Advancing EDM Through Fundamental Insight Into The Process: Workpiece Workpiece
Advancing EDM Through Fundamental Insight Into The Process: Workpiece Workpiece
Advancing EDM Through Fundamental Insight Into The Process: Workpiece Workpiece
1 2 3 4
M. Kunieda (2), B. Lauwers (2), K. P. Rajurkar (1), B. M. Schumacher (1)
1
Tokyo University of Agriculture and Technology, Japan
2
Katholieke Universiteit Leuven, Belgium
3
University of Nebraska-Lincoln, USA
4
University of Applied Science St Gallen, Switzerland
Abstract
This paper aims to show the prospects of electrical discharge machining (EDM) technology by interrelating
recent achievements in fundamental studies on EDM with newly developed advanced application technologies.
Although gap phenomena in EDM are very complicated and hence not yet very well understood, recent
improvements in computers and electronic measuring instruments are contributing to new discoveries and
inventions in EDM technology. Such newly acquired insight sometimes raises questions on the validity of the
established theories of EDM phenomena, and EDM processes once believed to be impossible or unrealistic are
now becoming practical.
Keywords:
Electrical discharge machining (EDM), Wire electrical discharge machining (WEDM)
Figure 3: Wire electrical discharge machining (WEDM). Figure 4: Relaxation type pulse generator.
Gap voltage
Gate control circuit
Long delay Forward
0V
Time
Large gap
20 Ω
100V Tool electrode Time Proper gap
Short delay
Power supply Workpiece Retract
Time
Figure 5: Transistor type pulse generator. Small gap
0
0 AnoAnode
de
100
Gap
RadRiu
adius 200 Gap
s [μ[μm] 300 Catho
m] Cathode
de
Pulse duration, te µs
Figure 12: Temperature distribution in electrodes and
Figure 14: Relationship between removal amount and
gap obtained by magnetohydrodynamics analysis.
pulse duration.
10000
0.1mm
Temperature [K] [K]
Calculation model
Temperature
Heat flux q”
5000 Heat source area A
Measuring point
Fe
Fe
Foil electrode
Cu
Cu
Rod electrode
Foil electrode
0 Experimental Constantan wire
0 1 2 3 4 5
setup (φ0.1mm)
Time [µs] Thermocouple
Time [µs]
Figure 13: Calculated plasma temperature decrease
during discharge interval when material used for both Amplifier
anode and cathode is steel or copper. Figure 15: Method to obtain energy distributed
into electrode in single pulse discharge.
3.3 Energy distribution
The anode and cathode removal amounts are greatly
Energy distribution ratio
8000 Gap distance 0.5mm discharge. Their detection method, however, does not yet
6000 allow the measurement of the diameter of the arc column.
About the timing of material removal, there are still different
4000 findings. Zolotykh [11] reported that high-speed
Discharge duration: 300µs 5 µs photographs showed that most of the metal is ejected due
2000
to boiling of the superheated crater at the end of discharge
0 when the bubble pressure drops sharply, promoting the
-50 0 50 100 150 200 250 300 350 discharge of the gas dissolved in the molten metal. On the
other hand, Yoshida et al. [13] found that metal removed
Time µs
per pulse in air is almost equal to that in liquid, indicating
Figure 18: Plasma temperature at gap center during that metal removal can occur without a sharp drop of
and after discharge measured by spectroscopy.
bubble pressure. Observation of the gap of single pulse the plasma to be extinguished is short, leading to stable
discharge in dielectric liquid using X-ray also shows that machining. Difference in the plasma temperature decrease
85% of material removal occurs during the discharge calculated, shown in Figure 13, is a result of the difference
duration [39]. in the thermal diffusivity of the electrode material. Uno et al.
Xia [25] examined the influence of the assumptions used in [42] and Suzuki et al. [43] used CVD-carbon and
the boundary conditions: heat source diameter, heat flux electrically conductive CVD diamond as tool electrode
distribution in the heat source, and timing of metal removal, materials, respectively. Due to the high thermal diffusivity of
on the calculation results of temperature distributions in the these materials, EDM could be performed with almost no
electrodes. It was found that these assumptions exert a wear of the tool electrode.
significant influence on the calculation results of boiling Zingerman [44] states that Joule heating does not play a
point and melting point isothermal surfaces. Unfortunately, substantial role in the machining of metallic materials,
however, determining the boundary conditions is still a because electrical potential drops in metallic workpieces
controversial issue. Hence fundamental studies on the are negligibly small. According to the calculated results of
issue are highly looked forward to. Rich [45], however, the Joule heating is extremely
To show the influence of thermophysical properties of concentrated in a hemispherical volume directly under the
electrode materials on temperature distribution inside the discharge spot, and for high-resistivity metals, e.g., Hg, Sb,
electrode, the heat transfer equation was solved using a Fe, and Bi, the Joule heating is comparable to the energy
simplified model assuming an expanding circular heat input from the arc plasma. Saeki et al. [46] calculated the
source with a uniform heat flux and ignoring the metal workpiece temperature distribution considering the Joule
removal and temperature dependence of thermophysical heating as well as the heat flux from the arc column and
properties [40]. found that the removal of high-electric-resistivity material
(Si3N4-30wt%SiC) in a single discharge is greater than that
Figure 19 and Figure 20 show the calculated results when of steel due to Joule heating under the same discharge
steel and copper are used as the electrode material, current. However, it was found that a longer discharge
respectively, assuming the same energy distribution ratio of interval is necessary to deionize the arc plasma and
25%. Based on the formula obtained by Saito et al. [41] recover the insulation of the gap after each pulse, which
assuming that the heat source diameter is equal to the results in a lower material removal rate of high-resistivity
discharge crater diameter, the time dependent function of materials in a practical EDM.
