| Literature DB >> 19089201 |
Paola Colán Guzmán1, Fernando Furtado Antunes de Freitas, Paulo Martins Ferreira, César Antunes de Freitas, Kátia Rodrigues Reis.
Abstract
In long-term oral rehabilitation treatments, resistance of provisional crowns is a very important factor, especially in cases of an extensive edentulous distal space. The aim of this laboratorial study was to evaluate an acrylic resin cantilever-type prosthesis regarding the flexural strength of its in-balance portion as a function of its extension variation and reinforcement by two types of fibers (glass and polyaramid), considering that literature is not conclusive on this subject. Each specimen was composed by 3 total crowns at its mesial portion, each one attached to an implant component (abutment), while the distal portion (cantilever) had two crowns. Each specimen was constructed by injecting acrylic resin into a two-part silicone matrix placed on a metallic base. In each specimen, the crowns were fabricated with either acrylic resin (control group) or acrylic resin reinforced by glass (Fibrante, Angelus) or polyaramide (Kevlar 49, Du Pont) fibers. Compression load was applied on the cantilever, in a point located 7, 14 or 21 mm from the distal surface of the nearest crown with abutment, to simulate different extensions. The specimen was fixed on the metallic base and the force was applied until fracture in a universal test machine. Each one of the 9 sub-groups was composed by 10 specimens. Flexural strength means (in kgf) for the distances of 7, 14 and 21 mm were, respectively, 28.07, 8.27 and 6.39 for control group, 31.89, 9.18 and 5.16 for Kevlar 49 and 30.90, 9.31 and 6.86 for Fibrante. Data analysis ANOVA showed statistically significant difference (p<0.05) only regarding cantilever extension. Tukey's test detected significantly higher flexural strength for the 7 mm-distance, followed by 14 and 21 mm. Fracture was complete only on specimens of non-reinforced groups.Entities:
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Year: 2008 PMID: 19089201 PMCID: PMC4327629 DOI: 10.1590/s1678-77572008000200006
Source DB: PubMed Journal: J Appl Oral Sci ISSN: 1678-7757 Impact factor: 2.698
FIGURE 1Schematic drawing of the stainless steel base (dimensions in millimeters and angle in degrees). Two of the lateral orifices (p1 and p3) used to fix the prosthetic component with screws can be observed
FIGURE 2Lateral view of 3 prosthetic components attached to the metallic base at the bottom of lower portion of the silicone matrix
FIGURE 3Acrylic resin being injected through the proper orifice of the upper portion of the matrix (A); Appearance of the polymerized resin after removal of this portion (B)
FIGURE 4Lateral (A) and occlusal (B) view of a specimen ready to be tested
FIGURE 5Arrangement of fibers (both materials) contouring the abutments and extending to distal portion of the matrix (upper view) (A). In a lateral view (B), the fibers can be seen close to the top of abutments
FIGURE 6Specimen fixed on metallic base (upper view) (A) where the circles on the occlusal surface show possible load application points; Lateral view (B) where a metallic pin is applying force at the cantilever most distal point
Flexural strength values (in kgf) of each specimen (sp) of each studied sub-group, with the respective arithmetic mean (m) and standard deviation (sd)
| sp | Control | Kevlar 49 | Fibrante | ||||||
|---|---|---|---|---|---|---|---|---|---|
| 7 mm | 14 mm | 21 mm | 7 mm | 14 mm | 21 mm | 7 mm | 14 mm | 21 mm | |
| 1 | 30.50 | 6.35 | 8.25 | 28.40 | 13.25 | 4.05 | 31.70 | 7.60 | 9.65 |
| 2 | 32.00 | 8.45 | 5.85 | 33.30 | 6.25 | 4.55 | 35.70 | 10.65 | 7.50 |
| 3 | 22.00 | 8.70 | 5.20 | 36.05 | 9.20 | 4.85 | 32.55 | 9.18 | 7.53 |
| 4 | 22.50 | 7.15 | 5.55 | 30.15 | 10.50 | 5.60 | 25.20 | 13.98 | 7.65 |
| 5 | 26.75 | 8.75 | 5.50 | 28.60 | 9.30 | 5.35 | 36.15 | 8.58 | 3.73 |
| 6 | 32.45 | 10.10 | 6.50 | 35.20 | 10.40 | 6.30 | 33.75 | 12.33 | 6.98 |
| 7 | 21.75 | 10.30 | 6.60 | 33.95 | 8.60 | 4.60 | 31.80 | 9.43 | 7.55 |
| 8 | 37.50 | 6.85 | 6.55 | 27.40 | 6.45 | 6.25 | 32.40 | 7.88 | 4.50 |
| 9 | 23.75 | 10.80 | 7.65 | 33.15 | 8.45 | 5.15 | 22.90 | 5.13 | 8.20 |
| 10 | 31.50 | 5.30 | 6.30 | 32.65 | 9.35 | 4.95 | 26.80 | 8.33 | 5.35 |
|
| 28.07 | 8.27 | 6.39 | 31.89 | 9.18 | 5.16 | 30.90 | 9.31 | 6.86 |
|
| 5.47 | 1.83 | 0.96 | 3.03 | 2.02 | 0.73 | 4.45 | 2.51 | 1.80 |
ANOVA showed statistically significant difference among the sub-groups (f=620.9702; p<0.05) only for cantilever length, without interaction of factors. Tukey's test detected significant differences (p<0.05) among all cantilever lengths. To transform kgf in Newton (N), these values must be multiplied by factor 9.807.