• 제목/요약/키워드: strengthened beam

검색결과 407건 처리시간 0.024초

섬유복합체로 휨보강된 RC보의 박리하중 예측에 관한 연구 (The Prediction of Debonding Strength on the Reinforced Concrete Beams Strengthened with fiber Reinforced Polymer)

  • 홍건호;신영수
    • 콘크리트학회논문집
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    • 제17권6호
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    • pp.903-910
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    • 2005
  • 최근 철근콘크리트 구조물의 보강 방법으로 고인장강도를 갖는 섬유복합체를 부재의 외부에 부착시켜 휨 내력을 증진시키는 부착식 보강공법이 널리 사용되고 있으나, 부착되는 섬유복합체의 박리에 의한 파괴강도를 예측하여 설계식에 반영하기 위한 연구는 미흡한 것이 사실이다. 보강재의 박리에 의한 파괴는 부재 전체의 취성적인 파괴를 유도하게 되므로, 부재의 보강설계를 위해서는 이에 대한 검토가 필수적으로 요구되어 진다. 본 연구에서는 보강재의 부착강도에 큰 영향을 미치는 유효부착길이의 개념을 도입하여, 기존 연구 결과로부터 부재의 부착강도를 좌우하게 되는 유효부착길이를 산정 하였으며, 이와 같은 유효부착길이에 의한 보강재의 박리하중을 산정할 수 있는 설계식을 제안하였다. 제안된 설계식은 기존 연구자들의 실험 연구결과와 비교하여 그 신뢰성을 검증하도록 하였으며, 기존 연구자들의 제안식과의 비교를 통하여 본 제안식의 타당성을 증명하였다.

Numerical formulation of a new solid-layer finite element to simulate reinforced concrete structures strengthened by over-coating

  • Suarez-Suarez, Arturo;Dominguez-Ramírez, Norberto;Susarrey-Huerta, Orlando
    • Coupled systems mechanics
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    • 제11권5호
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    • pp.439-458
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    • 2022
  • Over-coating is one of the most popular engineering practices to strengthen Reinforced Concrete (RC) structures, due to the relative quickness and ease of construction. It consists of an external coat bonded to the outer surface of the structural RC element, either by the use of chemical adhesives, mechanical anchor bolts or simply mortar injection. In contrast to these constructive advantages, the numerical estimation of the bearing capacity of the strengthened reinforced concrete element is still complicated, not only for the complexity of modelling a flexible membrane or plate attached to a quasi-rigid solid, but also for the difficulties that raise of simulating any potential delamination between both materials. For these reasons, the standard engineering calculations used in the practice remain very approximated and clumsy. In this work, we propose the formulation of a new 2D solid-layer finite element capable to link a solid body with a flexible thin layer, as it were the "skin" of the body, allowing the potential delamination between both materials. In numerical terms, this "skin" element is intended to work as a transitional region between a solid body (modelled with a classical formulation of a standard quadrilateral four-nodes element) and a flexible coat layer (modelled with cubic beam element), dealing with the incompatibility of Degrees-Of-Freedom between them (two DOF for the solid and three DOF for the beam). The aim of the solid-layer element is to simplify the mesh construction of the strengthened RC element being aware of two aspects: a) to prevent the inappropriate use of very small solid elements to simulate the coat; b) to improve the numerical estimation of the real bearing capacity of the strengthened element when the coat is attached or detached from the solid body.

Numerical formulation solid-layer finite element to simulate reinforced concrete structures strengthened by over-coating

  • Arturo Suarez-Suarez;Norberto Dominguez-Ramirez;Orlando Susarrey-Huerta
    • Coupled systems mechanics
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    • 제12권6호
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    • pp.481-501
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    • 2023
  • Over-coating is one of the most popular engineering practices to strengthen Reinforced Concrete (RC) structures, due to the relative quickness and ease of construction. It consists of an external coat bonded to the outer surface of the structural RC element, either by the use of chemical adhesives, mechanical anchor bolts or simply mortar injection. In contrast to these constructive advantages, the numerical estimation of the bearing capacity of the strengthened reinforced concrete element is still complicated, not only for the complexity of modelling a flexible membrane or plate attached to a quasi-rigid solid, but also for the difficulties that raise of simulating any potential delamination between both materials. For these reasons, the standard engineering calculations used in the practice remain very approximated and clumsy. In this work, we propose the formulation of a new 2D solid-layer finite element capable to link a solid body with a flexible thin layer, as it were the "skin" of the body, allowing the potential delamination between both materials. In numerical terms, this "skin" element is intended to work as a transitional region between a solid body (modelled with a classical formulation of a standard quadrilateral four-nodes element) and a flexible coat layer (modelled with cubic beam element), dealing with the incompatibility of Degrees-OfFreedom between them (two DOF for the solid and three DOF for the beam). The aim of the solid-layer element is to simplify the mesh construction of the strengthened RC element being aware of two aspects: a) to prevent the inappropriate use of very small solid elements to simulate the coat; b) to improve the numerical estimation of the real bearing capacity of the strengthened element when the coat is attached or detached from the solid body.

