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钛-氧化锆种植体-基台界面的磨损:一项初步研究。

Wear at the titanium-zirconia implant-abutment interface: a pilot study.

机构信息

Maxillofacial Prosthetics, Memorial Sloan-Kettering Cancer Center, Dental Service, Department of Surgery, New York, New York, USA.

出版信息

Int J Oral Maxillofac Implants. 2011 Sep-Oct;26(5):970-5.

Abstract

PURPOSE

The purpose of this study was to use a clinical simulation to determine whether wear of the internal surface of a titanium implant was greater following connection and loading of a one-piece zirconia implant abutment or a titanium implant abutment.

MATERIALS AND METHODS

Two implants received zirconia abutments and two received titanium abutments. The implants were secured into four fiber-reinforced epoxy resin disks that had been prepared to receive the internal-connection implants. The assemblies were cyclically loaded off-axis for a total of 1,000,000 cycles. At various intervals, the abutments were removed, photographed, examined using scanning electron microscopy (SEM), and returned to the implants for further testing. The area of titanium transfer from the implants to the abutments observed in the SEM images was quantified using image analysis software.

RESULTS

The method was able to quantify the area of material transferred to the abutments. There was considerably more wear associated with the zirconia abutments, but the rate of wear slowed after about 250,000 cycles. Parabolic curves were fit to the data. The projected mean ± standard deviation maximum area (wear) values associated with the titanium and zirconia abutments were 15.8 ± 3.3 x 10³ Μm² and 131.8 ± 14.5 x 10³ Μm², respectively, and this difference was statistically significant (P = .0081).

CONCLUSIONS

The implants with the zirconia abutments showed a greater initial rate of wear and more total wear than the implants with the titanium abutments following cyclic loading. The amount of titanium transfer seen on the zirconia abutment increased with the number of loading cycles but appeared to be self-limiting. The clinical ramifications of this finding are unknown at this time; however, the potential for component loosening and subsequent fracture and/or the release of particulate titanium debris may be of concern.

摘要

目的

本研究旨在通过临床模拟来确定在连接和加载一体式氧化锆种植体基台或钛种植体基台后,内部连接表面的钛种植体磨损是否更大。

材料与方法

将两个种植体固定在四个纤维增强环氧树脂圆盘上,这些圆盘已准备好接收内部连接种植体。将组件以 100 万次的总循环周期进行偏轴循环加载。在不同的间隔时间,取出基台,拍照,用扫描电子显微镜(SEM)检查,并返回种植体进行进一步测试。使用图像分析软件定量分析 SEM 图像中观察到的钛从种植体转移到基台的面积。

结果

该方法能够定量测量转移到基台的材料面积。与氧化锆基台相关的磨损量相当大,但在大约 250,000 次循环后,磨损率会减缓。对数据进行了抛物线拟合。钛和氧化锆基台的预计平均±标准偏差最大面积(磨损)值分别为 15.8±3.3x10³ Μm²和 131.8±14.5x10³ Μm²,差异具有统计学意义(P=0.0081)。

结论

在循环加载后,与钛基台相比,具有氧化锆基台的种植体显示出更大的初始磨损率和更多的总磨损量。在氧化锆基台上观察到的钛转移量随着加载循环次数的增加而增加,但似乎存在自我限制。目前尚不清楚这一发现的临床意义,但组件松动以及随后的断裂和/或钛颗粒释放的潜在风险可能值得关注。

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