Mahmoud Ahmad, Wakabayashi Noriyuki, Takahashi Hidekazu, Ohyama Takashi
Division of Oral Health Sciences, Graduate School, Tokyo Medical and Dental University, Tokyo 113-8549, Japan.
J Prosthet Dent. 2005 Feb;93(2):183-8. doi: 10.1016/j.prosdent.2004.11.011.
There is little information about the deflection fatigue of clasps in relation to stress distribution.
The aim of this study was to investigate the fatigue resistance and permanent deformation of cast clasps made of titanium and other dental alloys and to relate the fatigue resistance with the calculated stress values.
Twenty-five Ti-6Al-7Nb, 25 Co-Cr, and 15 Type IV gold alloy clasps were subjected to cyclic deflection of preset values of 0.25 mm, 0.50 mm, or 0.75 mm, for 10 6 cycles (n = 14). Finite element models were created to calculate principal stresses within the specimens. Fatigue life, retentive force, and permanent deformation were recorded, and the fracture locations were determined microscopically. The results were characterized in relation to the stress within the clasps. One-way analysis of variance and Tamhane's post-hoc tests were used to compare the results of the 9 material-deflection groups (alpha=.05).
Ti-6Al-7Nb clasps exhibited significantly less permanent deformation than the other clasps under relatively greater deflections, indicating better adaptation to the tooth surface. However, the fatigue life of the Ti-6Al-7Nb clasps under 0.75-mm deflection, with the stress above the alloy's 0.2% yield strength, was significantly shorter than those under smaller deflections. The gold clasps showed significantly longer fatigue life than the other clasps under the 0.50-mm deflection. High-stress areas within the fatigue clasp specimens coincided with the fracture locations. The probabilities of fatigue fracture and permanent deformation were closely related to the material strengths and the preset deflections.
To minimize fatigue failures, the cast clasp should be designed with consideration of the stresses distributions within the clasps.
关于卡环的挠曲疲劳与应力分布的相关信息较少。
本研究的目的是调查由钛和其他牙科合金制成的铸造卡环的抗疲劳性和永久变形,并将抗疲劳性与计算出的应力值相关联。
对25个Ti-6Al-7Nb、25个钴铬合金和15个IV型金合金卡环进行0.25毫米、0.50毫米或0.75毫米预设值的循环挠曲,循环10^6次(n = 14)。创建有限元模型以计算试样内的主应力。记录疲劳寿命、固位力和永久变形,并通过显微镜确定断裂位置。根据卡环内的应力对结果进行表征。采用单因素方差分析和Tamhane事后检验比较9个材料-挠曲组的结果(α = 0.05)。
在相对较大的挠曲下,Ti-6Al-7Nb卡环比其他卡环表现出明显更小的永久变形,表明对牙面的适应性更好。然而,在0.75毫米挠曲下,Ti-6Al-7Nb卡环的应力高于合金的0.2%屈服强度,其疲劳寿命明显短于较小挠曲下的情况。在0.50毫米挠曲下,金合金卡环的疲劳寿命明显长于其他卡环。疲劳卡环试样内的高应力区域与断裂位置一致。疲劳断裂和永久变形的概率与材料强度和预设挠曲密切相关。
为了使疲劳失效最小化,铸造卡环的设计应考虑卡环内的应力分布。