• 구강회복응용과학지
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• 제22권4호
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• pp.329-340
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• 2006

Statement of problem: Damping of the peak force transmitted to implants has been reported by in vitro studies using impact forces on resin-veneered superstructures. Theoretical assumptions suggest that use of acrylic resin for the occlusal surfaces of a prosthesis would protect the connection between implant and bone. Therefore, the relationship between prosthesis materials and the force transmitted through the implant system also needs to be investigated under conditions that resemble the intraoral mechanical environment. Purpose: The purpose of this study was to analyze the fracture strength and modes of temporary prosthesis when a flange or occlusally extended structure were connected on the top of the abutment. Material and method: Modified abutments of winged and bulk design were made by casting the desired wax pattern which is made on the UCLA type plastic cylinder. Temporary crowns were made using templates on the modified abutments, and its fracture toughness and strain were compared to the traditional temporary prosthesis. To evaluate the effect of aging, 5.000 times of thermocycling were performed, and their result was compared to the 24hours specimen result. Results: The following conclusions were drawn from this study: 1. In the fracture toughness test, temporary crown's fracture line located next to the screw hole while modified designs with metal support showed fracture line on the metal and its propagation along the metal-resin interface. 2. Wing and bulk structure didn't show significant difference in the fracture toughness (p>0.05), but wing structure showed stress concentration on the screw hole area compared to bulk structure which showed even stress distribution. 3. In the fracture toughness test after thermocycling, wing and bulk structure showed increased or similar results in metal supported area while off-metal area and temporary crown showed decreased results. 4. In the strain measurement after thermocycling, its value increased in the temporary and bulk structure. However, wing structure showed decreased value in the loading point while increased value in the screw hole area. Conclusion: Wing type design showed compatible result to the bulk type that its application with composite resin prosthesis to the implant dentistry is considered promising.

• Restorative Dentistry and Endodontics
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• 제32권4호
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• pp.365-376
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• 2007

본 연구의 목적은 3종의 전체산부식 상아질 접착 시스템에서 적절한 산부식 시간과 접착제의 침투 능력에 대해 규명하고자 하였다. 우식이 없는 54개의 제3대구치의 상아질 표면을 5, 15, 25초 동안 산부식하고 산부식형 접착제 3종 (Scotchbond multipurpose, Single Bond, One Step) 을 도포한 후 복합레진을 충전하였다. 각 시편은 0회 (대조군) 또는 2000회 열순환 ($5^{\circ}C\;-\;55^{\circ}C$) (실험군) 후 미세인장강도를 측정하고 파단면을 관찰하여 다음과 같은 결론을 얻었다. 1. 실험군은 대조군에 비하여 결합강도가 감소하였으며, 특히 25초 산부식한 SM 및 SB군에서는 통계학적 유의차를 나타내었다. 2. 열순환 처리한 SM군과 SB군의 경우, 25초 간 산부식한 군이 5초 간 산부식한 군과 15초 간 산부식한 군에 비해 유의성 있게 낮은 결합강도를 나타냈다 (p < 0.05). 3. OS군의 경우, 산부식 시간 및 열순환 여부에 따른 유의성 있는 차이가 나타나지 않았다 (p > 0.05). 상아질 접착의 내구성은 접착제의 용매와 산부식 시간에 의해 영향을 받으며 특히, ethanol-based adhesive를 사용할 때 과도한 산부식은 유의해야 한다.

• The Journal of Advanced Prosthodontics
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• 제9권3호
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• pp.152-158
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• 2017

PURPOSE. The purpose of this study was to evaluate the influence of different coping thicknesses and veneer ceramic cooling rates on the failure load of zirconia-ceramic crowns. MATERIALS AND METHODS. Zirconia copings of two different thicknesses (0.5 mm or 1.5 mm; n=20 each) were fabricated from scanning 40 identical abutment models using a dental computer-aided design and computer-aided manufacturing system. Zirconia-ceramic crowns were completed by veneering feldspathic ceramics under different cooling rates (conventional or slow, n=20 each), resulting in 4 different groups (CONV05, SLOW05, CONV15, SLOW15; n=10 per group). Each crown was cemented on the abutment. 300,000 cycles of a 50-N load and thermocycling were applied on the crown, and then, a monotonic load was applied on each crown until failure. The mean failure loads were evaluated with two-way analysis of variance (P=.05). RESULTS. No cohesive or adhesive failure was observed after fatigue loading with thermocycling. Among the 4 groups, SLOW15 group (slow cooling and 1.5 mm chipping thickness) resulted in a significantly greater mean failure load than the other groups (P<.001). Coping fractures were only observed in SLOW15 group. CONCLUSION. The failure load of zirconia-ceramic crowns was significantly influenced by cooling rate as well as coping thickness. Under conventional cooling conditions, the mean failure load was not influenced by the coping thickness; however, under slow cooling conditions, the mean failure load was significantly influenced by the coping thickness.

