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Journal of Engineering Science and Technology Vol. 14, No. 3 (2019) 1344 - 1360 © School of Engineering, Taylor’s University
1344
POTENTIAL APPLICATION OF ACOUSTIC EMISSION TECHNIQUE FOR WELD STRUCTURE INTEGRITY
MONITORING UNDER DYNAMIC LOADING
S. V. RANGANAYAKULU1,*, RAMESH KUMAR BUDDU2, P. V. SASTRY3
1School of Engineering, Guru Nanak Institutions Technical Campus,
Ibrahimpatnam, Hyderabad-501506, India 2FRMDC Division, Institute for Plasma Research, Bhat, Gandhinagar-382428, India
3Research and Development Division, Bharat Heavy Electricals Limited,
Hyderabad-500035, India
*Corresponding Author: [email protected]
Abstract
Acoustic Emission (AE) has emerged as a potential assessment technique for
structural health monitoring and integrity inspection in nuclear components and
weld structures during in-service conditions. The present paper gives the
experimental results of Acoustic Emission monitoring technique applied to
welded specimens made out of AISI SS 316L steel, under dynamic stress
conditions roughly simulating the pre-failure conditions in the welded structures.
The weld samples are fabricated by deliberately implanting different types of
weld defects like porosity, slag and inclusions in the welded zone. These samples
are subjected to dynamic loading precisely converging on the welded zone, with
the help of a specially fabricated mechanical jig with a load cell. AE output
parameters like the number of counts, energy, amplitude, frequencies are
monitored during loading of the samples (until the physical appearance of failure)
and it is observed that samples with defective welds gave a distinctly higher yield
of AE parameters compared to sample without defects.
Keywords: Acoustic emission, Calibration, Fusion reactor, Welded structures.
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1. Introduction
The structural integrity of the nuclear components in case of nuclear reactors (both
fission and fusion) is of very serious concern as their failures can lead to the reactors
breakdown and affect the operational activities. Austenitic stainless steel materials
are widely used for the fabrication of various structural components for nuclear
reactor subsystems due to their superior mechanical properties, fatigue and
corrosion resistance properties at elevated temperatures. The components are
joined by various joining techniques to develop the structural components for
various subsystems development like vacuum vessel, supports structures and
pipeline components, etc. The weld joints, in general, comprise of weld defects and
residual stresses if the proper care is not taken during the welding process.
If these components are under substantial mechanical and thermal load
conditions, the localized stress releases within the material propagate and cause
micro cracks in the structure. The structures like nuclear, pressure vessels and
chemical plants during operation experience severe thermal, structural gradients,
which affect the components strength and cause catastrophes. Acoustic Emission
(AE) technique has evolved as the potential diagnostic tool for the structural health
monitoring and fault finding events in several nuclear installations like in for
fusion, fission reactor components and pressure vessels [1-7]. Acoustic emissions
(AE) are elastic stress waves generated by a rapid release of energy from localized
sources within material under stress or repeated loading. Cao et al. [8] explained
that acoustic emissions often originate from material defect related sources such as
microscopic deformation or microcrack generation/propagation within the material
due to external loads application. The generated Acoustic Emission signals in the
form of sound can be effectively tailored to detect the fault sources, detection of
fracture or failure of structures by employing proper transducers. One of the
advantages compared to other NDE techniques is the possibility to observe damage
processes during the entire load history without any disturbance to the specimen.
The basis for quantitative methods is a localization technique to extract the source
coordinates of the AE events as accurately as possible. The preventive maintenance
and structure health integrity monitoring mechanism for operational components
and instruments is highly desirable to avoid any kind of catastrophe failures, which
are detrimental for the operational scenarios of the nuclear reactors or pressure
vessels [9-11].
AE detection process uses various analysed process parameters recording like
hits, amplitude, energy, frequency and rise time, etc., to measure the system
response against the load conditions. According to Hase et al. [12] and Deuster
et al. [13], by appropriate calibration and utilisation of the analysis techniques,
the defects can be correlated with linear localised techniques. Droubi et al. [14]
reported that recently, the non-contact method was used by sending guided
acoustic waves with laser beam source to detect the weld defects from long
distance weld pipes, which is a potential demonstration AE by nondestructive
measurements. The present study has demonstrated the applicability of the
acoustic emission application and potential response characteristics under
dynamic load condition on welded plates with different type weld defects. The
study focused on the demonstration and feasibility of applying AE technique for
preventing failures or diagnosing the enhanced defects in joints of structure
components when subjected to the dynamic mechanical loading circumstances,
which are rational in nuclear installations.
