• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 춘계학술대회
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• pp.364-369
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• 2003

Crack propagation and AE characteristics of CFRP plain woven laminate composites are examined with acoustic sensor by AEDSP 32/16 board in PC system. AE signals are measured during the fracture behavior tests. The purpose of study is the estimation of the crack extension behavior effected between three kinds of fiber orientation for plain woven CFRP laminate composite and the relationship between AE characteristics and load-displacement curves and crack extension length.

• Journal of Advanced Marine Engineering and Technology
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• 제34권5호
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• pp.686-694
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• 2010

Continuing progress in high technology has created numerous industrial applications for new advanced composite materials. Among these materials, carbon fiber-reinforced plastic (CFRP) laminate composite is typically used for low-weight carrying structures that require high specific strength. In this study, the damage mechanism of a compact tension (CT) specimen of woven CFRP laminates is described in terms of strain and displacement changes and crack growth behavior. The digital image correlation (DIC) method (which is employed here as a computer vision technique) is analyzed. Acoustic emission (AE) characteristics are also acquired during fracture tests. The results demonstrate the usefulness of these methods in evaluating the damage mechanism for woven CFRP laminate composites. From the results, we show these methods are so useful in order to evaluate the damage mechanism for woven CFRP laminate composites.

• 대한기계학회논문집A
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• 제28권4호
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• pp.443-452
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• 2004

In recent year, composite materials are increasingly used in various fields of engineering because of its superior properties. The relationships of between crack propagation and AE characteristics fer CFRP plain woven laminate composites are examined. AE signals are measured during the fracture behavior tests. The purpose of study is to estimate the crack extension behavior with AE characteristics according to the load orientation fur plain woven CFRP laminate composite.

• 동력기계공학회지
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• 제14권5호
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• pp.17-23
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• 2010

In recent, the capacity of a commercial wind power has reached the range of 6 MW, with large plants being built world-wide on land and offshore. The rotor blades and the nacelle are exposed to external loads. Wind power system concepts are reviewed, and loadings by wind and gravity as important factors for the mechanical performance of the materials are considered. So, the mechanical properties of fiber composite materials are discussed. Plain woven fabrics Carbon Fiber Reinforced Plastics (CFRP) are advanced materials which combine the characteristics of the light weight, high stiffness, strength and chemical stability. However, Plain woven CFRP composite have a lot of problems, especially delamination, compared with common materials. Therefore, the aim of this work is to estimate the mechanical properties using the tensile specimen and to evaluate strain using the CNF specimen on plain woven CFRP composites. For the strain, we tried to apply to plain woven CFRP using Digital Image Correlation (DIC) method and strain gauge. DIC method can evaluate a strain change so it can predict a location of fracture.

• 동력기계공학회지
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• 제10권2호
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• pp.117-123
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• 2006

Woven fabrics composites are used as primary structural components in many applications because of their superior properties that offer high specific strength and stiffness. However, the complexity of the fabric structure makes understanding of their failure behavior very difficult. Also, laminate woven fabrics CFRP have unique failure mechanisms such as fiber bridging, fiber/matrix crack and so on. In particular, the delamination phenomenon of the composite materials is one of the most frequent failure mechanisms. So, we estimated interlaminar fracture and damage in composites using as ENF specimen by a 3 point bending test. And AE characteristics were examined for crack propagation on plain woven CFRP. We obtained the following conclusions from the results of the evaluation of the 3 point bending fracture test and AE characteristic estimation. AE counts of maximum crack length were obtained as $85.97{\times}10^4\;and\;93{\times}10^3\;for\;a_0/L=0.3$ and 0.6, respectively. Also the maximum amplitudes were over 80dB at both $a_0/L=0.3\;and\;0.6$. $G_{IIc}$ at that's $a_0/L$ ratio were obtained with $1.07kJ/m^2\;and\;3.79kJ/m^2$.

• International Journal of Safety
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• 제8권1호
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• pp.1-5
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• 2009

The CFRP composite has unique properties that offer high strength and stiffness, even though it has light weight. Therefore it can be used in many industrial applications. When mechanical fasteners are used for joining composites, high stress concentrations appear near the edge of holes prepared for accommodating structural bolts and rivets. This presence of high stress concentrations can be a source of damage. The aim of this work is to evaluate fracture behavior and patterns of plain woven CFRP with circular hole and repairing patch element. The maximum strength and pattern for the plain woven carbon composite specimen with the repaired circular hole were examined. From the results, we show that repairing of the CFRP composite specimen with ($\pi$) 3~5 mm of circular hole diameter results in load rising effect and the repairing is more effective as bigger hole specimen.

