• 폴리머
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• 제24권5호
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• pp.721-727
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• 2000

탄소섬유/에폭시 수지 복합재료의 기계적 계면 결합력을 증가시키기 위해 탄소섬유를 전해 니켈도금 표면처리하였다. 탄소섬유의 표면특성과 복합재료의 최종 기계적 물성은 각각 X-ray photoelectron spectroscopy (XPS)와 Interlaminar shear strength (ILSS) 측정을 통하여 알아보았다. 본 실험결과, 전해 니켈도금은 복합재료의 계면, 즉 강화재인 탄소섬유와 매트릭스간의 계면 결합력에 크게 영향을 미침을 알 수 있었으며, 특히 니켈도금 처리된 탄소섬유 표면에서 $O_{1s}$/$C_{1s}$ 비의 증가와 NiO 그룹 및 금속 니켈의 형성은 기계적 특성인 ILSS 증가의 요인으로 작용함을 알 수 있었다 또한, $O_{1s}$/$C_{1s}$비는 복합재료의 ILSS와 밀접한 관계가 있음을 고찰하였다.을 고찰하였다.

• 접착 및 계면
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• 제5권1호
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• pp.21-28
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• 2004

본 연구에서는 사슬말단에 chloropropyl 유기관능그룹을 가지고 있는 실란결합체인 3-chloropropyltrimethoxysilane(CTMS)을 사용하여 여러 농도에서 유리섬유 표면에 사이징 처리하여 유리섬유/나일론 6 및 유리직물/나이론 6 복합재료를 제조하였다. 단섬유 microbonding 시험에 의한 유리섬유/나일론 6 복합재료의 계면전단강도와 short-beam 전단시험과 동역학적 열특성 분석 방법을 통하여 유리직물/나일론 6 복합재료의 층간전단강도 및 저장탄성률에 미치는 결합체 농도의 영향을 각각 조사하였다. CTMS 결합제의 농도가 증가할수록 복합재료의 계면특성이 향상되었다. 결합제의 농도 변화에 대한 유리섬유강화 나일론 6 복합재료의 계면전단강도, 층간전단강도, 층간파단양상 그리고 저장탄성률 등 각 특성 변화의 경향이 서로 일치하였다.

• Carbon letters
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• 제5권1호
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• pp.18-22
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• 2004

The failure behaviours of unidirectional pultruded carbon fiber reinforced polymer (CFRP) composites were monitored by the electrical resistance measurement during tensile loading, three-point-bending, interlaminar shear loading. The tensile failure behaviour of carbon fiber tows was also investigated by the electrical resistance measurement. Infrared thermography non-destructive evaluation was performed in real time during tensile test of CFRP composites to validate the change of microdamage in the materials. Experiment results demonstrated that the CFRP composites and carbon fiber tows were damaged by different damage mechinsms during tensile loading, for the CFRP composites, mainly being in the forms of matrix damage and the debonding between matrix and fibers, while for the carbon fiber tows, mainly being in the forms of fiber fracture. The correlation between the infrared thermographs and the change in the electrical resistance could be regarded as an evidence of the damage mechanisms of the CFRP composites. During three-point-bending loading, the main damage forms were the simultaneity fracture of matrix and fibers firstly, then matrix cracking and the debonding between matrix and fiber were carried out. This results can be shown in Fig. 9(a) and (b). During interlaminar shear loading, the change in the electrical resistance was related to the damage degree of interlaminar structure. Electrical resistance measurement was more sensitive to the damage behaviour of the CFRP composites than the stress/time curve.

• 수산해양기술연구
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• 제31권3호
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• pp.272-278
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• 1995

