994, NEW YORK, WILEY & SONS., US, article BAXES, G. A.: "KEYING AND OVERLAYING.", pages: 280 - 283., XP002920734, 020895 * |
GOPALAN K., GOPALSAMI N.: "THERMAL-WAVE IMAGE PROCESSING FOR CHARACTERIZATION OF SUBSURFACE OFSUBSURFACE FLAWS IN MATERIALS.", PROCEEDINGS OF THE MIDWEST SYMPOSIUM ON CIRCUITS AND SYSTEMS. DETROIT, AUG. 16 - 18, 1993., NEW YORK, IEEE., US, vol. SYMP. 36, 16 August 1993 (1993-08-16), US, pages 1433 - 1435., XP000499838 * |
See also references of EP1064789A4 * |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001266125A (en) * | 2000-03-15 | 2001-09-28 | Olympus Optical Co Ltd | Substrate inspecting device |
US10242439B1 (en) | 2016-08-17 | 2019-03-26 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Contrast based imaging and analysis computer-implemented method to analyze pulse thermography data for nondestructive evaluation |
US10332248B1 (en) | 2016-08-17 | 2019-06-25 | The United States Of America As Represented By The Administator Of The National Aeronautics And Space Administration | Contrast based imaging and analysis computer-implemented method to analyze pulse thermography data for nondestructive evaluation |
US10728426B1 (en) | 2016-08-17 | 2020-07-28 | United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Contrast based imaging and analysis computer-implemented method to analyze pulse thermography data for nondestructive evaluation |
CN107192759A (en) * | 2017-06-09 | 2017-09-22 | 湖南大学 | A kind of photovoltaic cell lossless detection method and system based on sensing optical heat radiation |
Also Published As
Publication number | Publication date |
---|---|
JP2002505436A (en) | 2002-02-19 |
AU2974899A (en) | 1999-09-15 |
EP1064789A1 (en) | 2001-01-03 |
EP1064789A4 (en) | 2007-05-23 |
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