• Advanced Composite Materials
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• 제17권3호
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• pp.225-233
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• 2008

The analysis in this paper is focused on the pattern of mixing of filaments over a cross-section of hybrid yarns according to different combinations of reinforcement and matrix filament yarns through microscopic view. The volume content of filament in hybrid yarn cross-section was maintained at 50% for both reinforcement and matrix, and the hybrid yarns count at 600 tex throughout the experiments. It was observed from the experiments that diameters of reinforcement and matrix filaments have strong effects particularly on the pattern of mixing of filaments over a cross-section of hybrid yarns such that the hybrid yarns with more or less equal diameters of reinforcement and matrix filaments showed considerably even distributions over the hybrid yarn cross-section. This paper also investigates the possibility of hybridizing carbon/aramid, carbon/glass and aramid/glass matrices through the commingling process. In the experiment, several process parameters were selected and they include pressure, yarn oversupply-rate and different nozzle types. As a result of these experiments, it was concluded that the hybridized materials show better performance than individual reinforced filament yarns in terms of mechanical properties. For small tensile forces, the carbon/glass/matrix combination turned out to be good enough for general purpose applications.

• Elastomers and Composites
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• 제44권3호
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• pp.299-307
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• 2009

본 연구는 자동차 엔진의 구동을 각종 부대 장치로 전달하는데 사용되는 V-rib 벨트 재료의 내열성 및 내마모성을 향상시키기 위한 연구이다. 이를 위하여 고무 매트릭스는 EPDM과 CR, 그리고 충전제로 ZnO, 면 및 아라미드 섬유의 함량을 달리한 시편과 v-벨트를 만들어 내열성과 내마모성 그리고 기계적 성질을 조사하였다. CR 배합계에서 ZnO의 함량이 증가함에 따라 내마모성이 증가하였다. 또한 면섬유의 함량이 증가함에 따라 벨트상태에서 견딜 수 있는 구동시간은 증가하지만 내마모성은 감소하는 결과를 보였다. EPDM 배합계에서 면섬유의 충전한계는 30 phr정도였다. 또한 아라미드와 면섬유를 혼합 사용한 결과 구동시간과 내마모성을 동시에 증가시킬 수 있었으며, 그 단섬유의 최적 조성은 아라미드섬유/면섬유 비율이 1/5인 것으로 조사되었다. 동일한 면섬유 함량에서 EPDM 배합계 가 CR 배합계보다 우수한 물성을 보였다.

• 대한전기학회논문지:전기물성ㆍ응용부문C
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• 제51권9호
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• pp.430-435
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• 2002

The $SF_{6}$ gas insulated power equipments have the insulation systems which are composed of $SF_{6}$ gas and insulation paper. It is repored that their insulation abilities are influenced by the $SF_{6}$ gas gaps in those insulation systems and gas pressures. This paper describes partial discharge phenomena with $SF_{6}$ gas pressures in insulation system of $SF_{6}$ gas-insulation paper Specimens of $SF_{6}$ gas-insulation paper were prepared and aramid paper was used as insulation paper. Partial discharge inception voltages(PDIV) and breakdown voltages for the existence of $SF_{6}$ gas gaps were measured by short term tests with gas pressures. Also, average PD quantities and pulse counts, life times of each specimens were calculated from the results of long term aging tests with gas pressures. It was found that the $SF_{6}$ gas gaps decrease increasing rates of PDIV and brealdown voltages according to gas pressure increase and the insulation breakdown caused by the smaller PD quantities than 1[pC] at the high gas pressure of 300kPa is due to the increase of energy density with increase of gas pressure.

• 한국재료학회지
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• 제4권7호
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• pp.733-740
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• 1994

페놀수지 결합재에 보강섬유의 종류에 따라서 내염섬유 보강 복합재(OFRP), 탄소섬유 보강 복합재(CFRP), 유리섬유 보강 복합재(GFRP), 아라미드 섬유 보강 복합재(AFRP)를 제조하였다. 각 보강섬유의 분율을 달리함에 따라 마찰계수 및 마모율을 측정하여 각 보강섬유의 특성이 미치는 영향을 관찰하였다. 아라미드의 섬유량이 45tw%일 때 평균 마찰계수가 0.353-0.383으로 가장 높게 나타난 반면에 핏치계 탄소섬유를 45wt% 보강한 경우 0.164-0.190으로 가장 낮게 나타났다. AFRP와 CFRP의 마모율은 낮게 나타내었으며, GFRP와 OFRP는 섬유분율이 증가함에 따라 급격히 증가하는 양상을 보였다. OFRP는 마모 diagram이 불안정하였으며 CFRP와 AFRP는 대체적으로 안정한 형태를 나타내었다. GFRp는 상당히 불안정한 마모diagram을 나타낸 것으로 보아 마찰 안정성이 가장 떨어짐을 알 수 있었다.