the heat source diameter d(t) was determined as:
As a thermal machining process, EDM provides a means of
0.4
d (t ) = 2.4 × 10 −3 × t 0.4 × i e [m] (2) machining ceramic materials, irrespective of their hardness
and strength, provided that their electrical conductivity
Here, t is the time after ignition. Although the melting point values are of the order of 0.01 S/cm (100Ωcm) [47]. Owing
of copper (1357K) is lower than that of steel (1808K), the to the sometimes very different physical properties of the
melted zone of copper is considerably smaller than that of materials, electrical discharge processing produces a
steel due to its higher thermal diffusivity (1.1×10-4m2/s) than porous surface on which the binder phase has been
that of steel (2.0×10-5m2/s). With the expansion of the preferentially removed. Processing of thermo-shock
plasma radius, the melted zone is even resolidified during sensitive materials causes material to be removed by
the discharge duration in the case of copper. During the spalling.
discharge interval to, since the surface temperature at the
discharge spot drops rapidly in copper, the time needed for
Temperature, K
In-d r,
e
po pth l n
μmsition adia sitio
z, R po m
μ
t =10μs, t =100μs, 20μs after
d(t) = 50.8μm d(t)=121μm discharge
Figure 19: Temperature distribution in steel workpiece (cathode) (ie: 30A, te: 100μs, energy distribution to cathode: 25%)
Temperature, K
In-d
e r,
po pth l n
μmsition dia sitio
z,
Ra po m
μ
t =10μs, t =100μs, 20μs after
d(t) = 50.8μm d(t)=121μm discharge
Figure 20: Temperature distribution in copper workpiece (cathode) (ie: 30A, te: 100μs, energy distribution to cathode: 25%)
3.6 Chemical aspects liquid, and electrode materials with low melting point, at
EDM is undeniably a thermal process. However, by least at the surface. Thus, deterioration of surface quality
acknowledging that EDM is also a chemical process, new due to electrolysis in de-ionized water occurs [64]. When
findings and creative ideas can unexpectedly be obtained. ED-machining on high alloy steels in the commonly used
One of the applications of arc discharge was originally de-ionised water, toxic ions of heavy metals become
production of fine particles of metals [48]. Even now the dissolved in the dielectric. These are examples which
Reactive-Electrode Submerged-Arc (RESA) method [49] is demonstrate the importance of chemical aspects.
under investigation for producing ultrafine powders based 3.7 Role of dielectric liquid
on reaction between electrode materials and dielectric fluid. As described in Section 3.5, Zolotykh [11] and Snoeys and
It is well known that diamond-like carbon [50] and carbon Van Dijck [7, 8, 23] reported that most of the metal removal
nanotubes [51] can be produced using arc discharge occurs due to boiling of the superheated molten mass in
evaporation methods. the crater at the end of discharge because boiling of that
The EDM arc plasma temperature is high enough to not superheated metal is prevented by the bubble pressure
only evaporate the electrode materials and dielectric liquid during the discharge duration. Hockenberry et al. [12]
but dissociate and ionize their molecules and atoms. As stated that after the discharge termination when the
Hayakawa et al. [20] concluded, the EDM gap condition is expanded gas bubble starts to collapse due to its pressure
not in equilibrium during the discharge duration, and a large drop below atmospheric pressure, the gas bubble becomes
fraction of the discharge power is consumed in chemical fragmented and the liquid jets which penetrate the bubble
reactions. Eubank et al. [15] analyzed the enthalpy and impinge upon the electrode crater from all directions
increase in plasma involving dissociation and ionization of will strike the discharge crater and eject the molten metal.
water. Lauwers et al. [52, 53] investigated the cutting rate of On the other hand, Yoshida et al. [13] observed debris
WEDM of ceramics using de-ionized water, and pointed out formation and their distribution on the working surface due
that besides typical material removal mechanisms like to a single discharge. Figure 22(a) and 22(b) show the
melting and evaporation, other mechanisms such as distribution of debris obtained from single pulse discharge
decomposition and oxidation were identified. in air and liquid, respectively. In the case of discharge in
Toenshoff et al. [54] states that using a dielectric such as liquid, a solution of gelatin (25wt%) of 303K was used as
mineral oil or an organic fluid for ED sinking, hazardous dielectric liquid, and after the discharge the temperature of
fumes like polycyclic aromatic hydrocarbons, benzene, the experimental setup was lowered to freeze the gelatin to
vapour of mineral oil, mineral aerosols and various
by-products are generated by the dissociation of oil and its 8mm
additives. Kusano et al. [55] analyzed the components of Bubble boundary
the bubble generated using a hydrocarbon dielectric by gas 1.5mm
chromatography and showed that the volume fractions of - 8mm 8 -3mm
8 3mm
hydrogen gas and hydrocarbon gases, which involve
molecules with carbon atoms less than seven, are 56% and 8mm
36%, respectively, under a medium finishing condition. -1.5mm
Another example is the deposition of carbon on the anode - 8mm (b) In liquid
surface by the thermal decomposition of the working oil
(a) In air
(Figure 21). The white layer generated on workpieces
machined in hydrocarbon oils contains more carbon than Ie 32A, te 120μs
the base material, while that in a water dielectric contains Under 5μm 10 15 20 Over 30
less carbon than the base material [56]. Material removal Figure 22: Size and location of debris particles scattered
rates can be improved by supplying oxygen gas into the on electrode surface due to single pulse discharge.