• 대한치과보철학회지
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• 제31권4호
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• pp.482-505
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• 1993

The purpose of this study was to evaluate the fracture characteristics and the effect of resin bonding of laminate porcelain. In order to characterize the indentation-induced crack, Young's moduli and characteristic indentation dimensions were measured. The fatigue life under three point flexure test was measured using the electro-dynamic type fatigue machine, and the crack propagation with thermocycling was investigated on the condition of 15 second dwell time each in $5^{\circ}C\;and\;55^{\circ}C$ bath. The Vickers indentation pattern and the fracture surface were examined by an optical microscope and a scanning electron microscope (SEM). The results obtained were summarized as follows ; 1. Young's moduli(E) of the laminate porcelain and the resin cement used in this experiment were $62.56{\pm}3.79GPa$ and $15.01{\pm}0.12GPa$, respectively. 2. The initial crack size of the laminate porcelain was $69.19{\pm}5.94{\mu}m$ when an indentation load of 9.8N was applied, and the fracture toughness was $1.065{\pm}0.156MPa\;m^{1/2}$. 3. The fatigue life of laminate porcelain showed the constant fracture range at the stress level 27.46-35.30MPa. 4. When a cyclic flexure load was applied, the fatigue life of resin-bonded laminate porcelain was more decreased than that of laminate porcelain. 5. When a thermocycling was conducted, the crack growth rate of resin-bonded laminate porcelain was more increased than that of laminate porcelain. 6. Fracture surface showed the radial crack, the lateral crack, and the macroscopic crack branching region beneath the plastic deformation region when an indentation load of 9.8N was applied.

• 대한치과보철학회지
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• 제40권4호
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• pp.344-351
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• 2002

The purpose of this study is to compare tensile bond strength between Cr-Co alloy and three denture base resins after surface treatment. Following the manufacturer's instructions, 180 bonded specimens were made from three denture base resins (Lucitone 199. Paladent 20. POSS resin) and three surface treatment methods (sandblasting. metal primer. silicoating) 20 samples were made in each group and a half was ther-mocycled 1000 times between $5^{\circ}C$ and $55^{\circ}C$. The tensile bond strength was measured using an Instron with 5mm/min crosshead speed. Data was analyzed with one-way ANOVA, T-test and Duncan test. The results were as follows : 1. Samples with metal primer coating had significantly high tensile bond strength than the other surface treated groups (p<.05). Significantly low tensile bond strength was shown in sand blasted groups (p<.05). 2. No significant difference was observed in metal primer coating groups before and after ther-mocycling (p>.05) 3. Tensile bond strength was decreased in silicoated samples after thermocycling (p<.05). 4. Of the surface treated groups with metal primer, Lucitone 199 had the greatest bond strength and POSS resin and Paladent 20 were followed (p<.05). 5. Of the surface treated groups with silicoating, POSS resin and Lucitone 199 had greater bond strength than Paladent 20 (p<.05).

• 대한치과교정학회지
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• 제53권3호
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• pp.139-149
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• 2023

Objective: To assess the color stability and translucency of full cubic stabilized zirconia (FSZ) following orthodontic bonding with different surface treatments and coffee thermocycling (CTC). Methods: This in vitro study was conducted on 120 disc-shaped specimens of FSZ. Thirty specimens were selected as the control group and remained intact. The remaining specimens were randomly divided into three groups based on the type of surface treatment (n = 30): airborne particle abrasion (APA), silica-coating (CoJet), and carbon dioxide (CO₂) laser. After metal bracket bonding in the test groups, debonding and polishing were performed. Subsequently, all specimens underwent CTC (10,000 cycles). Color parameters, color difference (ΔE₀₀), and translucency parameter (TP) were measured three times at baseline (t0), after debonding and polishing (t1), and after CTC (t2). Data were statistically analyzed (α = 0.05). Results: Significant difference existed among the groups regarding ΔE₀₀t0t2 (p < 0.001). The APA group showed minimum (ΔE₀₀ = 1.15 ± 0.53) and the control group showed maximum (ΔE₀₀ = 0.19 ± 0.02) color stability, with no significant difference between the laser and CoJet groups (p = 0.511). The four groups were significantly different regarding ΔTPt0t2 (p < 0.001). Maximal increases in TP were noted in the CoJet (1.00 ± 0.18) and APA (1.04 ± 0.38) groups while minimal increase was recorded in the control group (0.1 ± 0.02). Conclusions: Orthodontic treatment makes zirconia restorations susceptible to discoloration and increased translucency. Nonetheless, the recorded ΔE₀₀ and ΔTP did not exceed the acceptability threshold.

