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Habibu Hussaini et al. Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 4, ( Part -1) April 2015, pp.90-95
www.ijera.com 90 | P a g e
Review of Space-charge Measurement using Pulsed Electro-
Acoustic Method: Advantages and Limitations
Habibu Hussaini*, Ashraf Ahmad Adam,*Ajagun Abimbola Susan*
*(Department of Electrical and Electronics Engineering, Federal University of Technology, Minna, Nigeria
ABSTRACT
The pulsed electro acoustic (PEA) technique is the most widely used method to measure space charge
distributions in insulating materials. The PEA technique has undergone some advancement since the over
twenty years it was first implemented such as in its spatial resolution and sensitivity. In this article a review of
the technique was carried out and its advantages, limitations, progress and prospects were discussed.
Keywords- Review, space charge, pulsed electro acoustic technique, insulating materials
I. INTRODUCTION
The presence of space charges in insulation
materials become cause for concern when they
accumulate and then distort the electric field
distribution within the material. This is because such
distortion generates high electric field that could lead
to breakdown, electrical aging [1] and electrostatic
discharge of the insulation materials [2], [3]. When
the space charge accumulates and garners a
reasonable density, its local field strength could
exceed the breakdown strength of the insulation
material; hence leading to the material failure [4].
The term space charge was first used to describe the
electronic charge that buildup in the space between
the cathode and anode of a vacuum diode, due to
electron emission from the cathode [4]. Space charge
is rarely found in equipment’s used under ac stress;
however, they exist in equipment being used under dc
stress [5]. Insulation materials are used to protect
high voltage equipment’s from overheating and
power loss, but these insulation materials often
experiences stress due to the high voltage the
equipment they are insulating carries. When they are
under stress the insulation materials easily get
damaged due to stress induced aging.
The pulsed electro-acoustic (PEA) method gives
quantitative information about the space charge
present in an insulation material [5] to help engineers
to design equipment’s that use insulation materials
such as HVDC cables better insulation materials, and
control of electrostatic discharge phenomena [6].
There are two major techniques used to measure
space charge in insulation materials and they are the
destructive and non-destructive techniques.
The destructive techniques involved the use of
powders (gives only qualitative information about the
insulation material); a filed mill or a capacitive probe
(gives quantitative information about the insulation
material) at the first attempt made to quantify space
charge in insulation materials. These techniques
involved the cutting of the insulation material into
slabs in order to measure space charge within it,
hence destroying the material [5]. The other
destructive techniques include thermally stimulated
current (TSC), thermally stimulated surface potential
(TSSP), and thermoluminescence (TL) methods [7],
[8], [9].
The non-destructive techniques [10], [11], [12] were
later developed over two decades ago to prevent
destruction of insulation materials during space
charge measurement and they include the thermal
shock method (TSM), the pressure wave propagation
(PWP) method, the laser induced pressure pulse
(LIPP) method, and the pulsed electro-acoustic (PEA)
method [5]. The non-destructive techniques used the
same physical effect to measure space charge, but
subject insulation materials sample for measurement
to different temporary disturbance; however the
information retrieved after measurement is identical
[3], [13]. The non-destructive techniques also require
calibration before the quantitative space charge
density can be obtained [14].
The two common methods used to measure space
charge distribution are the Pressure Wave
Propagation (PWP) method and Pulsed Electro-
acoustic (PEA) method. The PEA method can be
applied to AC or DC fields. However, its DC
application for measuring space charge would be the
focus of this paper review and its advantages,
limitations, progress and prospects discussed.
The paper is organized as follows: Section I of
the paper gave a general introduction on space charge
and its measurement techniques, the principle of
operation, calibration and system response of the
pulsed electro-acoustic technique was discussed in
section II, Section III talked about the advantages and
limitations of the PEA method, the progress and
prospects of the PEA technique was looked at in
section IV, Section V discussed the conclusion of the
review.
