• 제목/요약/키워드: composite plate

검색결과 1,756건 처리시간 0.032초

Development of Carbon Composite Bipolar Plates for Vanadium Redox Flow Batteries

  • Lee, Nam Jin;Lee, Seung-Wook;Kim, Ki Jae;Kim, Jae-Hun;Park, Min-Sik;Jeong, Goojin;Kim, Young-Jun;Byun, Dongjin
    • Bulletin of the Korean Chemical Society
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    • 제33권11호
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    • pp.3589-3592
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    • 2012
  • Carbon composite bipolar plates with various carbon black contents were prepared by a compression molding method. The electrical conductivity and electrochemical stability of the bipolar plates have been evaluated. It is found that the electrical conductivity increases with increasing carbon black contents up to 15 wt %. When the carbon black contents are greater than 15 wt %, the electrical conductivity decreases because of a poor compatibility between epoxy resin and carbon black, and a weakening of compaction in the carbon composite bipolar plate. Based on the results, it could be concluded that there are optimum carbon black contents when preparing the carbon composite bipolar plate. Corrosion tests show that the carbon composite bipolar plate with 15 wt % carbon black exhibits better electrochemical stability than a graphite bipolar plate under a highly acidic condition. When the optimized carbon composite bipolar plate is applied to vanadium redox flow cells, the performance of flow cells with the carbon composite bipolar plate is comparable to that of flow cells with the graphite bipolar plate.

Evaluation on structural behaviors of prestressed composite beams using external prestressing member

  • Ahn, Jin-Hee;Jung, Chi-Young;Kim, Sang-Hyo
    • Structural Engineering and Mechanics
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    • 제34권2호
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    • pp.247-275
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    • 2010
  • In this study, experimental, numerical, and analytical approaches were carried out to evaluate the behavior and prestressing effect of prestressed composite beam by external tendon and cover plate. Behavior of prestressed composite beam, load-carrying capacity, effects of prestressing, and ultimate strength were estimated. The contribution of the section increase of the prestressing method using tendon was less than the prestressing method using cover plate. In accordance with numerical and analytical approaches, the ultimate strength of the prestressed composite beam is shown to be the same value because strength is determined according to the plastic resistance moment and the plastic neutral axis; however, both plastic resistance moment and neutral axis are not affected by prestressing force but affected by sectional stiffness of the prestressing member. Based on these approaches, we concluded that the prestressing method using tendon can be useful in applications without an increase in self-weight, and the prestressing method using high-strength cover plate can be applied to reduce the deflection of the composite beam. The prestressing method using high-strength cover plate can also be used to induce prestress of the composite beam in the case of a large deflection due to a smaller sectional stiffness of the composite beam.

PEM 연료전지용 가스확산층-탄소 복합재료 분리판 조합체 개발 (Development of GDL-carbon Composite Bipolar Plate Assemblies for PEMFC)

  • 임준우
    • Composites Research
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    • 제34권6호
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    • pp.406-411
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    • 2021
  • PEM(양성자 교환막) 연료 전지는 부산물로 물 만을 생성하여 친환경 에너지원으로 각광받고 있다. 이러한 연료전지의 스택을 이루는 여러 부품들 중 연료전지의 효율을 결정짓는 분리판에 관한 연구가 활발히 진행되고 있다. 복합재료 분리판은 높은 강도와 강성 및 내식성을 갖지만 상대적으로 낮은 전기 전도도를 갖는 단점이 있다. 본 연구에서는 이러한 단점을 극복하고자 가스확산층(GDL)-복합재료 분리판 조합체를 개발하고 그 성능을 실험적으로 확인하였다. 선행 연구에서 개발된 흑연 포일 코팅법을 분리판과 GDL 간의 접촉 저항을 줄이기 위해 적용하였다. 또한, 스택 내의 전자 이동경로를 향상시키고 GDL과 분리판 사이의 접촉저항을 최소화하기 위하여 금속 박막을 이용하여 GDL-분리판 조합체를 제작하였다. 실험 결과 개발된 GDL-분리판 조합체는 기존의 복합재료 분리판과 비교하여 98% 낮은 전기저항을 갖는 것을 확인하였다.

Critical thrust force and feed rate determination in drilling of GFRP laminate with backup plate

  • Heidary, Hossein;Mehrpouya, Mohammad A.;Saghafi, Hamed;Minak, Giangiacomo
    • Structural Engineering and Mechanics
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    • 제73권6호
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    • pp.631-640
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    • 2020
  • Using backup plate is one of the most commonly used methods to decrease drilling-induced delamination of composite laminates. It has been shown that, the size of the delamination zone is related to the vertical element of cutting force named as thrust force. Also, direct control of thrust force is not a routine task, because, it depends on both drilling parameters and mechanical properties of the composite laminate. In this research, critical feed rate and thrust force are predicted analytically for delamination initiation in drilling of composite laminates with backup plate. Three common theories, linear elastic fracture mechanics, classical laminated plate and mechanics of oblique cutting, are used to model the problem. Based on the proposed analytical model, the effect of drill radius, chisel edge size, and backup plate size on the critical thrust force and feed rate are investigated. Experimental tests were carried out to prove analytical model.

