| Literature DB >> 32092128 |
Georgi Talmazov1, Nathan Veilleux2, Aous Abdulmajeed1, Sompop Bencharit1,2,3.
Abstract
This study evaluated the von Mises stress (MPa) and equivalent strain occurring around monolithic yttria-zirconia (Zir) implant using three clinically simulated finite element analysis (FEA) models for a missing maxillary central incisor. Two unidentified patients' cone-beam computed tomography (CBCT) datasets with and without right maxillary central incisor were used to create the FEA models. Three different FEA models were made with bone structures that represent a healed socket (HS), reduced bone width edentulous site (RB), and immediate extraction socket with graft (EG). A one-piece abutment-implant fixture mimicking Straumann Standard Plus tissue level RN 4.1 X 11.8mm, for titanium alloy (Ti) and Zir were modeled. 178 N oblique load and 200 N vertical load were used to simulate occlusal loading. Von Mises stress and equivalent strain values for around each implant model were measured. Within the HS and RB models the labial-cervical region in the cortical bone exhibited highest stress, with Zir having statistically significant lower stress-strain means than Ti in both labial and palatal aspects. For the EG model the labial-cervical area had no statistically significant difference between Ti and Zir; however, Zir performed better than Ti against the graft. FEA models suggest that Ti, a more elastic material than Zir, contributes to the transduction of more overall forces to the socket compared to Zir. Thus, compared to Ti implants, Zir implants may be less prone to peri-implant bone overloading and subsequent bone loss in high stress areas especially in the labial-cervical region of the cortical bone. Zir implants respond to occlusal loading differently than Ti implants. Zir implants may be more favorable in non-grafted edentulous or immediate extraction with grafting.Entities:
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Year: 2020 PMID: 32092128 PMCID: PMC7039452 DOI: 10.1371/journal.pone.0229360
Source DB: PubMed Journal: PLoS One ISSN: 1932-6203 Impact factor: 3.240
Fig 1FEA modeling workflow.
Fig 2FEA model, loading protocols, measurement sites, and implant design.
List of materials used in this finite element analysis, their properties and numeric values used for the simulation*.
| Y-TZP | Ti-6Al-4V | Cortical Bone | Trabecular Bone | Morselized Cancellous Bone53 | |
|---|---|---|---|---|---|
| Elastic Modulus (MPa) | 22000052 | 104800.317 | 170004 | 20009 | 10053 |
| Poisson's Ratio | 0.3152 | 0.317 | 0.426 | 0.410 | 0.253 |
| Mass Density (kg/m^3) | 600052 | 4428.787 | 19008 | 2702 | 3401 |
| Tensile Strength (MPa) | 74552 | 10507 | 524 | ||
| Compressive Strength (MPa) | 220052 | 848–10805 | 1304 | 1043 | |
| Yield Strength (MPa) | 30052 | 827.370887 | 496 | 4.83 | 501 |
*The empty cells indicate missing values that were not found in the literature and were not required for the FEA to compute. When available, the values were used to improve the accuracy of the model.
Fig 3FEA model and loading.
(A) HS Model Stress and Strain Distributions, (B) RB Model Stress and Strain Distributions, and (C) EG Model Stress and Strain Distributions.
Stresses and strains computed from three FEA models at 178 N oblique loading.
