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SURFACE CRACK DETECTION IN WELDS 
USING 
THERMOGRAPHY 
Submitted by, 
AKHIL .N .D, 
S7 ME, 
ROLL NO:9, 
GECBH
OVERVIEW 
 Purpose 
Principle & Theory 
Experimental Setup 
Results 
Discussion 
Conclusion 
 Purpose 
Principle & Theory 
Experimental Setup 
Results 
Discussion 
Conclusion
PURPOSE 
To employ Thermography principle to detect 
cracks in Welds 
Why THERMOGRAPHY???? 
Offers 
Non contact, fast inspection 
Ability to find even small cracks 
Can be used as a substitute for other NDT 
methods like eddy current, penetrant and 
magnetic particle testing
PRINCIPLE 
 Thermography is today used within non-destructive 
testing for detecting several different 
types of defects. 
 The possibility for using thermography for 
detecting surface cracks in welded metal plates has 
here been investigated. 
During testing the weld is illuminated using a 
high power infrared light source. 
Due to surface cracks acting like black bodies, 
they will absorb more energy than the surrounding 
metal and can be identified as a warmer area when 
imaged using an infrared camera. 
Notches as well as real longitudinal cold cracks in 
a weld are investigated using the presented 
method. 
The results show that thermography is promising 
as a method for detection cracks open to the surface
THEORY 
BASIC FORMULAE USED 
Kirchhoff's law: ελ =αλ 
Hagen-Rubens Relation: εL, λ =2√(2ωε0ρ) [ω - angular frequency] 
[ ε0 -electric constant] 
[ρ -electric resistivity ] 
the absorption of IR radiation in metals is relatively 
small and will generally decrease with increased wavelength. Most of 
the IR radiation is therefore reflected at the surface
A crack in a metal plate that is 
illuminated by high 
intensity IR light will absorb and emit 
more energy than the 
surroundings and will be visible as a 
hot-spot if imaged by an IR 
camera 
 If a crack is illuminated with a short pulse of IR radiation it 
needs to be inspected shortly after since the temperature will 
decay quickly as heat conduction transports heat from the crack 
into the material
SIZE OF CRACK 
 Crack should absorb enough energy to raise the temperature 
compared to the background so that the IR camera can differentiate 
them as two different temperatures. 
 Crack width determines the wavelength and energy of light they can 
absorb 
 Light with a wavelength that is longer than the crack’s width will 
quickly decay in intensity as it enters the crack and will in practice not 
enter the crack 
 The inclination of the crack will also affect the amount of radiation 
that falls into the crack and therefore the amount of energy absorbed. 
A practical limit to the size of cracks that can be detected also 
depends on the IR camera. The resolution of the camera together 
with the choice of lens will limit how small objects that can be imaged 
by the camera
EXPERIMENTAL SETUP 
Two types of IR sources 
were tested, 
a laser, as in Fig. 2a & 
a flashlamp, as in Fig. 2b 
WHY PREFER LASER 
a good source of easily focused, high energy monochromatic light, to evaluate the 
method 
The laser was a pulsed Nd:YAG laser with a wavelength of 1064 nm 
Deliver pulses with an energy of 1.54 J for 2 ms and the beam was spread using a 
lens so that the spot on the plate had a diameter of about 6 mm
WHY PREFER FLASH LAMB 
A flash lamp illuminates a wider area with a larger spectrum of wavelengths and has 
advantages, compared to the laser, in terms of portability, cost and safety 
The flash lamp used delivered a 10 ms, broadband pulse with a total energy of 6 kJ 
(although not all of the energy was directed towards the plate) 
When the flash lamp was mounted at a distance of about 20 cm from the weld it 
heated an area with a diameter of about 10 cm. 
PROBLEMS ASSOCIATED WITH USING FLASH LAMB 
Most of the light from a flash lamp is in the visual spectra with a smaller part of it in 
the IR. The IR light can interfere with the testing when it is reflected into the IR camera 
and is therefore often removed with a filter 
 In this case the IR part of the spectra was desired. So it was done by setting up both 
the camera and flash lamp at a large angle to the normal of the welded plate 
Here, COOLDOWN time is high. This causes reflections of the lamp in the weld to 
obstruct the radiation from the crack even after the flash. 
