• Composites Research
• /
• 제26권2호
• /
• pp.85-90
• /
• 2013

본 논문에서는 탄소섬유강화플라스틱 면재와 알루미늄 샌드위치 심재를 가지는 복합재 샌드위치의 제조와 3절점 굽힘 실험에 대해 연구하였다. 시편은 3가지 하니컴 종류(3.18 mm, 4.76 mm, 6.35 mm의 셀 크기)와 3가지 곡률 반지름(평판, r = 1.6 m, r = 1.3 m)을 가지도록 제작하였다. 샌드위치 곡률의 기준은 W-방향을 기준으로 제작 하였다. CFRP $2{\times}2$ 트윌의 인장에서 기계적 물성치(탄성계수, 강도, 푸아송 비)를 측정하여 그 값들을 다른 CFRP 섬유 적층판의 값과 비교하였다. 실험결과 평판 샌드위치 패널의 3절점 굽힘 실험에서 심재의 전단강도는 공개된 데이터에 비해 11-30% 낮게 나왔다. 제한된 시편 크기에서 1.3미터 곡률을 가지는 패널은 평판 패널에 비해 심재의 극한 전단강도가 0.8-3.8% 감소한 것으로 나타났다.

• Composites Research
• /
• 제20권4호
• /
• pp.1-8
• /
• 2007

본 연구에서는 에폭시 수지조합에 따른 탄소섬유강화 복합재 프리프레그 제작 및 극저온 인장시험을 통해 극저온에서 우수한 기계적 물성을 갖는 복합재 수지조합을 제시하였다. 환경챔버를 이용하여 상온으로부터 $-150^{\circ}C$ 까지 6회의 열-하중 사이클을 수행한 일방향 복합재 시편에 대하여 $-150^{\circ}C$에서 복합재의 인장강도와 강성을 측정하였다. 또한, $-150^{\circ}C$에서 복합재의 섬유수직방향 인장물성 및 면내 전단물성과 같은 모재 지배적인 물성 측정을 통해 수지조성변화가 섬유와 모재의 계면에 미치는 영향을 고찰하였다. 그 결과, bisphenol-A 형의 에폭시와 CTBN 고무 변성 형 필러를 비교적 다량으로 함유한 수지조성을 갖는 복합재 시편이 극저온에서 우수한 기계적 물성을 보임을 확인하였다.

• 한국전자파학회논문지
• /
• 제12권6호
• /
• pp.1002-1008
• /
• 2001

본 논문은 전파흡수기능을 갖는 경량, 고강도 고분자 복합재료의 재료 설계 및 전각흡수특성에 관한 연구이다. 전송선로 이론을 도입하여 다층구조 전파흡수체의 반사감쇠량 계산에 필요한 이론식을 제시하고, 각 층의 재료정수 및 두께의 함수로 계산한 전파흡수능 결과에 근거하여 각 층의 재질에 적합한 복합재료를 제시하였다. 본 연구에서 가장 중요한 결과는 페라이트 충진재를 사용하지 않은 3층 구조 (표면층/중간층/배면층)의 전파흡수구조재를 설계하였다는 점이다. 표면층 재료로는 저유전율 특성의 유리섬유 복합재료를 사용하고, 중간층 및 배면층에는 유전상수 및 도전손실이 큰 탄소섬유 복합재료를 사용하여 4~12 GHz 주파수 범위에서 10 dB 이상의 전파흡수특성을 얻을 수 있었다. 이에 반하여 흡수층/반사층으로 구성되는 2층 구조의 전파흡수구조재에서는 흡수층에 페라이트 충진재의 사용이 필수적이었다. 반사층 재질로 탄소섬유 복합재료를 사용하고, 횹수층 유리섬유 복합재료에 페라이트 충진재를 약 40 wt% 첨가함으로써 4~12 GHz 주파수 범위에서 10 dB 이상의 전파흡수특성을 얻을 수 있었다.

