• 한국철도학회:학술대회논문집
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• 한국철도학회 2010년도 춘계학술대회 논문집
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• pp.557-563
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• 2010

Mode II interlaminar fracture toughness was measured and fractured surfaces were observed of carbon/epoxy and glass/epoxy woven fabric composites for carbody structure. Woven fabric carbon/epoxy and glass/epoxy composites that made with prepreg and epoxy resin(RS1222) are used in carbody structure of Korean tilting train(TTX) and low floor bus. ENF(End Notched Flexure) specimens having $120mm{\times}20m{\times}5mm$ shape and 35mm initial crack were made with each composites and three point bending tests according to ASTM D790 were conducted for these specimens. Crack lengths in tests were recorded using optical microscope and digital camcorder. NL(Non Linear), 5% offset and Max. load points in load -displacement curves were checked and mode II interlaminar fracture toughness of these points were calculated and compared. Fractured surfaces of specimens were observed using optical microscope and mode II delamination behavior of each composites was discussed.

• Journal of Advanced Marine Engineering and Technology
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• 제34권2호
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• pp.296-302
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• 2010

If the fiber reinforced plastic is exposed to the moisture for a long period of time, most of moisture absorption occurs on the resin place, thus dropping cohesiveness between the molecules as the water molecules permeated between high molecular chains grant high molecular mobility and flexibility. Also as the micro crack occurs due to the permeation of moisture on the interface of glass fiber and epoxy resin, it is developed to the overall damage of interface place. Hence, the study on absorption is essential as the mechanical and physical properties of fiber reinforced composites are reduced. However, the study on absorption has the inconvenience needing to expose composite materials to fresh water or seawater for 1 month or up to 1 year. Therefore, this study has exposed fiber reinforced composites to fresh water and has developed a model with an accuracy of 98% after comparing the analysis value obtained by using ANSYS while basing on the experimental value of property decline by absorption and the basic properties of glass fiber and epoxy resin used in the experiment.

• 대한기계학회논문집A
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• 제25권10호
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• pp.1514-1519
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• 2001

This paper is concerned with design, manufacturing and performance test of LIPCA ( Lightweight Piezo- composite Curved Actuator) using a top carbon fiber composite layer with near -zero CTE(coefficient of thermal expansion), a middle PZT ceramic wafer and a bottom glass/epoxy layer with high CTE. The main point of this design is to replace the heavy metal layers of THUNDER by thigh tweight fiber reinforced plastic layers without losing capabilities to generate high force and large displacement. It is possible to save weight up to about 30% if we replace the metallic backing material by the light fiber composite layer. We can also have design flexibility by selecting the fiber direction and the size of prepreg layers. In addition to the lightweight advantage and design flexibility, the proposed device can be manufactured without adhesive layers when we use epoxy resin prepreg system. Glass/epoxy prepregs, a ceramic wafer with electrode surfaces, and a graphite/epoxy prepreg were simply stacked and cured at an elevated temperature (177 $^{circ}C$ after following an autoclave bagging process. It was found that the manufactured composite laminate device had a sufficient curvature after detached from a flat mold. The analysis method of the cure curvature of LIPCA using the classical lamination theory is presented. The predicted curvatures are fairly in agreement with the experimental ones. In order to investigate the merits of LIPCA, a performance test of both LIPCA and THUNDE$^{TM}$ were conducted under the same boundary conditions. From the experimental actuation tests, it was observed that the developed actuator could generate larger actuation displacement than THUNDERT$^{TM}$.

• Composites Research
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• 제34권5호
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• pp.269-276
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• 2021

프리프레그 압축성형(PCM, Prepreg Compression Molding) 공정은 고품질 CFRP(Carbon Fiber Reinforced Plastic) 제품을 제조할 수 있는 고속성형기술이다. 오토클레이브 공정에 비해 폐기물 발생이 적고 사이클타임을 크게 줄일 수 있어 항공우주 및 자동차 산업에서 다양한 연구가 진행되고 있다. 본 연구에서는 PCM 공정의 품질을 높이기 위해 프리프레그의 경화거동을 따라 프레스의 압축압력을 단계별로 증가시키는 성형법에 대해 연구하였고, 이러한 다단 압축 성형법이 우수한 품질의 CFRP 제품을 생산하고 사이클타임을 단축할 수 있는 좋은 수단임을 확인하였다. 그리고 상온에서 적층한 프리프레그를 금형에 투입하여 예열과 성형을 동시에 함으로써 별도의 예열 공정 없이 제품을 성형할 수 있었다. 또한 평판 성형에 최적화된 공정조건을 3차원 형상물에 동일하게 적용한 결과 외관상 평판과 유사한 제품을 공정조건 수립 과정 없이 만들 수 있었다.

• 한국안전학회지
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• 제19권4호
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• pp.31-35
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• 2004

The A17075/CFRP multi-layered hybrid laminate material consists of the alternating A17075-T6 sheets and carbon/epoxy prepregs of M40 fade. The influence of volume fraction and fiber orientation of A17075/CFRP layer on flexural properties of A17075/CFRP laminate alternating A17075-T6 and carbon/epoxy prepreg was investigated. The results obtained from the experimental analysis are as follows: 1. In the $0^{\circ}$ fiber orientation, the mont of increase of the flexural rigidity was $20.5\%$ at the $26.5\%$ volume fraction and $38.0\%\;at\;the\;35.7\%$ volume fraction compared with the flexural rigidity level(20.0GPa) of the $10\%$ volume fraction of CFRP. 2. In the $\pm45^{\circ}$ fiber orientation the amount of decrease of the flexural rigidity was $23.5\%\;at\;the\;20.0\%$ volume fraction and $31.5\%\;at\;the\;33.3\%$ volume fraction compared with the flexural rigidity level of the $10\%$ volume fraction of CFRP. 3. In the $0^{\circ}$ fiber orientation, the flexural strength was 481.5MPa at the $10\%$ volume fraction of CFRP and 583.8MPa at the $26.5\%$ volume fraction and 653.7MPa at the $35.7\%$ volume faction. 4. In the $\pm45^{\circ}$ fiber orientation, the flexural strength was 354.0MPa at the $20.0\%$ volume fraction of CFRP and 340.5MPa at the $33.3\%$ volume fraction.

