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191 protocols using s 4300

1

Comprehensive Filler Characterization Protocol

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The microstructure of the filler was observed using field-emission scanning electron microscopy (FE-SEM; S-4300, Hitachi High-Tech Corp., Tokyo, Japan). Prior to observation, the sample was coated with platinum via sputtering. The observation conditions were an acceleration voltage of 5 kV and a working distance of 15 mm.
The surface area and pore size distribution of the filler were estimated using the Brunauer–Emmett–Teller (BET) method and the Barrett–Joyner–Halenda (BJH) method, respectively, using nitrogen sorption–desorption curves measured by a porosimeter (QuadraSorb SI, Quantachrome Instruments, Boynton Beach, FL, USA).
The crystal phase of the filler was determined using X-ray diffraction (XRD; RINT 2100VLR/PC, Rigaku, Tokyo, Japan) with a Cu Kα X-ray source (λ = 1.5406 Å).
The silanization of the filler was examined by Fourier transform infrared (FT-IR) analysis using a spectrometer (IRSpirit, Shimadzu Corp., Kyoto, Japan) with a diffuse reflectance unit with a resolution of 4 cm−1.
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2

SEM Imaging of Polyethylene Precipitates

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Polyethylene precipitates were carefully transferred on an adhesive tape on a platform for SEM observation to avoid deformation of the specimens. Platinum deposition (4 nm thick) on the surface of the precipitates was conducted prior to observation using a field emission-scanning electron microscope (Hitachi High-Technologies Co., S-4300).
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3

Field-Emission Scanning Electron Microscopy

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Field-emission scanning electron microscopy (SEM) was performed using an S-4300 instrument (Hitachi High-Tech) together with the modified sample chamber, as shown in Fig. 1a.
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4

Surface Preparation of PEEK for Bonding

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Details regarding the PEEK blocks, resin cements, and primers used in this study are listed in Table 1. The PEEK block was cut to a thickness of 4 mm using a diamond wheel saw and was polished using emery paper #600. The polished PEEK surface was sandblasted at 0.2 MPa with 50 μm alumina particles using an airborne particle abrader (Jet Blast II, J. Morita, Suita, Japan). The surface morphology of the PEEK was observed using scanning electron microscopy (SEM; S-4300, Hitachi High-Tech, Tokyo, Japan). The obtained sandblasted PEEK was used for all subsequent experiments.
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5

Characterization of Discharged Lithium-Ion Cathodes

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For the characterization of discharged cathodes, the cells were disassembled in an Ar glovebox and the discharged cathodes were extracted from the cells. The cathodes were immersed in anhydrous MeCN for 24 h and rinsed with MeCN for three times to remove electrolytes and dried in vacuo at room temperature for 2 h. SEM images were obtained using SEM system (Hitachi high-technologies, S-4300) at an acceleration voltage of 1 kV. The samples were transferred from a glove box to the SEM chamber using a closed vessel to avoid exposure to the air. Powder X-ray diffraction (PXRD) patterns of the discharged cathodes were measured with a powder X-ray diffractometer (Rigaku, UltimaIV) in an air-sensitive sample holder. Measurements were performed at room temperature from 5 to 70˚ 2θ. Raman spectra were measured in an airtight quartz cell on a Raman spectrometer (JASCO, NRS-3200).
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6

Analyzing Porous Structure and VCM Release

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The relationship between the pore structure and VCM release profiles of CPC/VCM and PMMA/VCM was analyzed and compared. CPC/VCM without implantation was immersed in 20 mL of acetone for 10 min for dehydration, removed, and dried at room temperature; this process was not necessary for PMMA/VCM. Thin sections (1-2 mm thickness) of each test specimen were prepared using a microtome for scanning electron microscopy (SEM) analysis (S-4300, Hitachi High-Technologies) and the analysis of pore size distribution using mercury porosimetry (AutoPore IV9520, Micromeritics, Norcross, GA, USA).
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7

Scanning Electron Microscope Analysis of Luting Agents

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The three luting agents were evaluated with a scanning electron microscope (SEM, S-4300, Hitachi High-Technologies, Tokyo, Japan). Each luting agent was filled into the brass ring, polymerized with the curing unit, and stored in the dark for 30 min. The surfaces of the specimens were ground with a #1,200-grit silicon carbide abrasive paper. The specimens were then mounted on stubs and adequately dried in a vacuum desiccator for 24 h. After osmium coating with a sputter coater (HPC-1S, Vacuum Device, Mito, Japan) for 30 s, the specimens were observed with a microscope with an accelerating voltage of 15 kV.
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8

Failure Mode Analysis of Zirconia Composites

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To determine the failure mode, the fractured surfaces of the specimens were observed at 32× magnification using a stereoscopic microscope (Stemi DV4, Carl Zeiss, MicroImaging, Göttingen, Germany). The failure modes were categorized as follows: (A) adhesive failure at the zirconia/composite resin interface, (B) combination of adhesive failure at the zirconia/composite resin interface and cohesive failure within the composite resin, (C) adhesive failure at the zirconia/glazed layer interface, (D) combination of adhesive failure at the zirconia/ glazed layer interface and cohesive failure within the glazed layer, (E) adhesive failure at the glazed layer/ composite resin interface, (F) combination of adhesive failure at the glazed layer/composite resin interface and cohesive failure within the glazed layer, (G) combination of adhesive failure at the glazed layer/composite resin interface and cohesive failure within the composite resin, and (H) cohesive failure within the composite resin (Fig. 2). Representative specimens were sputter-coated with osmium (HPC-IS, Vacuum Device, Mito, Japan) and imaged by scanning electron microscope (SEM; S-4300, Hitachi High-Technologies, Tokyo, Japan). The representative specimens were also analyzed using an X-ray diffractometer (Miniflex, Rigaku, Tokyo, Japan) with Cu Kα radiation by scanning over the diffraction angle (2θ) range of 3°-90°.
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9

Sputter Coating and SEM Analysis

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Before primer application and after shear bond strength testing, the selected metal specimens were sputter coated with osmium for 30 s. The surfaces were then undertaken using SEM (S-4300, Hitachi High Technologies, Tokyo, Japan, and ERA-8800FE, Elionix, Tokyo, Japan) with an acceleration voltage of 15 kV.
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10

Characterization of SiC Powders and Sintered SiC

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A LA system (UP213, Electro Scientific Indutries (ESI), Portland, OR, USA) and an ICPMS instrument (Agilent 7500ce, Agilent Technologies, Tokyo, Japan) were used in this study (Table 2). A pressure vessel with a stainless-steel jacket (HU-50, San-ai Kagaku, Aichi, Japan) was used for the acid digestion of SiC powders and sintered SiC cracked with a hammer. SiC particles were observed by scanning electron microscopy (SEM; S-4300, Hitachi High Technologies, Tokyo, Japan). For SEM measurements, the surfaces of all the samples were coated with a Pt/Pd alloy by means of an ion sputtering device (E-1045, Hitachi High Technologies, Tokyo, Japan).
Dynamic light scattering (ELSZ-2000ZS, Otsuka Electronics Co., Osaka, Japan) was used to measure the diameter distribution of LAL-sampled particles. A semiconductor laser with a wavelength of 660 nm was used.
The LAL-sampled particles of sintered SiC and single-crystal SiC were placed on a glass slide by means of a needle, and their chemical compositions were measured by laser Raman microscopy (RAMAN-11, Nanophoton Corporation, Osaka, Japan; laser wavelength, 532 nm). This method enabled us to analyze individual particles.
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