• 구강회복응용과학지
• /
• 제34권2호
• /
• pp.89-96
• /
• 2018

목적: 본 연구의 목적은 비스 아크릴 복합 레진의 수리 시 지연시간, 표면처리, 수리재료가 미치는 영향을 전단 결합강도 비교를 통해 알아보고, 폴리메틸 메타크릴레이트 레진을 이용한 비스 아크릴 복합 레진 수리의 효용성을 평가하고자 하는 것이다. 연구 재료 및 방법: 총 90개의 비스 아크릴 복합 레진 시편을 제작하였고, 지연시간, 표면처리, 수리재료에 따라 10개씩 9개의 실험군으로 분류하였다. 각각의 시편들은 제작 직후 만능시험기를 사용하여 전단 결합강도를 측정하였고, 통계분석 프로그램(IBM SPSS statistics 20)을 이용하여 분석하였다. 전단 결합강도 측정 후 시편의 파절 단면을 관찰하였다. 결과: 시편 제작 직후, 접착제(bonding agent)를 이용하여 광중합형 유동성 복합 레진을 접착한 실험군에서 가장 높은 전단 결합강도를 보였다($17.54{\pm}3.14MPa$). 결론: 비스 아크릴 복합 레진을 수리할 때 경과시간에 따라 재제작 여부를 고려해야 하며, 효과적인 수리를 위해 사용부위나 목적에 따라 알맞은 재료와 표면처리 방법을 고려하는 것이 바람직할 것이다.

• Structural Engineering and Mechanics
• /
• 제84권6호
• /
• pp.799-811
• /
• 2022

Adhesive bonding has seen rapid development in recent years, with emphasis to composite patch repairing processes of geometric defects in aeronautical structures. However, its use is still limited given its low resistance to climatic conditions and requirement of specialized labor to avoid fabrication induced defects, such as air bubbles, cracks, and cavities. This work aims to numerically analyze, by the finite element method, the failure behavior of a damaged plate, in the form of a bonding defect, and repaired by an adhesively bonded composite patch. The position and size of the defect were studied. The results of the numerical analysis clearly showed that the position of the defect in the adhesive layer has a large effect on the value of J-Integral. The reduction in the value of J-Integral is also related to the composite stacking sequence which, according to the mechanical properties of the ply, provides better load transfer from the plate to the repair piece through the adhesive. In addition, the increase in the applied load significantly affects the value of the J-Integral at the crack tip in the presence of a bonding defect, even for small dimensions, by reducing the load transfer.

• 한국철도학회:학술대회논문집
• /
• 한국철도학회 2007년도 춘계학술대회 논문집
• /
• pp.132-137
• /
• 2007

This paper explains compressive behaviors of sandwich composite laminates with adhesively bonded patches. The sandwich composite laminate is used for a train carbody structure and is of an aluminum honeycomb core and CF1263 woven fabric carbon/epoxy faces. The sandwich composite laminates were damaged by low velocity impact. The damaged sandwich composite laminate was repaired using scarf repair method. Then, the strength restoration of it was assessed by compressive test. From the test, it could be known that the compressive strength was restored up to 91% of undamaged one.

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

• Composites Research
• /
• 제31권1호
• /
• pp.1-7
• /
• 2018

히트블랑켓을 이용한 통상의 복합재 패치 수리의 경우, 진공백만을 이용하여 접착제에 압력을 가하게 된다. 그러나 본 연구에서는 진공백 위에 다시 공기압을 추가로 가할 수 있는 가압장치를 개발하였다. 개발된 가압장치의 성능을 검증하기 위해 탄소섬유 복합재 적층판을 스카프 패치로 수리하고 인장시험을 수행하여, 결함이 없는 온전한 구조물과의 강도를 비교하였다. 또한 비교를 위해 오토클레이브를 사용하여 패치를 접착한 동일한 형상의 시편에 대한 인장시험도 같이 수행하였다. 시험 결과 외부압력 없이 히트블랑켓과 진공만으로 수리한 시편, 개발된 가압장치로 1 기압을 추가로 가하여 수리한 시편, 그리고 오토클레이브에서 동일한 외부압력을 가하면서 수리한 시편의 인장강도 회복율은 각각 74.9, 81.0, 78.2%로 나타났다. 수분을 포화시킨 시편에 대한 인장강도 시험과 상온건조 인장 피로시험의 결과에서도, 개발된 가압장치를 이용해 1 기압 외부압력으로 제작한 시편은 오토클레이브로 제작한 시편과 동일한 수준 이상의 강도를 보이는 것을 확인하였다.