RESEARCH ARTICLE OPEN ACCESS
Habibu Hussaini et al. Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 4, ( Part -1) April 2015, pp.90-95
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II. PULSED ELECTRO-ACOUSTIC
(PEA) METHOD
The pulsed electro-acoustic method was first created
in 1987 [15], [16, [17] by the research group of prof.
T. Takada working in cooperation with prof. C. M.
Cooke [5]. This is the most widely used technique in
the field of space charge measurement [18] compared
to other methods. It is cheap, simple in structure and
easy to implement.
2.1 Principle of Operation
The principle of the PEA technique is based on
the Lorentz force law and acoustic wave propagation
in one dimension [19].
The pulsed electro-acoustic technique involves
the application of high voltage, high frequency pulsed
voltage probe across the sample which space charge
profile is to be determined in order to stimulate
motion of its internal charges thereby generating
acoustic waves within the material [20] as shown in
Fig. 1. The acoustic waves generated then propagate
in the sample and are detected as electric signal by a
piezoelectric sensor connected to the ground
electrode. The amplitude of the signal is proportional
to the charge quantity [16]. The space charge
distribution is monitored as a function of time and
measured quantitatively. The density and polarity of
the space charge is obtained from the physical
characteristic of the generated acoustic wave.
However, the detected output signal in the PEA
method do not give the space charge profile of a
sample under measurement directly, due to the
limited frequency band of the ceramic piezoelectric
transducer (PZT) used [21]. A deconvolution
technique developed in 1988 [22] is used to obtain
the space charge profile of the sample.
Fig. 1: Principle of the PEA method. (a) Charged
regions give rise to acoustic waves under the effect of
a pulsed field (b) Piezoelectric sensor gives a voltage
vs(t). (c) Signal treatment gives the spatial
distribution of image and internal charges [6], [23].
The applied DC voltage is usually in the range of
5-40 kV, depending on the sample thickness. The
pulse voltage and width are in the range of 0.1-2 kV
and 5-200 ns, respectively [5]. The acoustic pressure
wave p(t) generated in the sample and the output
signal of the system both expressed as a function of
time is as shown in equation (1) and (2) respectively
[21].
𝑝 𝑡 = 𝐾[𝜍 0 𝑒 𝑝(𝑡) + 𝑢 𝑠𝑎 𝜌 𝜏 𝑒 𝑝 𝑡 − 𝜏 𝑑𝜏 +
∞
0
𝜍(𝑑)𝑒𝑝(𝑡− 𝑑𝑢𝑠𝑎)]
(1)
Where K is the transmission coefficient of the
acoustic wave in the ground electrode sample
interface, sampling time is t, d is the sample
thickness, and the acoustic velocity in the sample is
usa.
𝑣𝑠 𝑡 = 𝐾[𝜍1 + 𝜍2 + 𝑢 𝑠𝑎 ∆𝑇𝜌(𝑥 = 𝑢 𝑠𝑎 𝑡]𝑒 𝑝 (2)
Where σ1 and σ2 are the surface charges at the
electrodes, ∆Tis the width of the pulse, the bulk
charge is ρ, and e p is the amplitude of the pulse
voltage.
2.2 Calibration and System Response
Calibration is very significant and carried out in
order to get an accurate quantitative analysis of space
charge in solid dielectrics [24]. A novel calibration
method in the presence of space charge in dielectric
materials using the PEA techniques was developed in
[24]. The calibration enables the plot of the charge
profile in units of charge density, μ C/cm3
[21].
The system response of the PEA technique
comprises of the transducer and amplifier response
coupled with the attenuation and dispersion of the
acoustic wave as it moves through the system. The
distortion occurs in a situation whereby the
transducer and amplifier do not pass the complete
frequency content of the original acoustic signal [5].
Also, distortion occurs when the frequency response
of the amplifier is not flat, amplifier’s high cut-off
frequency is too low, or when both amplifier and
transducer act as a high-pass filter [5]. This affects
the accuracy of the quantitative analysis of the space
charge distribution. However, this effect of system
response is removed through appropriate calibration
method. The method adopted depends on the sample
[14].