• 한국군사과학기술학회지
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• 제9권3호
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• pp.88-94
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• 2006

In order to substitute current aluminum sabot and to increase the penetration performance of the kinetic energy projectiles, the research and development program for composites sabot has been conducted. For carbon/epoxy composites sabot, unidirectional carbon fiber reinforced epoxy prepreg was chosen and thick sectioned composites preforms with the different fiber angles along the circumferential direction of sabot were prepared by compression molding under the careful processing conditions at $150^{\circ}C$ for 1hour with $70kgf/cm^2$ curing pressure. The composites sabot demonstrated a weight reduction by approximately 30% than that of current aluminum sabot. The muzzle velocity of a kinetic energy projectile with composites sabot was measured to be about 63m/s higher than that with aluminum sabot. These results imply that the penetration performance is expected to be considerably increased when the composite sabot is applied to the kinetic energy projectiles.

• Composites Research
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• 제28권3호
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• pp.94-98
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• 2015

탄소섬유 에폭시 복합재료에 다양한 두께의 니켈 박막을 첨가한 복합재료를 제작하여 층간 계면 특성을 평가하고자 한다. 상온에서 스퍼터를 이용하여 니켈 박막을 프리프레그 위에 증착하고 이를 중간층으로 하여 복합재료를 제작하였다. 니켈 박막이 첨가된 탄소섬유 에폭시 복합재료는 니켈 박막 미첨가 탄소섬유 에폭시 복합재료에 비해 층간 전단 특성이 향상되었음을 확인하였다. 층간 파괴거동 분석을 위해 주사전자현미경으로 파단면을 관찰하였으며 니켈 박막이 복합재료 내에 층간 결합력을 높여 계면 특성을 향상시키며 전단시험 시 전단에너지를 흡수하는 역할을 한다는 것을 확인하였다.

• Elastomers and Composites
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• 제56권3호
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• pp.179-186
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• 2021

Carbon-based nanofillers, including nanodiamond (ND) and carbon nanotubes (CNTs), have been employed in epoxy matrixes for improving the toughness, using the tow prepreg method, of epoxy compounds for high pressure tanks. The reinforcing performance was compared with those of commercially available toughening fillers, including carboxyl-terminated butadiene acrylonitrile (CTBN) and block copolymers, such as poly(methyl methacrylate)-b-poly(butyl acrylate)-b-poly(methyl methacrylate) (BA-b-MMA). CTNB improved the mechanical performance at a relatively high filler loading of ~5 phr. Nanosized BA-b-MMA showed improved performance at a lower filler loading of ~2 phr. However, the mechanical properties deteriorated at a higher loading of ~5 phr because of the formation of larger aggregates. ND showed no significant improvement in mechanical properties because of aggregate formation. In contrast, surface-treated ND with epoxidized hydroxyl-terminated polybutadiene considerably improved the mechanical properties, notably the impact strength, because of more uniform dispersion of particles in the epoxy matrix. CNTs noticeably improved the flexural strength and impact strength at a filler loading of 0.5 phr. However, the improvements were lost with further addition of fillers because of CNT aggregation.

• Composites Research
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• 제35권6호
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• pp.412-418
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• 2022

메타크릴산과의 에스터화 반응을 통해 브롬화 에폭시 수지와 일반 에폭시 수지의 혼합물로부터 난연성 비닐에스터 핫멜트 필름을 제조하였고 이를 이용하여 탄소섬유와 비닐에스터 복합 프리프레그를 제조하였다. 저점도 비스페놀-A와 고점도 브롬화 비스페놀-A 에폭시 전구체를 혼합하여 필름 생산에 적합한 VE 수지의 점도를 최적화하였다. 경화된 VE 수지의 브롬 함량 증가는 비 브롬화 VE에 비해 제한 산소 지수(LOI)(39%), 25℃에서의 저장 탄성률(2.4 GPa) 및 잔류 탄화물(16.1%) 값을 더 증가시켰다. 합성한 VE 프리프레그의 수동 레이업과 후속 경화로 인장 및 굴곡 강도가 우수한 CF 강화 복합재를 성공적으로 제작하였다. 본 연구 결과는 스티렌이 없는 친환경적인 VE 복합 재료 공정의 향후 산업화에 대한 높은 가능성을 보여준다.

• 한국정밀공학회지
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• 제34권2호
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• pp.139-143
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• 2017

Finite element analysis was performed for a split-type CFRP bicycle frame, which was designed to apply a compression molding process with carbon fiber prepreg for a conventional bicycle. An epoxy adhesive material for joining the frames was selected by the extent of stress at joint interfaces. The split-type bicycle frame was then formed and its weak parts examined by the boundary conditions according to reliability tests. The results verified the reliability of the bicycle frame after modification of these weak parts. The finished product was manufactured by using this developed split-type bicycle frame.