• Journal of Mechanical Science and Technology
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• 제16권5호
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• pp.599-608
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• 2002

Finite element analysis for the stress intensity factor (SIF) at the skin/stiffener structure with inclined central crack repaired by composite stiffened panels is developed. A numerical investigation was conducted to characterize the fracture behavior and crack growth behavior at the inclined crack. In order to investigate the crack growth direction, maximum tangential stress (MTS) criterion are used. Also, this paper is to study the performance of the effective bonded composite patch repair of a plate containing an inclined central through-crack. The main objective of this research is the validation of the inclined crack patching design. In this paper, the reduction of stress intensity factors at the crack-tip and prediction of crack growth direction are determined to evaluate the effects of various non-dimensional design parameter including; composite patch thickness and stiffener distance. We report the results of finite element analysis on the stiffener locations and crack slant angles and discuss them in this paper. The research on cracked structure subjected to mixed mode loading is accomplished and concludes that more work using a different approaches is necessary. The authors hope the present study will aid those who are responsible for the repair of damaged aircraft structures and also provide general repair guidelines.

• 대한기계학회논문집A
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• 제24권9호
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• pp.2246-2251
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• 2000

Adhesive bonding repair methods has been used for a number of decades for construction of damaged structures. In order to evaluate the life of cracked aging aircraft structures, the repair technique which uses adhesively bonded boron/epoxy composite patches is being widely considered as a cost-effective and reliable method. But, this repair method contains many shortcomings. One of these shortcomings, debonding is major issue. When the adhesive shear stress increases, debonding is caused at the end of patch and plate interface. And this debonding is another defect except cracks propagation. In this paper, we assess safety at the cracked AI-plate repaired by Br/Epoxy composite patch. Firstly, from the view of fracture mechanics, reduction of stress intensity factors is determined by the variety of patch feature. Secondly, using the elastic analysis and finite element analysis, the distribution of adhesive shear stresses is acquired. Finally, The problem of how to optimize the geometric configurations of the patch has been discussed.

• Structural Engineering and Mechanics
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• 제84권1호
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• pp.49-61
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• 2022

This paper presents an experimental investigation into the effectiveness of using carbon fibre reinforced polymer (CFRP) and steel plates to repair damaged reinforced concrete (RC) beams with circular web openings at shear zones. It highlights the effectiveness of externally bonded CFRP and steel plates in repairing damaged RC beams by analysing the repaired beams'load capacity, deflection, strain, and failure mode. For the experiment, a total of five beams were used, with one solid beam as a control beam and the other four beams having an opening near the shear zone. Two beams with openings were repaired using inclined and vertical configuration CFRP plates, and the other two were repaired using inclined and vertical configuration steel plates. The results confirm the effectiveness of CFRP and steel plates for repairing damaged RC beams with circular openings. The CFRP and steel plates significantly increase ultimate capacity and reduce deflection under the openings. The inclined configuration of both CFRP and steel plates was more effective than the vertical configuration. Using an inclined configuration not only increases the ultimate capacity of the beams but also changes the mode of failure from shear to flexural.

• 한국결정성장학회지
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• 제25권6호
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• pp.290-293
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• 2015

최근 사회기반시설물의 구조물 유지관리 분야의 관심이 높아짐에 따라 새로운 유지관리 공법 및 신소재에 관한 연구가 활발히 진행되어지고 있다. 그중에서도 유지관리의 주요 대상인 교량 유지관리에는 탄소섬유를 이용한 공법이 주목을 받고 있다. 탄소섬유시트(Carbon Fiber Sheet, 이하 CFS)는 이미 여러 연구자들이 국내에서도 재료시험 및 보강공법에 관한 연구를 진행하여 연구결과가 보고되고 있지만, 탄소섬유 스트랜드 시트(Carbon Fiber Strand Sheet, 이하 CFSS)는 최근 새롭게 개발된 재료로써 아직까지 국내에는 연구 성과가 없는 실정이다. 따라서, 본 연구에서는 CFSS를 RC 상판 공시체에 접착보강하여 내피로성을 평가하였다. 그 결과, 무보강 RC 상판 공시체에 비해 약 25.3배의 보강 효과가 확인되었고, CFS 접착보강 RC 상판 공시체에 비교하여 약 1.2배의 보강 효과가 확인되었다.