The charge density calibration method for the
PEA technique is as given in equation (3) in
frequency domain [25], [26].
[
𝜍(0)
𝑢 𝑠𝑎 ∆𝜏
+ 𝑅(𝑓) +
𝜍 𝑎
𝑢 𝑠𝑎 ∆𝜏
exp⁡(−𝑗2𝜋𝑓
𝑎
𝑢 𝑠𝑎
)] =
𝜀0 𝜀 𝑟
𝑉 𝑑𝑐
𝑎
1
𝑢 𝑠𝑎 ∆𝜏
×
𝑉(𝑓)
𝑉0(𝑓)
(3)
Initially a DC voltage is applied to the sample to
induce surface charges, however in order to avoid
bulk charge formation, the voltage is set around 1-2
kV (low and short) for few seconds. The output signal
of the PEA method is a voltage as shown in equation
Habibu Hussaini et al. Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 4, ( Part -1) April 2015, pp.90-95
www.ijera.com 92 | P a g e
(3), the component is obtained from
calculation, the deconvolution procedure performed
in order to obtain the space charge distribution of a
sample is represented by the component in
which is the Fourier transform of the output
signal proportional to the surface charge density σ(0).
The Fourier transform of the space charge
distribution is V (f). The impulse of the system
function is . Component is the space
charge response recovery signal after the effect of the
system function is removed [25]. Subsequently, the
space charge signal is obtained. Further discussion on
PEA’s calibration can be found in [14], [24].
III. ADVANTAGES AND LIMITATIONS
The two most widely used non-destructive
techniques for space charge measurement are the
PEA and PWP methods [26]. The PWP is further
divided into two based on the generation principles of
the narrow acoustic wave. These are the Piezoelectric
Induced Pressure Wave (PIPW) method [12], and the
Laser Induced Pressure Propagation (LIPP) method
[27]. Both PIPW and LIPP have the same principle
for space charge measurement[28]. In order to look at
the advantages and limitations of the PEA technique,
this report first compared the two techniques
mentioned.
3.1 Comparison between the PEA and PWP
Methods
The comparison of the characteristics of both
techniques is as presented in TABLE 1.
TABLE 1
COMPARISON OF THE PEA AND PWP
METHODS adapted from [26]
Characterist
ics
PEA PWP
PIPWP LIPP
Excitation
method
Electric
pulse
Pressure
wave by
piezoelectr
ic device
Pressure
wave by
pulsed
laser
irradiation
Sample
thickness
100 µm-
20mm
100 µm-
1.0 mm
50 µm-
20mm
Relative
resolution
2-5% 2-5% 2-5%
Minimum
Space
resolution
~ 5 µm ~ 5 µm ~ 2 µm
Noise and
electric
shielding
High
voltage
and
signal
High voltage and electric
circuits separated by
coupling capacitor.
Cannot be used when
circuits
totally
separated
Can be
used in
the event
of corona
discharg
e
occurren
ce.
corona discharge occurs.
Fast
varying
space
charge
distribution
measureme
nt
Possible Possible No report
about it.
Measureme
nt signal
Pressure
signal
Displacem
ent current
Displacem
ent current
3.2 Advantages
The PEA method has the following advantages
over other techniques used in space charge
measurement;
1) Simple and Robust Equipment: This allows the
PEA method to be deployed in various
environments and industrial applications [24].
2) Safe Method: For the PEA both high voltage and
acoustic detecting circuits are electrically
separated through the ground electrode, as a
result protecting the amplifier and oscilloscope
from damage in the event of an electric
breakdown [29]. Hence, regarded as the safest
technique for space charge measurement in cable
samples through high voltage application.
3) Simple Principle of Operation: The PEA
techniques do not need complex mathematical
treatment just like the LIPP and PWP [14]. It has
a simple modeling and is easy to implement for
both plaque and cable samples [24].