discharge gaps filled with water-based dielectric liquid [57] h
or air [58]. Material removal rate using water based h
Distribution of debris diameter
Over 30μm
based on volume, %
Over 30μm
improved by mixing organic compounds into water, it did 60 60h
h
not compete with that of hydrocarbon oil [59, 60]. Some 40 40
5 h
publications, however, showed higher material removal rate 20
15
20μm 20
h
20μm
2 10 15μm
of water-based dielectrics [52, 53, 61-63], because water is 0 0h 10
5
dissociated by discharge to hydrogen and oxygen, resulting 20 60 120 200 360
h20 60 120 200 360
in oxidation of workpiece materials [52, 53, 62]. Discharge duration, μs Discharge duration, μs
In order to reach stable machining conditions in WEDM In air In liquid
(large gap width for the vibration of the wire) and to obtain a
high rising speed of the discharge current, it is necessary to Figure 23: Debris diameter distribution based on volume.
use a relatively high open voltage, less insulating dielectric
Total volume of generated
In liquid
10-4
In air
10-5
Anode(+)
debris, mm3
10-6
Carbon 10-7
deposition
10-8
0 100 200 300
Discharge duration, μs
Cathode (-)
Figure 21: Deposition of pyrolytic carbon on anode in Figure 24: Comparison of total volume of
hydrocarbon dielectric (SEIBU ELECTRIC & MACHINERY). generated debris between air and liquid.
keep the debris from scattering. Then distribution of the found that 80 to 90% of the working area was occupied by
size of debris generated by the single discharge was gas bubbles during the process as illustrated in Figure 27.
observed by an optical microscope. Figure 23 shows the Imai et al. [66] measured the bubble quantity in the working
debris diameter distribution in volume. Figure 24 shows the gap utilizing ultrasonic waves passed through the working
measured total volume of debris generated in air and in gap. The ultrasonic wave transmitted through the electrode
liquid. It is found that there are differences in the total and incident normal to the working surface was mostly
volume of the generated debris and the distribution of the reflected at the interface when the gap was not filled with
debris size between single pulse discharges in liquid and in dielectric liquid. They found that more than half of the
air when the discharge duration is short. No difference working area is occupied by bubbles at higher discharge
exists however for discharge durations longer than 90µs. currents, shorter discharge intervals and longer machining
The debris volume difference is very small when the periods between jump flushing motion of the tool electrode.
discharge duration te is long. This is because the discharge Thus Tanimura et al. [67] proposed a new EDM method in
column is located at the center of the bubble generated by which air mixed with water mist is supplied to the discharge
the discharge itself and the diameter of the bubble grows gap and found that the EDM in mist shows almost the same
up to several millimeters as shown later in Figure 29. machining abilities as conventional EDM. Karasawa et al.
Hence, as time elapses, the arc column environment [68] showed that the material removal rate with a dielectric
becomes equivalent to that of the discharge which occurs liquid poured into the gap in air is higher than that with the
in gas with the increase in the diameter of the bubble. gap submerged in a tub of the dielectric liquid because the
The above results indicate that metal removal can occur ability of flushing debris in the pouring method is higher
without a liquid dielectric. In air, however, most of debris than that in the submerging method. All the above results
particles were reattached to the workpiece surface, as suggest that removal itself does not require the gap to be
shown in Figure 25(a) [13]. This is because the melted entirely filled with liquid. It should be noted that findings
debris particles move with constant velocity in air and do obtained from single pulse discharges in a gap filled with a
not solidify until they hit the electrode surface. In the case dielectric liquid cannot always be extrapolated in the actual
of liquid, in contrast, the debris particles proceed straight EDM process. Natsu et al. [69] found that removal in a
through the gas bubble and penetrate the bubble wall, and single pulse discharge is greater than the material removal
as a result decelerate. They then solidify into a spherical per pulse in consecutive pulse discharges. They measured
shape under the influence of surface tension [12] as shown the change in the removal amount at anode and cathode
in Figure 25(b), confirming that the dielectric liquid is with increasing number of repetition of pulse discharges in
important for the cooling and flushing of debris particles but an originally fresh inter-electrode atmosphere which is
not for material removal. achieved by the jump action of the tool electrode, and
found that the removal amount per pulse decreases
Miyajima et al. [65] found that the working gap is mostly strongly with repetition.
occupied by bubbles although the working gap is
submerged in dielectric liquid. Figure 26 shows the bubble 3.8 Forces applied to electrodes
conglomerated in the discharge gap when machining was The force accompanying the discharge is caused mainly by
interrupted and the tool electrode was lifted to widen the the expansion and contraction of the bubble generated by
gap. From the volume of the conglomerated bubble it was the evaporation, dissociation and ionization of the dielectric
liquid and electrode materials. Figure 28 shows a model to
(a) In air (b) In iquid calculate the bubble oscillation in the gap between
parallel plane electrodes [9]. The model illustrates a case
that a bubble with a high pressure is generated at the
center of the gap between cylindrical electrodes. The
bubble expands and contracts periodically. The reaction
force applied to the tool electrode can be calculated by
integrating both the pressure in the bubble and that in
Figure 25: Shapes of debris generated in air and liquid. dielectric liquid over the working surface [70].
Photos in Figure 29 taken by Ikeda [71] show the oscillation
of the bubble generated by a single pulse discharge in a
Liquid surface gap between parallel plane electrodes. The reaction force
in Figure 29 was measured by Kunieda et al. [72] using the
Split Hopkinson Bar method [73], with which the influence
Tool electrode (+)
of the natural frequency of the measurement system was
(Copperφ20mm) successfully eliminated. At the initial state in which the
bubble is compressed, the force indicates the highest peak.
