• Magazine of the Korea Concrete Institute
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• v.13 no.2
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• pp.38-43
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• 2001

교량 하부구조 특히 교각 및 기초의 경우는 지반 또는 수중에 묻혀 있기 때문에 손상을 발견하기도 어렵고 또한 손상의 보수 및 보강이 곤란한 경우가 많다. 하부구조의 손상은 지반의 마모, 침하, 측방유동토압, 하상세굴, 홍수류, 선박 및 유하물에 의한 충격, 지진 등의 여러 원인에 의하여 발생된다. 이러한 손상은 지표수 및 지하수 배제공, 성토공, 지반개량공, 단면보수공, 세굴방지공, 내진보강공 등에 의하여 보수 및 보강이 행하여 진다. 본 고에서는 이러한 하부구조의 보수.보강공법 중 수중부에 실시되는 방법에 대하여 소개하고자 한다.

• Journal of the Korea institute for structural maintenance and inspection
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• v.9 no.1
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• pp.243-250
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• 2005

In elevated irrigation aquaducts, one can observe a common damage pattern. That is, cracks, and crushing of concrete are usually repeated at a certain interval even if no faults are found in the design and construction of the structures. To investigate the causes of this damage, longitudinal deformations of several aquaducts have been measured. The analysis of the measured data suggests that the damages are mainly caused by cumulative repetition of extension and contraction due to temperature changes.

• Proceedings of the Korean Institute of Industrial Safety Conference
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• 2001.11a
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• pp.118-123
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• 2001

항공기 운항 중에 손상된 부품의 교환이나 수리는 항공기 운항 시 안전 유지와 고가의 항공기 수명연장을 위하여 필수적이다. 여러 가지 손상이나 고장 중에서 균열은 기계적 체결요소(리벳, 볼트 등)나 패칭에 의하여 효과적으로 보수될 수 있다. 항공기 동체 보수 시 접착제 접합을 사용한 복합재료 패칭은 하부구조에 손상이 없이 균열진전을 줄일 수 있고 구멍의 생성으로 인한 응력 집중을 제거할 수 있으며 접합된 면을 외부로부터 차단시켜 부식을 방지하는 효과가 있어 많이 사용된다 특히 고강도 복합재료와 접착제의 개발로 인하여 손상된 구조의 보수를 위한 복합재료 패칭의 사용은 더욱 증가되고 있다.(중략)

• Composites Research
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• v.23 no.5
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• pp.15-21
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• 2010

In this study, repair and maintenance schemes of the damaged composite structure was investigated, and a repair process of the carbon/epoxy laminate composite structure was investigated numerically and experimentally. The composite laminates were damaged by drop weight type impact test machine. The damaged composite structure was repaired using external patch repair method after removing damaged area. The compressive strength test and analysis results after repairing the impact damaged specimens were compared with the compressive strength test and analysis results of undamaged specimens and impact damaged specimens. Finally, the strength recovery capability by repairing were investigated.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2004.05a
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• pp.96-96
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• 2004

고성능 섬유강화 복합재는 비강성과 비강도가 높고 내부식성과 피로특성이 우수하지만 외부에서 가해지는 하중에 의해 수지, 강화섬유와 수지와의 경계면, 적층 경계면 등에 육안으로 식별하기 어려운 손상이 유발될 가능성이 있으며 이로 인해 구조재로서의 역할을 하지 못하는 경우가 발생한다. 최근에는 외부하중으로 인해 복합재 구조재에 손상이 발생한 경우 자가치료제가 저장된 마이크로캡슐을 이용하여 손상을 보수하려는 시도가 행해지고 있다.(중략)

• Proceedings of the Korean Institute of Industrial Safety Conference
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• 2003.10a
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• pp.378-383
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• 2003

콘크리트 구조물은 여러 가지 원인에 의해 손상을 입거나 시간이 지남에 따라 노후화가 진행된다. 이와 같이 손상을 입거나 노후화가 진행된 구조물은 그 내구성능이 저하되어 계속 사용하기 위해서는 보수를 하거나 보강해야만 한다. 구조물을 보수하거나 보강하는 것은 구조물의 수명을 크게 연장하는 일로 여러 가지의 경제적인 효과가 있기 때문에 이에 대한 연구와 공법 개발 등이 활발히 이루어지고 있다.(중략)

