• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2004년도 추계학술발표대회 논문집
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• pp.131-134
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• 2004

In this paper, a representative unit volume (RUV) model was employed to simulate thermoforming process of carbon fabric-polymeric foam sandwich structures. Thermoforming simulations, which capture crimp angles and amplitude changes of carbon fabric with respect to different types of foams under the operating pressure were conducted with the help of RUV model. Changed shapes of tow structure after thermoforming were reflected in the two dimensional to determine mechanical properties of skin parts, i.e_ carbon fabric composites after thermoforming. Bending simulations with respect to different foam systems as well as different moduli of carbon fabric composites were successfully carried out by using properties obtained from two-dimensional analyses.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1997년도 가을 학술발표회 논문집
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• pp.126-133
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• 1997

For each construction material used, there is certain theoretical limit in sizes. For tall building construction, the reduction in slab weight is the first step to take in order to break such size limits. In this paper, the feasibility of such objective is proven and given by numerical analysis result. For a typical building slab, both concrete and advanced composite sandwich panels are considered. The concrete slab is treated as a special orthotropic plate to obtain more accurate result. For each panel, the deflection under the dead and live loads is compared, since both tensile and compressive strengths of the composites are far more higher than those of concrete. All types of sandwich panels considered, except one case, have weights less than one tenth of that of reinforced concrete slab, with deflections less than that of the concrete slab. The cost analysis result and manufacturing methods will be reported later.

• 한국철도학회논문집
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• 제3권2호
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• pp.92-99
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• 2000

Composites are very useful material for light train carbody due to its high specific strength and lightweight characteristics. The composites, called 3-D board, are developed with a special stitching method. In this process, the glass fiber fabrics of skin material and foam core material are stitched together with glass fiber thread. The glass thread in Z-axis turns into FRP form. The conventional delamination problem can be solved with 3-D sandwich structure. In addition, with the lower density of foam, the weight of the panel and the operation expenses can be highly reduced. To evaluate the usefulness of the 3-D board, the double-deck light train carbody is studied. The stress analyses are carried out under various loads and boundary conditions with FEM Code, ANSYS. On comparing with the aluminum carbody, 3-D board carbody can be reduced by about 2 ton for the total weight of carbody.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2013년도 춘계학술대회 논문집
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• pp.1365-1366
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• 2013

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2003년도 춘계학술발표대회 논문집
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• pp.157-160
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• 2003

Honeycomb sandwich composite structures have been widely used in aircraft and military industry because of light weight and high stiffness. Accurate mechanical properties of honeycomb materials are needed for analysis of sandwich composites. In this study, theoretical formula for elastic modulus of honeycomb materials was established considering bending and axial deformations of their walls. Finite-element analysis results were compared with theoretical ones of the longitudinal and transverse moduli of honeycomb materials. Consequently, the mechanical properties of honeycomb materials could be analytically predicted.

• Composites Research
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• 제16권3호
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• pp.18-24
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• 2003

샌드위치 구조물들은 적은 무게의 첨가로 높은 강성(stiffness)을 요구하는 조선업에 널리 사용되어져 왔다. 국부하중 조건 하에서 샌드위치 구조물에 대한 디자인 변수들을 고려하는 것은 중요시되어졌다. 이 연구는 샌드위치 보의 강도에 대한 core층의 밀도, core층의 두께 그리고 face층의 두께 비율의 영향을 기술하였다. 이차원 탄성이론에 바탕을 둔 파손 하중은 AS4/3501-6 facing과 polyurethane foam core 샌드위치 보의 3점 굴곡 실험 결과와 잘 일치 하였다. 또한 그러한 파손 하중들은 face층의 비율의 변화와 함께 비교되었다. 파괴 mode들의 교차점으로 결정되어진 최적조건은 강도(strength)와 강성(stiffness)에 대한 샌드위치 빔의 최적 core 밀도의 값이 결정되었다. 추가적으로 강도에 대한 최적조건과 그렇지 못한 샌드위치 보에 대한 face 두께 비율 효과가 하중 길이에 따라 비교되었으며, 강도와 강성이 core/face무게 비율과 항께 검토하였다.

