Yoshida K, Kamada K, Atsuta M
Department of Fixed Prosthodontics, School of Dentistry, Nagasaki University, Nagasaki, Japan.
J Prosthet Dent. 2001 Feb;85(2):184-9. doi: 10.1067/mpr.2001.113628.
Surface treatment of CAD/CAM-generated composite material is important for a strong bond of resin luting agents to composite material. Purpose. This study evaluated the shear bond strengths of 2 dual-cured resin luting agents to a CAD/CAM composite material and the effect of silane coupling agent and bonding resin on the bond strength.
Rectangular- and disk-shaped CAD/CAM composite materials were untreated or treated with 1 of the 2 silane coupling agents or bonding resin and then cemented together with 1 of the 2 dual-cured resin luting agents. Half of the specimens were stored in water at 37 degrees C for 24 hours, the other half thermocycled 50,000 times before shear bond strength testing. Shear bond strengths were measured with a servohydraulic mechanical testing machine, and results were analyzed with 2-way analysis of variance.
Surface treatment by silane coupling agent improved the shear bond strength when compared with nontreatment. Specimens treated with bonding resin showed significantly greater shear bond strength than the untreated groups. However, all specimens had the same adhesive failures at the composite-luting agent interface as untreated groups. When the CAD/CAM composite material was treated with 1 of the 2 silane coupling agents, no significant differences in bond strength were noted between water storage alone and after 50,000 thermocycles. For the 2 groups treated with bonding resin or silane coupling agent and cemented with 1 of the 2 dual-cured resin luting agents, there were significant increases in bond strength after 50,000 thermocycles, compared with specimens that were not subjected to thermal cycling. On the other hand, for the 2 untreated groups, there were significant decreases in bond strength after thermocycling. After 50,000 thermocycles, all specimens treated with silane coupling agent and then cemented with 1 of the 2 resin luting agents showed cohesive failures within the composite material.
The application of a silane coupling agent to the CAD/CAM composite surface provided the highest bond strength between the resin luting agent and composite after long-term thermal cycling.
CAD/CAM 生成的复合材料的表面处理对于树脂粘结剂与复合材料的牢固粘结很重要。目的:本研究评估了两种双重固化树脂粘结剂与 CAD/CAM 复合材料之间的剪切粘结强度,以及硅烷偶联剂和粘结树脂对粘结强度的影响。
将矩形和盘形的 CAD/CAM 复合材料不进行处理,或用两种硅烷偶联剂或粘结树脂中的一种进行处理,然后用两种双重固化树脂粘结剂中的一种粘结在一起。一半试样在 37℃水中储存 24 小时,另一半在进行剪切粘结强度测试前进行 50000 次热循环。用伺服液压机械试验机测量剪切粘结强度,结果用双向方差分析进行分析。
与未处理相比,硅烷偶联剂表面处理提高了剪切粘结强度。用粘结树脂处理的试样显示出比未处理组显著更高的剪切粘结强度。然而,所有试样在复合材料 - 粘结剂界面处与未处理组具有相同的粘结失败情况。当 CAD/CAM 复合材料用两种硅烷偶联剂中的一种处理时,单独储水和 50000 次热循环后粘结强度没有显著差异。对于用粘结树脂或硅烷偶联剂处理并用两种双重固化树脂粘结剂中的一种粘结的两组,与未进行热循环的试样相比,50000 次热循环后粘结强度显著增加。另一方面,对于两组未处理组,热循环后粘结强度显著降低。50000 次热循环后,所有用硅烷偶联剂处理然后用两种树脂粘结剂中的一种粘结的试样在复合材料内部显示出内聚破坏。
在 CAD/CAM 复合材料表面应用硅烷偶联剂在长期热循环后提供了树脂粘结剂与复合材料之间的最高粘结强度。