비부착 프리스트레스트 CFRP 판으로 보강된 콘크리트 거더의 비선형 해석 (Nonlinear Analysis of Concrete Girders Strengthened with Unboded Prestressed CFRP Plates)

  • 최규천;이재석
    • 대한토목학회논문집
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    • 제30권6A호
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    • pp.495-502
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    • 2010
  • 이 논문에서는 비부착 프리스트레스트 CFRP 판으로 보강된 콘크리트 거더의 비선형 휨거동에 대한 해석방법을 제시하였다. 비부착 프리스트레스트 CFRP 판으로 보강된 콘크리트 거더는 CFRP 판의 슬립(slip)으로 인해 인장력이 재분배되어 CFRP 판이 콘크리트에 부착된 경우에 비해 복잡한 비선형 거동을 보이게 된다. 따라서 이 논문에서는 비부착 프리스트레스트 CFRP 판을 여러 개의 곡선 요소로 모사하고, 화이버 뼈대요소의 각 절점에서 힘의 평형 관계를 이용하여 CFRP 판의 인장력을 재분배함으로써 슬립효과를 고려하였다. 이 논문에서 제시한 해석방법을 비부착 프리스트레스트 CFRP 판으로 보강된 콘크리트 보의 해석에 적용하여 해석방법의 정당성을 확인하였다. 또한 비부착 CFRP 판의 보강시점과 보강 전후에 발생한 콘크리트의 시간의존적 변형은 보의 처짐 거동에는 영향을 미치나 극한내력에는 영향을 미치지 않음을 확인하였고, 비부착 CFRP 판으로 보강하기 전에 발생한 콘크리트의 균열유무도 비부착 CFRP 판으로 보강한 후의 보의 극한거동에는 거의 영향을 미치지 않음을 확인하였다.

Composite aluminum-slab RC beam bonded by a prestressed hybrid carbon-glass composite material

  • Rabahi Abderezak;Tahar Hassaine Daouadji;Bensatallah Tayeb
    • Structural Engineering and Mechanics
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    • 제85권5호
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    • pp.573-592
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    • 2023
  • This paper presents a careful theoretical investigation into interfacial stresses in composite aluminum-slab reinforced concrete beam bonded by a prestressed hybrid carbon-glass composite material. The model is based on equilibrium and deformations compatibility requirements in and all parts of the strengthened beam, i.e., the aluminum beam, the slab reinforced concrete, the hybrid carbon-glass composite plate and the adhesive layer. The theoretical predictions are compared with other existing solutions. Numerical results from the present analysis are presented both to demonstrate the advantages of the present solution over existing ones and to illustrate the main characteristics of interfacial stress distributions. It is shown that the stresses at the interface are influenced by the material and geometry parameters of the composite beam. This research is helpful for the understanding on mechanical behaviour of the interface and design of the hybrid structures.

유리섬유보강 Epoxy-Panel로 보강된 철근콘크리트보의 거동해석 (Analysis of Behavior in RC Beams Strengthened by Gass-Fiber Reinforced Epoxy-Panel)

  • 이창훈;송하원;변근주
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 1998년도 가을 학술발표논문집(II)
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    • pp.444-449
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    • 1998
  • The Glass-Fiber Reinforced Epoxy-Panel(GFREP) is a composite material developed for repairing and strengthening of RC structures. The objective of this study is to verify the applicability of finite element modeling technique to analyze behaviors of RC beams strengthened by the GFREP. In this study, the basic material properties obtained by experiments on the GFREP and the reinforced concrete constitutive models were considered and the comparison between analyses and experiments of RC beam specimens strengthened by the GFREP was made. Although analysis method in this paper was reasonably good, the necessities which can consider the effect of plate-end shear and plate separation were recognized.

