• Defense and Technology
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• no.10 s.164
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• pp.38-42
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• 1992

복합재 압력용기의 제작 및 사용중에 발생하는 결함(손상)의 비파괴검사를 통해 구조물의 건전성을 평가하는 것은 제품의 품질보증 관점에서 아주 중요합니다. 복합재에서는 여러 종류의 결함이 동시에 존재할수 있으며, 결함-기계적 성질-비파괴특성 사이의 상호관계는 완전히 알려져 있지 않습니다. 이글에서는 복합재 연소관에 존재하는 결함의 위험도와 결함 탐지를 위한 비파괴 검사 기법에 대해 먼저 살펴보았습니다. Filament Winding으로 제조한 복합재 연소관의 Proof Testing과 관련해 음향방출(AE)법에 의한 최근의 연구결과를 살펴본 다음, 연소관의 신뢰도 확보를 위한 비파괴 평가 방법에 대해 앞으로의 연구 방향을 제시하였습니다

• Journal of the Korean Society for Nondestructive Testing
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• v.31 no.2
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• pp.139-143
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• 2011

The problem of delamination of composite tubes by impact has been acknowledged in aerospace and automobile industry. Non-destructive testing(NDT) methods in composite material structure are important to evaluate reliability of composite structure. There are many kinds of NDT methods which can detect the inside defect of the composite material such as Infrared Thermography(IRT). Infrared thermal imaging of object is different from that of a defect, in heated composite tubes with an internal defect, and then location and size of a defect can be measured by the analysis of thermal imaging pattern. In this study, Lock-in Infrared thermography detect internal defects of Impacted composite tubes by the inspection of infrared lay radiated from the surface of composite tubes.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2000.04a
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• pp.22-22
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• 2000

본 연구에서는 초음파 탐촉자의 접촉방식을 다양화하여 Immersion법/Bubbler법/Squirtor법으로 복합재 연소관을 탐상하는 방법에 대하여 연구하였으며, 이를 위하여 FRP의 delamination, FRP-EPDM간의 미접착을 모사한 복합재 연소관 모의결함시편을 제작하여 시험하였다. Immersion법에서는 일반적으로 사용되는 방법을 적용하였으며 Bubbler 및 Squirter법에서는 자체적으로 설계 및 제작한 치구를 이용하여 시험하였다. 이들 각 방법에 대하여 복합재 연소관 모의결함 시편의 결함부위에 대한 초음파 신호를 A-scan으로 비교하고 또한 C-scan하여 결함의 검출 정도를 비교하였다. 그리고 시험 자료를 바탕으로 데이터 값을 분석함으로써 복합재 연소관에서의 초음파 속도, 음향 임피던스, 반사율 및 투과율 등 복합재료의 초음파 특성을 산출하였으며 또한 건전신호와 결함신호에 대한 분류기준을 제시하였다.

• Composites Research
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• v.31 no.5
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• pp.246-250
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• 2018

In this paper, laser ultrasonic rotation scanning method was proposed to inspect and visualize defects in corner section of curved composite structure. L-shaped composite specimen with defects in its corner section were inspected using laser ultrasonic rotation scanning method. L-shaped specimens had artificial defects at three different depths to simulate delamination damage. All artificial defects were detected clearly in different time-of-flight according to their depths. Inspection result showed that the proposed method is suitable to inspect round corner section of curved composite structure without any special tools.

• Journal of the KSME
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• v.52 no.7
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• pp.40-44
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• 2012

이 글에서는 풍력발전시스템(wind energy conversion system)에 사용되는 대형 복합재 블레이드(composite blade)의 내부 결함 및 이를 통한 신뢰성 평가 동향에 대해 소개하고자 한다.

• Journal of the Korean Society of Propulsion Engineers
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• v.16 no.2
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• pp.65-72
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• 2012

A defect analysis program for a composite motor case was developed to apply the ultrasonic signal processing method, based on the ultrasonic pulse-echo method. With the proposed defect analysis program, defects of FRP delamination and FRP/Rubber disbond in the composite motor case could be quantitatively measured. The defects detected in the composite motor case were in good agreement with the results measured with the computed tomography and video microscope. This paper described the development process of the defect analysis program to convert the ultrasonic test data into the C-Scan images.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.9
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• pp.25-32
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• 2006

In this study, the characteristics of filament wound composite/aluminum ring specimens were investigated at cryogenic temperature. The ring specimens were manufactured using carbon fibre and Type B epoxy resin which had been developed for cryogenic use. As a result of measuring thermal strains at -150℃, it was found that compressive thermal stress was induced in composite part on the contrary, tensile thermal stress in aluminum part which was about 32% of yield stress and in turn, caused aluminum to be yielded at lower load level. In addition, Thermal strains which resulted from finite element analysis showed good agreement with those of the experiment. After 6 mechanical loading cycles had been applied to the ring specimen at -150℃, tensile tests were performed at -150℃ using a split disk fixture. As a result, it was shown that composite strength in a liner-composite tank structure which is for the use of cryogenic propellant tank would be decreased by auto-frettage pressure which is applied to it.

• Composites Research
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• v.30 no.6
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• pp.410-415
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• 2017

This paper predicted deformation due to thermal residual stress in composites using finite element analysis. Temperature cycle, Model shape, Laminate angle, Stacking sequence, chemical shrinkage of resin, and thermal expansion are affect composite deformation. Compare the results of the analytical model with the actual model of the same shape. This paper suggests that the analytical results can be applied to actual Model.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.05a
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• pp.264-267
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• 2006

One of the serious problems that make the flaw identification in a multi-layered thick composite panel more difficult is the interferenceeffect of the upper layer. To take care of such a problem, here we propose an image enhancement approach that can get rid of such an interference effect to ultrasonic C-scan images by a normalization of the acquired signals by a reference signals, and demonstrate its performance in the experiments. Specifically, three specimens with artificial flaws are prepared and ultrasonic C-scan images are acquired experimentally to eliminate the undesired interference effect. Cleat successes are observed in the present study demonstrating the high potential of the proposed algorithm as a practical image enhancement tool in many practical situations.

• Composites Research
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• v.32 no.1
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• pp.50-55
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• 2019

In this study, we investigated the effect of fiber alignment in helicoidal structure on the mechanical properties of biomimetic fiber-reinforced composites. Using finite element analysis, circular biomimetic fiber composites were designed and studied. Various amounts of pressure loads were applied to a surface of the composites, and then bending and failure behaviors of the composites were analyzed. The results showed various failure morphologies according to the orientation of the fibers, and it turned out that the fiber alignment in helicoidal structure significantly improved the bending strength of the composite under pressure loading. This was because the fiber alignment in various directions for each layer dispersed effectively the fracture energy from the external load into multiple directions.