• 폴리머
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• 제31권2호
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• pp.123-129
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• 2007

세 종류의 폴리올레핀 복합재료의 기계적인 특성과 파괴인성 메커니즘이 연구되었다. 기계적 특성을 조사하기 위해 인장 시험 및 아이조드 충격 시험이 수행되었다. 균열 선단 주위의 파손 메커니즘을 정확히 조사하기 위해 2노치-4점 굽힘 기법이 도입/적용되었다. 광학현미경과 투과형 전자현미경을 이용하여, 폴리올레핀 복합재료의 균열 선단 주변 국부적인 파괴인성 특성들이 관찰되었다. 이를 통한 구체적인 관찰은, 폴리올레핀 복합재료의 균열선단 주변에 전단밴딩, 크레이즈, 입자-수지간 분리, 고무입자의 캐비테이션, 크랙 휭 및 크랙 분기 등과 같은 다양한 파괴인성 메커니즘들이 존재함을 보여주었다. 이러한 파괴인성 메커니즘들은 아이조드 충격 시험에서 보여진 파괴인성 값의 증가에 대한 실질적인 원인으로 보여진다. 본 연구를 바탕으로, 2노치-4점 굽힘 기법은 폴리올레핀 복합재료의 파괴 거동과 그와 관련된 파괴인성 메커니즘을 기술할 수 있는 충분한 정보를 제공하였다.

• 대한기계학회논문집A
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• 제20권3호
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• pp.832-842
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• 1996

Fatigue life prediction and fatigue behavior of circular notched carbon fiber reinforced plastic laminates are presented. Point and average stress criteria by Whitney and Nuismer are generalized to fatigue fracture criteria for notched laminates. Residual strength degradation model and the assumptions on the stress redistribution are introduced during the derivation of prediction equations. S-N curve, Basquin's relation, and H and H's FLPE1 are chosen for evaluation of residual strength of unnotched laminates and six prediction equations are derived. Experiments are performed using Graphite/Epoxy laminates whose fiber orientation is $[0$^\circ$/+45$^\circ$/-45$^\circ$/90$^\circ$]s. Presented prediction equations are reasonably close to experimental data and proposed appoach is found to be suitable to predict fatigue life of notched composite laminates.

• 대한기계학회논문집
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• 제16권7호
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• pp.1285-1293
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• 1992

본 연구에서는 glass/epoxy 직조된 복합재료에 있어서 원공 및 판폭의 크기가 노치강도에 미치는 영향을 명확히 하고, 또한 노치강도 및 파괴조건과 위에서 언급한 특성길이와의 관계를 검토하였다.

• 대한기계학회논문집
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• 제8권5호
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• pp.425-434
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• 1984

본 연구에서는 ［0˚/90˚］$_{2s}$, Gr/Gp 복합 적층판에 대해서 접착면의 비율과 폴리에스테르 필름의 구멍의 형상이 적층판의 인장 성질과 파괴인성에 미치는 영향에 대한 실험적인 결과를 얻고자 한다.다.

• 대한치과의사협회지
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• 제48권4호
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• pp.297-307
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• 2010

Noncarious cervical lesions(NCCLs) are characterized as structural defects found on the tooth surface of the cement-enamel junction. Loss of tooth structure through noncarious mechanisms may vary in etiology and clinical presentation for each individual but presently many clinician now classify this as tooth failure of abfraction due to the stress applied in the cervical area of the tooth under oral physiological and pathological loads. In the current study, we investigated the stress distribution of maxillary premolar with NCCL using simulated 3D finite element analysis. The results were as follows: 1. In the sound maxillary premolar, the stresses were highly concentrated at cervical enamel surface of the mesiobuccal line angle, asymmetrically. 2. Once the lesion has been formed, the highest stress concentration was observed around the apex of the wedge shaped lesion. 3. In four types of NCCL, the patterns of stress distribution were similar and the peak stress was observed at mesial corner and also stresses concentrated at lesion apex. 4. Lesion cavity modification of rounding apex, reduced stress of lesion apex. 5. When restoring the notch-shaped lesion, material with high elastic modulus worked well at the lesion apex and material with low elastic modulus worked well at the cervical cavosurface margin.

• Steel and Composite Structures
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• 제42권4호
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• pp.553-568
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• 2022

This paper explored the viability of utilising titanium alloy bolts in the construction industry through an experimental programme, where a total of sixty-six titanium alloy (Ti/6Al/4V) bolts were tested under axial tension, pure shear and combined tension and shear. In addition, a series of Charpy V-notch specimens machined from titanium alloy bolts, conventional high-strength steel bolts, austenitic and duplex stainless steel bolts were tested for impact toughness comparisons. The obtained experimental results demonstrated that the axial tensile and pure shear capacities of titanium alloy bolts can be reasonably estimated by the current design standards for steel structures (Eurocode 3, AS 4100 and AISC 360). However, under the combined tension and shear loading conditions, significant underestimation by Eurocode 3 and unsafe predictions through AS 4100 and AISC 360 indicate that proper modifications are necessary to facilitate the safe and economic use of titanium alloy bolts. In addition, numerical models were developed to calibrate the fracture parameters of the tested titanium alloy bolts. Furthermore, a design-based selection process of titanium alloy bolts in the structural applications was proposed, in which the ultimate strength, ductility performance and corrosion resistance (including galvanic corrosion) of titanium alloy bolts was mainly considered.