4) Less Noisy Output Signal: This is due to the fact
that the PEA’s detection circuit can be shielded
electrically [29].
5) It has a lower cost compared to other technique
due to its simplicity.
3.3 Limitations
1) Only Two Dimensional Measurements: The
conventional PEA technique can only measure
space charge in amplitude and spatial location
along the thickness of a sample. The planar non
uniformities in the surface direction are not
accounted for.
2) Measurement of Cables with Different Radius:
The PEA technique has problem in the
measurement of cables with different radius as
modification is required of aluminium block
Habibu Hussaini et al. Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 4, ( Part -1) April 2015, pp.90-95
www.ijera.com 93 | P a g e
electrode, acoustic sensor, and PMMA absorber
before it allows the change in cable radius [29].
This is quite a tasking and time consuming thing
to do.
3) Spatial Resolution: The highest positional
resolution that can be obtained using the
conventional PEA technique is approximately 3
µm with deconvolution and 10 µm without
deconvolution [20]. This is because the system
spatial resolution is determined entirely by the
pulse width and sensor thickness [29]. As a
result, it cannot be used in applications with thin
samples as low as 10 µm and approximately 1
µm spatial resolution, such as electron beam
charge deposition in spacecraft charging and for
high energy and plasma physics apparatus.
IV. PROGRESS AND PROSPECTS OF
THE PEA METHOD
The PEA method has undergone some
improvements as discussed in the following;
4.1 Three-Dimensional Observation
New 3D PEA space charge measurement
systems were developed [30] using acoustic lens and
a new scanning system with small detecting electrode
[31] to improve the measurement capability of the
conventional PEA technique. The later allows space
charge accumulated in small areas such as defects in
insulating materials like voids, or trees, when high
voltage is applied on the insulation material to be
measured. The former allows accurate measurement
of 3-D space charge profiles when the profiles do not
change rapidly with time. This makes it easy to
monitor long time ageing phenomena [32].
4.2 High Resolution
A refined PEA measurement system was
developed [33] for use in thin dielectric materials.
The conventional PEA method was only able to
measure space charge of thick dielectrics materials of
about (1-5mm). The refined system was able to
improve the resolution of the PEA technique to 3 µm
using the Fast Fourier Transform deconvolution to
compensate for the piezoelectric sensor. Resolution in
the lateral and thickness direction has been improved
to approximately 100 µm and 2 µm respectively
making it possible to investigate internal charge
behaviors in composite materials such as insulation
layers of printed circuit boards [32].
4.3 Portable PEA System
The conventional PEA system data requires
computer deconvolution in order to display the space
charge distribution of an insulation material. Maeno
developed [23] a new PEA system whose output
signal can display the space charge distribution
directly on a portable oscilloscope without the need
for deconvolution. This makes it possible to measure
space charge distribution on site and can be used in
various industrial applications. However, the spatial
resolution of the space charge measurement of the
new system is 10 µm as that of the conventional
system [13].
Other advancements includes high repetition rate
(time resolution) system capable of measuring space
charge profile every 10 µs up to maximum of 1 ms
[34], and an increase sensitivity of approximately
0.03-0.15 C/mm3[2].
The future of the PEA technique would be in its
application in the nano dielectrics research field for
space charge measurement, especially their interfaces
with the electrodes [13], [35].
V. CONCLUSION
The PEA measurement technique for space
charge measurement has greatly improved since the
over twenty years it was first introduced, as a result
of advancement in technology. Most of the
limitations identified with the conventional PEA
system have been improved upon coupled with its
advantages; hence it would continue to be the most
widely used technique for some time to come.
