| Literature DB >> 34787719 |
Marie-Therese Heberer1, Hubert C Roggendorf2, Franz-Josef Faber3, Nicolai-Alexander Lawrenz4, Roland Frankenberger5, Matthias J Roggendorf5.
Abstract
OBJECTIVES: The aim of this study was to investigate whether file design and taper significantly influence microcrack initiation during machine preparation.Entities:
Keywords: Craze lines; Cutting-edge angle; Digital microscopy; Microcracks; Root dentin; Taper
Mesh:
Year: 2021 PMID: 34787719 PMCID: PMC8898247 DOI: 10.1007/s00784-021-04238-3
Source DB: PubMed Journal: Clin Oral Investig ISSN: 1432-6981 Impact factor: 3.573
Fig. 1The experimental procedure of the main trial
Overview of the experimental groups [17, 27, 29–34]
| Group | File system | File sequences | Manufacturer | Taper | Cross-section | Technique |
|---|---|---|---|---|---|---|
| I | #10/.04, #15/.05, #20/.06, #25/.05, #30/.06, #35/.04, #40/.04 | VDW Dental, Munich, Germany | Continuous taper .04 | S-shaped (active cutting) with a large chip space and small core diameter | Single-length (full rotation) | |
| II | Opener #30/.10, #40/.06 | Komet Dental, Lemgo, Germany | Continuous taper .06 | Double-S-shaped (active cutting) with a large chip space and small core diameter | Single-length (full rotation) | |
| III | SX, S1, S2, F1 (#20/.07), F2 (#25/.08), F3 (#30/.09), F4 (#40/.06) | Dentsply Sirona, Bensheim, Germany | Reverse taper .06 (different progressive tapers from 2% up to 11.5%) | Up to F3: slightly convex triangular (passive-cutting), F4 concave | Crown-down (pressure-less) technique (full rotation) | |
| IV | Occlusal cavity, composite filling, no preparation and filling | –- | –- | –- | –- | |
| Control | No treatment, no chewing simulation, only digital microscopic scans | –- | –- | –- | –- | |
Fig. 2Before starting the chewing simulation (baseline), the teeth were examined for microcracks from both contralateral sides with digital microscopic scans (Keyence VHX-5000, lens: Keyence VH-Z20T, Keyence Corp., Osaka, Japan) (magnification: 200 × , step z = 20 µm). The images were superimposed, and the crack growths were color-coded and measured afterwards
Fig. 3An overview of craze line propagation over the observation period of 3 years starting from baseline [µm]