• Composites Research
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• 제32권1호
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• pp.65-70
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• 2019

항공기 복합재료 날개 구조는 대부분 접착 혹은 패스너로 체결되어 있는데, 이러한 적층 구조 복합재료는 층간 강도가 취약하여 층간 분리가 일어나기 쉽다. 이러한 적층 복합재료의 단점을 보완하기 위해 두께 방향의 섬유를 보강한 3차원 직조형 복합재료를 통하여 강도, 손상 내구성, 충격 및 피로 하중을 향상시킬 수 있다. 또한, 자동화된 직조 공정에 의하여 단일 구조 near-net-shape의 프리폼 제조가 가능하기 때문에 공정 단축, 체결 부품 감소로 복합재료 전체 가격을 절감할 수 있다. 따라서 본 연구에서는 3차원 직조형 복합재료의 항공기 구조물 적용 가능성을 확인하기 위하여 3차원 프리폼의 기본적인 구조인 orthogonal(ORT), layer-to-layer(LTL), through-the-thickness(TTT) 패턴을 직조하고 이를 복합재료로 성형하여 압축 시험, 인장 시험, Open-hole 인장 시험을 하였다. 이 중 orthogonal 직조 복합재료가 인장 및 압축 탄성계수와 강도 모두 가장 높았으며 노치 민감도에서도 orthogonal 복합재료가 일방향 적층복합재료나 패브릭 적층 복합재료에 비하여 가장 우수한 특성을 보였다.

• Restorative Dentistry and Endodontics
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• 제26권4호
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• pp.332-340
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• 2001

Flowable composite resin has lower filler content, increased flow, and lower modules of elasticity. It is suggested that flowable composite resin can be bonded to the tooth structure intimately and absorb or dissipate the stress. Therefore, it may be advantageous to use flowable composite resin for the base material of class II restoration and for the class V restoraton. The purpose of this study was to evaluate the microleakage and shear bond strength of four flowable composite resins (Aeliteflo, Flow-It, Revolution, Ultraseal XT Plus) compared to Z100 using Scotchbond Multi Purpose dentin bonding system. To evaluate the microleakage, notch-shaped class V cavities were prepared on buccal and lingual surfaces of 80 extracted human premolars and molars on cementum margin. The teeth were randomly divided into non-thermocycling group (group 1) and thermocycling group (group 2) of 40 teeth each. The experimental teeth of each group were randomly divided onto five subgroups of eight samples (sixteen surfaces). The Scotchbond Multi-Purpose and composite resin were applied for each group following the manufacturer's instructions. the teeth of group 2 were thermocycled five hundred times between 5$^{\circ}C$ and 55$^{\circ}C$. The teeth of group 2 were placed in 2% methylene blue dye for 24 hours, then rinsed with tab water. The specimens were embedded in clear resin, and sectioned longitudinally with a diamond saw. The dye penetration on each of the specimen were observed with a stereomicioscope at $\times$20 magnification. To evaluate the shear bond strength, 60 teeth were divided into five groups of twelve teeth each. The experimental teeth were ground horizontally below the dentinoenamel junction, so that no enamel remained. After applying Scotchbond Multi-Purpose on the dentin surface, composite resin was applied in the shape of cylinder. The cylinder was 4mm in diameter and 2mm in thickness. Shear bond strength was measured using Instron with a cross-head speed of 0.5mm/min. After shear bond strength measurement, mode of failure was evaluated with a stereomicroscope at $\times$30 magnification. All data were statistically analyzed by One Way ANOVA and Student-Newman-Keuls method. The correlation between microleakage and shear bond strength was analyzed by linear regression. The results of this study were as follows ; 1. In non-thermocycling group, the leakage value of Z100 was significantly lower than those of flowable composite resins at the enamel and dentin margin, margin, except that Revolution showed the lower leakage value than that of Z100 at the dentin margin (p<0.05). 2. In thermocycling group, the leakage values of Z100 and Ultraseal XT Plus were lower than those of other subgroup at the enamel and dentin margin, except that Flow-It showed the lower leakage value than that of Ultraseal XT Plus at the dentin margin (p<0.05). 3. The leakage value of Z100 and Ultraseal XT Plus in thermocycling group were not higher than that in non-thermocycling group at the enamel margin. The leakage value of Z100 in thermocycling group was not higher than that in non-thermocycling group at the dentin margin (p<0.05). 4. As for the shear bond strength measurement, there were no statistically significant differences among groups (p<0.05). The shear bond strengths given in descending order were as follows: Z100(16.81$\pm$2.98 MPa), Flow-It(14.8$\pm$4.43 MPa), Aeliteflo(14.34$\pm$3.69 MPa), Revolution(13.46$\pm$4.23 MPa), Ultraseal XT Plus(12.83$\pm$3.16 MPa). 5. Failure modes of all specimens were adhesive failures. 6. There was no correlation between microleakage and shear bond strength.