강도가 각각 다른 세 종류의 프리프레그를 사용하여 일방향 CFRP를 적층하였으며, 모드 I과 모드 II 실험을 통하여 층간 파괴인성치를 고찰하였고, 또한 적층 섬유방향을 변화시킨 사교적층판의 그것도 함께 고찰하였으며, 이를 요약하면 다음과 같다. 1) 임계에너지 방출률 G 하(IC)의 값을 컴플라이언스 법, 수정 컴플라이언스 법, 그리고 보이론에 의해 계산하여 비교 검토한 결과 본 연구에서 사용한 수정식에 의한 값들이 거의 일치하였다. 2) G 하(IC) 값은 대체로 프리프레그의 C, B, A재의 순으로 높게 나타났으며, G 하(II C)의 값을 세가지 식에 의해 계산하여 비교 검토한 결과 거의 일치하였다. 3) 사교적층판의 경우 G 하(IC) 값은 [0/90] 하(6s), [0/45] 하(6s), [0/45/90] 하(6s)의 순으로 높게 나타났으며, G 하(II C)는 [0/90] 하(6s), [0/45/90] 하(6s), [0/45] 하(6s)의 순으로 높게 나타났다. 4) 사교적층판과 일방향의 임계에너지 방출률을 비교하였을 때, 모드 I의 경우 일방향의 결과가 다소 높았으며, 모드 II의 경우는 [0/45] 하(6s)의 결과는 거의 일치함을 알 수 있었다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2012년도 추계학술대회 논문집
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• pp.785-786
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• 2012

• 한국재료학회:학술대회논문집
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• 한국재료학회 1995년도 추계 학술발표 강연 및 논문개요집
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• pp.56-56
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• 1995

• The Korean Journal of Pain
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• 제28권1호
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• pp.64-65
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• 2015

• 대한기계학회논문집A
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• 제22권3호
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• pp.611-623
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• 1998

The delamination fracture of multidirectional carbon-fiber/epoxy laminates under the Mode I condition has been studied using the modified beam analysis for a fracture mechanics approach. It was found that the variation of fracture energy $G_IC$ with increasing length of the propagating crack exhibited a minimum for the pure interlaminar fracture and a maximum for the intraply fracture,i.e. a rising "R-curve", which was strongly affected by the degree of fiber bridging and crack-tip splitting arising in the global delamination. The maximum $G_IC$ value was significantly dependent on such types of delamination as no crack jumping, crack jumping into the adjacent ply and edge-delamination. It was shown also that the value of "effective flexural modulus" estimated from the modified beam analysis increased much with the development of fiber bridging behind the crack tip.ehind the crack tip.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2001년도 추계학술발표대회 논문집
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• pp.158-162
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• 2001

The effects of chemical treatment on Kevlar-29 fibers have been studied in a composite system. The surface characteristics of the Kevlar-29 fibers were characterized by pH, acid-base value and X-ray photoelectron spectroscopy (XPS). The mechanical interfacial properties of final composites were studied by interlaminar shear strength (ILSS) and critical stress intensity factor ($K_{IC}$). Also, the impact properties of the composites were investigated in the differentiating studies between initiation and propagation energies, and ductile index (DI) along with maximum farce and total energy. It was found that the chemical treatment with phosphoric acid ($H_3PO_4$) solution significantly affected the degree of adhesion at interfaces between fibers and resin matrix, resulting in improving the mechanical interfacial strength of the composites. This was probably due to the presence of chemical polar groups on Kevlar surfaces, leading to an increment of interfacial binding force in a composite system.

• Structural Engineering and Mechanics
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• 제43권6호
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• pp.739-759
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• 2012

The tailoring optimization technique recently developed by the author for improving structural response and energy absorption of composites is extended to sandwich shells using a previously developed zig-zag shell model with hierarchic representation of displacements. The in-plane variation of the stiffness properties of plies and the through-the thickness variation of the core properties are determined solving the Euler-Lagrange equations of an extremal problem in which the strain energy due to out-of-plane strains and stresses is minimised, while that due to their in-plane counterparts is maximised. In this way, the energy stored by unwanted out-of-plane modes involving weak properties is transferred to acceptable in-plane modes. As shown by the numerical applications, the critical interlaminar stress concentrations at the interfaces with the core are consistently reduced without any bending stiffness loss and the strength to debonding of faces from the core is improved. The structural model was recently developed by the author to accurately describe strain energy and interlaminar stresses from the constitutive equations. It a priori fulfills the displacement and stress contact conditions at the interfaces, considers a second order expansion of Lame's coefficients and a hierarchic representation that adapts to the variation of solutions. Its functional d.o.f. are the traditional mid-plane displacements and the shear rotations, so refinement implies no increase of the number of functional d.o.f. Sandwich shells are represented as multilayered shells made of layers with different thickness and material properties, the core being treated as a thick intermediate layer.