By placing both the camera and flash lamp at a large angle, the glow from the flash 
lamp, after the pulse, is reflected away from the camera, thus reducing its effect
IR CAMERA 
 A high speed, cooled, IR camera was used 
to observe the temperature distribution 
just after the heat pulse 
 The camera had a 14 bit detector with a 
resolution of up to 640 * 512 pixels and a 
temperature sensitivity of less than 20 mK 
 The camera was mounted at a distance of 
10–20 cm from the test piece which gave a 
spatial resolution of about 0.1–0.2 
mm/pixel.
Two different types of defects were used in this test 
Artificial defects, in the form of notches 
• 12 Notches are used 
• Sizes between 0.25 and 1.7 mm long, the depth were 
about half the length and the width varied from 80 to 400 μm. 
• All notches were manufactured in, or at the root of, the weld bead 
of a laser welded titanium plate using EDM 
real surface cracks 
• Tested on two long cracks in MIG (Metal Inert Gas) welded steel plates. 
• Widths ranging from 5 and 330 μm, measured using an optical microscope. 
The notches were tested using the Nd-YAG laser as a source 
and the cracks using the flashlamp.
RESULTS 
1. FOR Nd-YAG LASER 
 Testing of 12 notches in a 
laser welded titanium plate 
with Nd:YAG laser 
 It was possible to detect all 12 
notches that were manufactured in 
the weld using this method 
 The larger notches were visible in 
the IR image even without 
excitation, as faint marks in the 
weld, because of reflections in the 
surface, but those with a length 
shorter than 0.5 mm were not 
because the small size and depth 
made them indistinguishable from 
the background noise
 There is a good correlation between 
the measured length of the notch and 
the real length 
 The temperature difference between 
the notch and the surrounding metal 
for the notches in the weld increases 
with increased notch length 
 The temperature in the 1 mm long notch 
in the weld and the area surrounding 
that notch during testing can be seen in 
graph 
 The temperature difference is largest 
immediately after the laser pulse and 
decreases as the material cools down. 
 The result also shows that a small area 
around the notch had an elevated 
temperature because of heat conduction 
from the notch.
The temperature difference for the 
notches at the root of the weld is 
less than for those in the weld 
because the laser was aimed at the 
centre of the weld and had an 
energy profile where most of the 
energy was focused in the centre of 
the laser. For the shortest of the 
notches in the root of the weld the 
laser was realigned and centred 
over the notch, which is why the 
temperature difference is greater 
than for the other notches.
2. FOR FLASH LAMP 
 The real cracks were 
tested using a flashlamp 
instead of a laser to 
evaluate the flashlamp as 
a source of infrared 
radiation for this method. 
 The cracks can be seen as a line in the middle of the weld and this demonstrates that a 
flash lamp can be a viable IR source for this type of testing 
 In the images above some hot spots can be seen, these are oxides on the weld that are 
good absorbers of IR radiation and therefore increase significantly in temperature due to 
the flash. 
 The results from this test showed a size limit for detecting surface cracks at about 5–10 
μm, using this setup and equipment. 
 The contrast between the crack and the weld in this case is not as large compared to the 
notches due to the longer pulse length from the flash lamp compared to the laser causing 
reflections in the surrounding weld 
 The reflections can be seen in Fig as hot areas around the crack and makes the crack 
harder to detect.
FACTORS THAT MAY ALTER RESULT 
 Table showed that the shortest notch had the largest temperature increase due to 
the laser being realigned so that it was aimed at the notch and since most of the 
energy was in the centre of the laser beam it could absorb more energy. This 
shows the importance of properly illuminating the notches or cracks with the IR 
source 
 For weld inspection the whole width of the weld needs to be properly 
illuminated to make sure that no defects are overlooked. 