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탄소섬유판으로 휨보강된 철근 콘크리트보의 구조적 거동 (Structural Behavior of R/C Beams Strengthened with Carbon Fiber Laminate)

  • 김성철;이희경;유성훈;김중구;정란
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 1998년도 봄 학술발표회논문집(II)
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    • pp.607-612
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    • 1998
  • In this study, the behavior of R/C beam strengthened with carbon fiber laminate(C.F.L) is analyzed from the test results. Test parameters are the width, the thickness and the length of C.F.L. and method of construction. The failure mode and ultimate load are analyzed from these measured data. Test results shows that the peak moment of specimens strengthened with C.F.L is increased to 1.43~1.90 times of that of non-rehabilitation specimen. The wider lap width, larger amount of rehabilitation materials, the larger strength is obtained.

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Shear behavior of RC beams externally strengthened and anchored with CFRP composites

  • Al-Rousan, Rajai Z.
    • Structural Engineering and Mechanics
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    • 제63권4호
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    • pp.447-456
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    • 2017
  • The primary objective of this paper is to study the effectiveness of anchorage on the performance of shear deficient beams externally strengthened with CFRP composites. The overall behavior of the tested beams loaded up to failure, the onset of the cracking, and crack development with increased load and ductility were described. The use of CFRP composites is an effective technique to enhance the shear capacity of RC beams by using CFRP strips anchored into the tension side and from the top by 15-34% based on the investigated variables. Bonded anchorage of CFRP strips with width of 0.1h-0.3h to the beam resulted in a decrease in average interface bond stress and an increase in the effective strain of the FRP sheet at failure, which resulted in a higher shear capacity as compared with that of the U-wrapped beams without anchorage as well as delay or mitigate the sheet debonding from the concrete surface.

Debonding failure analysis of prestressed FRP strengthened RC beams

  • Hoque, Nusrat;Jumaat, Mohd Z.
    • Structural Engineering and Mechanics
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    • 제66권4호
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    • pp.543-555
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    • 2018
  • Fiber Reinforced Polymer (FRP), which has a high strength to weight ratio, are now regularly used for strengthening of deficient reinforced concrete (RC) structures. While various researches have been conducted on FRP strengthening, an area that still requires attention is predicting the debonding failure load of prestressed FRP strengthened RC beams. Application of prestressing increases the capacity and reduces the premature failure of the beams largely, though not entirely. Few analytical methods are available to predict the failure loads under flexure failure. With this paucity, this research proposes a method for predicting debonding failure induced by intermediate crack (IC) for prestressed FRP-strengthened beams. The method consists of a numerical study on beams retrofitted with prestressed FRP in the tension side of the beam. The method applies modified Branson moment-curvature analysis together with the global energy balance approach in combination with fracture mechanics criteria to predict failure load for complicated IC-induced failure. The numerically simulated results were compared with published experimental data and the average of theoretical to experimental debonding failure load is found to be 0.93 with a standard deviation of 0.09.

Hybrid 복합재료 보강 철근콘크리트 보의 광섬유센서를 이용한 부착파괴 모니터링 (Monitoring of Debonding Failure of Reinforced Concrete(RC) Beams Retrofitted with Hybrid Composites by Optical FBG Sensor)

  • 김기수;김종우;조윤범;민정현;신영수;정철
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2002년도 추계학술발표대회 논문집
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    • pp.208-211
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    • 2002
  • In RC beams strengthened with Epoxy-Bonded Fiber, debonding failure happens frequently. Moreover, through the life cycle, it is difficult to recognize clacks and deflections on the surface of concrete members strengthened with Epoxy- Bonded Fiber. For these reasons, we must always monitor the state of RC beams. The Optical FBG sensor is broadly accepted as a structural health monitoring device. The main objective of this paper is that it's possible to monitoring the debonding failure of R.C. beams strengthened with Epoxy-Bonded Fiber. For that, we fixed two Optical FBG sensors at the center of the beam and another two sensors in the end of Epoxy-Bonded Fiber, According to the comparison micro-strain between embeded sensor in concrete and that on the fiber surface, we can find the point which debonding failure occurs

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