• 한국산학기술학회논문지
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• 제21권11호
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• pp.86-93
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• 2020

국내 사회기반 시설물의 경우 70년대 이후로 건설되어 향후 신규건설에 대한 수요보다 유지보수에 대한 수요가 크게 증가할 것으로 전망된다. 더욱이 경주지진과 포항지진 이후로 과거 시공된 시설물의 내진성능에 대한 평가 및 보수 보강 사업이 이루어지고 있다. 본 연구에서는 보강공법 중 L형 GFRP 외부부착공법을 대상으로 하여 시험체를 설계하고, 에폭시와 화약식 타정 총으로 압력 핀을 시공하는 방법으로 외부부착된 L형 GFRP Plate의 보강효과를 확인하기 위하여 4점 휨 시험을 수행하였다. 실험결과를 바탕으로 L형 GFRP Plate의 보강효과를 확인하고, 국내의 "복합신소재시스템에 의한 철근콘크리트구조물의 보강설계 및 시공 지침서"에 따라 L형 GFRP 외부부착공법이 적용된 보의 거동에 대하여 평가하고 에폭시와 압력 핀을 조합하여 시공하는 부착방법의 효용성을 평가하였다. 실험 결과를 분석한 결과 지침에 따른 설계는 부재의 강도를 잘 예측하는 것으로 나타났으나, GFRP Plate 보강재의 손상을 동반하는 고정법의 사용으로 인하여 설계가정의 조건을 만족하는 파괴가 일어나지 않는 것으로 분석하였다.

• The Journal of Advanced Prosthodontics
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• 제12권5호
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• pp.322-328
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• 2020

PURPOSE. This study evaluated the shear bond strength between 3D printed provisional resin and conventional provisional resin depending on type of conventional provisional resin and different surface treatments of 3D printed resin. MATERIALS AND METHODS. Ninety-six disc-shaped specimens (Ø14 mm × 20 mm thickness) were printed with resin for 3D printing (Nextdent C&B, Vertex-Dental B. V., Soesterberg, Netherlands). After post-processing, the specimens were randomly divided into 8 groups (n=12) according to two types of conventional repair resin (methylmethacrylate and bis-acryl composite) and four different surface treatments: no additional treatment, air abrasion, soaking in methylmethacrylate (MMA) monomer, and soaking in MMA monomer after air abrasion. After surface treatment, each repair resin was bonded in cylindrical shape using a silicone mold. Specimens were stored in 37℃ distilled water for 24 hours. The shear bond strength was measured using a universal testing machine at a crosshead speed of 0.5 mm/min. Failure modes were analyzed by scanning electron microscope. Statistical analysis was done using one-way ANOVA test and Kruskal-Wallis test (α=.05). RESULTS. The group repaired with bis-acryl composite without additional surface treatment showed the highest mean shear bond strength. It was significantly higher than all four groups repaired with methylmethacrylate (P<.05). Additional surface treatments, neither mechanical nor chemical, increased the shear bond strength within methylmethacrylate groups and bis-acryl composite groups (P>.05). Failure mode analysis showed that cohesive failure was most frequent in both methylmethacrylate and bis-acryl composite groups. CONCLUSION. Our results suggest that when repairing 3D printed provisional restoration with conventional provisional resin, repair with bis-acryl composite without additional surface treatment is recommended.

