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用于牙科应用的激光烧结工业纯钛和Ti-6Al-4V合金的微观结构与力学性能

Microstructures and Mechanical Properties of Laser-Sintered Commercially Pure Ti and Ti-6Al-4V Alloy for Dental Applications.

作者信息

Okazaki Yoshimitsu, Ishino Akira

机构信息

Department of Life Science and Biotechnology, National Institute of Advanced Industrial Science and Technology, 1-1 Higashi 1-chome, Tsukuba, Ibaraki 305-8566, Japan.

IDS Co. Ltd., 3-5-4 Hongo, Bunkyo-ku, Tokyo 113-0033, Japan.

出版信息

Materials (Basel). 2020 Jan 29;13(3):609. doi: 10.3390/ma13030609.

DOI:10.3390/ma13030609
PMID:32013199
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC7041401/
Abstract

To apply laser-sintered titanium (Ti) materials to dental prostheses with a three-dimensional structure such as partial dentures, we examined the microstructures and mechanical properties of commercially pure (CP) Ti grade (G) 2 annealed after laser sintering and laser-sintered (as-built) Ti-6Al-4V alloy. The tensile and fatigue properties of CP Ti G 2 annealed at 700 °C for 2 h after laser sintering were close to those of wrought CP Ti G 2 annealed at the same temperature after hot forging. The ultimate tensile strengths (σ) of 90°- and 0°-direction-built CP Ti G 2 rods after laser sintering 10 times were 553 and 576 MPa and the total elongations (TE) of these rods were 26% and 28%, respectively. The fatigue strengths (σ) at 10 cycles of the 90°- and 0°-direction-built CP Ti G 2 rods after laser sintering 10 times were ~320 and ~365 MPa, respectively. The ratio σ/σ was in the range of 0.5-0.7. The changes in the chemical composition and mechanical properties after laser sintering 10 times were negligible. The fatigue strength of the laser-sintered Ti-6Al-4V alloy was ~600 MPa, which was close to that of wrought Ti-6Al-4V alloy. These findings indicate that the laser-sintered CP Ti and Ti-6Al-4V alloy can also be applied in dental prostheses similarly to laser-sintered Co-Cr-Mo alloy. In particular, it was clarified that laser sintering using CP Ti G 4 powder is useful for dental prostheses.

摘要

为了将激光烧结钛(Ti)材料应用于具有三维结构的牙科修复体,如局部义齿,我们研究了激光烧结后退火的商业纯(CP)Ti 2级和激光烧结(原状)Ti-6Al-4V合金的微观结构和力学性能。激光烧结后在700℃下退火2小时的CP Ti 2级的拉伸和疲劳性能与热锻后在相同温度下退火的锻造CP Ti 2级的性能相近。激光烧结10次后的90°和0°方向构建的CP Ti 2级棒材的极限抗拉强度(σ)分别为553和576 MPa,这些棒材的总伸长率(TE)分别为26%和28%。激光烧结10次后的90°和0°方向构建的CP Ti 2级棒材在10次循环时的疲劳强度(σ)分别约为320和365 MPa。σ/σ比值在0.5 - 0.7范围内。激光烧结10次后的化学成分和力学性能变化可忽略不计。激光烧结的Ti-6Al-4V合金的疲劳强度约为600 MPa,与锻造的Ti-6Al-4V合金相近。这些发现表明,激光烧结的CP Ti和Ti-6Al-4V合金也可以与激光烧结的Co-Cr-Mo合金类似地应用于牙科修复体。特别是,已阐明使用CP Ti 4级粉末进行激光烧结对牙科修复体是有用的。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9462/7041401/32cff994b570/materials-13-00609-g013.jpg
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https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9462/7041401/32cff994b570/materials-13-00609-g013.jpg
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https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9462/7041401/45d4c0771e3a/materials-13-00609-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9462/7041401/c7ad7813dcd9/materials-13-00609-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9462/7041401/a28d109d2af8/materials-13-00609-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9462/7041401/9f18e5b58499/materials-13-00609-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9462/7041401/20e047f69228/materials-13-00609-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9462/7041401/32cff994b570/materials-13-00609-g013.jpg

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