Page 21 - PR 2014 2016 10 Materials and Nanotechnology
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Materials and Nanotechnology | Progress Report  297





               600°C, in constant load mode at 250 and 319    characterization of the nitride layer was per-
               MPa. The techniques used in this study were    formed with the aid of optical microscopy
               optical microscopy and scanning electron mi-   (OM) and X-ray diffraction (XRD). Tensile tests
               croscopy. Fractographic analysis of the creep   were performed between 600 and 1000°C and
               tested samples showed necking and microcav-    deformation rates between 0.0002 and 0.002 s .
                                                                                                         -1
               ities. The creep results revealed a significant   The results have shown that nitrided sample
               increase in material strength.                 present expanded fcc phase and chromium
                                                              nitride (CrN) phases. Tensile tests showed
               Aiming at applications such as biomaterial,    that there was no significant difference in
               the effect of plasma nitriding on the Ti-6Al-4V   the yield strength and elongation between
               alloy in fatigue behavior has be studied. The   non-nitrided and plasma-nitrided samples at
               studies are being performed in the Ti-6Al-4V   the same temperatures. Serrated stress–strain
               alloy will be comparative in the alloy with and   behavior was observed in the curves obtained
               without nitriding.                             at 600 and 700°C, which was associated with
                                                              the dynamic strain aging effect. At 600°C, the
               Ti-Al intermetallic alloyss with an Al content   increase in strain rate promoted an increase
               between 35 and 65 (atomic%) are usually        of the amplitude and oscillation frequency of
               divided into two categories: single-phase or   the stress.
               two-phase alloys. The first group consists ex-
               clusively of the γ-TiAl phase, and the second,   Evaluation of adaptation and removal
               by the union of the γ-TiAl and α2-Ti3Al phases.   resistance of impacted abutment in small
               Single-phase alloys do not have a balanced set   diameter conical dental implant
               of properties. The dual phase alloys allow the
               desired characteristics to be systematized by   Dental implants of alloy Ti6Al4V (grade V)
               means of different microstructures, which can   of narrow diameter came to solve a constant
               be classified into several groups: (a) partially   situation in the current implantology, which
               lamellar, (b) near-γ, (c) duplex and D) com-   would be the installation of implants in re-
               pletely lamellar. The study has focused on the   duced mesiodistal spaces, mainly to allow a
               microstructural characterization of Ti-Al-type   final prosthesis with appropriate aesthetic
               alloys (Ti-44Al-4Nb-1Mo-B and Ti-48Al-2Cr-     requirement. Because it is a 2-part system,
               2Nb-B).                                        the installation of the abutment, made in the
                                                              same alloy, is performed by impaction because
               Nickel based superalloys                       its stabilization through a screw becomes in-

                                                              consistent due to difficulties in machining
               Inconel is a nickel-chromium-molybdenum        such tiny components. The abutment after
               superalloy with high corrosion resistance and   impaction in various ways in the implants
               strength at elevated temperatures. Surface     were sectioned at 2 mm from the implant
               modification of Inconel 625 has been carried   platform and the two halves were observed in
               out to improve mechanical properties at el-    a scanning electron microscope (SEM)(Figure
               evated temperatures. Creep and hot tensile     27), in order to measure the gap or the space
               tests were performed to evaluate the me-       between the implant/ abutment. Similarly,
               chanical properties at elevated temperatures.   after the abutments were impacted in the
               The surface modification that was carried out   implants, they were subjected to tensile test
               was plasma nitriding. The microstructural      to evaluate their required removal force. This
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