| Literature DB >> 21991454 |
Lokanath Garhnayak1, Hari Parkash, D K Sehgal, Veena Jain, Mirna Garhnayak.
Abstract
Purpose. To analyze the stress distribution in an endodontically treated maxillary central incisor restored with various post-core systems and assess the benefit of ferrule using finite element analysis. Material and Methods. Twelve models with metal ceramic crown were created based on the combination of three types of post-core systems (titanium post-composite resin core, nickel-chromium post-core, and fiber reinforced composite resin post-composite resin core), two varieties of posts (tapered, parallel), and with or without ferrule. 100 N load was applied in three directions and the von Mises stress was compared. Results. Ferrule made no difference in stress distribution for the titanium and nickel-chromium posts, though it showed some stress reduction in fiber-reinforced composite resin posts. Nickel-chromium cast post-core transmitted the least amount of stresses to the dentin despite producing the maximum stress. Conclusion. Incorporation of ferrule offered some degree of stress reduction in nonmetal post, and it increased the stresses within cervical dentin.Entities:
Year: 2011 PMID: 21991454 PMCID: PMC3168916 DOI: 10.5402/2011/102329
Source DB: PubMed Journal: ISRN Dent ISSN: 2090-4371
Dimensions of structures in FE model [6, 14–17].
| No. | Different parts in FE model | Dimensions (mm) |
|---|---|---|
| (1) | Tooth [ | |
| (a) Root length | 13.0 mm | |
| (b) Root diameter | 6.0 mm (cervical) | |
| (2) | Periodontal ligament [ | 0.2 mm (width) |
| (3) | Cortical bone [ | 1.2 mm (thickness) |
| (4) | Gutta Percha [ | 4.5 mm (length) |
| (5) | Endodontic post [ | |
| Length | 10.5 mm | |
| Diameter | 1.5 mm (parallel post) | |
| 0.6–1.5 mm (tapered post) | ||
| 10.5 mm (height) | ||
| (6) | Crown [ | 1.2 mm (thickness at cervical margin) |
| 2.0 mm (thickness at incisal edge) | ||
| (7) | Core [ | 6.5 mm (height) + 2 mm residual dentin |
| (8) | Ferrule design [ | 1.5 mm (length) |
Figure 1Geometry of finite element (FE) model.
Figure 2Mesh generated over ferrule model.
Figure 3Mesh generated over nonferrule model.
Material properties in FE model [5, 18–23].
| No. | Material | Modulus of elasticity (“ | Poisson's ratio (“ |
|---|---|---|---|
| (1) | Dentin [ | 18.6 | 0.31 |
| (2) | Periodontal ligament [ | 0.0000689 | 0.45 |
| (3) | Cortical bone [ | 13.7 | 0.30 |
| (4) | Gutta Percha [ | 0.069 | 0.45 |
| (5) | Titanium [ | 120.0 | 0.30 |
| (6) | Ni-Cr alloy [ | 203.6 | 0.30 |
| (7) | Fiber reinforced composite resin [ | 15.0 | 0.28 |
| (8) | Composite resin [ | 8.3 | 0.28 |
| (9) | Porcelain [ | 69.0 | 0.28 |
Comparison of stress* distribution between tapered and parallel posts of different materials with vertical load.
| Materials | Region† | Tapered post | Parallel post | ||
|---|---|---|---|---|---|
| Ferrule | Nonferrule | Ferrule | Nonferrule | ||
| Ti | A | 2.094 | 2.091 | 2.094 | 2.091 |
| B | 2.791 | 2.788 | 2.791 | 2.788 | |
| C | 3.489 | 3.485 | 2.791 | 2.788 | |
|
| |||||
| Ni-Cr | A | 4.470 | 4.470 | 3.832 | 4.470 |
| B | 4.470 | 4.470 | 3.832 | 3.832 | |
| C | 4.470 | 4.470 | 3.193 | 3.832 | |
|
| |||||
| RC | A | 0.7024 | 0.7014 | 0.7024 | 0.7016 |
| B | 0.7024 | 0.7014 | 0.7024 | 0.7016 | |
| C | 0.7024 | 0.7014 | 0.7024 | 0.7016 | |
*Maximum Von Mises stress in MPa.