• Restorative Dentistry and Endodontics
• /
• 제20권1호
• /
• pp.129-141
• /
• 1995

Composite resin and glass-ionomer cement can be used for the purpose of repair of defective amalgam restoration. The purpose of this study was to evaluate of shear bond strength of esthetic restorative materials to dental amalgam. The materials used in this study were Photo Clearfil Bright(light curing composite resin), Clearfil F II(chemical curing composite resin), Fuji II LC(light curing glass-ionomer cement), Fuji II (chemical curing glass-ionomer cement), All-Bond 2(intermediary), and Scotchbond Multi-Purpose (intermediary). A total of 120 acrylic cylinders with amalgam were divided into 8 groups After amalgam condensation, all specimens were stored for 48 hours in water at $37^{\circ}C$ and tested with Instron universal testing machine between amalgam and composite resins and glass-ionomer cements. The data were analyzes statiscally by ANOVA and Duncan test. The following results obtained ; 1. The shear bond strength of bonded composite resin to amalgam was higher than bonded glass-ionomer cement(P<.001). 2. The group 4 had highest shear bond strength with 15.45kgf/$cm^2$ and the group 5 had lowest shear bond strenght with 3.26kgf/$cm^2$(P<.001). 3. In the group 3, 4, 5, 6, the group 3, 4 with All-Bond 2 had higher shear bond strength than the group 5, 6 with Scotch bond MP both in light-curing and in chemical curing. 4. Both in composite resin and glass-ionomer cement, chemical curing materials had higher shear bond stength than light curing materials(P<.001).

• International Journal of Concrete Structures and Materials
• /
• 제3권2호
• /
• pp.127-131
• /
• 2009

Strengthening and repair of concrete structures using externally bonded fiber reinforced polymer (FRP) composite sheets has been popular around the world during the last two decades. However, premature failure due to debonding of the FRP is one of the important issues still to be resolved. Numerous research studies have dealt with the debonding problem in terms of Effective Bond Length (EBL), however, determination of this length has not yet been completely assessed. This paper summarizes previous works on the EBL and proposes a new relationship of the EBL with the FRP stiffness based on the existing experimental data collected in this study.

• Structural Engineering and Mechanics
• /
• 제61권3호
• /
• pp.325-334
• /
• 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
• /
• 제12권3호
• /
• pp.103-114
• /
• 2000

Recently, the need for strengthening reinforced concrete and prestressed concrete structure is increasing, particularly when there is an increase in load requirements, a change in use, a degradation problem, or some design/construction defects. Therefore, use of composite materials for structural repair presents several advantages and has been investigated all over the world. In this paper, the reinforced concrete slabs with epoxy - bonded AFRP sheed were experimentally investigated. Experimental data on strength. stiffness, material strain, deflection and mode of failure of strengthened slabs were obtained, and comparisons between the different flexural reinforcing schemes and reinforced concrete slabs without AFRP sheets were made It can be concluded that flexural strength of RC slabs strengthened with AFRP has increased, and that ductility of strengthened slabs has decreased.

• Steel and Composite Structures
• /
• 제14권1호
• /
• pp.41-55
• /
• 2013

Fiber reinforced polymers (FRP) materials are increasingly being used for strengthening and repair of steel structures. An issue that concerns engineers in steel members which are retrofitted with FRP is stress experienced due to temperature changes. The changing temperature affects the interface bond between the FRP and Steel. This research focused on the effects of cyclical thermal loadings on the interface properties of FRP bounded to steel members. Over fifty tests were conducted to investigate the thermal effects on bonding between FRP and steel, which were cycled from temperature of $-11^{\circ}C$ ($12^{\circ}F$) to $60^{\circ}C$ ($140^{\circ}F$) for 21-36 days. This investigation consisted of two test protocols, 1) the tensile test of epoxy resin, tack coat, FRP and FRP-steel plate, 2) tensile test of each FRP compound and FRP with steel after going through thermal cyclic loading. This investigation reveals an extensive reduction in the composite's strength.