• 한국융합학회논문지
• /
• 제9권12호
• /
• pp.175-180
• /
• 2018

본 연구에서는 CFRP를 적층각도 45도로 제작하고 구조용 접착제로 접착된 TDCB(Tapered Double Cantilever Beam) 시험편을 CATIA로 설계를 하였고, 유한요소해석 프로그램인 ANSYS를 이용하여 해석을 진행하였다. 연구 모델은 영국 산업 및 ISO 표준에 기초하여 설계하였으며, 모델 형상의 각도에 따라서 형상계수(m)를 변수로 설정하였다. 본 논문의 연구 결과로서, 모든 해석 시험편들 중에서 $4^{\circ}$ 인 경사 각도를 가진 시험편에서 최대 변형량은 12.628mm로 가장 높았으며 $8^{\circ}$에서 12.352mm으로 가장 낮은 값을 각각 보였다. 또한, 최대등가응력은 그 각도가 $6^{\circ}$에서 9210.3MPa가장 높았으며 $8^{\circ}$에서 4800.5MPa로 가장 낮은 값을 각각 보였다. 본 연구 결과를 통하여 CFRP로 제작된 적층각도를 가진 TDCB 구조물의 파손데이터를 확보할 수 있었으며, 본 연구결과를 토대로 얻은 CFRP로 접착된 TDCB 구조물의 파손데이터를 활용함으로서 실생활에서의 기계나 구조물에 융합하여 그 미적 감각을 나타낼 수 있다.

• Smart Structures and Systems
• /
• 제14권5호
• /
• pp.811-830
• /
• 2014

A numerical study has been carried out to simulate an innovative monitoring procedure to detect and localize damage in reinforced concrete beams retrofitted with carbon fiber reinforced polymer (CFRP) unidirectional laminates. The main novelty of the present simulation is its ability to conduct the electromechanical admittance monitoring technique by considerably compressing the amount of data required for damage detection and localization. A FEM simulation of electromechanical admittance-based sensing technique was employed by applying lead zirconate titanate (PZT) transducers to acquire impedance spectrum signatures. Response surface methodology (RSM) is finally adopted as a tool for solving inverse problems to estimate the location and size of damaged areas from the relationship between damage and electromechanical admittance changes computed at PZT transducer surfaces. This statistical metamodel technique allows polynomial models to be produced without requiring complicated modeling or numerous data sets after the generation of damage, leading to considerably lower cost of creating diagnostic database. Finally, a numerical example is carried out regarding a steel-reinforced concrete (RC) beam model monotonically loaded up to its failure which is also retrofitted by a CFRP laminate to verify the validity of the present metamodeling monitoring technique. The load-carrying capacity of concrete is predicted in the present paper by utilizing an Ottosen-type failure surface in order to better take into account the passive confinement behavior of retrofitted concrete material under the application of FRP laminate.

• 한국방재학회 논문집
• /
• 제4권2호
• /
• pp.29-34
• /
• 2004

철도차량의 내장재료로 사용되는 페놀수지의 laminate Panel과 sandwich panel의 화재특성을 콘칼로리미터를 이용하여 착화시간, 열방출율과 일산화탄소방출량을 비교, 조사하였다. 또한 기존 철도차량용 내장재료로 사용된 불포화 폴리에스터와 페놀수지와의 화재특성을 비교하였다. 페놀수지의 중량감소 및 열분해능을 DSC & TGA를 이용하여 측정하였다. 콘칼로미터 실험결과 착화시간, 열방출율 및 일산화탄소 생성량은 50kW 복사조건에서 더 높게 나타남을 알 수 있었으며, 동일한 복사열소건 하에서는 sandwich-페놀수지가 laminate-페놀수지보다 더 빨리 착화되었다. 기존 철도차량에 적용되었던 불포화 폴리에스터와 페놀수지와의 비교시험 결과 페놀수치의 화재성능이 발열량 및 일산화탄소 방출 모두에서 우수한 것으로 조사되었다.

• 한국자동차공학회논문집
• /
• 제14권1호
• /
• pp.79-85
• /
• 2006

CFRP(Carbon Fiber Reinforced Plastics) of the advanced composite materials as structural materials for vehicle, has a wide application in light-weigh structural materials of airplanes, ships and automobiles because of high strength and stiffness, However, there is a design variable to be considered in practical application of the laminate composite materials, these materials are vulnerable to transverse impact. This paper is to study the effects of stacking sequence and curvature on the penetration characteristics of composite laminate shell. They are stacked to $[0_3/90_3]S,\;[90_3/0_3]s\;and\;[0_2/90_3/0]s,\;[90_2/0_3/90]s$ and their interlaminar number two and four. They are manufactured to various curvature radius (R=100, 150, 200mm and $\infty$), When the specimen is subjected to transverse impact by a steel ball, the velocity of the steel ball was measured both before and after impact by determing the time for it to pass two ballistics-screen sensors located a known distance apart. The critical penetration energy of specimen A and B with less interfaces were a little higher than those of C and D. As the curvature increases, the critical penetration energy increases linearly because the resistance to the in-plane deformation as well as bending deformation increases, which need higher critical penetration energy. The specimen A and C have higher critical penetration energy than B and D because of different stacking sequences. We examined crack length through a penetration test. For the specimen A with 2interfaces, the longest circumferential direction crack length were observed on the first interface from the impact point. For the specimen B 4-interface, the longest circumferential direction crack length were observed on the second interface from the impact point.