• Restorative Dentistry and Endodontics
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• 제27권2호
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• pp.142-149
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• 2002

Low-viscosity composite resins may produce better sealed margins than stiffer compositions (KempScholte and Davidson, 1988: Crim, 1989). Plowable composites have been recommended for use in Class V cavities but it is also controversial because of its high rates of shrinkage. On the other hand, in the study comparing elastic moduli and leakage, the microfill had the least leakage (Rundle et at. 1997) Furthermore, in the 1996 survey of the Reality Editorial Team, microfills were the clear choice for abfraction lesions. The purpose of this study was to evaluate the microleakage of 6 compostite resins (2 hybrids, 2 microfills, and 2 flowable composites) with and without load cycling. Notch-shaped Class V cavities were prepared on buccal surface of 180 extracted human upper premolars on cementum margin. The teeth were randomly divided into non-load cycling group (group 1) and load cycling group (group 2) of 90 teeth each. The experimental teeth of each group were randomly divided into 6 subgroups of 15 samples. All preparations were etched, and Single bond was applied. Preparations were restored with the following materials (n=15) : hybrid composite resin [Z250(3M Dental Products Inc. St. Paul, USA), Denfil(Vericom, Ahnyang, Korea)], microfill [Heliomolar RO(Vivadent, Schaan, Liechtenstein), Micronew(Bisco Inc. Schaumburg, IL, USA)], and flowable composite［AeliteFlo(Bisco Inc. Schaumburg, IL, USA), Revolution(Kerr Corp. Orange, CA, USA)]. Teeth of group 2 were subjected to occlusal load (100N for 50,000 cycles) using chewing simulator(MTS 858 Mini Bionix II system, MTS Systems Corp. Minn. USA). All samples were coated with nail polish 1mm short of the restoration, placed in 2％ methylene blue for 24 hours, and sectioned with a diamond wheel. Enamel and dentin/cementum margins were analyzed for microleakage on a sclale of 0 (no leakage) to 3 (3/3 of wall). Results were statistically analyzed by Kruscal-Wallis One way analysis, Mann-Whitney U-test, and Student-Newmann-Keuls method. (p = 0.05) Results : 1. There was significantly less microleage in enamel margins than dentinal margins of all groups (p＜0.05) 2. There was no significant between six composite resin in enamel margin of group 1. 3. In dentin margin of group 1, flowable composite had more microleakage than others but not of significant differences. 4. there was no significant difference between six composite resin in enamel margin of group 2. 5. In dentin margin of group 2, the microleakage were R＞A =H=M＞D＞Z. But there was no significant differences. 6. In enamel margins, load cycling did not affect the marginal microleakage in significant degree. 7. In enamel margins, load cycling did affect the marginal microleakage only in Revolution. (p＜0.05).

• 대한치과보존학회:학술대회논문집
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• 대한치과보존학회 2008년도 Spring Scientific Meeting(the 129th) of Korean Academy if Conservative Dentistry
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• pp.246-257
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• 2008

이 연구의 목적은 3차원 유한요소분석법을 사용하여 교합력의 위치와 방향이 상악 제2소구치의 치경부 복합레진 수복물의 응력분포에 미치는 영향에 대해 평가해 보고자 하였다. 발치된 상악 제2소구치를 이용하여 micro-CT (SkyScan1072; SkyScan, Aartselaar, Belgium)로 스캔한 후 HyperMesh Ver 6.0 (Altair Engineering, Inc., Troy, USA)와 3D-DOCTOR (Able Software Co., Lexington, MA, USA)로 3차원 유한요소 모형을 제작하였다. 제작된 소구치 모형에 쐐기형 와동을 형성하고 탄성계수가 서로 다른 혼합형 복합레진과 흐름성 복합레진으로 각각 수복하였다. 수복 후 설측교두의 협측사면 세 위치에 각각 수직, 20도, 40도의 각도로 하중을 가한 후 응력분포를 ANSYS Ver 9.0 (Swanson Analysis Systems. Inc., Houston, USA) 프로그램을 이용하여 인장 응력의 분포를 분석한 바 하중 위치와 관계없이 하중방향의 각도가 증가할수록, 또한 수복재료의 탄성 계수가 높을수록 인장응력도 증가하는 것으로 보아 교합력의 방향과 수복재료의 탄성계수가 치경부 수복물의 응력분포에 중요한 영향을 미치는 요소로 사료된다.