Comparison of differently shaped testing specimens for simulation of thermomechanical cycles.
Behulova, Maria
1. INTRODUCTION
In the field of production and treatment of materials for
automotive industry, the great attention is paid to relatively cheap low
alloyed steels (Stankova et al, 2005, Masek et al, 2006). A special
combination of microstructural, mechanical and utility material
properties of these steels can be achieved by proper alloying and
following suitable heat or thermomechanical treatment.
Newly designed processes of thermomechanical treatment (TMT) are
tested using laboratory simulators. In this paper, five testing
specimens for simulator of thermomechanical cycles with different shapes
are analysed using FEM simulation to evaluate and compare the homogenity
of temperature fields in their active parts and stability by applied
clamping force.
2. EXPERIMENTAL MEASUREMENT
Laboratory simulator of TMT SMITWELD with module TTU 2002 installed
at the TU Chemnitz (Fig. 1a) is designated for experimental
investigation of material behavior during TMT with the maximum
deformation rate of 2 mm. [s.sup.-1] and clamping force of 20 kN.
The specimen with the length of 81 mm and active cylindrical part
with the diameter of 6 mm and the high of 11 mm is at this time used for
experimental measurements (Fig. 1b). Before experiment, the Ni-CrNi
thermocouple is welded on the surface in the central part of active
cylindrical zone for very accurate temperature measurement (Fig. 1c).
The surface in the active zone is covered by a protective antioxidant coating. Testing sample is then screwed in jaws of simulator and
subjected to TMT. Specimen heating is realised by direct electrical
heating, cooling can be assured by air, nitrogen or water. Process of
TMT is controlled by computer using prescribed thermal, deformation and
loading regimes.
[FIGURE 1 OMITTED]
3. SIMULATION MODEL
Five specimens with different shapes (Fig. 2) were analysed using
the finite element code ANSYS 10.0. The length of all specimens is 81
mm. The active part of specimens has cylindrical shape with the diameter
of 6 mm and the length of 11 mm. The middle carrying part of the
specimen 1 (Fig. 2a) is comprised of conical and cylindrical parts
finished by a notch. The specimen 2 (Fig. 2b) has extended middle part
with the successive change in diameter from the active to the clamping
part. The middle part of the specimen 3 (Fig. 2c) is cylindrical with
the diameter larger then in the active part. The specimen 4 (Fig. 2d) is
equipped in the middle cylindrical part by five notches and the specimen
5 (Fig. 2e) by five threads.
For the analysis of temperature fields in specimens during direct
electrical heating as well as stability analysis, simulation models were
prepared including development of geometrical model, FEM model,
definition of nonlinear material properties, initial conditions,
boundary conditions and loading for electric, thermal and static
problems.
Analysis of electric fields was based on the solution of Laplace
equation in the form (Novak, 2001)
div([sigma] gradV) = 0 (1)
where [sigma] is electric conductivity and V electric potential.
Transient temperature field in solids can be described by
Fourier-Kirchhoff partial differential equation (Incropera & DeWitt,
1996)
c[rho] [partial derivative]T/[partial derivative]t =
div([lambda]gradT) + [q.sub.v], (2)
in which [rho] is the density, c--the specific heat capacity,
[lambda]--thermal conductivity and [q.sub.v]--volume density of internal
heat sources, i. e. the heat generated in unit volume per second. By
resistance heating this term corresponds to the Joule heat computed by
electric analysis.
[FIGURE 2 OMITTED]
Nonlinear buckling analysis with gradually increasing loads was
applied to find the load level at which a specimen became unstable
(Ansys, 2005).
Specimens with suggested shapes were numerically tested for the
steels with the chemical composition of
0.1C-0.25Si-1.25Mn-0.3Ni-0.01N-0.03Al [wt. %]. Electric, thermal and
mechanical properties were supposed to be temperature dependent.
