| Literature DB >> 35769992 |
Jia-Qing Wang1,2,3, Yuan Zhang1,4, Min Pang1,4, Yue-Qiu Wang1,4, Jun Yuan1,4, Hui Peng1,4, Wen Zhang1,4, Lu Dai1,4, Hong-Wei Li1,2.
Abstract
Taper implants differ greatly from anatomical teeth in shape. In this study, seven three-dimensional finite element models were established, including a conventional taper implant and six root-analog implants with different root numbers and shapes. Vertical, horizontal, and oblique instantaneous loads of 100 N were applied to the models to obtain stress distribution in the implant, mucosa, cortical bone, and cancellous bone. ANSYS was used to perform the analysis under hypothetical experimental conditions. We find the stresses in all the implants and surrounding tissues varied by loading direction, the sequence of stress magnitude is vertical load, oblique load, and then horizontal load. The maximum stress values in root-analog implants were significantly less than in the taper implant. Moreover, stress distribution in the former was equalized contrary to the concentrated stress in the latter. Root-analog implants with different root geometry also revealed a pattern: stresses in multiple-root implant models were lower than those in single-root implants under the same load. The implant with a long and rounded root distributed the stress more uniformly, and it was mainly concentrated on the implant itself and cancellous bone. However, the opposite effect was observed in the short implant on mucosa and cortical bone. The root geometry of anatomical teeth can modify their functions. A uniform-shaped implant can hardly meet their functional requirements. Thus, the root-analog implant could be a possible solution.Entities:
Keywords: biomechanics; finite element analysis; root-analog implant; stress; tapered implant
Year: 2022 PMID: 35769992 PMCID: PMC9234945 DOI: 10.3389/fgene.2022.915679
Source DB: PubMed Journal: Front Genet ISSN: 1664-8021 Impact factor: 4.772
FIGURE 1FEA models of RAIs and surrounding tissues.
Elastic modulus and Poisson ratio of different materials.
| Material | Elastic modulus (GPa) | Poisson ratio (μ) |
|---|---|---|
| Cortical bone | 13.7 | 0.30 |
| Cancellous bone | 1.85 | 0.30 |
| Mucosa | 0.003 | 0.45 |
| Titanium | 110 | 0.35 |
Maximum stress values when RAIs and tapered implant are subjected to 100-N vertical load.
| Dental implant models | Implant (MPa) | Mucous membrane (MPa) | Cancellous bone (MPa) | Cortical bone (MPa) |
|---|---|---|---|---|
| 26 | 5.4983 | 0.0019240 | 2.0921 | 4.2940 |
| 46 | 6.1727 | 0.0021796 | 1.6009 | 4.9725 |
| 34 | 14.5890 | 0.0053000 | 3.5547 | 12.7400 |
| 13 | 12.7000 | 0.0041022 | 2.3722 | 6.6353 |
| 12 | 17.2340 | 0.0030784 | 3.6631 | 10.702 |
| 11 | 13.2870 | 0.0030641 | 2.0395 | 9.3141 |
| Tapered implant | 67.4090 | 0.0059824 | 6.6965 | 6.1804 |
Maximum stress values when RAIs and tapered implant are subjected to 100-N oblique load.
| Dental implant models | Implant (MPa) | Mucous membrane (MPa) | Cancellous bone (MPa) | Cortical bone (MPa) |
|---|---|---|---|---|
| 26 | 20.3480 | 0.0074868 | 3.5900 | 16.5680 |
| 46 | 22.3470 | 0.0077840 | 2.8923 | 19.6660 |
| 34 | 42.8330 | 0.0151570 | 5.8313 | 37.8790 |
| 13 | 9.8724 | 0.0065159 | 3.8088 | 12.1410 |
| 12 | 31.7050 | 0.0078445 | 7.7121 | 30.190 |
| 11 | 12.0520 | 0.0034788 | 2.9090 | 12.1230 |
| Tapered implant | 341.0300 | 0.0496360 | 19.9350 | 37.8830 |
FIGURE 2Stress distribution of 26 under 100-N load.
FIGURE 8Stress distribution of the tapered implant under 100-N load.
FIGURE 3Stress distribution of 46 under 100-N load.
FIGURE 4Stress distribution of 34 under 100-N load.
FIGURE 5Stress distribution of 13 under 100-N load.
FIGURE 7Stress distribution of 11 under 100-N load.
Maximum stress values when RAIs and tapered implant are subjected to 100-N horizontal load.
| Dental implant models | Implant (MPa) | Mucous membrane (MPa) | Cancellous bone (MPa) | Cortical bone (MPa) |
|---|---|---|---|---|
| 26 | 14.5640 | 0.0049187 | 2.7979 | 11.2400 |
| 46 | 27.8630 | 0.0092178 | 2.6464 | 22.9080 |
| 34 | 53.4920 | 0.0185430 | 6.5350 | 46.7240 |
| 13 | 16.9160 | 0.0096245 | 5.1270 | 17.9760 |
| 12 | 49.5080 | 0.0154300 | 14.7280 | 43.431 |
| 11 | 21.6190 | 0.0082758 | 2.6395 | 29.1180 |
| Tapered implant | 578.9900 | 0.0912870 | 32.0940 | 64.8470 |