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www.ijera.com 94 | P a g e
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Review of Space-charge Measurement using Pulsed Electro- Acoustic Method: Advantages and Limitations

  • 1. Habibu Hussaini et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 4, ( Part -1) April 2015, pp.90-95 www.ijera.com 90 | P a g e Review of Space-charge Measurement using Pulsed Electro- Acoustic Method: Advantages and Limitations Habibu Hussaini*, Ashraf Ahmad Adam,*Ajagun Abimbola Susan* *(Department of Electrical and Electronics Engineering, Federal University of Technology, Minna, Nigeria ABSTRACT The pulsed electro acoustic (PEA) technique is the most widely used method to measure space charge distributions in insulating materials. The PEA technique has undergone some advancement since the over twenty years it was first implemented such as in its spatial resolution and sensitivity. In this article a review of the technique was carried out and its advantages, limitations, progress and prospects were discussed. Keywords- Review, space charge, pulsed electro acoustic technique, insulating materials I. INTRODUCTION The presence of space charges in insulation materials become cause for concern when they accumulate and then distort the electric field distribution within the material. This is because such distortion generates high electric field that could lead to breakdown, electrical aging [1] and electrostatic discharge of the insulation materials [2], [3]. When the space charge accumulates and garners a reasonable density, its local field strength could exceed the breakdown strength of the insulation material; hence leading to the material failure [4]. The term space charge was first used to describe the electronic charge that buildup in the space between the cathode and anode of a vacuum diode, due to electron emission from the cathode [4]. Space charge is rarely found in equipment’s used under ac stress; however, they exist in equipment being used under dc stress [5]. Insulation materials are used to protect high voltage equipment’s from overheating and power loss, but these insulation materials often experiences stress due to the high voltage the equipment they are insulating carries. When they are under stress the insulation materials easily get damaged due to stress induced aging. The pulsed electro-acoustic (PEA) method gives quantitative information about the space charge present in an insulation material [5] to help engineers to design equipment’s that use insulation materials such as HVDC cables better insulation materials, and control of electrostatic discharge phenomena [6]. There are two major techniques used to measure space charge in insulation materials and they are the destructive and non-destructive techniques. The destructive techniques involved the use of powders (gives only qualitative information about the insulation material); a filed mill or a capacitive probe (gives quantitative information about the insulation material) at the first attempt made to quantify space charge in insulation materials. These techniques involved the cutting of the insulation material into slabs in order to measure space charge within it, hence destroying the material [5]. The other destructive techniques include thermally stimulated current (TSC), thermally stimulated surface potential (TSSP), and thermoluminescence (TL) methods [7], [8], [9]. The non-destructive techniques [10], [11], [12] were later developed over two decades ago to prevent destruction of insulation materials during space charge measurement and they include the thermal shock method (TSM), the pressure wave propagation (PWP) method, the laser induced pressure pulse (LIPP) method, and the pulsed electro-acoustic (PEA) method [5]. The non-destructive techniques used the same physical effect to measure space charge, but subject insulation materials sample for measurement to different temporary disturbance; however the information retrieved after measurement is identical [3], [13]. The non-destructive techniques also require calibration before the quantitative space charge density can be obtained [14]. The two common methods used to measure space charge distribution are the Pressure Wave Propagation (PWP) method and Pulsed Electro- acoustic (PEA) method. The PEA method can be applied to AC or DC fields. However, its DC application for measuring space charge would be the focus of this paper review and its advantages, limitations, progress and prospects discussed. The paper is organized as follows: Section I of the paper gave a general introduction on space charge and its measurement techniques, the principle of operation, calibration and system response of the pulsed electro-acoustic technique was discussed in section II, Section III talked about the advantages and limitations of the PEA method, the progress and prospects of the PEA technique was looked at in section IV, Section V discussed the conclusion of the review. RESEARCH ARTICLE OPEN ACCESS
