• Composites Research
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• 제26권3호
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• pp.189-194
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• 2013

본 연구에서는 단방향, 직교방향, 임의의 방향 총 세 방향성을 가진 아마섬유에 첨가형 난연제로 널리 쓰이는 나노클레이를 분사한 뒤, 이 섬유를 복합재료의 제조에 사용하였다. 나노클레이는 분산성이 다른 세가지 분사방법을 사용하였으며, 제조에 사용한 기지재는 열가소성 수지인 폴리프로필렌과 열경화성 수지인 에폭시이다. 다구찌 실험계획법을 이용해서 실험을 단순화 하였으며, 실험결과 인장강도, 탄성계수, 총 충격흡수에너지, 열 방출율에 대한 최적의 복합재료 제조 조건을 얻을 수 있었다.

• Composites Research
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• 제22권6호
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• pp.1-6
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• 2009

탄소나노튜브 고분자 복합체는, 외력에 의한 변형에 따라 전기적 저항이 변화하는 피에조저항(piezoresistivity) 거동을 나타낸다. 피에조저항은 고분자 모재 내에서 탄소나노튜브가 형성하는 전기전도망(conductive network)의 변화에 의해서 발현된다. 피에조저항 낮은 탄소나노튜브 함유량에서 더 현저하게 나타난다. 탄소섬유, 카본블랙 등 타 탄소기반 소재에 비해 전기전도도와 길이 대 직경비(aspect ratio)가 월등히 우수하기 때문에, 낮은 탄소나노튜브의 함유량에서도 스트레인 센싱시스템을 구현할 수 있다. 본 연구에서는, 구조물에 부착 또는 임베드 시켜서 구조물의 건전성을 실시간을 진단할 수 있는 탄소나노튜브 고분자 복합체 기반 센싱시스템을 개발하였다. 센서는 열가소성 수지와 다중벽 탄소나노튜브를 사용하여 필름 형태로 제조되었으며, 센싱 성능은 나노복합체를 구조물에 부착한 후 인장, 굽힘, 압축 등의 다양한 형태의 하중을 가하면서 평가하였다.

• 한국산학기술학회:학술대회논문집
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• 한국산학기술학회 2009년도 추계학술발표논문집
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• pp.671-674
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• 2009

본 논문에서는 Base resin으로 열가소성 고분자인 PPS(Poly(phenylene sulfide))를 사용하였으며, 물리적 및 화학적 특성을 증대시키기 위해 주 첨가제로는 Expanded graphite와 보조 첨가제로 Glass fiber와 Carbon fiber를 사용하여 2가지의 복합 소재를 제조 하였다. 제조한 복합소재를 활용하여 최적의 사출 조건(사출 압력, 가열시간, 금형온도 등)으로 사출을 하였으며, 각각의 최종 시편을 four point probe 장치를 사용하여 전기전도도를 측정 비교 하였다.

• Composites Research
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• 제26권5호
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• pp.273-278
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• 2013

PLA/PP polymer blends in various ratios (PLA:PP = 9:1, 4:1, 3:1, and 1:1), and their composites (PLA:PP = 1:1) with sisal fiber (10, 15 and 20 wt%) were fabricated using MAPP as compatibilizer. The aim of the work was to reduce the cost of biodegradable composites as well as to improve the impact strength of PLA using PP, a relatively cheaper thermoplastic. The developed composites were characterized for their morphological and mechanical properties. The tensile strength and modulus of the blends were decreased with increasing PP content whereas the strain at break and impact strength are increased. The tensile strength, modulus and water absorption were increased for hybrid composites with increasing fiber content.

• 한국해양공학회지
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• 제10권4호
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• pp.58-66
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• 1996

The purpose of this investigation is to estimate the strength with the variations of the notch shape and the adgesive condition at the fiber/matrix micro interface of E-glass/PP laminates. To promote the degradation of the adhesive condition at the fiber/matrix micro interface without matrix dissolution loss, low-, hot-wet and spiking tests were carried out. The absorpotion properties and the tensile properties were compared accrding to the fiber orientation and the content. The results show that, firstly, saturated moisture absorption was reached at 5cycles and their absorptions of RD-40, UD-42 and UD-50 are 0.68%, 0.63%, 0.60%, respectively. Secondly, all the specimens investigated were mostly degraded at 5cycle, whereas UD-50 having ellipse shaped notch the least decrement of strength.