Workpiece (-) With the expansion of the bubble, the force decreases
(carbon steel) according to the decrease of the bubble pressure. The
P(r)
Pressure distribution
Tool electrode
Discharge location
Atmospheric
Gap width Bubble Dielectric
Dielectric pressure
contaminated Workpiece
with debris
Initial diameter of bubble
Figure 28: Pressure distribution in bubble generated by
Figure 27: Schematic view of working surface. single pulse discharge in gap filled with dielectric liquid.
Photographed
Dielectric reakdown
by Ikeda [71]
Reaction force, N 50
0
Dielectric breakdown
- 50 Discharge duration
0 Dielectric 2breakdown 4
Time, ms
Figure 29: Oscilation of bubble observed by Ikeda [71] and reaction force measured by Split Hopkinson
Bar method (ie 30A, te 150μs, gap width 0.15mm, anode: copper φ20mm, cathode: steel φ20mm).
force even becomes negative because the bubble distribution of the debris. On the other hand, due to the
continues to expand even after the bubble pressure falls extended gap width, servo gap control becomes easy.
below the atmospheric pressure due to the inertia of the Otherwise it is difficult to keep gap widths of several µm
dielectric liquid which is moving radially away from the constant.
discharge spot. When the diameter of the bubble reaches A simplest explanation for the decrease in the dielectric
the maximum, the absolute value of the negative force breakdown strength is that the electrically conductive
becomes maximum. Then, the bubble starts contracting, debris particles reduce the apparent gap width by a
and the force increases showing a dumping oscillation due distance equal to the diameter of the particles. However,
to the viscosity of the dielectric liquid. the measured gap width is occasionally larger than 100µm,
Since the natural frequencies of EDM machine structures whereas the measured average diameter of debris particles
are much lower than the frequency components included in is only 25µm under a certain pulse condition. This result
the reaction force waveform, the gap width cannot respond can be explained in terms of the movement of debris
to the change in the force. Furthermore, the reaction force particles in the gap, which was observed by Suda et al. [78],
in a series of pulse discharges decreases with time while Bommeli et al [4], Schumacher [79] and Kunieda et al. [80].
the working gap fills with bubbles generated by each They found that the debris particles move between the
discharge [70, 72]. Hence influence of the force caused by anode and cathode in a direction perpendicular to the
each pulse discharge is negligibly small in sinking EDM. electrode surfaces due to electrophoresis. They also
However, it causes vibration and deflection of electrodes in observed that some particles are linked in series to form
the cases of wire EDM and micro EDM. chains parallel to the electric fields.
It is also known that an electrostatic force occurs between From the observed results Bommeli et al. [4] and Kunieda
the tool electrode and workpiece [74, 75] mainly during the et al. [80] hypothesized that in the gap there are numerous
discharge delay time in which an open voltage is applied chains of particles which almost bridge the gap and that
between them. In WEDM, when the discharge energy is discharge occurs at the site at which the end of a chain is
small, the influence of the electrostatic force cannot be closest to the opposite electrode surface. Bommeli et al. [4]
ignored in comparison with the above mentioned reaction statistically investigated the distribution of ignition delay
force. Although the electrostatic force per unit length along time to demonstrate that discharge occurs after an
the wire electrode is small compared with the reaction force, activation time which is necessary for debris particles to
the total electrostatic force may not be negligible, because form bridges between the electrodes. Kunieda et al.
the force can be applied at any point on the wire which is calculated the electrophoresis-induced motion of a particle
facing with the workpiece surface. Electromagnetic force and found that the time interval for 30µm diameter steel
can also be applied to the wire electrode at any location particle to reciprocate between the parallel plane
where the workpiece is facing the wire electrode, because electrodes and the average velocity were 1.32ms and
high frequency current pulses generate an electric current 0.136m/s, respectively showing a good agreement with the
flow on the workpiece surface in parallel with the wire results of observation using a high-speed video camera.
electrode due to skin-effects [5, 75, 76]. The velocity is high enough for the last particle to enter
small gaps between the end of the bridge already present
4 PROCESS STABILITY and the opposite electrode surface and ignite the discharge
4.1 Factors determining discharge location during the ignition delay time.
Basically discharge occurs where the gap width is shortest. In order to further study the influence of debris particles, a
This principle guarantees the replicating accuracy of EDM. debris particle with a diameter of 5µm is placed in a gap of
To obtain an electric discharge in clean oil the gap width 20µm in width as shown in Figure 30. If it is true that
must be less than several µm. However, since the dielectric discharge occurs at a point where the gap is shortest, the
liquid is contaminated with electrically conductive debris discharge will probably occur at the point where the debris
particles, whose average diameter is one third to half of the particle is placed. In this experiment [81], the gap was filled
gap width, discharge occurs through the debris particles, with a clean EDM working oil and the surface roughness of
resulting in gap width much larger than that for an the electrodes was 0.8µm Rz. However, the experimental
uncontaminated dielectric [4, 77-79]. This fact sometimes results showed that in most cases, the discharge crater
causes reduced replicating accuracy due to the uneven could not be found at the point where the debris particle
50mm ie= i1+ i2
i1 i2
ro ro
20μm
Discharge Tool electrode
rc rc
5μm R1 R2
Debris particle
Workpiece
Figure 30: Discharge location is determined in
not deterministic but probabilistic way. Figure 31: Principle of measuring discharge locations.
was placed. This is because occurrence of discharge is a Feed of tool electrode
probabilistic phenomenon and the probability of occurrence
of discharge per unit area is not zero even if the gap width Elede
Electrode
location
Electrode
Electrode
105mm
location
105mm
Spark
location
Electrode
Spark
Spark
105
105
Servo feed
20μm
20μm
Correlation dimension dm
30
improved because the lateral gaps of the groove became
25
narrower and more uniform.