| HS MODEL | |||||||||
|---|---|---|---|---|---|---|---|---|---|
| Stress (MPa) | Strain | ||||||||
| Ti-6Al-4V | Y-TZP | P-value | Ti-6Al-4V | Y-TZP | P-value | ||||
| Labial | Implant (S4) | 39.18±9.84 | 43.18±8.13 | 0.0004 | Labial | Implant (S4) | 3.51E-04±2.59E-05 | 1.80E-04±6.55E-06 | 4E-10 |
| Cortical (S4) | 13.3±5.91 | 10.4±3.82 | 0.002 | Cortical (S4) | 7.87E-04±1.53E-04 | 6.09E-04±8.40E-05 | 2E-05 | ||
| Trabecular (S2) | 3.90±1.02 | 4.05±1.16 | 0.01 | Trabecular (S2) | 1.39E-03±5.01E-04 | 1.43E-03±5.40E-04 | 0.01 | ||
| Palatal | Implant (S3) | 22.1±7.36 | 25.58±7.33 | 2E-05 | Palatal | Implant (S3) | 1.94E-04±1.73E-05 | 1.06E-04±4.63E-06 | 3E-09 |
| Cortical (S3) | 6.15±4.51 | 4.28±2.47 | 0.009 | Cortical (S3) | 3.31E-04±1.05E-04 | 2.36E-04±5.49E-05 | 0.0001 | ||
| Trabecular (S1) | 0.22±0.0638 | 0.19±0.0809 | 0.2 | Trabecular (S1) | 1.18E-04±3.38E-05 | 1.12E-04±9.81E-06 | 0.3 | ||
| RB MODEL | |||||||||
| Stress (MPa) | Strain | ||||||||
| Ti-6Al-4V | Y-TZP | P-value | Ti-6Al-4V | Y-TZP | P-value | ||||
| Labial | Implant (S4) | 45.93±9.21 | 47.2±10.3 | 0.08 | Labial | Implant (S4) | 3.89E-04±2.46E-05 | 1.89E-04±1.22E-05 | 1E-12 |
| Cortical (S4) | 48.6±18.8 | 45.9±20.7 | 0.04 | Cortical (S4) | 1.71E-03±6.51E-04 | 1.46E-03±9.04E-04 | 0.008 | ||
| Trabecular (S2) | 0.311±0.225 | 0.227±0.13 | 0.01 | Trabecular (S2) | 1.77E-04±9.77E-05 | 1.30E-04±5.61E-05 | 0.003 | ||
| Palatal | Implant (S3) | 20.51±10.6 | 22.689±10.4 | 0.0003 | Palatal | Implant (S3) | 1.92E-04±3.86E-05 | 9.97E-05±1.63E-05 | 2E-07 |
| Cortical (S3) | 10.24±7.21 | 9.11±5.22 | 0.07 | Cortical (S3) | 6.86E-04±2.57E-04 | 5.98E-04±1.75E-04 | 0.004 | ||
| Trabecular (S1) | 0.38±0.129 | 0.36±0.134 | 0.01 | Trabecular (S1) | 1.50E-04±4.92E-05 | 1.65E-04±4.72E-05 | 0.0002 | ||
| EG MODEL | |||||||||
| Stress (MPa) | Strain | ||||||||
| Ti-6Al-4V | Y-TZP | P-value | Ti-6Al-4V | Y-TZP | P-value | ||||
| Labial | Implant (S2) | 55.41±4.56 | 57.34±5.20 | 8E-06 | Labial | Implant (S2) | 4.75E-04±2.51E-05 | 2.36E-04±1.27E-05 | 2E-13 |
| Cortical (S3) | 3.44±0.544 | 3.17±0.997 | 0.1 | Cortical (S3) | 1.44E-04±2.06E-05 | 1.31E-04±4.36E-05 | 0.09 | ||
| Graft (S2) | 0.566±0.124 | 0.429±0.0844 | 1E-06 | Graft (S2) | 4.44E-03±7.55E-04 | 3.36E-03±5.10E-04 | 1E-07 | ||
| Palatal | Implant (S1) | 40.46±1.95 | 42.18±4.13 | 0.04 | Palatal | Implant (S1) | 3.24E-04±8.39E-06 | 1.68E-04±8.17E-06 | 7E-19 |
| Cortical (S1) | 11.5±5.65 | 6.83±2.87 | 0.0002 | Cortical (S1) | 5.24E-04±3.11E-05 | 3.18E-04±2.80E-05 | 8E-17 | ||
Stresses and strains computed from three FEA models at 200 N loading along implant axis.