• Steel and Composite Structures
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• 제20권4호
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• pp.951-962
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• 2016

The determination of the stress intensity factor at the crack tip is one of the most widely used methods to predict the fatigue life of aircraft structures. This prediction is more complicated for repaired cracks with bonded composite patch. This study is used to compute the stress intensity factor (SIF) and crack opening displacement (COD) for cracks repaired with single and double-sided composite patches. The effect of the presence of disbond region in adhesive at the crack was taken into consideration. The results show that there is a considerable reduction in the asymptotic value of the stress-intensity factors and the crack opening displacement at the crack tip. The use of a double-sided patch suppresses the bending effect due to the eccentricity of the patch on one side only.

• 대한기계학회논문집A
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• 제25권12호
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• pp.2091-2099
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• 2001

Fatigue crack growth behavior of inclined cracked Al 6061-T6 thick aluminum plate(6mm) repaired with the bonded composite patch was studied. A 0°inclined crack bonded reinforced composite patch and 15°, 30°, 45°, 60°inclined crack plates were tested. The effect of patch and inclined angle were studied and compared to each other. Also we investigated to the crack propagation direction and debonding behavior during the fatigue crack growth test. In this paper. a study was con(ducted to get an fatigue life, fatigue crack growth ratio and crack growth direction. Finally, the effectiveness of composite patch on inclined cracked plate was investigated. The results demonstrated thats there was a definite variation in fatigue life and fatigue crack growth behavior depending on the inclined crack angle.

• Structural Engineering and Mechanics
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• 제61권3호
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• pp.325-334
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• 2017

In the present study, a numerical model for probability analysis of optimal design of fatigue non-uniform crack growth behaviour of a cracked aluminium 2024 T3 plate repaired with a bonded composite patch is investigated. The proposed 3D numerical model has advanced in literatures, which gathers in a unique study: problems of reliability, optimization, fatigue, cracks and repair of plates subjected to tensile loadings. To achieve this aim, a finite element modelling is carried out to determine the evolution of the stress intensity factor at the crack tip Paris law is used to predict the fatigue life for a give n crack. To have an optimal volume of our patch satisfied the practical fatigue life, a procedure of optimization is proposed. Finally, the probabilistic analysis is performed in order to a show that optimized patch design is influenced by uncertainties related to mechanical and geometrical properties during the manufacturing process.

• 콘크리트학회논문집
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• 제20권6호
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• pp.765-772
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• 2008

철근콘크리트 구조물은 일반적으로 재료적 특성에 따른 크리프 및 건조수축으로 인하여 장기변형이 발생하며, 이러한 변형으로 인한 구조물의 처짐을 허용 한계 이하로 유지시키는 것이 사용성 확보 측면에서 중요하다 할 수 있다. 노후된 RC보의 성능 개선을 위하여 다양항 보수 보강 방법이 사용되고 있으며 이중 대표적인 방법으로 FRP 외부부착 공법이 있다. 재료적인 성질이 우수한 FRP는 RC구조물의 보강 재료로써 현재 널리 사용되고 있으며, 일시적인 하중 뿐만 아니라 지속 하중 하에서도 향상된 보강 성능을 제공해야 한다. 따라서 FRP가 외부 부착된 RC 부재에 지속 하중이 작용할 때 콘크리트의 크리프 및 건조수축의 영향으로 인한 시간 의존적 장기 거동을 정확히 예측하는 방법이 필요하다. 본 논문에서는 FRP가 외부 부착된 RC보의 장기 처짐 예측을 위해서, CFRP와 GFRP로 보강된 실험체를 제작하고, 25 kN의 지속하중을 470일간 가하여 시간 변화에 따른 처짐을 측정하였다. 또한, 이러한 처짐의 예측을 위하여 ACI-209 code 및 CEB-FIP code에 근거하여 크리프계수와 건조수축변형률을 산정하였으며, EMM과 AEMM을 사용한 ACI-318기준, Branson's method 그리고, Mayer's method를 사용하여 FRP가 외부 부착된 RC보의 장기 처짐을 예측하였다. 실험 결과, CFRP보 보강된 실험체가 가장 높은 장기 사용성을 보였으며, Mayer's method가 장기처짐에 대한 실험값을 가장 근사하게 예측한다는 것을 확인할 수 있었다.