20
0 500 1000 15 The working gap can be flushed by a fresh dielectric fluid
0 500 1000
No. of dischages Discharge locations jetted from nozzles placed adjacent to the discharge gap.
10
No. of discharge Masuzawa et al. [94] however reported that jetting of
5
0
dielectric fluid merely from one direction causes increased
Attractor dimension of 0 5 10 15 20 25 30 density of debris particles in the downstream, resulting in
discharge locations Embedding dimensions m uneven distribution of gap width deteriorating the
Figure 34: Chaos found in distribution of discharge locations. machining accuracy. Hence they demonstrated that
flushing from both sides, alternate flushing, and sweeping
flushing is preferable. Pressure or suction flushing through
400
holes in the electrode or workpiece remains one of the
most efficient flushing methods at least if those holes have
Temperature, ℃
Without superimposition 0
800 1600 2400 Time [μs]
Gap current [A]
4
2 ie is
0
0 40 80 100 160 Open Normal Arcing Arcing Short Time [μs]
circuit spark 1 2 circuit
Discharge location, mm
Wire electrode Figure 38: Voltage and current waveforms of
the five basic EDM gap states [104, 105].
Workpiece
Lower brush Upper brush
Discharge interval to [μs]
50 Start point
Figure 36: Control of discharge locations by
Arcing and short-circuit zone
3 Arcing zone
-2.0 -1.0 0 1.0 2.0
Conventional Multi spark Servo reference voltage us [V]
Figure 37: Principle of multi-spark EDM method. Figure 39: Algorithm of steepest ascent path [107].
determined by the servo reference voltage, to seek the
Discharge
current
highest value of the pulse efficiency in order to achieve the
maximum machining rate. Removal rate
To reflect the dynamic behavior of the EDM process, a
dynamic modeling approach so called self-tuning control
Time
was proposed [108]. In this model, the outputs which are
used to adjust the servo reference voltage and discharge
interval are based on the detection of the type of pulses that Surface
Tool wear ratio
occur in the gap (see Figure 38). During machining, the roughness
outputs are maintained at the level of reference values
which are manually set according to given machining
conditions. To improve machining productivity, this model
has been simplified by linearizing the output value with the Figure 40: Relation between discharge current
machining gap size. During machining, the difference waveforms and machining characteristics.
between the output of the process and the output of the discharge duration result in higher material removal rates.
reference model is controlled at a minimum value [109]. To At the same time, low tool electrode wear can also be
address the internal dynamic characteristics of the closed satisfied because the carbon layer deposited on the anode
loop servo system for stabilizing the machining process, the tool electrode is thicker when longer discharge durations
adaptive servo system was modified into a self-tuning are used [21, 25-31]. However, surface roughness is not
regulator system [110]. good because the crater generated by each pulse
When a deep and narrow cavity is machined, electrode discharge is large. Thus this pulse condition is normally
jumping operation is always used to retract the tool from the used in rough machining.
machining area to improve the flushing condition. In the On the other hand, the pulse condition with longer
adaptive jumping control system, the system output is discharge duration and lower peak current brings about
calculated based on the ratio of the sum of abnormal both lower tool electrode wear ratio and better surface
discharge time to the total pulse on-time. When the roughness. However, the lower heat flux due to the lower
machining depth increases, the ratio of the jump-down time current density at the discharge spot results in lower energy
in one jumping cycle is reduced to avoid harmful arcing [111, efficiency of material removal compared with the pulse
112]. condition with shorter discharge duration and higher peak
EDM lacks a direct link between the theoretical models of current even though the same pulse energy is applied. In
material removal mechanism and industrial applications. In this situation, the melted and evaporated regions in the
many cases, empirical knowledge is helpful for deciding workpiece are small and most of the energy distributed to
machining parameters without explicit mathematical models. the workpiece is dissipated inside the workpiece due to
Such expert knowledge is simply expressed as IF-THEN heat conduction. Obviously, the material removal per pulse
rules to describe the relationship between the input and is small. In addition, longer discharge duration results in
output of system. Therefore, they are applied in on-line lower discharge frequency per unit time. Thus this pulse
control, off-line process planning and operator assistance. condition is suitable for finishing.
There are many research results published on fuzzy logic Finally, pulse conditions with shorter discharge duration
control either on sinking EDM or on wire EDM [113-118]. and higher peak current provide better surface roughness
An artificial neural network consists of many neurons due to smaller discharge crater. Moreover, although
arranged in different layers. Each neuron is connected to material removal per pulse is not large, it is large enough
every neuron in the previous and following layers with a compared with the pulse condition with longer discharge
variable weight. The self-learning algorithm automatically duration and lower peak current under the same discharge
adjusts these weights based on training input-output sets. energy per pulse because energy efficiency is higher due to
Neural networks have been used to optimize EDM sinking larger heat flux. Higher repetition rate of discharge per unit
process to improve gap width control, harmful arc time due to shorter discharge duration further increases the
prevention and high machining accuracy [119, 120]. They material removal rate. However, the tool electrode wear
are also used in WEDM to estimate the workpiece height ratio is high because the carbon layer deposited on the tool
and maintain optimal and stable machining [121]. electrode is thin. This is why extremely short discharge
To integrate EDM within the next generation agile duration and high peak current compared with the case of
manufacturing environment, a system with communication sinking EDM, for example 1µs and 100A, are used in
function through internet has been developed. The Web WEDM, where the problem of tool electrode wear is
Home Page Browser window is used to browse information insignificant.