 Since only the surface of the plate and surfaces inside the crack are heated, the 
measured temperature will quickly decrease as the heat spreads into the material. 
Because of this the material needs to be inspected immediately after the heat is 
applied, the time it takes for the crack to cool down depends on the amount of 
energy applied. . The IR source therefore needs to completely shut off within this 
time to avoid direct reflections of the source being seen in the metal instead of the 
surface temperature, alternatively operate at a wavelength not visible to the 
camera 
 Since the flash lamp radiates as a blackbody due to a high temperature it takes 
relatively long time to cool down and, in this case, the glow of the lamp lasted 
about 1 s and obscured the heat from the cracks. In order to make this method 
work with a flash lamp it was necessary to aim both the camera and the lamp in a 
way that minimized the refection from the lamp in the weld that could be seen by 
the camera.
 By changing the wavelengths it could be possible to improve the signal to 
noise ratio 
 The wavelength used by the IR camera should not be in the same area as the 
IR source to reduce the problem of reflections, but should still be as close to 
the peak of the black body radiation curve for the temperature in the cracks. 
A filter can be used, if a laser is used as a source, to block that wavelength 
from being detected in the camera.
CONCLUSION 
 It was shown that thermography can be used for detecting surface 
cracks in welds 
 Tests were performed using both notches and real cracks with either 
a laser or a flash lamp as the IR source. 
 The smallest crack width that could be detected was about5–10 μm. 
 Lasers are large and expensive but it can be easily controlled in terms 
of size of the area that is heated and the pulse length 
 Flash lamps are smaller and easier to move around but suffer from 
long pulse lengths that will negatively affect the inspection if it is not 
treated properly Since thermography offers non-contact, fast 
inspection with a good ability for finding even small surface cracks it 
is suitable for automated inspection and could be used as an 
alternative to eddy current, penetrant and magnetic particle testing.
REFERENCES 
 Hung YY, Chen YS, Ng SP, Liu L, Huang YH, Luk BL, et al. Review 
and comparison of shearography and active thermography for 
nondestructive evaluation. Mater Sci Eng R 2009;64:73–112. 
 Siegel R, Howell J. Thermal Radiation Heat Transfer. 4th ed: Taylor 
& Francis; 2002. 
 www.sciencedirect.com 
 http://en.wikipedia.org 
 www.britannica.com
THANK YOU 
FOR 
YOUR 
ATTENTION
QUESTIONS?????

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SURFACE CRACK DETECTION IN WELDS USING THERMOGRAPHY

  • 1. SURFACE CRACK DETECTION IN WELDS USING THERMOGRAPHY Submitted by, AKHIL .N .D, S7 ME, ROLL NO:9, GECBH
  • 2. OVERVIEW  Purpose Principle & Theory Experimental Setup Results Discussion Conclusion  Purpose Principle & Theory Experimental Setup Results Discussion Conclusion
  • 3. PURPOSE To employ Thermography principle to detect cracks in Welds Why THERMOGRAPHY???? Offers Non contact, fast inspection Ability to find even small cracks Can be used as a substitute for other NDT methods like eddy current, penetrant and magnetic particle testing
  • 4. PRINCIPLE  Thermography is today used within non-destructive testing for detecting several different types of defects.  The possibility for using thermography for detecting surface cracks in welded metal plates has here been investigated. During testing the weld is illuminated using a high power infrared light source. Due to surface cracks acting like black bodies, they will absorb more energy than the surrounding metal and can be identified as a warmer area when imaged using an infrared camera. Notches as well as real longitudinal cold cracks in a weld are investigated using the presented method. The results show that thermography is promising as a method for detection cracks open to the surface
  • 5. THEORY BASIC FORMULAE USED Kirchhoff's law: ελ =αλ Hagen-Rubens Relation: εL, λ =2√(2ωε0ρ) [ω - angular frequency] [ ε0 -electric constant] [ρ -electric resistivity ] the absorption of IR radiation in metals is relatively small and will generally decrease with increased wavelength. Most of the IR radiation is therefore reflected at the surface
  • 6. A crack in a metal plate that is illuminated by high intensity IR light will absorb and emit more energy than the surroundings and will be visible as a hot-spot if imaged by an IR camera  If a crack is illuminated with a short pulse of IR radiation it needs to be inspected shortly after since the temperature will decay quickly as heat conduction transports heat from the crack into the material