• Earthquakes and Structures
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• 제16권3호
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• pp.369-373
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• 2019

Construction industry is one of the largest markets for composite materials. Composite materials are mostly utilized as surface coatings or concrete reinforcements, and they can hardly be found as a load bearing member in buildings. The three-dimensional composite structures with considerable bending, compressive and shear strengths are capable to be used as construction load bearing members. However, these composites cannot compete with other materials due to higher manufacturing costs. If the cost issue is resolved or their excellent performance is taken into consideration to overcome disadvantages related to economic-competitive challenges, these 3D composites can significantly reduce the construction time and result in lighter and safer buildings. Sandwich composite panels reinforced with 3D woven glass fabrics are amongst composites with highest bending strength. The current study investigates the possibility of utilizing these composite materials to construct ceilings and their application as slabs. One-to-one scale experimental loading of these composite panels shows a remarkable bending strength. Simulation results using ABAQUS software, also indicate that theoretical predictions of bending behavior of these panels are in good agreement with the observed experimental results.

• 임산에너지
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• 제17권1호
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• pp.36-46
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• 1998

이 연구는 점탄성 고분자재료를 사용하여 진동·충격음 흡수성능을 지니는 목질계 복합재료의 제조를 목적으로, 가소화 PVC의 동적점탄성 및 고분자 적층 복합체의 진동흡수성능에 미치는 고분자의 점탄성의 영향을 검토하였다. 가소제는 디옥틸프탈레이트(DOP)를 사용하여, 20∼140 phr까지 첨가하였다. 고분자의 동적점탄성의 측정은 Rheovibron을 사용하여 110Hzdml 인장진동을 가하여, -100∼150℃까지 매분 1℃를 상승시키면서 측정하였다. PVC와 DOP는 전조성에서 완전상용성이었으며, T(E"max)와 T(tan δmax)는 가소제의 첨가량이 증가함에 따라 저온 측으로 이동하였다. 고분자 적층 복합체의 진동흡수성능은 Rheovibron을 개조한 양단지지 중심하중에 의한 강제 휨진동법 및 공진법에 하나인 양단자유 휨진동법을 사용하였다. 샌드위치구조 복합체의 진동흡수계수(tanδc)는 고분자의 손실계수(tanδ)와 정의 상관성을 나타내었으며, 피복체의 진동흡수계수는 고분자의 손실탄성률(E")에 의존하는 경향을 나타내었다. 또한 샌드위치구조 복합체의 대수감쇠율(Δc)은 tanδc곡선과 유사한 곡선을 나타내었다.

• Composites Research
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• 제21권1호
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• pp.22-29
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• 2008

본 논문은 유리섬유 에폭시 면재에 알루미늄 하니컴 샌드위치 복합재가 적용된 저상버스 차체에 대한 정면충돌과 전복에 대한 특성에 대해 연구하였다. 이때 충돌과 전복 해석은 외연유한요소 해석 프로그램인 LS-DYNA3D를 이용하였다. 차체 구조물에 적용되는 적층 복합재 면재에 대해 기계적 특성시험을 통하여 물성을 획득하였고, 직교이방성 특성을 갖는 하니컴 심재의 물성은 유효등가손상 모델을 적용하였다. 저상버스의 충돌 해석은 60km/h의 속도로 정면충돌 사고를 모사하여 해석을 수행하였고, 전복해석은 유럽 안전법규 ECE-R66의 시험 방법을 고려하여 해석하였다. 저상버스의 정면충돌과 전복에 대해 운전자와 승객의 생존 공간 안전성에 관한 결과를 보여준다. 또한, 수정된 Chang-Chang 파손기준식은 충돌과 전복해석에 대한 복합재 구조물의 파손 모드 예측에 추천된다.

• Smart Structures and Systems
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• 제16권6호
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• pp.1023-1047
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• 2015

In this study, the optimal location of the MR fluid segments in a partially treated laminated composite sandwich plate has been identified to maximize the natural frequencies and the loss factors. The finite element formulation is used to derive the governing differential equations of motion for a partially treated laminated composite sandwich plate embedded with MR fluid and rubber material as the core layer and laminated composite plate as the face layers. An optimization problem is formulated and solved by combining finite element analysis (FEA) and genetic algorithm (GA) to obtain the optimal locations to yield maximum natural frequency and loss factor corresponding to first five modes of flexural vibration of the sandwich plate with various combinations of weighting factors under various boundary conditions. The proposed methodology is validated by comparing the natural frequencies evaluated at optimal locations of MR fluid pockets identified through GA coupled with FEA and the experimental measurements. The converged results suggest that the optimal location of MR fluid pockets is strongly influenced not only by the boundary conditions and modes of vibrations but also by the objectives of maximization of natural frequency and loss factors either individually or combined. The optimal layout could be useful to apply the MR fluid pockets at critical components of large structure to realize more efficient and compact vibration control mechanism with variable damping.