on the Internet. The complete data during monitoring can be 5.2 Factors influencing tool electrode wear ratio
recorded and displayed. The recorded data can then be Influence of polarity
used for off-line analysis and comparison of the effects of
different machining conditions [122, 123]. As shown in Figure 16, the energy dissipation into the
anode is greater than into the cathode. Nevertheless, in
5 MACHINING CHARACTERISTICS sinking EDM, polarity of the tool electrode is normally
positive except when a very short discharge duration is
5.1 Influence of pulse conditions used. This is because the carbon layer which is deposited
Figure 40 shows three machining characteristics which are on the anode surface due to thermal dissociation of the
most important in EDM practice: material removal rate, hydrocarbon oil protects the anode surface from wear.
surface roughness and tool electrode wear ratio. Here the Since the carbon layer is thick when the discharge duration
tool electrode wear ratio is defined as the ratio of volume of is long, the tool electrode wear ratio is low with the polarity
tool electrode wear to the volume of workpiece removal. of positive tool electrode under the pulse condition of
Requirements for any two of the characteristics can be longer discharge durations. On the contrary, a negative tool
satisfied if the remaining one is sacrificed using the electrode is used considering the energy distribution in the
discharge current waveforms indicated in Figure 40. cases of finish machining and micromachining where
However, there is no current waveform which can satisfy all deposition of carbon layer is scarce and of WEDM in which
the requirements. deionized water is normally used as dielectric liquid.
Current waveforms with larger peak current and longer
Influence of thermal properties of electrode materials tool electrode is almost zero because a micro rod is first
Since EDM is a thermal process, the influence of thermal made on the same machine by WEDG, followed by
properties of electrode materials on the removal volume is reversing its polarity to use the micro rod as tool electrode
significant. When the heat flux from the arc column is equal, to machine micro holes without loosening the chuck.
higher heat conductivity results in lower temperature on the Tool electrode wear
electrode surface. Hence materials with higher heat On-machine forming of micro rods is also possible using a
conductivity are suitable as tool electrodes. On the other block tool electrode as shown in Figure 42. However, wear
hand, under the same temperature distribution inside the of the block deteriorates the machining accuracy. In WEDG,
electrode, when the surface temperature is not over the there is no problem of wear, because a renewable wire is
boiling point or melting point, removal does not occur. used as tool electrode. Since the wire is guided by the
Hence materials with higher melting point and boiling point groove of the wire guide, machining accuracy is not
are also suitable as tool electrodes. The results of heat deteriorated by the wire vibration unlike the WEDM
conduction analysis shown in Figure 19 and 20 indicate process.
that although both melting point and boiling point of copper
are lower than those of steel, copper is more suitable as a Reaction force
tool electrode because copper has a much higher heat As shown in Figure 29, the peak of the reaction force
conductivity than steel. Thus, considering the higher generated by a single pulse discharge is remarkably large.
energy distribution to the anode, carbon layer deposition on Use of a block electrode causes discharge even at the end
the anode, and the thermal properties of electrode of the micro rod which is being formed, thus exciting
materials, it should be possible to select appropriate vibration of the micro rod. In WEDG, however, the bending
discharge current waveforms, polarity, and tool electrode moment applied to the almost finished micro rod is
materials to obtain minimum tool electrode wear ratio even insignificant because discharge only occurs at the foot of
lower than several %. the rod being formed.
Relaxation type pulse generator
6 CHALLENGES IN MINIATURIZATION
In micro EDM, the relaxation type pulse generator shown in
6.1 Strategy found in WEDG Figure 4 is still being used. If the transistor type is used, it
EDM processes are widely used for the micro-machining of takes at least several tens of ns for the discharge current to
fuel injection nozzles, spinneret holes for synthetic fibers, diminish to zero after detecting the occurrence of discharge
electronics and optical devices, micro-mechanical parts, because the electric circuit for detecting the occurrence of
and micro-tools for producing these devices. Figure 41 discharge, the circuit for generating an output signal to
shows the Wire Electro-Discharge Grinding (WEDG) switch off the power transistor and the power transistor
method which was developed by Masuzawa et al. [124]. itself have a certain amount of delay time. Hence it is
Using a wire electrode traveling along the groove of a wire difficult to keep the constant discharge duration shorter
guide, a micro rod can be machined like in a turning than several tens of ns using the transistor type pulse
process. Then, on the same machine, by reversing the generator.
polarity of the machined micro rod, micro holes of less than Stray capacitance
10 µm in diameter can be drilled by EDM. The following are
When the relaxation type pulse generator in Figure 4 is
the essential problems of micro EDM which were
used, capacitance of the capacitor should be decreased to
elucidated and solved by Masuzawa [125] through the
obtain smaller discharge energy per pulse. In the actual
development of the WEDG method.
EDM machine, however, stray capacitance exists between
On-machine forming of tool electrodes the electric feeders, between the tool electrode holder and
When a micro tool electrode is purchased or made using work table, and between the tool electrode and workpiece.
another machine in the machine shop and held by the Hence all the charge stored in the stray capacitance is
chuck of the micro EDM machine, the micro tool electrode discharged to the working gap together with the charge
is always off-centered more or less from the rotation axis of stored in the capacitor wired to the circuit as shown in
the spindle. In the WEDG machine, however, run-out of the Figure 43. This means the minimum discharge energy per
pulse is determined by the stray capacitance. Hence
Workpiece shortening of electric feeders and use of electrical insulator
for the tool electrode holder and work table materials are
effective for reducing discharge energy. In the final finishing,
Dielectric liquid when minimum discharge energy is necessary, the
capacitor is not wired and machining is conducted with the
stray capacitance only. Since the working surface area
Wire electrode between the tool electrode and workpiece in WEDG is
narrower than that in the block electrode method, smaller
stray capacitance of the working gap is advantageous to
Wire guide WEDG for the limit of miniaturization.
