Fracture strength evaluation of complete denture based on FEM analysis and fracture mechanics concepts.
Cernescu, Anghel ; Faur, Nicolae ; Bortun, Cristina 等
1. INTRODUCTION
Total dentures are generally for old persons, for rebalancing dental-jaw bone device, in cases patients no longer have any
dento-parodonthal units. Total dentures are made of acrylic resins and
artificial teeth. Resins composite consist of three primary ingredients:
an organic resin matrix, inorganic filler particles and a coupling agent
(Craig R.G. et al., 2002). Processing technology of these materials
sometimes lead to obtain total dentures with small defects which can
initiate cracks and resulting in failure of total denture before the
expected lifetime (Beyli M.S. et al., 1981).
Following an inspection of a denture made of acrylic resin Eclipse,
were observed some pore and cracks, Fig. 1. For fracture strength
evaluation of total denture was used finite element analysis and was
calculated the stress intensity factors for two located cracks and were
compared with fracture toughness of the material.
The fracture toughness, [K.sub.IC], is a material property that
characterizes the resistance of a material to fracture in the presence
of a crack and is used to estimate the relation between failure stress
and defect size for a material in service.
[FIGURE 1 OMITTED]
2. MATERIAL AND METHOD
For this analysis was used a geometric model of the total denture
obtained by 3D scanning with Roland 3D scanner, model LPX-1200, Fig. 2.
The point cloud resulted from scanning process was imported in
PixformPro software and has been transformed by reverse
engineering" technique into a network surfaces. These surfaces were
exported as igs file and open in SolidWorks CAD software as solid model
(Y.Y. Cheng et al., 2010), (Yuchun S. et al., 2009)
[FIGURE 2 OMITTED]
This model was imported into finite element software--ABAQUS/CAE
V6.6 and was evaluated the state of stress and the stress intensity
factors, [K.sub.1], for two cracks (Darbar U.R. et al., 1995), (Rees
J.S. et al., 1990).
The Eclipse resins have a linear elastic behaviour with following
mechanical properties (Narva K.K. et al., 2005), (Ward I.M., 1990):
--Young's modulus: E = 2908.45 MPa
--The Ultimate Tensile Strength: [[sigma].sub.u] = 59.49 MPa
--Fracture toughness: [K.sub.IC] = 24.93 MPaVmm
For numerical analysis the model was meshed with a total of 117632
quadratic elements and the boundary conditions consist of three supports
with displacements imposed by 0.1 and 0.2 mm as in Figure 3 and the
surface normal pressure of 0.2 MPa applied uniformly distributed on the
contact surfaces of teeth with conjugated denture, Fig. 4.
[FIGURE 3 OMITTED]
[FIGURE 4 OMITTED]
In Figure 5 is given the distribution of maximum principal stress
showing areas of maximum loading. Based on this distribution, in the
second part of this analysis we considered two cracks for which we
calculated the stress intensity factors, Fig. 6 and 7.
[FIGURE 5 OMITTED]
[FIGURE 6 OMITTED]
[FIGURE 7 OMITTED]
The two cracks considered for analysis were located in the most
loaded areas of the denture. FEM analysis on a 3D model enables an
evaluation of the triaxial state of stress and also allows calculation
of the stress intensity factors for the two cracks corresponding to
fracture mode I and II ([K.sub.1] and [K.sub.2]).
3. RESULTS AND CONCLUSIONS
The results of this analysis are listed in table 1.
This study allows evaluating the fracture strength of dentures in
presence of cracks or defects. The FEM analysis was performed by
calculating the linear-elastic Fracture Mechanics parameters,
represented by stress intensity factors and comparing them with fracture
toughness of the material.
While they are in a loaded area, at a crack1 tip is a predominant
compression stress state which cause a non-extension of crack1. Through
its position, the crack2 have an extension from the initial value of
1.92 mm to 5.32 mm final value, after entering into a compression zone
where is stopped.
4. ACKNOWLEDGEMENTS
This study was supported by the project PERFORM ERA ID57649,
CONTRACT POSDRU/89/1.5/S/57649.
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Tab. 1. The values of crack lengts and stress intensity factors
for considered cracks
Fracture
Initial Final toughness,
length length [K.sub.IC]
Cracks [mm] [mm] SIF [MPaVmm] [MPaVmm]
Crack1 1.12 1.12 [K.sub.1] = -22.6 24.93
[K.sub.2] = 8.9
Crack2 1.96 5.32 [K.sub.1] = -2.33
[K.sub.2] = -3.12