• Journal of Electrical Engineering and Technology
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• 제11권5호
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• pp.1372-1376
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• 2016

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2009년도 추계학술대회 논문집
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• pp.150-150
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• 2009

In this paper, various kinds of epoxy based nanocomposites were made and AC breakdown properties of nano-$TiO_2$ and micro-silica filler mixture of epoxy based composites were studied by sphere to sphere electrode. Moreover, nano- and micro-filler combinations were adopted as an approach toward practical application of nanocomposite insulating materials. AC breakdown test was performed at room temperature $(25^{\circ}C)$, $80^{\circ}C$ and $100^{\circ}C$. The result shows breakdown strength about non-filled, nano-scale $TiO_2$, micro-scale silica and nano-$TiO_2$, micro-silica filled epoxy composites.

• 공업화학
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• 제32권4호
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• pp.449-455
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• 2021

복합재료는 단일물질이 갖는 각각의 특성을 복합화 함으로써 우수한 물성을 갖도록 구성한 물질로 금속 및 고분자의 성능을 뛰어넘는 재료로써 각광받고 있다. 다만, 생산시간이 길고, 단가가 비싼 단점이 있어 이를 극복하기 위해 많은 연구가 진행되고 있다. 본 연구에서는 복합재료의 대량생산 시 시간을 단축할 수 있는 에폭시 수지 경화제를 개발하였고, 난연성을 부여하여 이의 적용성을 확대하고자 하였다. 기본 물질로 사용한 에폭시 수지는 bisphenol F 및 resorcinol 구조의 에폭시 2종을 사용하였으며, 난연성을 부여하기 위하여 9,10-dihydro-9-oxa-10-phosphaphenantrene-10-oxide(DOPO)를 이용하여 변성하였다. 첨가제로는 triethylphosphate (TEP) 및 bis[(5-ethyl-2-methyl-1,3,2-dioxaphosphorinan-5-yl)methyl] methyl phosphonate P,P'-dioxide (FR-001)을 사용하여 7종의 조성물을 배합하였고, 열적 특성(겔화시간, 유리전이온도), 난연 성능을 평가하여 high pressure resin transfer molding (HP-RTM) 공법에 적용 가능한 에폭시 기지재를 개발하였다.

• Composites Research
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• 제35권6호
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• pp.425-430
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• 2022

수소가스용 압력용기의 안전성 평가를 위해 다양한 내구성 시험이 요구된다. 고온 정압 시험은 고압(875 bar) 하에 고온(85℃ 이상)에서 장시간(1,000시간) 유지하여 수소 용기의 내구성을 시험하는 방법이며 승용차용 용기에 한정되어 있다. 하지만 대용량 수소버스용 용기와 관련된 고온 정압 시험의 국제 기준은 논의 초기 단계이며, 시험의 효율성 및 신뢰성 측면에서 가속시험 기준 제시 등의 현실적 보완이 필요하다. 본 연구에서는 수소버스용 내압용기의 고온 정압 시험 기준을 정립하기 위해 열적환경에 노출된 내압용기 복합재의 기계적 물성평가를 진행하였다. 복합재의 인장강도는 수지의 유리전이온도에 가까워질수록 수지의 열화로 인해 강도가 감소한다. 또한 장시간 유지 시 수지의 후경화로 인해 인장강도의 재상승을 확인할 수 있었다. 따라서 대용량 수소버스용 압력용기의 고온 정압 시험은 탄소섬유 복합재의 에폭시 수지 물성을 바탕으로 시험 조건을 설정해야 한다.

• Composites Research
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• 제36권3호
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• pp.154-161
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• 2023

본 연구에서는 경량화를 위해 금속 링크를 탄소섬유/에폭시 복합재 링크로 대체하고자 파손 기준을 이용하여 복합재 링크가 주어진 하중 조건을 견딜 수 있는지를 평가하였다. 복합재의 파손 양상을 예측하기 위해 MMF 기준을 이용하였고, 기계적 시험을 수행하여 MMF의 기준 강도 파라미터를 구하였다. 연구결과 링크의 구멍 주위에서 응력집중이 발생하였고, 특히 굽힘 하중을 받을 때 링크 끝단과 구멍 주위에서 취약함이 드러났다. 파손 지수로부터 파손 양상을 예측하였고 매트릭스 인장 파손이 링크 끝단에서, 그리고 구멍 주위에서는 섬유의 압축 파손이 예측되었다. 본 연구를 통해 확보된 방법과 결과는 경량화를 위해 금속 부품을 탄소섬유/에폭시 복합재로 대체할 때 특정 하중 조건 하에서 복합재의 안전성을 평가하는 유용한 지침으로 활용할 수 있을 것이다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2000년도 춘계학술발표대회 논문집
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• pp.149-153
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• 2000