| HS MODEL | |||||||||
| Stress (MPa) | Strain | ||||||||
| Ti-6Al-4V | Y-TZP | P-value | Ti-6Al-4V | Y-TZP | P-value | ||||
| Labial | Implant (S4) | 17.88±2.52 | 18.81±2.96 | 0.03 | Labial | Implant (S4) | 1.41E-04±9.37E-06 | 6.89E-05±5.71E-06 | 4E-12 |
| Cortical (S4) | 9.48±2.53 | 8.26±2.15 | 0.0003 | Cortical (S4) | 5.12E-04±5.31E-05 | 4.50E-04±4.32E-05 | 5E-06 | ||
| Trabecular (S2) | 4.32±0.966 | 4.12±1.05 | 0.002 | Trabecular (S2) | 1.54E-03±5.52E-04 | 1.47E-03±5.52E-04 | 4E-05 | ||
| Palatal | Implant (S3) | 12.0±3.5 | 12.7±3.5 | 0.006 | Palatal | Implant (S3) | 1.03E-04±6.54E-06 | 5.11E-05±2.71E-06 | 2E-11 |
| Cortical (S3) | 8.44±3.77 | 7.76±2.94 | 0.04 | Cortical (S3) | 4.48E-04±6.88E-05 | 4.15E-04±5.20E-05 | 0.0001 | ||
| Trabecular (S1) | 0.85±0.502 | 0.78±0.572 | 0.02 | Trabecular (S1) | 5.12E-04±6.46E-05 | 4.88E-04±9.00E-05 | 0.01 | ||
| RB MODEL | |||||||||
| Stress (MPa) | Strain | ||||||||
| Ti-6Al-4V | Y-TZP | P-value | Ti-6Al-4V | Y-TZP | P-value | ||||
| Labial | Implant (S4) | 23.15±9.90 | 23.11±10.62 | 0.5 | Labial | Implant (S4) | 2.24E-04±4.25E-05 | 1.05E-04±2.11E-05 | 1E-08 |
| Cortical (S4) | 39.9±16.5 | 37.7±17.6 | 0.04 | Cortical (S4) | 1.30E-03±5.28E-04 | 1.13E-03±7.10E-04 | 0.01 | ||
| Trabecular (S2) | 0.394±0.208 | 0.273±0.11 | 0.004 | Trabecular (S2) | 2.17E-04±9.33E-05 | 1.42E-04±3.78E-05 | 0.001 | ||
| Palatal | Implant (S3) | 12.02±3.23 | 12.82±3.68 | 0.01 | Palatal | Implant (S3) | 1.02E-04±6.02E-06 | 5.15E-05±4.00E-06 | 1E-13 |
| Cortical (S3) | 8.22±2.79 | 7.50±2.27 | 0.004 | Cortical (S3) | 4.57E-04±9.74E-05 | 4.18E-04±7.65E-05 | 0.0001 | ||
| Trabecular (S1) | 0.78±0.271 | 0.73±0.283 | 0.002 | Trabecular (S1) | 4.13E-04±8.60E-05 | 3.86E-04±8.65E-05 | 0.00004 | ||
| EG MODEL | |||||||||
| Stress (MPa) | Strain | ||||||||
| Ti-6Al-4V | Y-TZP | P-value | Ti-6Al-4V | Y-TZP | P-value | ||||
| Labial | Implant (S2) | 18.31±1.09 | 18.13±1.02 | 8E-05 | Labial | Implant (S2) | 1.54E-04±6.95E-06 | 7.27E-05±3.19E-06 | 7E-14 |
| Cortical (S3) | 0.639±0.196 | 0.609±0.264 | 0.2 | Cortical (S3) | 2.69E-05±8.52E-06 | 2.56E-05±1.17E-05 | 0.2 | ||
| Graft (S2) | 0.148±0.0318 | 0.105±0.0209 | 3E-07 | Graft (S2) | 1.16E-03±1.96E-04 | 8.26E-04±1.29E-04 | 4E-08 | ||
| Palatal | Implant (S1) | 15.80±1.84 | 16.24±1.16 | 0.07 | Palatal | Implant (S1) | 1.36E-04±1.14E-05 | 6.51E-05±3.18E-06 | 3E-10 |
| Cortical (S1) | 3.82±3.22 | 2.13±1.92 | 0.001 | Cortical (S1) | 1.50E-04±7.34E-06 | 8.17E-05±5.53E-06 | 9E-15 | ||
Fig 4Model loading at 178 N oblique for HS (4A), RB (4B), and EG (4C); at 200 N vertical for HS (4D), RB (4E), and EG (4F); and the summary of the two loading protocols (4G) and (4H).