• 한국생산제조학회지
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• 제21권6호
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• pp.1003-1007
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• 2012

A nondestructive technique would be very useful. Advanced NDE T-ray (terahertz ray) techniques of technology and instrumentation has provided a probing field on the electromagnetic spectrum. However, the T-ray is limited in order to penetrate a conducting material to some degree. Here, the T-ray would not go through easily the CFRP composite laminates since carbon fibers are electrically conducting while the epoxy matrix is not. So, investigation of terahertz time domain spectroscopy (THz TDS) was made and reflection and transmission configurations were studied for a 48-ply thermoplastic PPS(poly-phenylene sulfide)-based CFRP solid laminate. It is found that the electrical conductivity of CFRP composites depends on the direction of unidirectional fibers.

• 한국산학기술학회:학술대회논문집
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• 한국산학기술학회 2010년도 춘계학술발표논문집 2부
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• pp.1241-1244
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• 2010

본 논문에서는 Base resin으로 열가소성 고분자인 PP(Polypropylene)를 사용하였으며, 물리적 및 화학적 특성을 증대시키기 위해 주 첨가제로는 Expanded graphite와 보조 첨가제로 Multiwall carbon nanotube를 사용하여 2가지의 복합 소재를 제조 하였다. 제조한 복합소재를 활용하여 compression molding을 하였으며, 각 함량별 시편을 four point probe 장치를 사용하여 전기전도도를 측정 비교 하였다.

• 유변학
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• 제10권2호
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• pp.57-64
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• 1998

A pultrusion resin impregnation (PRI) die, which has been developed recently in our laboratory, was used to pre-pare various composite system. The continuous fiber reinforced composites of glass fiber/polypropylene(GFPP) and glass fiber/polyamide 6 (GFPA) were first manufactured by means of the PRI die and then cut into chopped pellets of predet-ermined length. These pellets and either virgin or modified thermoplastic resin were melt-mixed by a twin screw extruder to prepare GF/PA/PP and GF/PA/PPMA system. The mechanical properties of these blends were investigated and discussed in terms of their morphological observations. These preliminary results revealed that this new impregnation die could be suc-cessfully applied to produce prepregs suitavle for the final shaping process.

• Composites Research
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• 제31권3호
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• pp.83-87
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• 2018

An object in the Low Earth Orbit (LEO) is affected by many environmental conditions unlike earth's surface such as, Atomic oxygen (AO), Ultraviolet Radiation (UV), thermal cycling, High Vacuum and Micrometeoroids and Orbital Debris (MMOD) impacts. The effect of all these parameters have to be carefully considered when designing a space structure, as it could be very critical for a space mission. Polybenzimidazole (PBI) is a high performance thermoplastic polymer that could be a suitable material for space missions because of its excellent resistance to these environmental factors. A thin coating of PBI polymer on the carbon epoxy composite laminate (referred as CFRP) was found to improve the energy absorption capability of the laminate in event of a hypervelocity impact. However, the overall efficiency of the shield also depends on other factors like placement and orientation of the laminates, standoff distances and the number of shielding layers. This paper studies the effectiveness of using a PBI coating on the front bumper in a multi-shock shield design for enhanced hypervelocity impact resistance. A thin PBI coating of 43 micron was observed to improve the shielding efficiency of the CFRP laminate by 22.06% when exposed to LEO environment conditions in a simulation chamber. To study the effectiveness of PBI coating in a hypervelocity impact situation, experiments were conducted on the CFRP and the PBI coated CFRP laminates with projectile velocities between 2.2 to 3.2 km/s. It was observed that the mass loss of the CFRP laminates decreased 7% when coated by a thin layer of PBI. However, the study of mass loss and damage area on a witness plate showed CFRP case to have better shielding efficiency than PBI coated CFRP laminate case. Therefore, it is recommended that PBI coating on the front bumper is not so effective in improving the overall hypervelocity impact resistance of the space structure.

• Composites Research
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• 제28권5호
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• pp.249-253
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• 2015

본 연구는 탄소섬유 펼침 기술을 이용한 적층 복합재료의 특성을 평가하였다. 섬유 펼침 기술이 적용되어 기존 12 K 탄소섬유 토우의 폭이 7 mm에서 20 mm로 늘어나면서 두께가 더 얇아졌다. 폴리프로필렌 필름을 spread tow에 함침시켜 프리프레그를 만들고 이를 적층 후 열압축 성형을 통해 시편을 제조하였으며 이들의 기공함유량 및 인장, 굴곡 시험을 통해 물리적, 기계적 물성을 평가하였다. 그 결과, 탄소섬유 펼침 기술이 적용된 적층 복합재료의 기공함유량이 기존의 섬유 토우를 사용한 것보다 작게 나타났고, 섬유함유량이 낮았음에도 불구하고 기계적 물성이 향상됨을 알 수 있었다.