• 한국안전학회지
• /
• 제31권3호
• /
• pp.16-21
• /
• 2016

Carbon Fiber Reinforced Plastic(CFRP) composite with a higher specific strength and rigidity is more excellent than conventional metallic materials or other organic polymer of FRP. It has been widely used in vehicles, aerospaces and high technology industries which are associated with nuclear power fields. However, CFRP laminated composite has several disadvantages as like a delamination, matrix brittleness and anisotropic fibers that are the weak points of the crack initiation. In this present work, the reinforced silicon carbide(SiC) particles were added to the interlayer of CFRP laminates in order to mitigate the physical vulnerability affecting the cracking and breaking of the matrix in the CFRP laminated composite because of excellent specific strength and thermal shock resistance characteristics of SiC. The 1wt% of SiC particles were spread into the CFRP prepreg by using a spray coating method. After that, CFRP prepregs were laminated for the specimen. Also, the twill woven type CFRP prepreg was used because it has excellent workability. Thus the mechanical and fracture behaviors of the twill woven CFRP laminated composite reinforced with SiC particles were investigated with the acoustic emission(AE) method under a fracture test. The results show that the SiC particles enhance the mechanical and fracture characteristics of the twill CFRP laminate composite.

• 대한금속재료학회지
• /
• 제50권9호
• /
• pp.697-702
• /
• 2012

In this study, unidirectional and plain woven carbon fiber reinforced magnesium matrix composite laminates were fabricated by the liquid pressing infiltration process, and evolutions of the microstructure and compressive strength of the composite laminates under corrosion were investigated by static immersion tests. In the case of the unidirectional composite laminate, the main microstructural damage during immersion appeared as a form of corrosion induced cracks, which were formed at both CF/Mg interfaces and the interfaces between layers. On the otherhand, wrap/fill interface cracks were mainly formed in the plain woven composite laminate, without any cracks at the CF/Mg interface. The formation of these cracks was considered to be associated with internal thermal residual stress, which was generated during cooling after the fabrication process of these materials. As a consequence of the corrosion induced cracks, the thickness of both laminates increased in directions vertical to the fibers with increasing immersion time. With increasing immersion time, the compressive strengths of both composite laminates also decreased continuously. It was found that the plain woven composite laminates have superior corrosion resistance and stability under a corrosive condition than unidirectional laminates.

• 한국안전학회지
• /
• 제17권3호
• /
• pp.7-12
• /
• 2002

The object of this paper is to investigate collapse characteristics of CF/Epoxy(Carbon Fiber/Epoxy resin) composite tubes on the change of interlaminar number and fiber orientation angle of outer and to evaluate reappearance of collapse characteristics on the change of tension strength of fibers under static and impact axial compression loads. When a CF/Epoxy composite tube is mushed, static/impact energy is consumed by friction between the loading plate and the splayed fiends of the tube, by fracture of the fibers, matrix and their interface. In general, CF/Epoxy tube with 6 interlaminar number(C-type) absorbed more energy than other tubes(A, B, D-types). The maximum collapse load seemed to increase as the interlaminar number of such tubes increases. The collapse mode depended upon orientation angle of outer of CF/Epoxy tubes and loading status(static/impact). Typical collapse modes of CF/Epoxy tubes are wedge collapse mode, splaying collapse mode and fragmentation collapse mode. The wedge collapse mode was shorn in case of CF/Epoxy tubes with 0$^{\circ}$ orientation angle of outer under static and impact loadings. The splaying collapse mode was shown in only case of CF/Epoxy tubes with 90$^{\circ}$ orientation angie or outer under static loadings, however in impact tests those were collapsed in fragmentation mode. So that CF/Epoxy tube with 6 interlaminar number and 90$^{\circ}$ outer orientation angle presented to the optimal collapse characteristics.