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2. Experimental Procedure
2.1. Materials
AISI SS316L plates of dimensions 70 mm ×16 mm × 10 mm are chosen as the
experimental materials for the study and are joined by manual metal arc welding
process and Tungsten Inert Gas (TIG) welding process. Single V groove with 600
bevel angle and 1 mm root height, a good finish is made before joint preparation.
The weld current of ~ 200 A and voltage of 12 V DC is used in the joining process.
ER 316L filler rods of 2.5 mm diameter and ~ 4-5 weld passes are used for the
welding. The weld joints of the final size of 140 mm × 16 mm × 10 mm are prepared
to study the defects response upon load. Weld zone of ~ 20 mm is maintained in all
the weld samples. Different types of weld defects are introduced in the welded zone
deliberately in the samples during the welding process. Three categories of samples
are fabricated as good weld plates (no weld defects), with porosity and slag
inclusions in the welded zones. Each set of 5 samples are tested for repeatability
check. The weld joints quality has been analysed with X-ray radiography to spot
the defects in the welds. The radiography images of different weld samples with
and without defects are shown in Fig. 1 for details.
Fig. 1. Weld defects (slag and porosity) samples
with X-ray radiography result.
2.2. Dynamic load cell for characterisation
The dynamic loading test of the samples has been carried out by using a specially
designed mechanical jig system, which is shown in Fig. 2. This has an arrangement in
such a way that the location of welded zone of the sample is subjected to the localised
force in a uniform manner and the fracture of the sample can take place after the plastic
deformation under an applied force. The technique is similar to the three-point bend
testing of the welded samples. This process is carried by keeping the welded samples
placed on two anvils and compressed at the centre with a mandrel. The mandrel is
pushed uniformly by bending movement at the centre where the weld zone is located.
The details of the test mechanical jig unit and with samples are shown in Figs. 2 (a) and
(b) for reference.
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(a) Mechanical jig unit. (b) Mechanical jig system
with sensors and samples.
Fig. 2. Specially designed mechanical jig system.
2.3Acoustic emission set-up and calibration process
The dynamic load characteristics analysis has been carried out by using a two-
channel Acoustic emission system (Physical Acoustics Corporation, Model:
SB141; USA), which consists of two sets of AE sensors attached to preamplifier
and amplifier and measurement data analysis software by AE Win soft to analyse
the events in form of counts, rise time, energy, events, frequency and amplitude as
output parameters. The schematic of the measurement scheme is shown in Fig. 3.
Fig. 3. Calibration scheme of AE set up measuring system.
The standard calibration of the weld sample without any weld defect has been
carried out. The velocities are changed by the variation in frequency. The
calibration helps in identifying the generated frequencies during the acoustic events
during the loading conditions. The calibration with two sensors AE system
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attachment has been carried to establish characteristics of the transducer used with
reference to the load exposed and the accurate location mapping to capture the
events of acoustic emission. Based on studies by Lee et al. [15], a frequency
response of a specific sensor with the load input can be expressed in terms of
velocity, displacement parameters, which is the most common representation of
calibration. During this process, the sensitivity of the sensor is established with the
given range of output frequency (acoustic emission) as per the input load.
According to Hase et al. [12], the dispersion curves using phase velocity and group
velocity of the tested weld plate material with the applied load tests with pencil lead
calibration technique are shown in Figs. 4(a) and (b), with the measured
frequencies, in which, is a similar procedure as reported [12]. This further confirms
the variation of the stress-energy released during the applied loading on to the weld
samples and events measured in terms of counts, energy, rise time and amplitude,
etc., with a known source.
(a) Phase velocities of SS316L weld sample during calibration.
(b) Group velocities of SS316L weld sample during calibration.
Fig. 4. Phase and group velocities
of SS316L weld sample during calibration.