  • 7. SIZE OF CRACK  Crack should absorb enough energy to raise the temperature compared to the background so that the IR camera can differentiate them as two different temperatures.  Crack width determines the wavelength and energy of light they can absorb  Light with a wavelength that is longer than the crack’s width will quickly decay in intensity as it enters the crack and will in practice not enter the crack  The inclination of the crack will also affect the amount of radiation that falls into the crack and therefore the amount of energy absorbed. A practical limit to the size of cracks that can be detected also depends on the IR camera. The resolution of the camera together with the choice of lens will limit how small objects that can be imaged by the camera
  • 8. EXPERIMENTAL SETUP Two types of IR sources were tested, a laser, as in Fig. 2a & a flashlamp, as in Fig. 2b WHY PREFER LASER a good source of easily focused, high energy monochromatic light, to evaluate the method The laser was a pulsed Nd:YAG laser with a wavelength of 1064 nm Deliver pulses with an energy of 1.54 J for 2 ms and the beam was spread using a lens so that the spot on the plate had a diameter of about 6 mm
  • 9. WHY PREFER FLASH LAMB A flash lamp illuminates a wider area with a larger spectrum of wavelengths and has advantages, compared to the laser, in terms of portability, cost and safety The flash lamp used delivered a 10 ms, broadband pulse with a total energy of 6 kJ (although not all of the energy was directed towards the plate) When the flash lamp was mounted at a distance of about 20 cm from the weld it heated an area with a diameter of about 10 cm. PROBLEMS ASSOCIATED WITH USING FLASH LAMB Most of the light from a flash lamp is in the visual spectra with a smaller part of it in the IR. The IR light can interfere with the testing when it is reflected into the IR camera and is therefore often removed with a filter  In this case the IR part of the spectra was desired. So it was done by setting up both the camera and flash lamp at a large angle to the normal of the welded plate Here, COOLDOWN time is high. This causes reflections of the lamp in the weld to obstruct the radiation from the crack even after the flash. By placing both the camera and flash lamp at a large angle, the glow from the flash lamp, after the pulse, is reflected away from the camera, thus reducing its effect
  • 10. IR CAMERA  A high speed, cooled, IR camera was used to observe the temperature distribution just after the heat pulse  The camera had a 14 bit detector with a resolution of up to 640 * 512 pixels and a temperature sensitivity of less than 20 mK  The camera was mounted at a distance of 10–20 cm from the test piece which gave a spatial resolution of about 0.1–0.2 mm/pixel.
  • 11. Two different types of defects were used in this test Artificial defects, in the form of notches • 12 Notches are used • Sizes between 0.25 and 1.7 mm long, the depth were about half the length and the width varied from 80 to 400 μm. • All notches were manufactured in, or at the root of, the weld bead of a laser welded titanium plate using EDM real surface cracks • Tested on two long cracks in MIG (Metal Inert Gas) welded steel plates. • Widths ranging from 5 and 330 μm, measured using an optical microscope. The notches were tested using the Nd-YAG laser as a source and the cracks using the flashlamp.
  • 12. RESULTS 1. FOR Nd-YAG LASER  Testing of 12 notches in a laser welded titanium plate with Nd:YAG laser  It was possible to detect all 12 notches that were manufactured in the weld using this method  The larger notches were visible in the IR image even without excitation, as faint marks in the weld, because of reflections in the surface, but those with a length shorter than 0.5 mm were not because the small size and depth made them indistinguishable from the background noise
  • 13.  There is a good correlation between the measured length of the notch and the real length  The temperature difference between the notch and the surrounding metal for the notches in the weld increases with increased notch length  The temperature in the 1 mm long notch in the weld and the area surrounding that notch during testing can be seen in graph  The temperature difference is largest immediately after the laser pulse and decreases as the material cools down.  The result also shows that a small area around the notch had an elevated temperature because of heat conduction from the notch.
