The aim of this study was to determine the photocatalytic effect of doped-TiO 2 nanoparticles (NPs) on teeth bleaching with an aid of 3% H2O2 and laser irradiation. For the study, Mo-N-TiO2 NPs were prepared. The characteristics of the prepared NPs, NPs morphology and light absorbance, were evaluated. Photocatalytic reactions of NPs were tested using 10 ppm methylene blue (MB) solution. Extracted teeth were pasted using carbomer gel for color differences measurements. Mo-N-TiO2 NPs have close to round shape with some tens nm size. Their absorbance was higher and longer than that of TiO 2 NPs. For MB solution, Mo-N-TiO2 with 3% H2O2 condition showed much decrease in absorbance after laser irradiation for 20 min. Also, regardless of wavelength, Mo-N-TiO2 NPs produced much greater color difference (whitening) on teeth after 3 h than that by 15% H2O2 .

The purpose of the present study was to assess the temperature change and compressive property of bulk-fill composites (BFCs) by the light curing. Seven resin-based composites (RBCs), including five BFCs, were chosen to evaluate their maximum temperature rise and exothermic heat during and after light curing and compressive strength (CS) and modulus (CM) for 4-mm thick state. Light attenuation coefficients (ACs) showed reasonably high correlation with filler content (vol% and wt%).Except one resin product, AC values of BFCs were lower than those of RBCs tested. All the tested specimens showed temperature rise (9.8-23.6℃) and exothermic heat (4.2-18.3℃) for 4-mm thick case. CS and CM values of the tested specimens ranged approximately 69 to 116 MPa and 1.3 to 2.8 GPa, respectively. The difference of temperature changes and compressive properties (CS and CM) between BFCs and RBCs was not consistent and had no statistically consistent significance.

The effect of the cooling rate on changes in hardness, flexural strength, and microstructure of zirconia core ceramics was investigated during simulated porcelain firing without layering porcelain on the zirconia core ceramic. Three cooling rates were tested: 227.5 ℃/min, which is the rate suggested by the manufacturer, Stage 0 (taking the ceramic out of the firing chamber immediately after firing and bench cooling to room temperature), and Stage 3 (cooling to 600 ℃ with the firing chamber closed and then bench cooling to room temperature (33 ℃/min)). In the Stage 0 group and the group cooled at the rate suggested by the manufacturer, the hardness increased compared to the group before firing (p<0.001). The hardness of the Stage 3 group was not different from that of the group before firing (p>0.05). The grain size of the specimen groups whose hardness increased after firing was reduced by recrystallization, but the Stage 3 group had coarsened grains. In all test groups before and after firing, only the tetragonal phase was observed. In particular, a metastable phase (T’) in which the axial ratio (c/a ratio = c/√ 2a) was closer to 1 coexisted with the tetragonal phase. The flexural strength of the zirconia core did not exhibit a significant difference with respect to the cooling rate (p>0.05).

The purpose of the present study was to assess the temperature change and compressive property of bulk-fill composites (BFCs) by the light curing. Seven resin-based composites (RBCs), including five BFCs, were chosen to evaluate their maximum temperature rise and exothermic heat during and after light curing and compressive strength (CS) and modulus (CM) for 4-mm thick state. Light attenuation coefficients (ACs) showed reasonably high correlation with filler content (vol% and wt%).Except one resin product, AC values of BFCs were lower than those of RBCs tested. All the tested specimens showed temperature rise (9.8-23.6℃) and exothermic heat (4.2-18.3℃) for 4-mm thick case. CS and CM values of the tested specimens ranged approximately 69 to 116 MPa and 1.3 to 2.8 GPa, respectively. The difference of temperature changes and compressive properties (CS and CM) between BFCs and RBCs was not consistent and had no statistically consistent significance.

The effect of the cooling rate on changes in hardness, flexural strength, and microstructure of zirconia core ceramics was investigated during simulated porcelain firing without layering porcelain on the zirconia core ceramic. Three cooling rates were tested: 227.5 ℃/min, which is the rate suggested by the manufacturer, Stage 0 (taking the ceramic out of the firing chamber immediately after firing and bench cooling to room temperature), and Stage 3 (cooling to 600 ℃ with the firing chamber closed and then bench cooling to room temperature (33 ℃/min)). In the Stage 0 group and the group cooled at the rate suggested by the manufacturer, the hardness increased compared to the group before firing (p<0.001). The hardness of the Stage 3 group was not different from that of the group before firing (p>0.05). The grain size of the specimen groups whose hardness increased after firing was reduced by recrystallization, but the Stage 3 group had coarsened grains. In all test groups before and after firing, only the tetragonal phase was observed. In particular, a metastable phase (T’) in which the axial ratio (c/a ratio = c/√ 2a) was closer to 1 coexisted with the tetragonal phase. The flexural strength of the zirconia core did not exhibit a significant difference with respect to the cooling rate (p>0.05).

