• 전자공학회논문지 IE
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• v.48 no.4
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• pp.1-6
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• 2011

In this paper we show the LCD simulator for defect inspection using image processing algorithm and neural network. The defect inspection algorithm of the LCD consists of preprocessing, feature extraction and defect classification. Preprocess removes noise from LCD image, using morphology operator and neural network is used for the defect classification. Sample images with scratch, pinhole, and spot from real LCD color filter image are used. From some experiments results, the proposed algorithms show that defect detected and classified in the ratio of 92.3% and 94.5 respectively. Accordingly, in this paper, a possibility of practical implementation of the LCD defect inspection system is finally suggested.

• 전자공학회논문지 IE
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• v.48 no.2
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• pp.26-31
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• 2011

In this paper we show the LCD simulator for defect inspection using image processing algorithm and neural network. The defect inspection algorithm of the LCD consists of preprocessing, feature extraction and defect classification. Preprocess removes noise from LCD image, using morphology operator and neural network is used for the defect classification. Sample images with scratch, pinhole, and spot from real LCD color filter image are used. From some experiments results, the proposed algorithms show that defect detected and classified in the ratio of 92.3% and 94.5 respectively. Accordingly, in this paper, a possibility of practical implementation of the LCD defect inspection system is finally suggested.

• Journal of the Korean Magnetics Society
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• v.26 no.1
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• pp.24-30
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• 2016

MFL (Magnetic flux leakage) type nondestructive testing has been used for inspection of underground gas pipelines to find metal defects by detecting magnetic leakage signal. Because the underground gas pipeline is exposed by environment such as high pressure with great humidity, external defects are easily formed on the surface of pipelines and they are being grouped respectively. These adjacent defects cause the signal distortion of leakage flux so that it is hard to estimate the shape information of defects. In this paper, we performed to study of the signal distortion and compensating method for multiple defects in MFL type nondestructive testing system by using 3D FEM simulation. This paper proposes the basic algorithm of defect signal analysis on multiple defects on the surface of 30 inch diameter pipeline.

• Proceedings of the KIEE Conference
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• 2011.07a
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• pp.2085-2086
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• 2011

전력설비의 절연물이 사용 환경 영향을 받아 열화되어 방전이 발생하게 되는데, 이 때 발생하는 방전의 크기 및 량은 절연물의 결함 형태와 환경에 영향을 받아 다양하게 나타난다. 절연물 결함에서 발생하는 신호는 열, 전자파, 초음파, 빛의 형태이며, 이들 신호가 복합적으로 방출된다. 결함을 갖는 절연물 종류에 따라 발생하는 이상 신호 패턴을 분석하여 절연성능 저하를 검출할 수 있고, 절연성능 저하 원인 규명에도 활용된다. 본 연구에서는 전력설비에 사용하고 있는 결함 또는 열화된 애자류의 이상신호 발생의 근본원인을 고찰하였으며, 이들의 신호를 검출하는 적절한 방법을 제시하였다.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.02a
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• pp.371-371
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• 2013

사파이어 단결정 웨이퍼는 제조과정에서 결정 성장 조건 및 기계적 연마에 의하여 내부적인 결함이 발생할 수 있다. 사파이어 단결정은 일반적으로 LED용 기판 재료로 사용되며, 내부결함이 발생 시 기판 위의 GaN 등 layer의 결함도 함께 증가하므로 기판의 결함을 줄이는 과정이 중요한 이슈이다. 이 과정에 X-선 토포그래피는 단결정의 내부 결함을 모니터링 하는데 있어서 매우 유용한 방법이다. 이에 본 연구에서는 사파이어 단결정 웨이퍼에 내재하는 결함 형태를 X-선 Lang 토포그래피 방법(X-ray Lang Topography)으로 이미징하여 관찰, 분석하였다. Lang 토포그래피 방법은 X-선 투과법으로 넓은 부분을 우수한 강도와 분해능으로 내부 결함을 관찰할 수 있는 장점을 지니고 있다. X-선 source는 Mo $k{\alpha}$ 1을 사용하였으며, 시료는 c-plane 사파이어 웨이퍼를 사용하였다. 사파이어 웨이퍼의 (110), (102) 회절면의 X-선 토포그래피 이미지를 통해 전위 결함의 유형에 따른 이미지 패턴의 형성 메커니즘에 대해 연구하였고, 측정 회절면과 두께, 표면 데미지에 따른 전위 결함 이미지의 변화를 확인하였다. X-선 토포그래피 이미지를 통해 단결정 c-plane 사파이어 웨이퍼의 전위 결함의 형성 메카니즘 연구와 유형별 이미지와 회절면, 두께, 표면 데미지에 따른 이미지 변화 등을 확인하였다.

• Journal of the Korean Crystal Growth and Crystal Technology
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• v.16 no.2
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• pp.66-70
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• 2006

Various kind of structural defects are observed to be present on the oxidized surface of the silicon crystal which was previously damaged mechanically. The formation of such defects was found to depend on the amount of damage induced and the temperature of thermal oxidation. It was confirmed by the measurement of minority carrier life time that gettering capability decreases as the size of the defects increase. The strained layer which is formed due to smaller amount of damage or lower oxidation temperature believed to has higher capability of gettering over defects like dislocation loops or stacking faults.