Substituting composite structures for conventional metallic structures has many advantages because of higher specific stiffness and specific strength of composite materials. In this work, one-piece propeller shafts composed of carbonfepoxy and glass/epoxy composites were designed and manufactured for a rear wheel drive automobile satisfying three design specifications, such as static torque transmission capability, torsional buckling and the fundamental natural bending frequency. Single lap adhesively bonded joint was employed to join the composite shaft and the aluminum yoke. For the optimal adhesive joining of the composite propeller shaft to the aluminum yoke, the torque transmission capability of the adhesively bonded composite shaft was calculated with respect to bonding length and yoke thickness by finite element method and compared with the experimental result. Then an optimal design method was proposed based on the failure model which incorporated the nonlinear mechanical behavior of aluminum yoke and epoxy adhesive. From the experiments and FEM analyses, it was found that the static torque transmission capability of composite propeller shaft was maximum at the critical yoke thickness, and it saturated beyond the critical length. Also, it was found that the one-piece composite propeller shaft had 40% weight saving effect compared with a two-piece steel propeller shaft.

• Advances in materials Research
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• 제5권3호
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• pp.171-179
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• 2016

Fusion and characterization of bisphenol-A diglycidyl ether based thermosetting polymer mortars containing an epoxy resin, Fly ash and Rock sand are presented here for the Experimental study. The specimens have been prepared by means of an innovative process, in mild conditions, of commercial epoxy resin, Fly ash and Rock sand based paste. In this way, thermosetting based hybrid mortars characterized by a different content of normalized Fly ash and Rock sand by a homogeneous dispersion of the resin have been obtained. Once hardened, these new composite materials show improved compressive strength and toughness in respect to both the Fly ash and the Rock sand pastes since the Resin provides a more cohesive microstructure, with a reduced amount of micro cracks. The micro structural characterization allows pointing out the presence of an Interfacial Transition Zone similar to that observed in cement based mortars. A correlation between micro-structural features and mechanical properties of the mortar has also been studied.

• Steel and Composite Structures
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• 제35권5호
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• pp.627-634
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• 2020

The past years were marked by an increase in the use of wood waste in civil and mechanical constructions. Date palm waste remains also one of the most solicited renewable and recyclable natural resources in the composition of composite materials. In Algeria, a great amount of this type of plant wastes accumulates every year. In order to make use of this waste, a new wood-epoxy composite material based on date palm petiole particleboard is developed. It makes use of date palm petiole particleboard as reinforcement and epoxy resin as matrix. The size of the particles reinforcement are between 1~3 mm and proportion of reinforcement used is 37%. In this work, experimental and numerical studies are conducted in order to characterize the wood fibre-epoxy plates. Firstly, experimental modal analysis test was carried out to determine Young's modulus of the elaborated material. Then, in order to validate the results, compression test was conducted. Furthermore, additional information about the shear modulus of this material is obtained by performing an experimental modal analysis to extract the first torsional mode. Moreover, a finite element model is developed using ANSYS software to simulate the vibration behaviour of the plates. The results show a good agreement with the experimental modal analysis, which confirms the values of Young's modulus and shear modulus.

• Tribology and Lubricants
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• 제36권3호
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• pp.133-138
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• 2020

In this paper, we present an experimental investigation of the friction coefficient and wear area change of carbon/epoxy and E-glass/epoxy composites depending on the fiber direction (0°/90°). We compared the results of the case where the sliding direction is parallel to the fiber direction (0°) with that of the case where it is perpendicular to the fiber direction (90°). The ball-on-plate wear test equipment was used to cause wear in both directions. Two types of specimens were prepared with thicknesses of 3 mm-one made of carbon fiber reinforced plastic composite (CFRP) and the other of glass fiber reinforced plastic composite (GFRP). A normal force of 20 N was applied to the specimen and the sliding speed was 10 mm/s and the sliding distance was set to 20 m to perform the wear test. The CFRP demonstrates superior tribological characteristics compared to the GFRP. This outcome is attributed to graphitization of carbon, which serves as solid lubricating particles. In addition, both CFRP and GFRP are worn more in the 90° direction than in the 0° direction. This is due to the greater occurrence of fiber breakage and separation in the 90° direction than in the 0° direction. This study is expected to be utilized as basic data for understanding the friction and wear characteristics of CFRP and GFRP composites along the fiber direction and to apply the appropriate material.

• Composites Research
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• 제28권4호
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• pp.182-190
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• 2015

The phenomenological evolution laws of damage can be defined either based on residual life or residual strength. The failure of a specimen can be defined immediately after or before fracture. The former is called in this paper by "failure defined by approach I" and the latter "failure defined by approach II." Usually at failure there is a discontinuity of loading variables and, because of this, damage at failure is discontinuous. Therefore the values of damage at failure by two different approaches are not the same. Based on this idea the sequence effects of the phenomenological evolution law of damage given by $dD/dN=g(D)f({\Phi})$ were studied. Thin-walled graphite/epoxy tubes consisting of four of $[{\pm}45]_s$ laminates were used for the experimental study of sequence effects and the effects of mean stress on fatigue life. It was found that the sequence effects in two step uniaxial fatigue for $[{\pm}45]_s$ graphite/epoxy tubular specimen showed that a high-low block loading sequence was less damaging than a low-high one.