In this study, Au-Pt-Pd metal-ceramic alloy was examined by varying cooling rate during simulated porcelain firing cycles to investigate the effect of cooling rate on hardness and related microstructure during simulated firing. The final hardness was different according to the cooling rate after the simulated porcelain firing cycles. The reduction in hardness value was smaller after cooling at the faster cooling rate (Stage 0) than the value after slower rate (Stage 3). In the ice-quenched specimens after oxidation treatment (OXI-IQ), homogenization was slightly occurred, and the hardness decreased apparently compared to that of the as-cast specimens (AS-CAST). In the specimens cooled at Stage 0 and Stage 3 after oxidation, the hardness increased apparently compared to the ice-quenched specimens, even though the hardness decreased later by further firing simulation.The final hardness was lower in the specimen cooled at the slower rate (Stage 3) than the faster rate (Stage 0), and it seems to be due to the coarsening of the microstructure. The matrix and precipitates were consisted of FCC (face-centered-cubic) structure rich in Au. The Au content was higher in the matrix and the Pt content was higher in the precipitates, which corresponded to the Au-Pt binary phase diagram.

The objective of this study was to investigate the effect of different cooling rates and subsequent post-firing heat treatment on the final hardness of a metal-ceramic alloy. For this, Specimens of Pd-Ag-In-Sn alloy underwent simulated firing at two different cooling rates, followed by post-firing heat treatment. Hardness measurement, microstructure observation, and crystal structure analysis were conducted on the firing simulated and post-firing heat-treated specimens to analyze the causes of hardness variations. The experimental results showed that the difference in cooling rates during simulated firing had an impact on the final hardness of the alloy, and the specimens cooled at the slowest rate (Stage 3) exhibited higher hardness at all firing Stages compared to the specimens cooled at the highest rate (Stage 0). Regardless of the difference in cooling rates during the firing process, the hardness of the alloy significantly increased by the post-firing heat treatment. The increase in hardness by the post-firing heat treatment was attributed to the formation of fine precipitates in the matrix, and the precipitation reaction occurred as a result of the decrease in solubility of (Pd, Ag, Au) 3 (In, Sn, Zn) phase in the Pd-Ag-rich matrix. The clinical significance of this study is that performing the post-firing heat treatment demonstrates effectiveness in increasing the reduced hardness after porcelain firing in metal-ceramic alloys.

In this study, Au-Pt-Pd metal-ceramic alloy was examined by varying cooling rate during simulated porcelain firing cycles to investigate the effect of cooling rate on hardness and related microstructure during simulated firing. The final hardness was different according to the cooling rate after the simulated porcelain firing cycles. The reduction in hardness value was smaller after cooling at the faster cooling rate (Stage 0) than the value after slower rate (Stage 3). In the ice-quenched specimens after oxidation treatment (OXI-IQ), homogenization was slightly occurred, and the hardness decreased apparently compared to that of the as-cast specimens (AS-CAST). In the specimens cooled at Stage 0 and Stage 3 after oxidation, the hardness increased apparently compared to the ice-quenched specimens, even though the hardness decreased later by further firing simulation.The final hardness was lower in the specimen cooled at the slower rate (Stage 3) than the faster rate (Stage 0), and it seems to be due to the coarsening of the microstructure. The matrix and precipitates were consisted of FCC (face-centered-cubic) structure rich in Au. The Au content was higher in the matrix and the Pt content was higher in the precipitates, which corresponded to the Au-Pt binary phase diagram.

In this experiment, the alloy having the composition of 49.5Pd-40Ag-9In-1Ga (wt.%) was used to find the most effective cooling rate for the hardening of alloy during porcelain firing simulation. In each stage of firing simulation, ice-quenching or cooling at the most effective cooling rate for hardening of the alloy was done after firing to observe changes in the hardness and associated microstructures during the firing and subsequent cooling. For this purpose, the firing simulated alloy was characterized by analyzing the changes in hardness, microstructure, crystal structure and the elemental distribution. The hardness of alloy decreased by cooling after oxidation treatment, which was induced by the homogenization of the specimen. In this alloy, the most effective cooling rate for alloy hardening after oxidation treatment was Stage 0. During the porcelain firing simulation until the final firing stage, the cooling rate was set to Stage 0, and the complete firing simulation was performed until the final firing stage, Glaze. As a result, the final hardness of the metal substructure obtained after complete firing simulation was lower than that of the as-cast specimen. The decrease in hardness caused by the porcelain firing simulation results from a reduction in the interface between the precipitates of face-centered tetragonal structures and the matrix of face-centered cubic structures as the precipitates coarsen.

This study investigated the effect of the difference in the cooling rates on the optical properties of zirconia during the simulated firing of porcelain, without a porcelain layer on a zirconia core ceramic. No difference was observed in the average transmittance of zirconia with the cooling rate during simulated firing (p>0.05). In all groups, the average transmittance decreased from approximately 44% to approximately 28% (p<0.001) as the thickness increased from 0.51 mm to 2.0 mm. No difference was observed in the translucency and opalescence parameters of zirconia with the cooling rate during the simulated firing of porcelain (p>0.05). In all groups, the translucency decreased from approximately 16 to approximately 5 (p<0.001), while the opalescence increased from approximately 6 to approximately 11 (p<0.001) as the thickness increased from 0.51 mm to 2.00 mm. Thus, the average transmittance and translucency parameter decreased exponentially as the thickness increased in all groups regardless of the cooling rate during simulated porcelain firing, while the opalescence parameter increased in a parabolic manner. Therefore, in this study, even if porcelain is fired at a cooling rate higher or lower than the typical cooling rate when manufacturing a prosthesis with a zirconia core, the optical properties of zirconia are not expected to be significantly affected.