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3. Results and Discussion
The experiments are carried out with the given load to study the behaviour of
acoustic emission features in both the good and weld defect samples (porosity, slag
inclusions). The acoustic emission data was collected at the weld zone location by
applying stress load and detected data is processed in the form of events, counts,
amplitude, energy and frequency are recorded and analysed. As per Fig. 5, the load
applied in the weld zone of the good weld sample has shown in the form of events,
counts, energy and amplitude and cumulative counts with reference to the position
of the weld zone. The test plate undergoes slow stress form due to the applied load
and the AE monitoring system records the acoustic emission released data in the
form of events, counts, energy, cumulative counts. As shown in Figs. 5 to 8, the
counts are recorded with calibrated weld position of the sample in the range of 60
mm - 80 mm to evaluate the events as of weld zone region.
As soon as the microcrack/crack initiated, the counts and energy release
condition shows a sudden rise in the measurement of recorded AE events data.
Once when the sample began with plastic deformation, there was no further AE
events recorded, the events suddenly started to reduce and disappear. The variation
includes the arrival of the events on the sensors with the event generation. The
amplitude and frequency were recorded, in which, waveform and FFT analysed
spectra are shown in Figs. 9 and 10.
Fig. 5. Variation of event vs. position with respect to
AE data on defects free weld sample.
Fig. 6. Variation of count vs. time (s) with respect to
AE data on defects free weld sample.
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Fig. 7. Variation of energy vs. time (s) with respect
to AE data on defects free weld sample.
Fig. 8. Variation of count vs. amplitude with respect
to AE data on defects free weld sample.
Fig. 9. Raw AE data during loading with
frequency (micro sec) in sensors 1, 2.
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Fig. 10. FFT analysed data with amplitude vs. frequency.
In the case of weld joint with porosity, weld defect is subjected to the loading
condition, the AE events start initiated much earlier and the intensity-released
energy is higher than the sample without weld defects. This indicates the
mechanism of the stress release due to the stored energy release due to the applied
loading has contributed towards higher measured data in all forms. The events
recorded under the porosity weld defect are shown in Figs. 11 to 14.
Fig. 11. Variation of events vs. x-position with respect
to AE data on porosity defects weld sample.
Fig. 12. Variation of count vs. time (s) with respect
to AE data on Porosity defects weld sample.
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Fig. 13. Variation of energy vs. time (s) with respect
to AE data on porosity defects weld sample.
Fig. 14. Variation of count vs. amplitude with respect
to AE data on porosity defects weld sample.
The events, counts, energy and amplitude data has shown significant
enhancement compared to weld sample without defects as shown in Figs. 5 to 8.
This phenomenon is analogous to the release of stress wave locally in the welded
region during the loaded condition in the form of acoustic emission frequencies
recorded by sensors at each end attached to the weld sample. The stress
concentration released under the dynamic loading has shown significant influence
on the higher counts, amplitude, the energy released during the crack initiation and
enhanced stress energy waves measured in AE system data. The crack initiation
and plastic deformation zone in the welded zone have shown significant events
enhancement in measured AE data with porosity defect sample data compared to
the without defect sample data. This corresponds to the role of weld defects causing
stress release during the dynamic loading into the localised welded parts, which
have scope towards the failure of components due to the mechanical events in
service conditions.
As shown in Figs. 15 and 16 are the characteristic waveforms recorded during
the applied load and the FFT analysed data, which reveals the burst emission of AE
data events in both the channels received are having 280 kHz and 290 kHz. The
gradual increase in amplitude is attributed towards the crack initiation with initial
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loading and final fractures in the weld zone after the plastic deformation takes place
when compared to Figs. 9 and 10.
Fig. 15. Raw AE data during loading with
frequency (micro-sec) in sensors 1, 2.
Fig. 16. FFT analysed data with amplitude vs. frequency.
Similarly, in case of the sample with slag inclusion defects, the load test
conditions have revealed significant enhancement and rise in the AE recorded data
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in terms of events, counts, energy and amplitude compared to sample without
defects. The measured data, (Figs. 17 to 20) is shown for the slag inclusion sample.
The data enhancement contribution has revealed the stress release in terms of the
acoustic frequencies, which are more prominent than the good weld sample (defects
free). The parameters events, energy and amplitude show a similar trend of rising
in both the weld defect samples under the dynamic load condition in AE recorded
data. However, the slag inclusion defect sample has shown relatively low events
data compared with porosity condition defect sample. This further confirms to the
generation of the event during the crack initiation and propagation process has
proclamation more stress energy during the loading and is reflected in the where
the burst emissions occur in the form of acoustic emission events. As shown in
Figs. 21 and 22, the measured waveform recorded during the AE data collected
with burst mode emissions at different frequencies in both the sensors attached
during loading condition. The lower frequency recorded as 60 kHz and 85 kHz are
observed in the peak data of the FFT analysed waveform. This further count to the
lower emission caused compared with porosity weld defect sample.