Some attempts [126, 127] were made to replace the
Figure 41: Wire electro-discharge grinding
relaxation type pulse generator with the transistor type
(WEDG) method [124]. pulse generator in micro EDM, and a minimum discharge
Pulse generator
R
C Stray capacitance
Micro rod workpiece Tool electrode
Workpiece
Figure 42: On-the-machine forming of micro rod Figure 43: Charge stored in both stray capacitance
using block electrode. and condenser is discharged.
duration of 30ns was achieved [126]. However, even if Discharge crater size
future developments of electronics devices can further Figure 45(a) shows a discharge crater generated on the
reduce the delay time existent in the transistor type pulse tungsten anode surface when using a capacitance of
generator, the discharge energy can never be smaller than 3300pF. Figure 45(b) shows a discharge crater generated
the energy stored in the stray capacitance. with stray capacitance only. Even with the minimum
Masuzawa et al. conducted assembly [128], milling [129], discharge energy, diameter of the discharge crater
blanking [130], electrochemical discharge machining [131], measures 2µm, indicating that the minimum discharge
and ultrasonic machining [132], based on the crater size may influence on the limit of miniaturization. As
on-the-machine manufacturing of micro jigs, cutting tools, described in Section 5.2, under the pulse conditions used
blanking tools, tool electrodes, and horns using the WEDG in micro EDM, since the carbon layer is scarcely deposited
method. on the anode surface due to the extremely short discharge
6.2 Factors influencing limits of miniaturization in duration, polarity of workpiece is normally positive because
micro EDM energy distribution into anode is larger than that into
cathode. Thus Han et al. [134] compared the diameter of
Kawakami et al. [133] examined the limits of minimum craters generated on an anode and a cathode workpiece
machinable size using the WEDG method. Cemented and found that the diameter was 2µm and 0.8µm,
tungsten carbide rods of 0.3mm in diameter with a WC respectively (Figure 46). However, the minimum diameter
particle size of 0.4µm were used as the workpiece. The of the micro rod machined by WEDG using the reversed
relationship between the target rod diameter and machined polarity was almost the same as that using the normal
rod diameter was obtained as shown in Figure 44. Red polarity. This was probably because the machining time
marks in Figure 44 indicate machining failure due to was about eight times longer than the normal polarity.
breakage of the micro rod. It should be noted that micro
rods smaller than 2.3µm in diameter were not obtained. Since discharge energy is 1/2(Cu02), decreasing the open
Deviation in the machined rod diameter from the target rod voltage u0 is effective for reducing the crater size. Thus
diameter was obviously caused by the positioning error and Egashira et al. [135] decreased the voltage of the power
thermal deformation of the equipment, and by the source to 20V and obtained the minimum rod diameter of
inaccuracy of wire electrode diameter used in WEDG. 1µm as shown in Figure 47.
However, these are not the reasons why rod diameters Residual stress
under 2.3µm were never obtained. If they were, one would There are two kinds of residual stress which may influence
have obtained successful results in the vacant zone since the limit of miniaturization. One is residual stress already
machining was repeated in great numbers. Therefore, in present prior to machining, and the other is residual stress
this case, plausible reasons would be the size of the caused by EDM.
discharge crater, sub-surface layer damaged by EDM,
residual stress, and material structure of the workpiece. Residual stress already present prior to machining, for
example, can be found in tungsten rods which are
produced by plastic deformation using the wire drawing
Machined rod diameter, μm
Figure 44: Relationship between target rod diameter Figure 47: Tungsten rod of 1μm diameter fabricated by
and machined rod diameter (WC grain size : 0.4μm). WEDG (Open voltage: 20V, stray capacitance) [135].
300µm 300µm
11.5μm
2μm
Before annealing
Without After annealing at 1000K
(a) C=3300 pF, open (b) Stray capacitance
voltage 110V only, open voltage 40V Figure 48: Influence of residual stress already present prior to
machining (tungsten rod, C=3300pF, open voltage 110V).
Figure 45: Discharge craters generated on tungsten anode.
10µm 10µm
Inlet Outlet
(c) Hole machined by formed rod
n=4: Multi-hole machining Figure 55: Irregular hole made by self-drilled hole
Figure 51: μEDMn method [142] method (open voltage: 110V,capacitance: 100pF).
rod and micro hole can be machined in a single process corrosion resistance, and tribological properties can be
without positioning control in the radial direction. obtained when the polarity of the workpiece is positive.