  • 2. Habibu Hussaini et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 4, ( Part -1) April 2015, pp.90-95 www.ijera.com 91 | P a g e II. PULSED ELECTRO-ACOUSTIC (PEA) METHOD The pulsed electro-acoustic method was first created in 1987 [15], [16, [17] by the research group of prof. T. Takada working in cooperation with prof. C. M. Cooke [5]. This is the most widely used technique in the field of space charge measurement [18] compared to other methods. It is cheap, simple in structure and easy to implement. 2.1 Principle of Operation The principle of the PEA technique is based on the Lorentz force law and acoustic wave propagation in one dimension [19]. The pulsed electro-acoustic technique involves the application of high voltage, high frequency pulsed voltage probe across the sample which space charge profile is to be determined in order to stimulate motion of its internal charges thereby generating acoustic waves within the material [20] as shown in Fig. 1. The acoustic waves generated then propagate in the sample and are detected as electric signal by a piezoelectric sensor connected to the ground electrode. The amplitude of the signal is proportional to the charge quantity [16]. The space charge distribution is monitored as a function of time and measured quantitatively. The density and polarity of the space charge is obtained from the physical characteristic of the generated acoustic wave. However, the detected output signal in the PEA method do not give the space charge profile of a sample under measurement directly, due to the limited frequency band of the ceramic piezoelectric transducer (PZT) used [21]. A deconvolution technique developed in 1988 [22] is used to obtain the space charge profile of the sample. Fig. 1: Principle of the PEA method. (a) Charged regions give rise to acoustic waves under the effect of a pulsed field (b) Piezoelectric sensor gives a voltage vs(t). (c) Signal treatment gives the spatial distribution of image and internal charges [6], [23]. The applied DC voltage is usually in the range of 5-40 kV, depending on the sample thickness. The pulse voltage and width are in the range of 0.1-2 kV and 5-200 ns, respectively [5]. The acoustic pressure wave p(t) generated in the sample and the output signal of the system both expressed as a function of time is as shown in equation (1) and (2) respectively [21]. 𝑝 𝑡 = 𝐾[𝜍 0 𝑒 𝑝(𝑡) + 𝑢 𝑠𝑎 𝜌 𝜏 𝑒 𝑝 𝑡 − 𝜏 𝑑𝜏 + ∞ 0 𝜍(𝑑)𝑒𝑝(𝑡− 𝑑𝑢𝑠𝑎)] (1) Where K is the transmission coefficient of the acoustic wave in the ground electrode sample interface, sampling time is t, d is the sample thickness, and the acoustic velocity in the sample is usa. 𝑣𝑠 𝑡 = 𝐾[𝜍1 + 𝜍2 + 𝑢 𝑠𝑎 ∆𝑇𝜌(𝑥 = 𝑢 𝑠𝑎 𝑡]𝑒 𝑝 (2) Where σ1 and σ2 are the surface charges at the electrodes, ∆Tis the width of the pulse, the bulk charge is ρ, and e p is the amplitude of the pulse voltage. 2.2 Calibration and System Response Calibration is very significant and carried out in order to get an accurate quantitative analysis of space charge in solid dielectrics [24]. A novel calibration method in the presence of space charge in dielectric materials using the PEA techniques was developed in [24]. The calibration enables the plot of the charge profile in units of charge density, μ C/cm3 [21]. The system response of the PEA technique comprises of the transducer and amplifier response coupled with the attenuation and dispersion of the acoustic wave as it moves through the system. The distortion occurs in a situation whereby the transducer and amplifier do not pass the complete frequency content of the original acoustic signal [5]. Also, distortion occurs when the frequency response of the amplifier is not flat, amplifier’s high cut-off frequency is too low, or when both amplifier and transducer act as a high-pass filter [5]. This affects the accuracy of the quantitative analysis of the space charge distribution. However, this effect of system response is removed through appropriate calibration method. The method adopted depends on the sample [14]. The charge density calibration method for the PEA technique is as given in equation (3) in frequency domain [25], [26]. [ 𝜍(0) 𝑢 𝑠𝑎 ∆𝜏 + 𝑅(𝑓) + 𝜍 𝑎 𝑢 𝑠𝑎 ∆𝜏 exp⁡(−𝑗2𝜋𝑓 𝑎 𝑢 𝑠𝑎 )] = 𝜀0 𝜀 𝑟 𝑉 𝑑𝑐 𝑎 1 𝑢 𝑠𝑎 ∆𝜏 × 𝑉(𝑓) 𝑉0(𝑓) (3) Initially a DC voltage is applied to the sample to induce surface charges, however in order to avoid bulk charge formation, the voltage is set around 1-2 kV (low and short) for few seconds. The output signal of the PEA method is a voltage as shown in equation
