• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2001년도 춘계학술발표대회 논문집
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• pp.244-249
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• 2001

In this paper, we present the simultaneous measurement of the fabricaition strain and temperature during and after cure of unsymmetric composite laminate uising fiber optic sensors. Fiber Bragg grating/extrinsic Fabry-Perot interferometric (FBG/EFPl) hybrid sensors are used to measure those measurands. The characteristic matrix of sensor is analytically derived and measurements can be done without sensor calibration. A wavelength-swept fiber laser is utilized as a light source. FBG/EFPI sensors are embedded in a graphite/epoxy unsymmetric cross-ply composite laminate at different direction and different location. We perform the real time measurement of fabrication strains and temperatures at two points of the composite laminate during cure process in an autoclave. Also, the thermal strains and temperatures of the fabricated laminate are measured in thermal chamber. Through these experiments, we can provide a basis for the efficient smart processing of composite and know the thermal behavior of unsymmetric cross-ply composite laminate.

• 대한기계학회논문집A
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• 제26권6호
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• pp.1047-1052
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• 2002

The impact value, the interfacial shear strength, the tensile strength and the fracture strain of Nb/MoSi$_2$laminate composites, which were associated with the interfacial reaction layer, have been investigated. Three types of Nb/MoSi$_2$ laminate composites alternating sintered MoSi$_2$ layers and Nb foils were fabricated as the parameter of hot press temperature. The thickness of interfacial reaction layer of Nb/MoSi$_2$ laminate composites increased with increasing the fabrication temperature. The growth of interfacial reaction layer increased the interfacial shear strength and led to the decrease of impact value in Nb/MoSi$_2$ laminate composites. It was also found that in order to maximize the fracture energy of Nb/MoSi$_2$ laminate composites, interfacial shear strength and the thickness of interfacial reaction layer must be secured appropriately.

• 대한치과보철학회지
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• 제37권2호
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• pp.143-166
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• 1999

The success of porcelain laminate veneer depends on the bond strength between tooth structure and ceramic restoration and the design of tooth preparation. In particular, incisal coverage and incisal finish line are the two most important factors in long-term fracture resistance. Although the majority of clinicians are practicing incisal coverage and there are various opinions on the geo-metrical ratio between the clinical crown length of the remaining tooth structure and the length of incisal extension in porcelain laminate veneer and the optimal incisal finish lines. scientific evidence still loaves much to be desired. The purpose of this study was to determine the effects of the amounts of incisal coverage and the types of incisal finish line on the stress distribution in maxillary anterior porcelain laminate veneers under two different loading conditions. Three-dimensional finite element models of a maxillary anterior porcelain veneer with differ-ent amounts of incisal coverage ; 0, 1, 2, and 3mm and different incisal finish lines feathered edge, incisal bevel, reverse bevel and lingual chamfer with various amounts of lingual extension were developed. 300N force was applied at the point 0.5mm cervical of the linguoincisal edge in two loading conditions ; A) 125 degrees, B) 132 degrees. Tensile and compressive stress in ceramic and shear stress in the resin cement layer were analyzed using three-dimensional finite element method. The results were as follows : 1. The types of incisal finish line had more influence on the stress distribution in porcelain laminate veneer than the amounts of incisal coverage. 2. In case of no incisal coverage, incisal beveled laminate exhibited more evenly distributed tensile stress than feathered edged laminate. And in case of incisal coverage, reverse beveled laminate and lingual chamfered laminate with 1mm lingual extension exhibited more evenly distributed tensile stress than lingual chamfered laminates with 2mm and 3mm lingual extension. 3. As long as the lingual chamfer goes, less tensile stress was found at the incisal edge, while much more tensile stress was found at the lingual margin area in proportion to the length of lingual extension. 4. Under 125 degree load, tensile stress in porcelain laminate veneer had increased compared with that under 132 degree load and the difference exhibited by the change of the amount of tooth support was larger. 5. The types of incisal finish line and the distance from the incisal finish line to the loading point had more influence on the shear stress distribution in the resin cement layer than the amounts of incisal coverage. In contrast loading condition had little influence.

• 센서학회지
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• 제8권6호
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• pp.440-447
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• 1999

지능형 복합재료 구조물(Smart Composite Structures) 사용 시 부하되는 인장하중과 복합재료의 경화 시 발생하는 열하중은 복합재료 내에 삽입된 광섬유 센서의 기계적 거동에 직접적인 영향을 미친다. 게다가 복합재료의 적층 순서 및 코팅층의 유무에 따라 광섬유 센서 내의 웅력 분포는 달라지게 된다. 또한, 복합재료 적층판 내에서 발생된 균열은 적층판 전체의 파괴뿐만 아니라 광섬유 센서의 파괴에 큰 영향을 미치게 된다. 그러므로, 본 연구에서는 인장하중 및 열하중이 가해지는 복합재료 적층판 내에 삽입된 광섬유 센서의 응력분포를 유한요소해석을 통해 알아보고, 복합재료 적층판의 적층 순서에 따른 영향과 광섬유 센서에 코팅을 하였을 경우 광섬유 센서 내의 응력분포에 미치는 영향을 알아보았다. 또, 인장실험을 통하여 적층판 내에서 발생한 균열이 광섬유 센서의 파괴에 미치는 영향을 알아보았다.

