| Literature DB >> 28959748 |
Zarei I1, Khajehpour S1, Sabouri A2, Haghnegahdar Az3, Jafari K4.
Abstract
STATEMENT OF PROBLEM: Impacts and accidents are considered as the main fac- tors in losing the teeth, so the analysis and design of the implants that they can be more resistant against impacts is very important. One of the important nu- merical methods having widespread application in various fields of engineering sciences is the finite element method. Among its wide applications, the study of distribution of power in complex structures can be noted.Entities:
Keywords: Finite Element; Cortical Bone; Dental Implant ; Stress; Thread
Year: 2016 PMID: 28959748 PMCID: PMC5608057
Source DB: PubMed Journal: J Dent Biomater ISSN: 2383-3971
Figure1The three-dimensional view of the bone by the Mimics 10.01 software
Figure2The implants designed in Solid works software
Figure3The placement of the implants and abatement in the bone
The mechanical properties of the materials used in the study
| Material | Elastic Moduls (GPa) | Possion Ratio(V) | Density (g/cm-3) |
|---|---|---|---|
| Titanium | 110 | 0.35 | 4.5 |
| Cortical Bone | 1.34 | 0.30 | 0.71 |
| Trabecular Bone | 0.15 | 0.30 | 1.86 |
Figure4Imposing the bending loading towards the implant
Figure5Imposing the axial loading towards the implant
The maximum amounts of stress imposed on various layers of the bone and implant in the axial loading (MPa)
| Cortical Bone | Trabecular Bone | Implant Titanium | |
|---|---|---|---|
| First group: Straight | 2.4 | 4.3 | 82.1 |
| Second group: Tapered | 0.8 | 8.7 | 187.4 |
| Third group: Tapered II | 0.8 | 6.7 | 85.3 |
Figure6The distribution pattern and place of maximum stress on the trabecular bone layer in the first group
Figure7The distribution pattern and place of maximum stress on the trabecular bone in the second group
Figure8Comparison of behavior in various models of thread regarding the stress distribution on the trabecular bone in the axial loading
The maximum stress on different layers of the bone and implant under the bending loading
| Cortical Bone | Trabecular Bone | Implant Titanium | |
|---|---|---|---|
| First group: Straight | 1.6 | 5.2 | 75.9 |
| Second group: Tapered | 0.7 | 7.4 | 126.9 |
| Third group: Tapered II | 1.1 | 5.1 | 53.8 |
Figure9The stress distribution pattern on the cortical bone in the bending loading
Figure10The comparison of stress distribution on the cortical bone in bending loading for various thread design