Specimens with the initial temperature of 20[degrees]C were loaded by
the time variable voltage during heating period of 60 s. During the
first 10 seconds, the voltage was 0.5 V with its following decrease to
the value 0.47 V. Specimen cooling by mechanisms of free convection and
radiation to the air with the temperature of 20[degrees]C was
considered. For buckling analysis, specimens were constrained on the
bottom surface and loaded by buckling axis force on the top surface.
Developed simulation model and solution procedure were verified using
experimental measurements at TU Chemnitz (Behulova et al, 2006).
4. RESULTS
During direct electric heating, specimens are heated due to the
Joule heat generated in specimens by passing of electric current. For
illustration, the distribution of current density j and internal heat
sources (Joule heat) [q.sub.v] in the specimen 1 at the end of heating
in the time of 60 second is shown in Fig. 3. Maximal values of current
density and Joule heat were computed for the specimen 4.
Fig. 4 illustrates temperature fields in analysed specimens and
their active zones in the time of 60 seconds. Temperatures in the
clamping parts of specimens are approximately the same for all specimens
attaining the values from 20[degrees]C to 200[degrees]C. Maximal
temperature at the end of heating of 1105[degrees]C was reached in the
specimen 1. Maximal temperatures of specimens 3, 4 and 5 are lower than
maximal temperatures reached by heating of specimens 1 and 2 but the
temperature differences in the active cylindrical parts are considerably
lower. The most homogeneous temperature field in active part is in the
specimen 4 with five notches in middle part.
[FIGURE 3 OMITTED]
[FIGURE 4 OMITTED]
[FIGURE 5 OMITTED]
This result can be confirmed also by the temperature distribution
along the rotation axis of specimen active parts at the end of heating
(Fig. 5). Maximal temperature differences approximately 330[degrees]C
were computed for the specimen 1. In term of homogenity of temperature
distribution, the specimen 4 seems to be the most favorable.
On the other hand, the results of buckling analysis (Table 1)
revealed that this specimen can be loaded during experimental TMT only
by smaller clamping force. The real behavior of the specimen 4 under
higher deformation loading can be seen from figure in the Table 1.
5. CONCLUSIONS
Based on the numerical analysis of temperature fields by direct
electric heating, the specimen 4 can be recommended for TMT testing of
steels using the laboratory simulator of thermomechanical cycles.
However, according results of buckling analysis, the specimen 4 can be
loaded by smaller clamping force that currently used specimen 1.
6. REFERENCES
Ansys Theoretical Manual, Release 10.0, SAS IP, Inc., (2005).
Behulova, M., Stankova, H. & Masek, B. (2006). Analysis of
temperature distribution in samples by direct electrical heating.
Materials Science and Technology [online]. Vol. 7, No. 1. ISSN 1335-9053.
Incropera, F., P. &DeWitt, D. P. (1996). Fundamentals of Heat
and Mass Transfer. New York, J. Wiley&Sons, ISBN 0-471-30460-3.
Masek, B.; Stankova, H.; Novy, Z. & Meyer, L. W. (2005).
Development of new incremental forming strategies for low-alloyed TRIP
steels, 8th Int. Conference on Technology of Plasticity, Verona, ISBN
88-87331-74-X
Novak, P. (2001). Zdklady elektrotepelnej techniky. (Fundamentals
of electrothermal Technique). Kosice, Mercury-Smekal, 2001.
Stankova, H.; Masek, B. & Meyer, L. W. (2006). The Influence of
the Incremental Deformation Intensity on the Microstructure Development,
7th Int. Conference on Production Engineering and Design for
Development, PEDD 7, ISBN 12-7340-49-8, 2006, Cairo, Egypt.
7. ACKNOWLEDGEMENT
The research has been supported by the project VEGA MS and SAV of
the Slovak Republic No. 1/0837/08 and DAAD A/07/01388.
Tab. 1. Computed buckling forces for
analysed specimens.
Specimen Buckling
force [kN]
1 20.1
2 16.3
3 15.9
4 8.4
5 9.8