Figure 53 shows a simple but novel idea proposed by Mohri et al. [147] and Goto et al. [148] found that alloying
Yamazaki et al. [144] to machine micro rods and holes speed can be improved significantly by using partially
without using any special equipment like WEDG. With the sintered or green compacted materials such as Cu, Al,
polarity of a rod electrode negative, the rod electrode is WC-Co, and Ti as tool electrode. This is because the wear
rotated and fed into a plate electrode to make a hole. After ratio of these materials is high due to the low thermal
the rod electrode returns to its initial position, the rod conductivity of these materials. As shown in Figure 56 [148],
electrode is moved from the center of the hole at a certain a hard material (TiC) layer is coated on the workpiece
distance. Next the polarity of the rod electrode is reversed, surface since Ti is carbonized in the hydrocarbon oil. Using
and then the rod electrode is fed into the plate electrode the same setup as the usual EDM process, harder and
either with or without rotation. Positioning of the rod thicker layer coating with a higher bonding strength can be
electrode in reference to the tool electrode is not necessary conducted in a shorter time compared with the
because self-drilled holes are utilized as the tool electrodes. conventional methods like CVD and PVD. Figure 57 shows
Figure 54 shows a micro rod of 4µm in diameter formed by a cross-section of a TiC layer formed on carbon steel in
this method. Using this rod electrode as tool electrode, eight minutes [149]. Applications of this method to cutting
micro holes with a diameter of 5µm was perforated on a tools and blanking tools show that tool life becomes
copper plate. In Figure 55, a cross-shaped right-angled slot significantly longer [148, 150]. Various types of powder and
was formed using a rod electrode. Positioning the rod compact were proposed depending on workpiece materials
electrode on each corner of the cross-shaped slot without a and alloyed layers for the applications to steel rolls, molds,
rotation, EDM was performed to form the cross-shaped rod dies, cutting tools, turbines and aeroengine components
with reversed polarity. Using this cross-shaped electrode, [151-153]. To make this process possible, a negative
cross-shaped holes were formed on a plate. polarity of the tool electrode and a long discharge duration
is used. Under these conditions, as described in Section
7 INNOVATIVE EDM TECHNOLOGIES 3.3, the material removal rate of the cathode (tool
electrode) is higher than that of the anode and carbon
7.1 Electrical discharge coating and alloying coming from the hydrocarbon dielectric is deposited on the
EDM is undeniably classified as a removal process. anode (workpiece). The worn tool electrode material (Ti)
However, the EDM process can also be used as a surface and the deposited carbon yields the TiC coating.
treatment method and/or an additive process. White layers Hayakawa et al. [154] fabricated a micro structure shown in
generated on a steel workpiece machined by EDM using Figure 58 using EDM deposition in air. The suitable
hydrocarbon dielectric have a higher carbon content than discharge conditions for this process were predicted from
the base material and hence shows increased resistance to the transient temperature analysis of the tool electrode and
abrasion and corrosion [56, 64, 97, 145]. Under the high workpiece. To enhance the wear of the tool electrode, its
temperature of the discharge column, the white layer can polarity was set positive, which is opposite to the above
absorb carbon from the gases formed in the discharge coating and alloying methods, because removal rate of the
column from the hydrocarbon dielectric. Since WEDM anode is higher than that of the cathode in air.
normally takes place in deionized water, a discharge
column with a high oxygen and hydrogen content is built up. 7.2 Coloring of Titanium alloy using EDM process
In particular the oxygen causes decarbonization of the Minami et al. [155] developed a new method of coloring
material metal surface, thus increasing the density of alloys, titanium alloys using the WEDM process. Since deionized
which are generally chromium and nickel. This also water is normally used in WEDM, an oxide layer is formed
increases the corrosion-resistance of the surface [64]. over the surface of the anode workpiece due to electrolysis.
Narumiya et al. [97] reported that the workpiece machined It is known that the surface of titanium alloy and stainless
using a powder (Si, SiC or Al) suspended oil shows not only steel can be colored by anodic oxidation due to the
improved surface roughness but also increased corrosion interference of light in the oxide film formed by electrolysis.
resistance compared to the surface machined without
powder. Masui et al. [146] added fine tungsten powder in
the dielectric fluid to form an alloyed layer and found that Tool electrode (+)
great improvements in surface roughness, hardness,
Servo deposit
Hydrocarbon
Ti electrode
dielectric Power Work (-) Work (-) Work (-)
supply
Hard layer
Figure 58: Fabrication of micro-structure using EDM deposition
(Tool and workpiece: carbon steel, medium: air) [154].
-
Workpiece W ire e le c tro d e
Incident beam Interfering beams
W o rk p ie c e
(T ita n iu m a llo y)
Figure 56: Principle of EDM surface modification [148]. +
air P ro c e s s in g
d ire c tio n
h TiO2 film
Ti
absorption 1 s t-c u t s u rfa c e C o lo re d s u rfa c e
TiC layer (6µm)
Interference of light
S45C
Guide
Debris
Workpiece
Figure 61: Machining of insulating ceramics by
wire EDM (workpiece: Si3N4 ) [161]. Figure 62: Dry EDM milling.
- Heat affected zones such as the white layer are thin microscopes, high-speed imaging devices, and software
and micro cracks are few. tools for numerical analysis, fundamental studies are
- Process reaction force is negligible. progressing step by step, and some of the common EDM
knowledge which have been accepted for a long time are
- Gap is narrower than conventional EDM. being modified. On the other hand, given that numerous
- There is no corrosion which is caused by electrolysis discharge gap phenomena have yet to be fully understood,
when deionized water is used as dielectric fluid. the potentials of EDM technology may not be fully realized.
Hence dry EDM is also suitable for WEDM and micro EDM Undoubtedly, continuous efforts are expected to lead to
owing to the negligible process reaction force and the further developments of the EDM technology in the future.
minimized surface damage. Furudate et al. [171,172] found
that, when it is applied to finish-cutting in WEDM (Figure 9 ACKNOWLEDGEMENTS
63), straightness and geometrical accuracy of the finished The authors would like to acknowledge the following
surface are excellent owing to the significantly reduced colleagues who contributed to this paper: Prof. D. Allen, Dr.
vibration of the wire electrode due to the considerably H. Altena, Dr. P. Bleys, Dr. A. Goto, Dr. S. Hayakawa, Dr. T.
smaller process force compared with that in conventional Ishida, Prof. F. Klocke, Prof. J. Kozak, Prof. J.P. Kruth, Prof.
WEDM. G. N. Levy, Dr. D. Lung, Mr. T. Masaki, Dr. K. Masui, Prof. T.
Masuzawa, Prof. T. Matsuo, Dr. H. Minami, Prof. N. Mohri,
Prof. W. Natsu, Prof. Y. Takeuchi, Prof. Y. Uno, Prof. Z.Y.
Wire electrode Yu.
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