| Literature DB >> 28678947 |
Rafael Soares Gomes1, Caroline Mathias Carvalho de Souza2, Edmara Tatiely Pedroso Bergamo1, Dimorvan Bordin1, Altair Antoninha Del Bel Cury1.
Abstract
OBJECTIVE: In this study, marginal and internal misfit and fracture load with and without thermal-mechanical aging (TMA) of monolithic ZLS and lithium disilicate (LDS) crowns were evaluated.Entities:
Mesh:
Substances:
Year: 2017 PMID: 28678947 PMCID: PMC5482251 DOI: 10.1590/1678-7757-2016-0233
Source DB: PubMed Journal: J Appl Oral Sci ISSN: 1678-7757 Impact factor: 2.698
Figure 1A: Points used for the measurement of marginal gap (MG) and absolute marginal discrepancy (AMD). B: Points used for the measurement of axial gap (AG) and occlusal gap (OG)
Marginal gap (MG), absolute marginal discrepancy (AMD), axial gap (AG), and occlusal gap (OG) values (µm; n=8; mean±standard deviation)
| Group | MG | AMD | AG | OG |
|---|---|---|---|---|
| LDS | 41.45±18.11a | 180.67±23.23a | 96.07±30.19a | 255.80±65.05a |
| ZLS | 101.86±32.12b | 235.54±35.75b | 100.09±23.83a | 252.68±35.18a |
LDS, lithium disilicate; ZLS, zirconia-reinforced lithium silicate. Different superscripted letters indicate significant differences between materials (Student’s t-test, p<0.05).
Figure 2A: Cervical area of the lithium disilicate crown with no chipping. B: Cervical area of the zirconia-reinforced lithium silicate crown, showing chipping at the edge (arrows)
Two-way ANOVA (2x2) of material, aging condition, and interactions between these variables
| Source | SS | df | MS | F | P |
|---|---|---|---|---|---|
| Material | 2946302.1 | 1 | 2946302.1 | 38.13 | .000 |
| Aging condition | 74643.6 | 1 | 74643.6 | 0.97 | .332 |
| Material*Aging condition | 114260.1 | 1 | 114260.1 | 1.48 | .232 |
| Error | 2781347.9 | 36 | 77259.7 |
SS, Sum of Squares; df, degree freedom; MS, Mean Square
Figure 3Mean fracture loads of LDS and ZLS crowns before and after thermal-mechanical aging. Bars indicate standard deviations and different letters indicate significant differences (two-way ANOVA, p<0.05)
Figure 4Fractographic image showing fracture origin (O), direction of crack propagation (dcp), arrest lines (A), and hackle lines (H)
Figure 5Weibull distribution showing failure probability according to the applied load