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.9
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• pp.862-868
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• 2010

Development of a small scale aircraft has been carried out for the BASA(Bilateral Aviation Safety Agreement) program in Korea. This aircraft adopted all the composite structures for environmental friendly by low fuel consumption due to its lightness behavior. However the composite structure has s disadvantage which is very weak against impact due to foreign object damages. Therefore the aim of this study is focusing on the damage evaluation and repair techniques of the aircraft composite structure. The damages of composite laminates including the carbon/epoxy UD laminate and the carbon/epoxy fabric face sheets-honeycomb core sandwich laminate were simulated by a drop weight type impact test equipment and the damaged specimen were repaired using the external patch repair method after removing damaged area. The compressive strength test and analysis results after repairing the impact damaged specimens were compared with the compressive strength test and analysis results of undamaged specimens and impact damaged specimens. Finally, the strength recovery capability by repairing were investigated.

• Composites Research
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• v.27 no.2
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• pp.77-81
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• 2014

In this study, it was performed damage assessment and repair of small scale aircraft adopted on composite. This aircraft adopted the sandwich structure to skin of wing. This study aims to investigate the residual strength of sandwich composites with nomex honeycomb core and carbon fiber face sheets after the open hole damage by the experimental investigation. The 4-point bending tests were used to find the bending strength, and the open hole was applied to introduce the simulated damage on the specimen. The bending strength test results after open hole were compared with the results of no damaged specimen test. In addition, The damaged composite structure was repaired using external patch repair method after removing damaged area. After that, this study presents comparison results of the experimental investigation between the damaged and the repaired specimen. It was found that the bending strength of repaired specimen was recovered up to 95% of undamaged specimen.

• Journal of the Korean Institute of Gas
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• v.20 no.4
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• pp.33-43
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• 2016

Grinding, weld deposition, type A sleeve, type B sleeve, composite sleeve, hot tapping and clamp are used as the method to repair the buried pipelines in the United States, UK and Europe. In the event of defect to the pipeline, they have repaired the pipeline through the fitness-for-service assessments. In addition, they have guidelines for the possible repair methods to apply to each type of damage, which is occurred due to the 3rd party construction or corrosion. According to the KGS FS551, Safety Validation in Detail including ECDA(External Corrosion Direct Assessment) as one method of integrity management should be carried out for the old pipeline which supply natural gas as the middle pressure in Korea. Where a defect on the pipelines is found, on the result of Safety Validation in Detail, the pipelines should be repaired or replaced by new piping. However, there are no guidelines or regulations regarding the repair and reinforcement of pipeline, so that, cutting the damaged pipeline and replacing it as a segment of new pipe is the only way in Korea until now. We have suggested pipeline repair methods including type A, B sleeve, composite sleeve, after the survey of foreign repair method and standards including the method of United States and the United Kingdom, and after analysis of the results on pipeline repair test including type A, type B sleeve and composite sleeve.

• Journal of the Korea Concrete Institute
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• v.15 no.1
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• pp.1-10
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• 2003

The purpose of this study is to evaluate the capacities of repaired structural walls with different shear span ratios(1, 2, 3). Experimental tests were carried out. In this study three isolated large-scale wall specimens were made. The original wall specimens were tested until the drift reaches more than 3%. The region of the damaged specimen with the crack larger than 0.2 mm is replaced by new concrete. Also, severly distorted reinforcements were also replaced by new reinforcements. The crack smaller than 0.2 mm was cured by epoxy resin. Because of the space limitation of the laboratory the dimensions of all walls are the same. The shear-span ratio was controlled by the combination of axial and lateral force using the special test setting. All specimens were tested using the incremental quasi static cyclic load until failure occurs. Test results show that strength of repaired walls was almost equivalent to that of original walls. However, deformation capacities of repaired wall specimens are inferior to the original wall specimens.