  • 3. Habibu Hussaini et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 4, ( Part -1) April 2015, pp.90-95 www.ijera.com 92 | P a g e (3), the component is obtained from calculation, the deconvolution procedure performed in order to obtain the space charge distribution of a sample is represented by the component in which is the Fourier transform of the output signal proportional to the surface charge density σ(0). The Fourier transform of the space charge distribution is V (f). The impulse of the system function is . Component is the space charge response recovery signal after the effect of the system function is removed [25]. Subsequently, the space charge signal is obtained. Further discussion on PEA’s calibration can be found in [14], [24]. III. ADVANTAGES AND LIMITATIONS The two most widely used non-destructive techniques for space charge measurement are the PEA and PWP methods [26]. The PWP is further divided into two based on the generation principles of the narrow acoustic wave. These are the Piezoelectric Induced Pressure Wave (PIPW) method [12], and the Laser Induced Pressure Propagation (LIPP) method [27]. Both PIPW and LIPP have the same principle for space charge measurement[28]. In order to look at the advantages and limitations of the PEA technique, this report first compared the two techniques mentioned. 3.1 Comparison between the PEA and PWP Methods The comparison of the characteristics of both techniques is as presented in TABLE 1. TABLE 1 COMPARISON OF THE PEA AND PWP METHODS adapted from [26] Characterist ics PEA PWP PIPWP LIPP Excitation method Electric pulse Pressure wave by piezoelectr ic device Pressure wave by pulsed laser irradiation Sample thickness 100 µm- 20mm 100 µm- 1.0 mm 50 µm- 20mm Relative resolution 2-5% 2-5% 2-5% Minimum Space resolution ~ 5 µm ~ 5 µm ~ 2 µm Noise and electric shielding High voltage and signal High voltage and electric circuits separated by coupling capacitor. Cannot be used when circuits totally separated Can be used in the event of corona discharg e occurren ce. corona discharge occurs. Fast varying space charge distribution measureme nt Possible Possible No report about it. Measureme nt signal Pressure signal Displacem ent current Displacem ent current 3.2 Advantages The PEA method has the following advantages over other techniques used in space charge measurement; 1) Simple and Robust Equipment: This allows the PEA method to be deployed in various environments and industrial applications [24]. 2) Safe Method: For the PEA both high voltage and acoustic detecting circuits are electrically separated through the ground electrode, as a result protecting the amplifier and oscilloscope from damage in the event of an electric breakdown [29]. Hence, regarded as the safest technique for space charge measurement in cable samples through high voltage application. 3) Simple Principle of Operation: The PEA techniques do not need complex mathematical treatment just like the LIPP and PWP [14]. It has a simple modeling and is easy to implement for both plaque and cable samples [24]. 4) Less Noisy Output Signal: This is due to the fact that the PEA’s detection circuit can be shielded electrically [29]. 5) It has a lower cost compared to other technique due to its simplicity. 3.3 Limitations 1) Only Two Dimensional Measurements: The conventional PEA technique can only measure space charge in amplitude and spatial location along the thickness of a sample. The planar non uniformities in the surface direction are not accounted for. 2) Measurement of Cables with Different Radius: The PEA technique has problem in the measurement of cables with different radius as modification is required of aluminium block
