Temperature field in EDM of ceramics composites.
Opran, Constantin ; Blajina, Olvidiu
1. INTRODUCTION
Technical ceramics is characterized (Dumitras, & Opran, 1994)
as a composite type engineering material, with more than one fragile
phase, discretely crystalline, or amorphous. It is obtained in a
solidification and forming technological process, at high temperatures
and pressures where the resulting material should be, at least, 30% of
crystalline structure (Spur, 1889).
Ceramic composite represents a hole material system, anisotropic and non-homogenous, made of two or more various materials, with on
purpose made interfaces (Schneider, 1991). There are two main phases of
the material: the matrix and the reinforcing element (Vaia & Wagner,
2004).
In this paper an electro-conductive composite ceramic is studied.
It is made of two refractory materials: one electrical non-conductive
([Al.sub.2][O.sub.3]) and one electrical conductive (TiC). They are made
of the ceramic phase--[Al.sub.2][O.sub.3], whose size is 3 urn, the
metal phase--TiC, whose size is 5 urn and the binder--Zr[O.sub.2]. As
the percent of TiC is from 30% up to 45% and the maximum binder percent
is 1% it results that the [Al.sub.2][O.sub.3] percent is the biggest
(all results in 100%). The studies were carried out on
[Al.sub.2][O.sub.3] + 30%TiC, conventionally named
[E.sub.c]C[C.sub.s]-[Al.sub.2][O.sub.3]/TiC.
2. METHODOLOGY
The fundamental principle of the massive electrode electrical
discharge machining by shape copying (EDM-[S.sub.m][C.sub.o]) is that of
the controlled erosion of the material, as result of the controlled
electrical discharges between the part and the electrode, within a
dielectric fluid environment (Opran, 1997).
A schematic model of EDM-[S.sub.m][C.sub.o] for
[E.sub.c]C[C.sub.s]-[Al.sub.2][O.sub.3]/TiC is made in Figure 1. The
microscope images of the sample part, are shown in Figure 2, before
(2.a) and after (2.b) EDM, using: [i.sub.e] is the electric current
intensity ([i.sub.e] = 3.13 A); [t.sub.i] is the impulse time ([t.sub.i]
= 6 [micro]s); [t.sub.0] is the pause time ([t.sub.0] = 190 [micro]s).
Obtaining a mathematical model of the temperature distribution
field, by considering the inter-dependences of the electrical discharge
process factors (energy distribution within part, electrode, dielectric,
plasma channel and pressure ball limits) is possible only if some
specific assumptions are made:
* the part is considered to be continuous, heterogeneous and
isotropic, as an elastic environment under thermal shock;
* the interactions of the material, dielectric and their
constituents are ignored;
* the resultant thermal flux toward the ceramic material is
considered to be a semi-infinity solid;
* the intensity of thermal flux Q(x, t) acts as a non-linear filed,
depending on time t and point's position x;
* the thermal flux radius [r.sub.t], acts like a non-linear field;
* there is a thermal influenced semi-spherical zone, within the
material, whose radius is [r.sub.t];
* the detached zone, resulting from EDM thermal shock is determined
by the position of the isotherms of temperature;
* the reference surface is always situated between two subsequent
electrical discharges, so as the isotherms for detaching of material
refers to the new resulting surface of the previously discharge;
* because of the fact that the thermal extension coefficient a
differs for the considered components, [Al.sub.2][O.sub.3] and TiC,
while electrical discharging, there do appear an oscillatory spatial
residual contractions and stress field;
* the oscillatory spatial residual contractions field determines
the micro-fractures, micro-cracking and has a role in their propagation
and in detaching of material, by fragmentation, on EDM thermal shock.
[FIGURE 1 OMITTED]
[FIGURE 2 OMITTED]
The heat distribution, within the considered granular
[Al.sub.2][O.sub.3]/TiC material, is according to Cattaneo law
(Schneider & Petzov, 1996):
[tau]dQ(x,t)/dt + Q(x,t) = -k grad([theta]-[[theta].sub.0])(x,t)
(1)
where: t is the time of a singular electrical discharge process
[[micro]s]; Q(x, t)--the thermal flux intensity variation, as function
of time and of three-dimensional vector x; k--the thermal conductivity
of material [W/mm[degrees]K]; 90[[theta].sub.0]--the initial temperature
of material, [[theta].sub.0] = 293[degrees]K; [theta]--the temperature
of material at time t [[degrees]K]; [tau]--the relaxing time, when a
stationary thermal flux is set into the material [[micro]s].
3. MATHEMATICAL MODEL OF THE TEMPERATURE DISTRIBUTION FIELD
The constitutive equations for ceramic composite
([E.sub.c]C[C.sub.s]) are the equations of a material with the
properties: granular, thermo-viscous-elastic, linear integral type,
symmetrical axial, isotropic, submitted to a thermal high tide and
having finite speeds of the heat propagate like wave inside the
material.
The simplified constitutive equations, that determine the thermal
field intensity, are the following (Opran et al., 2007):
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (2)
where: s is the time variable; 0 index is the initial state at time
[t.sub.0] (the beginning of a singular electro-erosion discharge).
According to the balance equation of the energy, resulted through
the application of the classic equation of the energy law, we obtain the
equation writed in cylindrical coordinates:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (3)
It verifies the following:
* the initial condition:
([theta] - [[theta].sub.0]) (r, z, 0) = 0 (4)
* the boundary conditions:
([theta] - [[theta].sub.0]) ([r.sub.t], 0, t) = 0 (5)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (6)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (7)
where: [v.sub.[theta]] is the thermal wave speed; Q(t)-the thermal
field in time interval [0, [t.sub.c]].
Finally, we find the following solution of the equation (3):
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]. (8)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]. (9)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (10)
If checking the above obtained model, for real experimental
conditions [k.sub.0] = 20 W/mm[degrees]K; [v.sub.[theta]] = 0.22;
[r.sub.t] = [10.sup.-5] m; [tau] = [10.sup.-14] s; [[alpha].sub.0] = 8 x
[10.sup.-6]/[degrees]K), the result is ([theta]-[[theta].sub.0])(0, 0,
[10.sup.-6]) < 3 x [10.sup.-5][[degrees]K], meaning different from
zero.
4. CONCLUSION
In practice, the electrical discharge machining represents an
efficiently procedure for the getting ceramics composites
([E.sub.c]C[C.sub.s]) parts, according to the prescribed technical
conditions.
The technical ceramics composite [Al.sub.2][O.sub.3]/TiC were
studied and the machining procedure considered was massive electrode
electrical discharge, by shape copying EDM-[S.sub.m][C.sub.o]. The
displacement of thermal field in EDM-[S.sub.m][C.sub.o] determines the
terms machining and the machining results.
The constitutive equation is specific for the answer of the
material to EDM. There was determined a mathematical model of the
temperature distribution field in EDM-[S.sub.m][C.sub.o], as function of
thermal flux radius, thermal influenced zone radius, radial direction of
machined part and time. The model has been check by using values
suitable for real conditions.
The results of the researches presented in this paper allows the
determination of the optimal machining parameters and obtaining
processed surfaces with superior quality and precision, in according of
the market requirements.
5. REFERENCES
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compozite, ceramice si minerale, Ed. Tehnica, Bucharest, Romania
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electroeroziune a unor materiale ceramice, Doctoral Thesis, University
Politehnica of Bucharest, Romania
Opran, C.; Blajina, O. & Iliescu, M. (2007). Researches on
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Romania
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Vaia, R. & Wagner, D. (2004). Framework for nanocomposites,
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