• 대한치과보철학회지
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• 제51권2호
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• pp.73-81
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• 2013

연구 목적: 이 연구의 목적은 지르코니아 표면처리에 따른 3종의 레진시멘트와 지르코니아의 전단결합강도를 평가하기 위함이다. 연구 재료 및 방법: 총 143개의 디스크 모양의 지르코니아 블록(HASS Co., Gangneung, Korea) 시편을 제작하고 총 13개군(n=11)으로 나누었다. 그중9개군은 표면처리 방식(1. 알루미나 분사, 2. 알루미나 분사와 지르코니아 라이너의 도포, 3.알루미나 분사와 Rocatec (3M ESPE, Seefeld, Germany) 처리) 및 사용한 3종류의 레진시멘트(Bistite II (Tokuyama Dental Co., Japan), Panavia F2.0 (Kuraray Medical, Japan), Super-bond C&B (Sun Medical, Japan))에 따라 나누어 열순환처리 전 접착강도 실험을 시행하였다. 열순환처리 전 접착강도 실험은 위 3종류의 레진시멘트를 3가지 방법으로 표면처리한 지르코니아 시편에 접착하고, 상온의 증류수에 24시간 동안 보관한 후, 전단결합강도를 측정하였다. 열순환처리 후 접착강도 실험은, 열순환처리 전 접착강도 실험에서 우수한 전단결합강도를 보인 지르코니아 표면처리군(알루미나 분사와 Rocatec 처리를 하고 3종류의 레진시멘트를 접착한 3개의 군)과 대조군으로 알루미나만으로 표면처리 후 Super-bond C&B를 접착한 1개의 군을 대상으로 $5^{\circ}C$와 $55^{\circ}C$사이에서 5,000회 열순환처리를 시행하고 전단결합강도를 측정하였다. 결과: 열순환처리 전 접착강도 실험에서는 알루미나 분사와 Rocatec 처리를 한 지르코니아 표면에 Super-bond C&B를 접착한 군이 가장 높은 전단결합강도를 보였다. Super-bond C&B를 사용한 군이 다른 시멘트 군보다 유의성 있게 높은 전단결합강도를 보였으며, 지르코니아 표면에 Rocatec 처리를 한 군이 다른 표면처리를 한 군보다 유의성 있게 높은 전단결합강도를 보였다. 열순환처리를 한 후에는, Rocatec 처리를 한 지르코니아 표면에 Super-bond C&B를 접착한 군만이 유일하게 전단결합강도가 증가하였으며, 다른 모든 군에서는 전단결합강도가 감소하였다. 결론: 본 실험에서는 Super-bond C&B 시멘트가 가장 높은 전단결합강도를 보였으며, Rocatec 시스템은 레진시멘트와 지르코니아의 전단결합강도를 향상시키는 방법이 될 것이라고 사료된다.

• Journal of Korean Dental Science
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• 제8권2호
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• pp.49-56
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• 2015