• 구강회복응용과학지
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• 제28권2호
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• pp.191-200
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• 2012

도재 라미네이트 비니어(Porcelain laminate veneer, PLV)는 아주 얇은 도재를 치면에 직접 적용시키는 술식으로 전치부 심미 개선을 목적으로 전부피개관 대신에 보존적으로 사용될 수 있다. 그러나 PLV의 성공을 높이기 위해 치질 삭제량을 적절히 조절하는 것은 어려울 뿐만 아니라, 각 치아마다 법랑질 두께가 다양하고 증령에 따라 치관구조 역시 변화하기 때문에 치아 삭제시 주의가 필요하다. 즉 치아 순면을 따라 일관되게 삭제하는 기존의 방법을 이용할 경우 법랑질이 얇아진 부위에서는 상아질이 노출될 위험이 있다. 이를 방지하기 위해 다양한 치아 삭제 방법들이 소개되고 있는데 진단 납형제작을 통한 실리콘 인덱스와 아크릴릭 레진 mock-up을 이용한 방법은 최종적인 수복물의 형태에 기초하여 치아를 삭제할 수 있어 불필요한 법랑질 삭제를 줄이고 상아질 노출을 최소화할 수 있다. 또한 비정상적으로 배열된 치아 삭제시에도 적절한 삭제량 결정이 어려워 삭제량이 과도해지거나 부족해지기 쉬운데, 최종 보철물의 형태를 기준으로 실리콘 인덱스를 제작하면 이를 방지할 수 있다.

• 대한심미치과학회지
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• 제22권1호
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• pp.4-8
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• 2013

This clinical report shows the importance of selecting appropriate materials in fabricating laminate veneer restorations. Such cases should be carefully selected to ensure bonding durability, providing consistently reliable prognosis.

• Journal of Mechanical Science and Technology
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• 제14권8호
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• pp.823-829
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• 2000

[ $Nb/MoSi_2$ ]laminate composites have been successfully fabricated by hot pressing in a graphite mould. Lamination of Nb foil and $MoSi_2$ layer showed a sufficient improvement in the absorbed impact energy compared to that of monolithic $MoSi_2$ material. The impact value of $Nb/MoSi_2$ laminate composites obviously is reduced when sintered at temperatures higher than 1523K, even if the composite density contributing to impact load increased along with fabricating temperatures. Impact value of laminate composites was also drastically decreased with the growth of reaction layer after the heat treatment. However, it was effective to increase the pressure at the same sintering temperature for the improvement of the impact value.

• 대한기계학회논문집
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• 제15권2호
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• pp.611-617
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• 1991

Effective stiffness of short fiber composite with a three-dimensional random orientation of fibers is derived theoretically and compared with available experimental data. The laminate analogy and transformed laminate analogy are used for modulus prediction of 2-D and 3-D random composites, respectively. The effective stiffness of random oriented fiber composite can be expressed in terms of longitudinal and transverse stiffnesses of unidirectional composites. The result of transformed laminate analogy is more accurate than other approaches such as, Christensen-Waals equational and Lavengood-Goettler equation, etc. Also the effective properties of random oriented fiber composite can be expressed in terms of fiber and matrix properties such as elastic modulus, shear modulus and Poisson's ratio.

• 한국기계가공학회지
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• 제15권1호
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• pp.50-60
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• 2016

Laminate composites have a number of excellent characteristics in aspects of strength, stiffness, bending, and buckling. Buckling and postbuckling analysis of laminate composites with layups of [90/0]2s, $[{\pm}45/90/0]s$, $[{\pm}45]2s$ has been carried using the Total Lagrangian nonlinear Newton-Raphson method. The formulation of a geometrically nonlinear composite shell element based on a nonlinear large deformation method is presented. The used element is an eight-node degenerated shell element with six degrees of freedom. Square, circular cylinder, and arch panel laminate geometries were analyzed to verify the effects of the layups on the buckling and postbuckling behavior. The results showed that the effects of laminate layups on bucking and postbuckling behavior and the present formulation showed very good agreement with existing references.

• Composites Research
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• 제14권6호
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• pp.38-46
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• 2001

본 연구에서는, 전자파 흡수능을 가진 경사 복합재료 적층판를 설계할 수 있는 최적화 코드를 개발하였다. 또한, 유리 섬유/에폭시 직조 적층판, 알루미늄 첨가물을 함유간 유리섬유/에폭시 직조 적층판과 카본/에폭시 직조 적층판의 유전율을 구하고, 최적화 로드를 이용하여 3층형 전자파 흡수 복합재료 적층판을 개발하였다. 실험에 사용된 복합재료 적층판은 모두 전자기적으로 면내등방성을 가지며 따라서, 동축선과 망분석기를 이용하여 유전율을 측정하였다. 이 로드는 전자기적으로 직교이방성을 가지는 고분자기지 복합재료의 적층각을 포함한 다양한 변수를 고려할 수 있다.