Comparison of three-dimensional finite element and photoelastic results for a scroller shaft.
Rusu-Casandra, Aurelia ; Iliescu, Nicolae ; Baciu, Florin 等
1. INTRODUCTION
The scroller shafts (Fig.1) which are parts of several
technological equipments have the function to transport the material to
be processed from the supply to the injecting or cutting compartment, by
developing a certain compression force that provides the required
pressure for a constant flow rate evacuation (Mott, 2005). In order to
carry out this function, the scroller shafts are made with variable
geometry (the step is decreasing and the height of the flanks is
increasing towards the compression compartment) therefore the stress
state in the flanks is different from one coil to another and difficult
to calculate with classical analytical methods (Rusu-Casandra, 2008).
On evaluating various alternative methods of analysis, both
analytical and experimental, the three-dimensional finite element and
the three-dimensional photoelastic methods have been chosen for the
stress analysis of a scroller shaft. In order to perform a structural
optimization of the scroller shaft, it was necessary to validate the
mathematical model of calculation using the photoelasticity technique.
(Iliescu, Atanasiu, 2006; Paipetis, 1990).
2. NUMERICAL CALCULUS
A finite element study was performed using SOLIDWORKS software (***
2009). The finite element mesh (Fig.2) was generated for the model using
3D elements with four nodes (Huebner et al., 2001).
Two identical models with a Poisson's ratio value applicable
to photoelastic materials subjected to variable pressure have been
supplementary loaded one with a compression force P=30 N and the other
with a torque T=2 Nm applied on the crank of the scroller shaft.
[FIGURE 1 OMITTED]
Both the applied loads and boundary conditions used for the finite
element model were chosen to be similar to those of the photoelastic
model. The contour plots of the principal stresses difference
[[sigma].sub.1]-- [[sigma].sub.2] in the two models subjected to
compression and torsion respectively, obtained using the finite element
method, are presented in Fig. 3 and Fig. 4.
3. PHOTOELASTIC INVESTIGATION
The "frozen stress" method of the three-dimensional
photoelasticity was used next. The two models have been made of an epoxy
resin, Araldite D at 1:1 scale, by cold casting, in moulds of silicone
rubber. The material to be processed simulated by textile pieces imbued
in silicone oil was introduced into each feeder and transported in the
processing compartment using a crank. Both assemblies have been fed
until the shafts were self-locked.
[FIGURE 2 OMITTED]
[FIGURE 3 OMITTED]
[FIGURE 4 OMITTED]
The test procedure consisted of a cycle in which the two assemblies
were heated slowly to 1000 and held 30 min to reach equilibrium. Then
one of the models was compressed with a force P=30 N and the other
loaded with a torque T=2 Nm through a weight placed on the crank. With
loads maintained, the models were cooled at 20C per hour to room
temperature. The photoelastic patterns were "frozen" into
models by the above procedure. After cooling, slices with thickness of 5
mm used for analysing the models were taken, so that the middle plane of
slices included the geometric axis of the scroller shaft.
A disc made of the same material as the models, diametrical compressed, followed the same thermal cycle. The disc was used to
calibrate the material, resulting the stress photoelastic constant of
the model [f.sub.[sigma]] = 38 x [10.sup.-3] MPa / fringe.
When polarized light from a circular polariscope was passed through
the slices of the two models, fringe-patterns were obtained. Figure 5
and Fig. 6 show the isochromatic patterns photographed for the two
investigated models subjected to compression and torsion respectively.
In Fig. 7 and Fig. 8 are plotted the curves of the principal stresses
difference [[sigma].sub.1] - [[sigma].sub.2] on the boundary of the two
models, using the above isochromatic patterns.
4. CONCLUSIONS
The analysis of stresses in a scroller shaft was performed
numerically and experimentally for two cases of loading: compression and
torsion, In both cases the structure was subjected also to variable
pressure. The results obtained led to the following conclusions:
compartment is high in both models, theoretical and experimental
(Fig. 3 and Fig. 7). The values decrease on the flanks of coils two and
three towards the crank end of the shaft. On the real structure the
distribution of stresses is similar to that on the models and the
magnitude of the stresses can be readily calculated if the real
compression force is known.
[FIGURE 5 OMITTED]
[FIGURE 6 OMITTED]
b) Regarding the second case of loading, i.e. torsion, Fig. 4 and
Fig. 8 reveal that the stresses in the two models, theoretical and
experimental, have lower values, exception making the two ends of the
shaft.
c) The agreement between the calculated and the measured results is
good, very small differences may be seen.
As a general conclusion, it can be remarked that the scroller shaft
has the main function to transport the material to the processing
compartment, the maximum stresses occurring in the first coil flank and
in the cross-sections of the two ends of the shaft. This study should
find important use in scroller shaft design optimization.
[FIGURE 7 OMITTED]
[FIGURE 8 OMITTED]
5. REFERENCES
Huebner, K.; Dewhirst, D.; Smith, D.& Byrom, T. (2001). The
Finite Element Method for Engineers, Wiley-Interscience, ISBN 978-0471370789, Canada
Iliescu, N.; Atanasiu, C. (2006). Metode tensometrice in inginerie
(Stress Analysis Techniques in Engineering), Editura AGIR, ISBN
973-720-078-0, Bucuresti
Mott, R. (2005). Machine Elements in Mechanical Design, Pearson
Prentice Hall, ISBN 0130618853, United Kingdom
Paipetis, S. (1990). Photoelasticity in Engineering Practice,
Routledge, ISBN 978-0853343639, United Kingdom
Rusu-Casandra, A. (2008). Elasticity in Engineering, Editura AGIR,
ISBN 978-973-720-188-1, Bucuresti
*** (2009) Solidworks User Manual, Dassault Systemes SolidWorks
Corp, Concord, MA, USA