Purpose: The effect of accelerated aging on color stability of various dual-cured self-adhesive resin cements were evaluated in this study. Materials and Methods: Color stability was examined using three different brands of dual-cured self-adhesive resin cements: G-CEM LinkAce (GC America), MaxCem Elite (Kerr), and PermaCem 2.0 (DMG) with the equivalent color shade. Each resin cement was filled with Teflon mold which has 6 mm diameter and 2 mm thickness. Each specimen was light cured for 20 seconds using light emitting diode (LED) light curing unit. In order to evaluate the effect of accelerated aging on color stability, color parameters (Commission Internationale de l'Eclairage, CIE $L^*$, $a^*$, $b^*$) and color differences (${\Delta}E^*$) were measured at three times: immediately, after 24 hours, and after thermocycling. The $L^*$, $a^*$, $b^*$ values were analyzed using Friedman test and ${\Delta}E^*$ values on the effect of 24 hours and accelerated aging were analyzed using t-test. These values were compared with the limit value of color difference (${\Delta}E^*=3.7$) for dental restoration. One-way ANOVA and Scheff's test (P<0.05) were performed to analyze each ${\Delta}E^*$ values between cements at each test period. Result: There was statistically significant difference in comparison of color specification ($L^*$, $a^*$, $b^*$) values after accelerated aging except $L^*$ value of G-CEM LinkAce (P<0.05). After 24 hours, color difference (${\Delta}E^*$) values were ranged from 2.47 to 3.48 and $L^*$ values decreased and $b^*$ values increased in all types of cement and MaxCem Elite had high color stability (P<0.05). After thermocycling, color change's tendency of cement was varied and color difference (${\Delta}E^*$) values were ranged from 0.82 to 2.87 and G-CEM LinkAce had high color stability (P<0.05). Conclusion: Color stability of dual-cured self-adhesive resin cements after accelerated aging was evaluated and statistically significant color changes occurred within clinically acceptable range.

• 한국토양동물학회지
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• 제5권2호
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• pp.119-123
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• 2000

변온조건이 파밤나방 (Spodoptera exigua (H bner)) 유충과 영의 발육에 미치는 영향이 분석되어졌다. 정온조건에서 사육하였을 때 발육영점온도는 발육태와 유충영기에 따라 다르지만 평균 13$^{\circ}C$로 추정되었다. 이 발육영점온도를 기준으로 동등한 일일유효온도를 갖는 세 가지 다른 발육 온도조건을 설정하였다. 정온조건에 비해 변온조건은 발육속도를 뚜렸하게 변화시켰다. 동일한 최고온도(2$0^{\circ}C$)를 가졌던 두 가지 일일 변온조건중에서 저온기간이 상대적으로 높았던 조건(1$0^{\circ}C$)은 발육속도를 촉진시킨 반면 저온기간의 온도가 낮았던 조건(5$^{\circ}C$C)은 오히려 저해효과를 나타냈다.

• 대한소아치과학회지
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• 제34권3호
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• pp.359-369
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• 2007

본 연구는 다양한 순환 및 시효 조건 하에서 제V급 복합레진 수복물의 표면전색이 미세변연누출에 미치는 효과에 대해 알아보고자 하였다. 100개의 건전한 소구치의 협면에 제V급 와동을 형성하고 제조사의 지시대로 광중합형 복합레진으로 수복하였다. 무작위로 나누어 표면전색을 시행하지 않는 I군과 표면을 산부식 후 표면전색을 시행한 II군으로 설정한 후 열순환(thermocycling)을 하였다. 각 군에서 하위군(A군= 열순환 외 다른 시효조건이 없는 군, B군=칫솔질군, C군=부하순환군, D군=칫솔질과 부하순환을 모두 시행한 군, E군=6개월간 증류수에 보관한 군)으로 나누어 각각에 맞는 시효조건을 시행하였다. 2% methylene blue 용액에 침윤시켜 변연의 미세누출정도를 평가하여 다음과 같은 결과를 얻었다. 1. 표면전색을 시행하지 않은 군의 교합변연과 치은변연에서 시효조건에 따른 미세누출의 유의한 차이는 보이지 않았다(p>0.05). 2. 표면전색을 시행한 군의 교합변연에서는 시효조건에 따른 미세누출의 유의한 차이가 없었다(p>0.05). 3. 표면전색을 시행한 군의 치은변연에서는 부하순환이나 6개월간 증류수에서 보관하는 시효과정을 거친 군에서 미세누출이 유의하게 크게 나타났다(p<0.05). 4. 시효조건이 없는 군과 칫솔질군의 경우, 표면전색을 시행한 군이 표면전색을 시행하지 않은 군에 비해 유의하게 적은 미세누출결과를 보였다(p<0.05). 5. 부하순환을 시행한 군과 6개월간 증류수에서 보관한 경우에는 표면전색을 시행한 군과 표면전색을 시행하지 않은 군 사이에 미세누출의 차이가 있었지만 유의차가 없었다(p>0.05). 따라서 이 연구의 결과는 변연부분의 미세간격으로 침투한 표면전색제가 처음에는 미세누출을 감소하는데 효과를 보여주었으나, 교합시 교두가 휘어져서 생기는 응력과 장기간의 수분흡수로 인한 변화를 견디기에 불충분함을 보여주었다.