• Korean Journal of Materials Research
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• v.11 no.3
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• pp.159-163
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• 2001

The success of SDB (silicon wafer direct bonding) technology can be estabilished by bonding on the bonded interface with no defects and Preventing temperature dependent bubbles. In this research, we observed the behavior of the intrinsic bubbles by transmitting the infrared light and the increase of the bubble pressure was found. And, the $SiO_2$-$SiO_2$ bonded wafer was achieved, which generates no intrinsic bubbles in the annealing under the atmospheric pressure. The intrinsic bubbles in the $SiO_2$-$SiO_2$ bonded wafer were generated in the annealing in the ultra high vacuum. This experimental result shows the relation between the bubble growth and the pressure.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 2010.04a
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• pp.43-43
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• 2010

국내에 천연가스버스가 보급된 이래 5차례의 용기파열 사고가 발생하였는데 그중 2005년 8월 전주 덕진충전소에서 발생한 용기파열사고는 CNG용기의 라이너를 감싸고 있는 복합재료가 손상되어 발생한 사고로 보고되었다. 복합재료용기의 외피손상이 원인이 되어 발생한 사고사례는 해외에서 약 13건이 보고되었다. CNG용기 외피손상은 용기룰 고정하는 스트랩과 밀접한 관련이 있다. 용기고정이 불완전하면 슬립이 발생하고 이는 복합재의 손상으로 이어진다. 본 연구에서는 ISO 19078, CGA C6.4 등 국제코드의 규정을 고려하여 국내에서 제조된 Type 2, 3, 4 용기와 외국에서 생산된 Type 3 용기를 대상으로 결함깊이, 길이, 넓이에 따른 복합재료 결함 내구성시험을 수행하여 CNG용기의 내구성능을 평가하였고, 시험과 동일한 조건으로 복합재료 손상결함 조건을 컴퓨터로 전산모사하여 시험결과의 타당성과 유효성을 비교 검증하였다. 실험결과, Type 2 용기의 경우, 11,250회의 최소반복가압 회수를 충족하였으나 외피손상부와 반복가압에 따른 실제누출부위가 일치하지 않아 실험조건을 달리한 추가실험이 요구되었다. Type 3 용기의 경우에는 복합재 결함부위와 누수부위가 일치된 시험용기의 수는 67%정도로, 복합재료 용기의 수명을 저하시키는 원인으로 라이너와 외피손상이 서로 밀접한 관련이 있음을 확인하였다. Type 4 용기는 국제기준에서 요구하는 반복횟수를 만족하였고, 손상깊이 0.75mm와 1.25mm에서 반복가압회수가 60,000회 이상이 되어도 누설이 발생되지 않았다. 이는 라이너의 재질이 폴리머로서 균일한데다 탄소섬유 복합재료층 위에 유리섬유 복합재료 층이 1.5mm 정도 추가로 적층되어 있어서 3등급의 손상결함(결함깊이 1.25mm)에서도 구조 층이 전혀 손상되지 않은 것으로 판단되며, 이는 Type 2 용기의 강재라이너나 Type 3의 알루미늄 라이너와 비교하여 Type 4 용기의 폴리에틸렌 라이너의 물성이 반복성능이 탁월함을 확인할 수 있었다.

• The Korean Journal of Air & Space Law and Policy
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• v.20 no.2
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• pp.59-158
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• 2005

When a military aircraft suffers damages due to the defects in its design, manufacturing or notification, all of which are generally understood as products liability defects, the obvious compensation is sought as it would in other consumer good case. However, there exist clear yet unappreciated difference between general consumer goods and military aircraft, as far as products liability law is concerned - some sort of recovery should be obtained even when there exist only defects, not damages, to the aircraft because of the implication of defective parts is much grave than what can be expected in a consumer goods case. While certain anticipatory measures do exist in manual or at negotiation stages for the safety of military aircraft, such measures are ineffective, if not ambiguous, in recovery effort in the post-accident stage In another word, the standardized military procurement contract manuals and boilerplate forms do not appreciate the unique and dangerous military nature of military aircraft. There are many unique legal issues which can arise when trying to prevent defective aircraft or parts, or to recover compensations for accident due to such defects. At two-level, the government should establish legal system (or countermeasures if you'd like) for purchasing safer military aircraft. First, one should be able to work with legal ground and policy that allows selecting and purchasing safer goods - the purpose of such contract is not litigious, but rather in acquiring what are most reliable. Second, in case the defects do arise and lead to damages, solid legal principles and instructions should be established for effectively pursuing appropriate company, (usually a aerospace industry giant with much experience) for products liability - the purpose of such pursuit is inevitable for a public official, since he or she is no private business man with much flexibilities, even to the point of waiving such compensatory right for future business purposes. This article tries to identify problems in methods of procuring military aircraft or parts - after reviewing on how the military can improve on legal and policy grounds for procuring what will be the focus of future military strength, it will offer some of the ways to effectively handling and resolving a liability issues.

• Journal of Korea Multimedia Society
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• v.14 no.1
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• pp.76-84
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• 2011

Embedded Systems need to ensure real-time of the task response time depending on the applied fields of it. And task could be faulty due to various reasons in real time systems. Therefore in this paper, we design a task scheduler that guarantees deadlines of periodic tasks and considers a fault tolerance of defective task in embedded system with a single processor. In order to provide real-time, we classify tasks with periodic/aperiodic tasks and applies RMS(Rate Monotonic Scheduling) method to schedule periodic tasks and can guarantees execution of aperiodic tasks by managing surplus times obtained after analyzing the execution time of periodic tasks. In order to provide fault tolerance, we manage backup times and reexecute a fault task to restore it's conditions.