• Composites Research
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• 제26권2호
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• pp.141-145
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• 2013

본 연구에서는 CFRP 적층판에 다양한 종류의 부직포를 삽입하여 모드 II 층간파괴인성을 평가하고, 파단면의 SEM 분석을 통해 층간파괴인성의 증가 원인을 파악하였다. 모드 II 층간파괴인성값($J/m^2$)은 ENF실험에 의하여 얻어졌으며, 부직포를 삽입하지 않은 시편과 3종류의 부직포(8 $g/m^2$의 탄소부직포, 10 $g/m^2$의 유리부직포, 8 $g/m^2$의 폴리에스테르부직포)가 각각 삽입된 시험편들이 준비되었다. 각 시험편들에 대한 모드 II 층간파괴인성값은 부직포를 삽입하지 않은 시편을 기준으로 탄소부직포를 삽입한 시편은 197.7% 증가하였고, 유리부직포를 삽입한 시편은 약 135.4% 증가하였으며, 폴리에스테르부직포를 삽입한 시편은 약 158.7% 증가하였다. 부직포 삽입에 의한 모드 II 층간파괴인성값의 증가 원인은 SEM 분석에 의한 결과 단섬유의 섬유가교(Fiber bridging), 섬유파단(Fiber breakage), 헥클(Hackle) 등의 발생에 기인된 것으로 확인되었다.

• 대한기계학회논문집A
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• 제38권11호
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• pp.1239-1243
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• 2014

탄소섬유 강화플라스틱은 비강도, 비강성이 크고, 높은 감쇠 특성과 중량감소 측면에서 우수한 특성을 나타낸다. 그러나 탄소섬유 강화플라스틱은 재료의 적층각 또는 적층 순서에 따라 기계적 특성 차이가 크다. 또한 인장과 굽힘과 같은 하중을 받을 때 금속과 달리 파괴 예측이 어렵다. 본 연구에서는 최근 실생활에 밀접한 휴대용 스마트기기에 CFRP 적용을 위한 외부 충격에 정형화, 최적화 설계방식을 제시하고자 한다. CFRP 를 적층각도별 기계적 특성을 얻고자 인장실험을 하였고, 각 적층각도별 체결 특성을 얻고자 판에 탭 가공 후 토크 측정기를 이용하여 풀림 토크와 체결토크를 측정하였다. 위 두 실험에 비교 분석하여 최적의 조건을 찾고자 한다. 인장실험에서 적층각이 Woven 시편에서 강도와 강성 값이 가장 우수하였다. 또한 복합재료에서는 기지와 적층배열 때문에 풀림방지 코팅나사의 효과를 보기 힘들다. [$0_8/+45_2/-45_2/90_8$]s 에서 체결력이 가장 우수했으나, 인장응력이 상대적으로 낮았다. 핸드폰에 적용을 위해 인장 특성과 체결력을 모두 충족하는 최적의 시편은 Woven 이다.

• 한국안전학회지
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• 제20권1호
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• pp.49-54
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• 2005

Recently, many kinds of advanced composite materials have been used in various industry fields. Among them, fabric CFRP composites are being used as primary structural components in many applications because of their superior properties. However, the complexity of the fabric structure makes understanding of their failure behavior very difficult. The mechanical strength and crack propagation of plain woven carbon fiber fabric laminate composites are examined by acoustic emission(AE) method. AE signals are acquired during the tensile test and fracture tests. Thus, the relationship between AE signal and mechanical behavior curves and crack extension length are shown. Also the interlaminar fracture toughness in terms of AE characteristics are discussed in viewpoint of crack propagation behavior.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2000년도 추계학술발표대회 논문집
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• pp.110-114
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• 2000

The Interlaminar fracture behavior of hybrid composite with non-woven carbon tissue was investigated under Mode I (DCB) and Mode II (ENF) loading condition. Hybrid composites were manufactured by means of inserting a non-woven tissue between prepreg layers. Two kinds of specimens were prepared from [0]$_{24}$ and [$0_{12}/0_{12}$]. Where, the symbol "/" means that a non-woven carbon tissue was located at 0/0 mid-plane of the specimen. The interlaminar fracture toughness of hybrid composites was compared with that of CFRP. The fracture surfaces of the specimens were observed using optical microscope and SEM, and the failure mechanism was discussed. The hybrid laminates, which are made by inserting non-woven carbon tissue between layers, were shown to be effective to remarkably improve Mode II fracture toughness.toughness.