• 한국철도학회논문집
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• 제12권4호
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• pp.590-596
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• 2009

본 연구에서는 탄소, 유리, 케블라 및 탄소-케블라 하이브리드 섬유로 제작된 원형튜브를 이용하여 각 소재별 에너지 흡수특성과 파손메커니즘을 규명하였다. 이를 위해 각 튜브에 대한 10mm/min의 준정적 압축시험을 수행하였다. 시험결과 탄소섬유 튜브가 가장 에너지 흡수특성이 우수했으며 탄소-케블라 하이브리드 섬유 튜브가 가장 낮은 에너지 흡수율을 보였다. 또한, 각 소재별 에너지 흡수메커니즘을 분석한 결과 탄소 및 유리섬유튜브는 취성파괴 모드로 압축되었다. 또한, 케블라 섬유 튜브는 국부좌굴에 의한 접힘모드가 지배적이고, 탄소와 케블라 하이브리드 섬유 튜브의 경우 단층굽힘과 국부좌굴모드가 혼합되어 나타났다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2000년도 추계학술발표대회 논문집
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• pp.115-118
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• 2000

The development of high-strength fibers such as boron/epoxy and carbon/epoxy and adhesives has made it possible to repair cracked metallic plates by bonding reinforcing patches to the plate over the crack. In this study, aluminum 6061-T6 alloy plates with the high strength are applied to specimens with a cracked bolt hole to study the effect of diverse patch materials on the fatigue behavior of this structure. Additionally, the observation of the effort of different patch sizes on the specimen was performed. The results shows that the patch repair can improve the static strength by about 17% and the fatigue life by 200% compared with non-repaired case. And it was also revealed that the patching method along to crack growth direction is mort efficient in cost and weight reduction.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2005년도 추계학술대회 논문집
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• pp.1037-1041
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• 2005

It is well-known that the corrosive behavior of PMC (polymer matrix composite) structure is much better than the metal structure in the marine environment. The understanding of fracture behavior of PMC in the deep-sea environment is essential to expand its use in the marine industry. For a present study, fracture tests have been performed under four different pressure levels such as 0.1 MPa, 100 MPa, 200 MPa, and 270 MPa using the seawater-absorbed carbon/epoxy composite samples. Fracture toughness was determined from the work factor approach as a function of hydrostatic pressure. It was found that fracture behavior was a linear elastic for all pressure levels. The fracture toughness increased with increasing pressure.

• 한국재료학회:학술대회논문집
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• 한국재료학회 1992년도 추계학술발표강연 및 논문개요집
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• pp.134-137
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• 1992

• Composites Research
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• 제32권6호
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• pp.349-354
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• 2019

복합재료 중심인장선의 구성은 강화재로 사용되는 탄소섬유 및 유리섬유와 기지재로 사용되는 속경화 열경화성 에폭시로 되어있다. 본 연구에서는 가공송전선의 복합소재 중심인장선(ACCC)에 사용되는 에폭시 경화물에 대하여 분석하였다. 다관능성 에폭시 중 4관능성 에폭시(PA 806)을 사용하고 MNAn, HHPA 두가지 경화제 및 경화 촉진제를 사용하여 에폭시 경화물을 만들고 이를 분석하였다. 경화제의 종류 및 경화 촉진제의 함량에 따른 최적조건을 도출하였다.

• 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.

• Composites Research
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• 제28권1호
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• pp.1-5
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• 2015

In this paper the influence of fiber orientation of basalt and carbon inter-ply fabrics on the flexural properties of hybrid composite laminates was experimentally investigated. Four types of basalt/carbon/epoxy inter-ply hybrid composite laminates with varying angle ply orientation of reinforced basalt fiber and fixed orientation of carbon fiber were fabricated using hand lay-up technique. Three point bending test was performed according to ASTM 7264. The fracture surface analysis was carried out by scanning electron microscope (SEM). The results obtained from the four laminates were compared. Lay-up pattern of $[0B/+30B/-30B/0C]_S$ exhibits the best properties in terms of flexural strength and flexural modulus. Scanning electron microscopy results on the fracture surface showed that the interfacial de-bonding between the fibers and epoxy resin is a dominant fracture mode for all fiber lay-up schemes.

• 수산해양교육연구
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• 제9권2호
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• pp.188-197
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• 1997

The fracture toughness of three different kinds of epoxy-matrix composites containing the same volume fraction of reinforcement and the variation of fracture toughness of glass-carbon fiber/epoxy hybrid composites due to the change of test temperature and different glass fiber content were investigated in this study. Glass fiber/epoxy composite provided much higher fracture toughness than that of other composites because of the high strain at failure of glass fiber. Particularly the carbon fiber/epoxy composite exhibited the low fracture toughness caused by the low strain energy absorbing capacity of carbon fiber. And it was found that the strain at failure of reinforcement and interfacial delamination absorbing a significant amount of impact energy played an important role to increase fracture toughness of composites. The fracture toughness of the glass-carbon fiber hybrid composites increased with increasing the glass fiber content and decreased with raising the test temperature. The residual stress arising from the different thermal expansion between the matrix and reinforcement influenced the fracture toughness of composites.

• 대한기계학회논문집A
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• 제24권2호
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• pp.338-346
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• 2000

Although the net-shape molding of composites is generally recommended, molded composites are frequently required cutting or grinding due to the dimensional inaccuracy for precision machine elements . During the composite machining operations such as cutting and grinding, the temperature at the cutting point may increase beyond the allowed limit due to the low thermal conductivity of composites, which might degrade the matrix of composite. Therefore, in this work, the temperature at the cutting point during cut-off grinding of carbon fiber epoxy composites was measured. The cutting force and surface roughness were also measured to investigate the cut-off grinding characteristics of the composites. The experiments were performed both under dry and wet grinding conditions with respect to cutting speed and feed rate. From the experimental investigation, the optimal conditions for the composite cut-off grinding were suggested.

• 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.