하프 PC판과 후타설콘크리트 접합면의 면내전단강도에 관한 실험적 연구 (An Experimental Study on In-Plane Shear Strength of the Interface between Half PC Plate and Cast-in-Place Concrete Plate)

  • 신동원;고만영;이동우;김용부
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 1998년도 가을 학술발표논문집(II)
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    • pp.513-518
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    • 1998
  • In Half Precast Concrete Method, such as composite slab and composite wall, Interface between half PC plate and cast-in-place concrete is occurred. And this interface endure lastly in-plane shear which is occurred by external force. Therefore, test was executed to study in-plane shear strength of interface between half PC plate and cast-in-place concrete. In this test, Experimental parameters are finishing condition of the interface, cohesion of concrete, existence and nonexistence of re-bar truss, and angle and direction of lattice of re-bar truss. Comparing and analyzing experimental results, conclusions are obtained as follows. (1) In-plane shear strength of wide interface in composite plate is more affected by the roughness of interface than re-bar truss. And cohesion of concrete contribute to increasing in-plane shear strength. Therefore it seems that the interface should be roughen and kept clean to improve in-plane shear strength. (2) It seems that shear friction equation in ACI code can be sagely available for design of in-plane shear of composite plate.

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Buckling optimization of laminated composite plate with elliptical cutout using ANN and GA

  • Nicholas, P. Emmanuel;Padmanaban, K.P.;Vasudevan, D.
    • Structural Engineering and Mechanics
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    • 제52권4호
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    • pp.815-827
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    • 2014
  • Buckling optimization of laminated composite plates is significant as they fail because of buckling under in-plane compressive loading. The plate is usually modeled without cutout so that the buckling strength is found analytically using classical laminate plate theory (CLPT). However in real world applications, the composite plates are modeled with cutouts for getting them assembled and to offer the provisions like windows, doors and control system. Finite element analysis (FEA) is used to analyze the buckling strength of the plate with cutouts and it leads to high computational cost when the plate is optimized. In this article, a genetic algorithm based optimization technique is used to optimize the composite plate with cutout. The computational time is highly reduced by replacing FEA with artificial neural network (ANN). The effectiveness of the proposed method is explored with two numerical examples.

RM 등기하 판요소를 이용한 적층판의 자유진동 및 선형좌굴 해석 (Vibration and Buckling Analysis of Laminated Composite Plates using RM Isogeometric General Plate Element)

  • 김하룡;이상진
    • 한국공간구조학회논문집
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    • 제14권2호
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    • pp.59-68
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    • 2014
  • A study on the vibration and buckling analyses of laminated composite plates is described in this paper. In order to carry out the analyses of laminated composite plates, a NURBS-based isogeometric general plate element based on Reissner-Mindlin (RM) theory is developed. The non-uniform rational B-spline (NURBS) is used to represent the geometry of plate and the unknown displacement field and therefore, all terms required in this element formulation are consistently derived by using NURBS basis function. Numerical examples are conducted to investigate the accuracy and reliability of the present plate element. From numerical results, the present plate element can produce the isogeometric solutions with sufficient accuracy. Finally, the present isogeometric solutions are provided as future reference solutions.

Buckling analysis of plates reinforced by Graphene platelet based on Halpin-Tsai and Reddy theories

  • Javani, Rasool;Bidgoli, Mahmood Rabani;Kolahchi, Reza
    • Steel and Composite Structures
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    • 제31권4호
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    • pp.419-426
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    • 2019
  • In this paper, buckling analyses of composite plate reinforced by Graphen platelate (GPL) is studied. The Halphin-Tsai model is used for obtaining the effective material properties of nano composite plate. The nano composite plate is modeled by Third order shear deformation theory (TSDT). The elastic medium is simulated by Winkler model. Employing nonlinear strains-displacements, stress-strain, the energy equations of plate are obtained and using Hamilton's principal, the governing equations are derived. The governing equations are solved based on Navier method. The effect of GPL volume percent, geometrical parameters of plate and elastic foundation on the buckling load are investigated. Results showed that with increasing GPLs volume percent, the buckling load increases.

A refined discrete triangular Mindlin element for laminated composite plates

  • Ge, Zengjie;Chen, Wanji
    • Structural Engineering and Mechanics
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    • 제14권5호
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    • pp.575-593
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    • 2002
  • Based on the Mindlin plate theory, a refined discrete 15-DOF triangular laminated composite plate finite element RDTMLC with the re-constitution of the shear strain is proposed. For constituting the element displacement function, the exact displacement function of the Timoshenko's laminated composite beam as the displacement on the element boundary is used to derive the element displacements. The proposed element can be used for the analysis of both moderately thick and thin laminated composite plate, and the convergence for the very thin situation can be ensured theoretically. Numerical examples presented show that the present model indeed possesses the properties of higher accuracy for anisotropic laminated composite plates and is free of locking even for extremely thin laminated plates.

SPH 기법을 이용한 복합 적층판의 초고속 충돌 해석 (Numerical simulation of hypervelocity impacts on laminated composite plate targets using SPH method)

  • 이재훈;서송원;민옥기
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 추계학술대회
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    • pp.331-336
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    • 2004
  • This paper is concerned with numerical simulation of hypervelocity impacts(HVIs) of a projectile on laminated composite plate targets using SPH method. A one-parameter visco-plasticity model and damage model is used to describe the HVIs response of composite materials. The numerical simulation was carried out for a steel projectile striking to aluminum plate targets and for an aluminum projectile striking to laminated graphite/epoxy (Gr/Ep) composite plate targets. Through the numerical simulation, comparison with the HVIs response of isotropic materials and composite materials is discussed.

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