Fig. 17. Variation of events vs. X-position with respect
to AE data on Slag defects weld sample.
Fig. 18. Variation of count vs. time (s) with respect
to AE data on slag defects weld sample.
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Fig. 19. Variation of energy vs. time (s) with respect
to AE data on slag defects weld sample.
Fig. 20. Variation of count vs. amplitude with respect
to AE data on slag defects weld sample.
Fig. 21. Raw AE data during loading with
frequency (micro sec) in sensors 1, 2.
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Fig. 22. FFT analysed data with amplitude vs. frequency.
The recorded AE in continuous mode and burst mode conditions due to the
applied dynamic load and the events recorded during the initial stage, crack
initiation and crack propagation (fracture mode) and release of stress concentration
due to the weld defect samples are shown in Figs. 23 to 25. The waveform recorded
initial condition shows that the dominant frequency at 60 kHz in FFT analysed the
signal. In the case of crack initiated during the dynamic load application stage prior
to the plastic deformation, the released energy in the form of recorded frequency
was shown burst mode emission characteristics in Fig. 24 shown dominant peak
frequencies at 40 kHz and 130 kHz. The crack propagation region where the
complete fracture initiated, the burst emissions with peak amplitudes of 50 kHz and
120 kHz frequencies. This reveals the contribution of the acoustic emission events,
which are due to the defects caused a failure like cracks of the structure under the
dynamic loading conditions.
The present study postures the capability of the acoustic emission technique as
a potential diagnostic in preventing the failures due to the excess load to the
mechanical structures and integrity aspects. This detection method can be applied
for structural health monitoring technique towards the examination of heavy
structural materials during the in-service condition of the structural steel welded
components. Acoustic emission system can be used as a potential diagnostic
technique to monitor the failure events on structural integrity during the mechanical
operation loads.
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Fig. 23. AE data and FFT waveform analysed
during the initial load condition.
Fig. 24. AE data and FFT waveform analysed during crack initiation.
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Fig. 25. AE data and FFT waveform analysed
during the crack propagation under stress condition.
4. Conclusion
The present study reports the detailed examinations carried under the dynamic load
applied to weld structures with different weld defects.
The AE system can be exploited to demonstrate the structural stability
condition of the weld joint steel structure during the dynamic load
conditions been studied by setting up the special mechanical cell with
localized load supply system with AE system integration towards
demonstration of the event registration during failure conditions in the
structural integrity of the components.
The good welded joint under dynamic load with special designed
mechanical jig system has shown the AE events in the form of events,
counts, energy and amplitude with respect to the weld position during the
crack initiation and propagation.
The weld sample with porosity condition has shown the increase in the AE
measured parameters like counts, energy and amplitude with position
contribution from the excess stress energy release (burst modes) due to the
weld defect region.
The sample with slag inclusion has shown the AE measured data parameters
relatively lower than the porosity sample but enhanced than the good weld
sample. This further confirms that the stress release under dynamic load on the
inclusion weld defect samples shows less amount of stress released during the
load applied condition.
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The tailored AE measurements data events can be logically interpreted and
inspection can be upheld for the critical component structures and welded joint
regions where the critical failure is anticipated or prevention is necessary. The
monitoring of AE parameters of defect-free and weld defect (porosity) samples
adequately demonstrates that AE technique is a potential for online health integrity
monitoring of premier and critical installations like nuclear reactors, pressure
vessels and chemical plants under service loads.
Acknowledgements
One of the Authors, S. V. Ranganayakulu, is grateful to Board of Research in
Fusion Science and Technology of Department of Atomic Energy (Project No.
NFP-MAT-F12-01) for sanction of grant-in-aid to carry out this word as part of the
execution of the academic research project.
Nomenclatures
K Frequency FFT analysed data in kilo 1000 (Fig. 16)
T Time in seconds (s)
Abbreviations
AE Acoustic Emission
AISI American Iron and Steel Institute
ASTM American Society for Testing Material
FFT Fast Fourier Transform
LLT Linear Location Technique
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