• 한국재료학회지
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• 제29권1호
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• pp.43-51
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• 2019

Nacre of abalone shell features a "brick-and-mortar" microstructure, in which micro-plates of calcium carbonate are bonded by nanometers-thick layers of chitin and proteins. Due to the microstructure and its unique toughening mechanisms, nacre possesses an excellent combination of specific strength, stiffness and toughness. This study deals with the possibility of using nacre fragments obtained from abalone shell for making a bulletproof armor system. A composite plate laminated with abalone shell fragments is made and compression and bend tests are carried out. In addition, a bulletproof test is performed with hybrid armor systems which are composed of an alumina plate, a composite plate, and aramid woven fabric to verify the ballistic performance of nacre. The compressive strength of the composite plate is around 258.3 MPa. The bend strength and modulus of the composite plate decrease according to the plate thickness and are about 149.2 MPa and 50.3 GPa, respectively, for a 4.85 mm thick plate. The hybrid armor system with a planar density of $45.2kg/m^2$, which is composed of an 8 mm thick alumina plate, a 2.4 mm thick composite plate, and 18 layers of aramid woven fabric, satisfy the NIJ Standard 0101.06 : 2008 Armor Type IV. These results show that a composite plate laminated with abalone shell fragments can be used for a bulletproof armor system as an interlayer between ceramic and fabric to decrease the armor system's weight.

• Composites Research
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• 제37권3호
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• pp.186-189
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• 2024

본 연구는 나노필러가 혼합된 열가소성 탄소섬유강화 복합재료(Carbon fiber reinforced thermoplastic polymer, CFRTP)의 물성을 비교 평가하였다. Polyamide 6 (PA6) 수지에 Multi-wall carbon nano tube (MWCNT), Silicon oxide, Core shell rubber, Aramid nano fiber 등의 다양한 나노필러를 혼합한 후, 이를 기지재(Matrix)로 탄소섬유강화복합 재료(CFRP)를 제조하여 그 물성을 측정하였다. 나노필러의 종류와 혼합비율에 따라, 인장강도, 층간계면결합력 (Inter-laminar shear strength), Izod 충격 강도 등이 측정되었다. 인장 강도와 충격 강도의 경우 Core shell rubber를 혼합한 경우 가장 높은 물성을 가졌으나, 계면결합력은 silicon oxide를 1 wt.% 이하 혼합하였을 때 최적값을 가졌다.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 1999년도 제29회 춘계학술대회
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• pp.92-100
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• 1999

Friction characteristics of automotive friction materials according to the types of phenolic resin were investigated by using a pad-on-disk type friction tester. Four different simplified friction materials bound with Bakelite$^{TM}$ and Xylok$^{TM}$ phenolic resin were studied in this work. Two different modes of drag test(constant initial temperature test and constant interval test) were employed to analyze the effects of the binders on friction characteristics. Friction materials containing modified Xylok$^{TM}$ resin showed good heat resistance and friction stability. The results also showed that aramid fiber played important roles in improving friction stability and weard wear

• 한국염색가공학회:학술대회논문집
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• 한국염색가공학회 2008년도 제38차 학술발표대회
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• pp.187-189
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• 2008

아라미드 섬유는 화학적으로 치밀한 구조 때문에 염료의 침투가 어려워 염색이 곤란하다. 염료의 침투가 용이하도록 팽윤제를 사용하여 염색하는 방법이 주로 사용되고 있지만 만족스러운 염착률을 얻을 수 없다. 본 연구에서는 기존의 방법에 중성염을 첨가하여 아라미드를 염색함으로써 중성염이 아라미드 염색에 미치는 영향에 대해 알아보았다. 연구 결과, 중성염을 사용하지 않은 경우에 비해 염색성이 향상되는 것을 확인할 수 있었다. 또한 연구에 사용된 3종의 중성염 중에서 NaCl을 사용한 경우에 가장 우수한 염색성을 나타내어 현장에서 경제적으로 적용 가능한 아라미드 염색법이 될 것으로 기대된다.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 1999년도 학회창립 10주년 기념 1999년도 가을 학술발표회 논문집
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• pp.717-720
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• 1999

Recently, the fiber composite materials such as carbon fiber, glass fiber, or aramid, have been frequently used in strengthening reinforced concrete structures. The fiber composite materials typically have orthotropic characteristic and the strength changes significantly acording to the direction of fibers and the method of the lamination. In this study, an algorithm to estimate the stress-strain relationship of the composite materials which have different fiber directions and symmetric or non-symmetric lamination has been developed by using Tsai-Hill and Tsai-Wu failure criteria and progressive laminate failure theory. This algorithm has been implemented to several stress-strain models for the laterally confined concrete compression members such as Mander, Hosotani, and Nakatsuka. The evaluated stress-strain behaviors by the different models are discussed.

• Composites Research
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• 제13권3호
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• pp.21-29
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• 2000

The optimum design of hybrid laminated composites for iso-strain structure has been studied by controling fiber orientations and thicknesses of each layer. Fiber orientations and thicknesses of each layer for iso-strain structure were designed. Combining the laminates of each layer of different reinforcing material, the constitutions of hybrid laminated composite for iso-strain structure were obtained. All these calculations were formed on computer systems, automatically for the hybridization. Using the data of some specific laminated composite such as glass and aramid reinforced composites, the constitutions of hybrid laminated composites for iso-strains structure were designed and verified by lamination theory. The strains of each layer of hybrid laminated composites are calculated and they turned out to be good agreements with the results obtained lamination theory.