Kajima Yuka, Takaichi Atsushi, Nakamoto Takayuki, Kimura Takahiro, Yogo Yoshiaki, Ashida Maki, Doi Hisashi, Nomura Naoyuki, Takahashi Hidekazu, Hanawa Takao, Wakabayashi Noriyuki
Removable Partial Prosthodontics, Oral Health Sciences, Graduate School of Medical and Dental Sciences, Tokyo Medical and Dental University, 1-5-45 Yushima, Bunkyo-ku, Tokyo 113-8549, Japan.
Removable Partial Prosthodontics, Oral Health Sciences, Graduate School of Medical and Dental Sciences, Tokyo Medical and Dental University, 1-5-45 Yushima, Bunkyo-ku, Tokyo 113-8549, Japan.
J Mech Behav Biomed Mater. 2016 Jun;59:446-458. doi: 10.1016/j.jmbbm.2016.02.032. Epub 2016 Mar 4.
We aimed to investigate the fatigue strength of Co-Cr-Mo clasps for removable partial dentures prepared by selective laser melting (SLM). The Co-Cr-Mo alloy specimens for tensile tests (dumbbell specimens) and fatigue tests (clasp specimens) were prepared by SLM with varying angles between the building and longitudinal directions (i.e., 0° (TL0, FL0), 45° (TL45, FL45), and 90° (TL90, FL90)). The clasp specimens were subjected to cyclic deformations of 0.25mm and 0.50mm for 10(6) cycles. The SLM specimens showed no obvious mechanical anisotropy in tensile tests and exhibited significantly higher yield strength and ultimate tensile strength than the cast specimens under all conditions. In contrast, a high degree of anisotropy in fatigue performance associated with the build orientation was found. For specimens under the 0.50mm deflection, FL90 exhibited significantly longer fatigue life (205,418 cycles) than the cast specimens (112,770 cycles). In contrast, the fatigue lives of FL0 (28,484 cycles) and FL45 (43,465 cycles) were significantly shorter. The surface roughnesses of FL0 and FL45 were considerably higher than those of the cast specimens, whereas there were no significant differences between FL90 and the cast specimens. Electron backscatter diffraction (EBSD) analysis indicated the grains of FL0 showed preferential close to <001> orientation of the γ phase along the normal direction to the fracture surface. In contrast, the FL45 and FL90 grains showed no significant preferential orientation. Fatigue strength may therefore be affected by a number of factors, including surface roughness and crystal orientation. The SLM process is a promising candidate for preparing tough removable partial denture frameworks, as long as the appropriate build direction is adopted.
我们旨在研究通过选择性激光熔化(SLM)制备的可摘局部义齿钴铬钼卡环的疲劳强度。通过SLM制备了用于拉伸试验的钴铬钼合金试样(哑铃形试样)和疲劳试验的卡环试样,构建方向与纵向方向之间的夹角各不相同(即0°(TL0、FL0)、45°(TL45、FL45)和90°(TL90、FL90))。卡环试样承受0.25mm和0.50mm的循环变形,循环次数为10⁶次。SLM试样在拉伸试验中未表现出明显的力学各向异性,并且在所有条件下均表现出比铸造试样显著更高的屈服强度和极限抗拉强度。相比之下,发现疲劳性能与构建方向相关的高度各向异性。对于挠度为0.50mm的试样,FL90的疲劳寿命(205,418次循环)明显长于铸造试样(112,770次循环)。相比之下,FL0(28,484次循环)和FL45(43,465次循环)的疲劳寿命明显更短。FL0和FL45的表面粗糙度明显高于铸造试样,而FL90与铸造试样之间没有显著差异。电子背散射衍射(EBSD)分析表明,FL0的晶粒在垂直于断裂表面的方向上优先接近γ相的<001>取向。相比之下,FL45和FL90的晶粒没有明显的优先取向。因此,疲劳强度可能受多种因素影响,包括表面粗糙度和晶体取向。只要采用合适的构建方向,SLM工艺就是制备坚固的可摘局部义齿框架的有前途的候选方法。