| Literature DB >> 20467562 |
Dorival Pedroso da Silva1, Claudia Cazal, Fernanda Campos Sousa de Almeida, Reinaldo Brito E Dias, Rafael Yagüe Ballester.
Abstract
The purpose of this research was to evaluate the maximum stress around osseointegrated implants and alveolar ridge, in a mandible with left partial resection through a photoelastic mandibular model. The first group consisted of two implants: traditional model (T), implants placed in the position of both canines; fulcrum model (F), implants placed in the position of left canine CL and right lateral incisor LiR. Both models linked through a bar and clips. The second group was consisted of three implants, with implants placed in the position of both canines (CR and CL) and the right lateral incisor (LiR), which composed four groups: (1) model with 3 "O" rings, (2) model 2 ERAs, bar with clips, (3) model 2 ERAs bar without clips; (4) model "O" ring bar and ERA. An axial and an oblique load of 6.8 kgf was applied on a overdenture at the 1st Pm, 2nd Pm, and 1st M. Results showed that the area around the left canine (CL) was practically free of stress; the left lateral incisor (LiL) developed only small tensions, and low stress in all the other cases; the right canine tooth suffered the largest concentrations of stress, mainly with the ERA retention mechanism.Entities:
Year: 2010 PMID: 20467562 PMCID: PMC2868185 DOI: 10.1155/2010/780670
Source DB: PubMed Journal: Int J Dent ISSN: 1687-8728
Figure 1(a) Traditional model, (b) Fulcrun model, (c) Three implants with “O” rings, (d) “O” ring in the left canine, ERA in the right canine, linked with hader bar, (e) an example of overdenture.
Averages of the relative tensions (fringes/cm number) in the apex of the implants, corresponding to the interactions, support/group system × angle of incidence of the force (n = 18), and support/group system × place of incidence of the force (n = 12).
| Support/Group | Angle of Load* | Place of Load** | ||||
|---|---|---|---|---|---|---|
| Perpendicular | Inclined | 1st Pm | 2nd Pm | 1st M | ||
| 01 | T (CaL) | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
| 02 | T (CaR) | 1.84 | 1.08 | 1.93 | 1.35 | 1.09 |
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| 03 | F (CaL) | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
| 04 | F (LiR) | 0.87 | 1.56 | 1.41 | 1.25 | 0.99 |
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| 05 | 3 “O” (CaL) | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
| 06 | 3 “O” (LiR) | 0.00 | 0.76 | 0.57 | 0.31 | 0.26 |
| 07 | 3 “O” (CaR) | 1.60 | 2.50 | 2.24 | 1.77 | 2.14 |
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| 08 | 2 ERAs + clip (CaL) | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
| 09 | 2 ERAs + clip (LiR) | 0.17 | 0.59 | 0.57 | 0.37 | 0.21 |
| 10 | 2 ERAs + clip (CaR) | 1.60 | 4.86 | 3.65 | 3.18 | 2.87 |
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| 11 | 2 ERAs no clip (CaL) | 0.00 | 0.00 | 0.00 | 0.00 | 0.00 |
| 12 | 2 ERAs no clip (LiR) | 0.10 | 0.52 | 0.37 | 0.31 | 0.26 |
| 13 | 2 ERAs no clip (CaR) | 1.98 | 4.90 | 4.01 | 3.54 | 2.76 |
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| 14 | (“O” CaL) (ERA CaR) (CaL) | 0.00 | 0.07 | 0.10 | 0.00 | 0.00 |
| 15 | (“O” CaL) (ERA CaR) (LiR) | 0.14 | 0.73 | 0.52 | 0.47 | 0.31 |
| 16 | (“O” CaL) (ERA CaR) (CaR) | 2.57 | 0.80 | 1.98 | 1.77 | 1.30 |
*Tukey (5%) = 0.859 (interaction support/group system × angle of incidence of the force). Letters for comparisons a to i, when same averages are similar.
**Tukey (5%) = 1.107 (interaction support/group system × place of incidence of the force). Letters for comparisons k to v, excluding m, when same averages are similar.
Averages of the relative tensions (fringes/cm number) in the edges of the implants, corresponding to the interactions, system apparel (implant system Type) × angle of incidence of the force (n = 03) and system apparel × place of incidence of the force (n = 02).
| Support/Group | Angle of Load* | Place of Load** | ||||
|---|---|---|---|---|---|---|
| Perpendicular | Inclined | 1st Pm | 2nd Pm | 1st M | ||
| 01 | T (Ridge) | 0.63 | 0.83 | 0.31 | 0.94 | 0.94 |
| 02 | F (Ridge) | 2.50 | 1.04 | 1.56 | 1.88 | 1.88 |
| 03 | 3 “O” (Ridge) | 1.25 | 1.25 | 0.63 | 1.25 | 1.88 |
| 04 | 2 ERAs + clip (Ridge) | 1.25 | 1.25 | 0.94 | 0.94 | 1.88 |
| 05 | 2 ERAs no clip (Ridge) | 1.25 | 1.46 | 0.94 | 1.25 | 1.88 |
| 06 | (“O” CaL) (ERA CaR) (Ridge) | 1.46 | 2.29 | 1.88 | 1.88 | 1.88 |
*Tukey (5%) = 1.205 (interaction system apparel × angle of incidence of the force). Letters for comparisons a to c, when same, averages are similar.
**Tukey (5%) = 1.604 (interaction system apparel × place of incidence of the force). Letter for comparison d, when equal, averages are similar.