  • 4. Habibu Hussaini et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 4, ( Part -1) April 2015, pp.90-95 www.ijera.com 93 | P a g e electrode, acoustic sensor, and PMMA absorber before it allows the change in cable radius [29]. This is quite a tasking and time consuming thing to do. 3) Spatial Resolution: The highest positional resolution that can be obtained using the conventional PEA technique is approximately 3 µm with deconvolution and 10 µm without deconvolution [20]. This is because the system spatial resolution is determined entirely by the pulse width and sensor thickness [29]. As a result, it cannot be used in applications with thin samples as low as 10 µm and approximately 1 µm spatial resolution, such as electron beam charge deposition in spacecraft charging and for high energy and plasma physics apparatus. IV. PROGRESS AND PROSPECTS OF THE PEA METHOD The PEA method has undergone some improvements as discussed in the following; 4.1 Three-Dimensional Observation New 3D PEA space charge measurement systems were developed [30] using acoustic lens and a new scanning system with small detecting electrode [31] to improve the measurement capability of the conventional PEA technique. The later allows space charge accumulated in small areas such as defects in insulating materials like voids, or trees, when high voltage is applied on the insulation material to be measured. The former allows accurate measurement of 3-D space charge profiles when the profiles do not change rapidly with time. This makes it easy to monitor long time ageing phenomena [32]. 4.2 High Resolution A refined PEA measurement system was developed [33] for use in thin dielectric materials. The conventional PEA method was only able to measure space charge of thick dielectrics materials of about (1-5mm). The refined system was able to improve the resolution of the PEA technique to 3 µm using the Fast Fourier Transform deconvolution to compensate for the piezoelectric sensor. Resolution in the lateral and thickness direction has been improved to approximately 100 µm and 2 µm respectively making it possible to investigate internal charge behaviors in composite materials such as insulation layers of printed circuit boards [32]. 4.3 Portable PEA System The conventional PEA system data requires computer deconvolution in order to display the space charge distribution of an insulation material. Maeno developed [23] a new PEA system whose output signal can display the space charge distribution directly on a portable oscilloscope without the need for deconvolution. This makes it possible to measure space charge distribution on site and can be used in various industrial applications. However, the spatial resolution of the space charge measurement of the new system is 10 µm as that of the conventional system [13]. Other advancements includes high repetition rate (time resolution) system capable of measuring space charge profile every 10 µs up to maximum of 1 ms [34], and an increase sensitivity of approximately 0.03-0.15 C/mm3[2]. The future of the PEA technique would be in its application in the nano dielectrics research field for space charge measurement, especially their interfaces with the electrodes [13], [35]. V. CONCLUSION The PEA measurement technique for space charge measurement has greatly improved since the over twenty years it was first introduced, as a result of advancement in technology. Most of the limitations identified with the conventional PEA system have been improved upon coupled with its advantages; hence it would continue to be the most widely used technique for some time to come. REFERENCES [1] L. Dissado, G. Mazzanti and G. Montanari, "The role of trapped space charges in the electrical aging of insulating materials," IEEE Transactions on Dielectrics and Electrical Insulation., vol. 4, no. 5, pp. 496- 506, 1997. [2] K. Fukunaga, "Progress and Prospects in PEA Space Charge Measurement Techniques," IEEE Electrical Insulation Magazine, vol. 24, no. 3, pp. 26-37, 2008. [3] S. Hol´e, T. Ditchi and J. Lewiner, "Non- destructive Methods for Space Charge Distribution Measurements: What are the Differences?," IEEE Transactions on Dielectrics and Electrical Insulation, vol. 10, no. 4, pp. 670-677, 2003. [4] T. Hanley, R. Burford, R. Fleming and K. Barber, "A general review of polymeric insulation for use in HVDC cables," IEEE Electrical Insulation Magazine, vol. 19, no. 1, pp. 13-24, 2003. [5] P. Morshuis and M. Jeroense, "Space Charge Measurements on Impregnated Paper: A Review of the PEA Method and a Dicussion of Results," IEEE Electrical Insulation Magazine, vol. 13, no. 3, pp. 26- 35, 1997. [6] O. Gallot-Lavallée, V. Griseri, G. Teyssedre and C. Laurent, "The Pulsed Electro- Acoustic Technique in Research on Dielectrics for Electrical Engineering," RS -
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