  • 14. The temperature difference for the notches at the root of the weld is less than for those in the weld because the laser was aimed at the centre of the weld and had an energy profile where most of the energy was focused in the centre of the laser. For the shortest of the notches in the root of the weld the laser was realigned and centred over the notch, which is why the temperature difference is greater than for the other notches.
  • 15. 2. FOR FLASH LAMP  The real cracks were tested using a flashlamp instead of a laser to evaluate the flashlamp as a source of infrared radiation for this method.  The cracks can be seen as a line in the middle of the weld and this demonstrates that a flash lamp can be a viable IR source for this type of testing  In the images above some hot spots can be seen, these are oxides on the weld that are good absorbers of IR radiation and therefore increase significantly in temperature due to the flash.  The results from this test showed a size limit for detecting surface cracks at about 5–10 μm, using this setup and equipment.  The contrast between the crack and the weld in this case is not as large compared to the notches due to the longer pulse length from the flash lamp compared to the laser causing reflections in the surrounding weld  The reflections can be seen in Fig as hot areas around the crack and makes the crack harder to detect.
  • 16. FACTORS THAT MAY ALTER RESULT  Table showed that the shortest notch had the largest temperature increase due to the laser being realigned so that it was aimed at the notch and since most of the energy was in the centre of the laser beam it could absorb more energy. This shows the importance of properly illuminating the notches or cracks with the IR source  For weld inspection the whole width of the weld needs to be properly illuminated to make sure that no defects are overlooked.  Since only the surface of the plate and surfaces inside the crack are heated, the measured temperature will quickly decrease as the heat spreads into the material. Because of this the material needs to be inspected immediately after the heat is applied, the time it takes for the crack to cool down depends on the amount of energy applied. . The IR source therefore needs to completely shut off within this time to avoid direct reflections of the source being seen in the metal instead of the surface temperature, alternatively operate at a wavelength not visible to the camera  Since the flash lamp radiates as a blackbody due to a high temperature it takes relatively long time to cool down and, in this case, the glow of the lamp lasted about 1 s and obscured the heat from the cracks. In order to make this method work with a flash lamp it was necessary to aim both the camera and the lamp in a way that minimized the refection from the lamp in the weld that could be seen by the camera.
  • 17.  By changing the wavelengths it could be possible to improve the signal to noise ratio  The wavelength used by the IR camera should not be in the same area as the IR source to reduce the problem of reflections, but should still be as close to the peak of the black body radiation curve for the temperature in the cracks. A filter can be used, if a laser is used as a source, to block that wavelength from being detected in the camera.
  • 18. CONCLUSION  It was shown that thermography can be used for detecting surface cracks in welds  Tests were performed using both notches and real cracks with either a laser or a flash lamp as the IR source.  The smallest crack width that could be detected was about5–10 μm.  Lasers are large and expensive but it can be easily controlled in terms of size of the area that is heated and the pulse length  Flash lamps are smaller and easier to move around but suffer from long pulse lengths that will negatively affect the inspection if it is not treated properly Since thermography offers non-contact, fast inspection with a good ability for finding even small surface cracks it is suitable for automated inspection and could be used as an alternative to eddy current, penetrant and magnetic particle testing.
  • 19. REFERENCES  Hung YY, Chen YS, Ng SP, Liu L, Huang YH, Luk BL, et al. Review and comparison of shearography and active thermography for nondestructive evaluation. Mater Sci Eng R 2009;64:73–112.  Siegel R, Howell J. Thermal Radiation Heat Transfer. 4th ed: Taylor & Francis; 2002.  www.sciencedirect.com  http://en.wikipedia.org  www.britannica.com
  • 20. THANK YOU FOR YOUR ATTENTION