A—cervical one-third; B—middle one-third; C—apical one-third.
Comparison of stress* distribution between tapered and parallel posts of different materials with oblique load.
| Materials | Region† | Tapered post | Parallel post | ||
|---|---|---|---|---|---|
| Ferrule | Nonferrule | Ferrule | Nonferrule | ||
| Ti | A | 5.807 | 6.403 | 5.795 | 6.384 |
| B | 7.258 | 8.537 | 7.243 | 8.512 | |
| C | 8.710 | 8.537 | 7.243 | 8.512 | |
|
| |||||
| Ni-Cr | A | 10.24 | 10.24 | 10.76 | 10.94 |
| B | 11.38 | 11.38 | 11.95 | 12.16 | |
| C | 10.24 | 10.24 | 10.76 | 10.94 | |
|
| |||||
| FRC | A | 4.195 | 4.136 | 4.189 | 4.133 |
| B | 2.797 | 3.102 | 2.793 | 3.100 | |
| C | 6.992 | 7.236 | 6.981 | 8.265 | |
*Maximum Von Mises stress in MPa.
A—cervical one-third; B—middle one-third; C—apical one-third.
Comparison of stress* distribution between tapered and parallel posts of different materials with horizontal load.
| Materials | Region† | Tapered post | Parallel post | ||
|---|---|---|---|---|---|
| Ferrule | Nonferrule | Ferrule | Nonferrule | ||
| Ti | A | 9.804 | 10.26 | 9.802 | 10.24 |
| B | 11.76 | 13.19 | 13.72 | 13.17 | |
| C | 13.72 | 13.19 | 11.76 | 11.71 | |
|
| |||||
| Ni-Cr | A | 14.08 | 14.07 | 15.08 | 15.29 |
| B | 15.65 | 15.63 | 16.76 | 16.99 | |
| C | 14.08 | 14.07 | 15.08 | 15.29 | |
|
| |||||
| FRC | A | 5.525 | 5.626 | 5.516 | 5.625 |
| B | 3.684 | 5.626 | 3.678 | 5.626 | |
| C | 9.206 | 11.25 | 9.192 | 12.65 | |
*Maximum Von Mises stress in MPa.
A—cervical one-third; B—middle one-third; C—apical one-third.
Comparison of stress* distribution with different posts having ferrule and nonferrule design in the cervical dentin.
| Materials | Load† | Tapered post | Parallel post | ||
|---|---|---|---|---|---|
| Ferrule | Nonferrule | Ferrule | Nonferrule | ||
| Ti | V | 3.489 | 3.485 | 3.489 | 3.485 |
| O | 18.87 | 13.87 | 18.83 | 13.83 | |
| H | 25.49 | 19.06 | 25.48 | 19.02 | |
|
| |||||
| Ni-Cr | V | 2.555 | 2.555 | 2.555 | 2.555 |
| O | 12.52 | 12.51 | 11.95 | 13.36 | |
| H | 17.21 | 17.19 | 18.43 | 18.68 | |
|
| |||||
| FRC | V | 3.510 | 3.505 | 3.510 | 3.505 |
| O | 19.57 | 14.47 | 19.54 | 14.46 | |
| H | 25.77 | 19.69 | 25.73 | 19.68 | |
*Maximum Von Mises stress in MPa.
V—vertical load; O—oblique load (45° angle); H—horizontal load.
Figure 4“Wedging effect” with tapered post.
Figure 5Poorly defined “wedging effect” with parallel post.
Figure 6Increased stresses (von Mises) in cervical dentin with ferrule design.
Figure 7Reduced stresses (von Mises) in cervical dentin without ferrule design.