• Aerospace Engineering and Technology
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• v.4 no.2
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• pp.71-78
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• 2005

The purpose of FMECA is to identify parts and design whose damage can effect the mission performance and to improve the spacecraft design using these data. In consequence of this analysis, each failure mode which can be happened during operation and manufacturing period is identified, and their effects on mission performance are reviewed. In this technical report, the FMECA procedures and results for the satellite which is now under development are showed.

• Proceedings of the Korean Nuclear Society Conference
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• 1998.05a
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• pp.252-257
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• 1998

국내 원전에 신뢰도 기반 정비(RCM : Reliability Centered Maintenance) 기법을 도입하기 위해 수행하고 있는 영광 1,2호기 시법계통 RCM 분석에서 관련 기기의 고장데이터를 RCM 분석 방법론에 따라 분석하였다. 본 논문에서는 작업의뢰서와 작업보고서 기록내용을 토대로 지배적인 고장모드 및 다빈도 고장발생 기기를 파악하여 고장원인을 분석하였으며, 기기 유형으로 분류하여 고장들을 분석하였다. 분석결과 지배적인 고장모드는 EPRI에서 분류한 고장모드에 모두 포함되었으며, 고장빈도가 높은 기기의 고장원인은 운전환경, 사용유체, 운전형태, 기기 형식 등에 따라 고장메커니즘이 다르게 나타나는 것으로 분석되었다. 기기 유형으로 분류하여 고장모드별로 고장율을 분석한 결과 미국의 Generic Data(IEEE Std 500-1984)와 근소한 차이를 보이거나 약간 낮은 것으로 분석되었으며, 고장율이 높은 기기 유형을 단위 기기별로 세분화하여 분석한 결과 공기구동 조절벨브의 외부누설 고장율은 1.10E-06 이지만 충전유량 조절밸브의 고장율은 1.70E-05로서 약 10배 정도로 고장율이 높은 것으로 분석되었다. 기기별로 세분화한 고장을 분석 결과는 시범계통 RCM 분석시 고장모드 영향분석(FMEA. Failure Mode and Effective Analysis) 단계에서 필수기기를 선정하는 하나의 인자로 활용하였으며, 고장율의 역수로 구한 고장간 평균시간(MTBF:Mean Time Between Failure)은 정비주기 선정시 기초데이터로 활용된다.

• Journal of Korea Society of Industrial Information Systems
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• v.16 no.5
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• pp.107-114
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• 2011

The purpose of this paper is to develop a reliability estimation process of agricultural machinery components using field failure data. Estimating the durability is a time-consuming in the product development process. Using the field data of tractor, failures for major parts are investigated and databases are developed. Accelerated life test using the stress analysis could improve Weibull B10 considerably. This estimation process is useful for preparing the design input and planning the durability target.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.12
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• pp.1193-1200
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• 2008

The procedure of design for reliability which consists of reliability analysis and Failure Modes and Effects Analysis(FMEA) is established and reliability assesment is performed for the nano-satellite air-launching rocket, Mirinae II. By means of using the reliability analysis result, the feasibility to insert the Mirinae II to the target orbit for given mission time under operating environment is assessed. During the reliability analysis process, the system is categorized by Work Breakdown Structure(WBS), and reliability structure is defined by both Reliability Block Diagram(RBD) and schematics of the system. FMEA is used to determine the risk priority number of components and parts. The target reliability is satisfied by changing the design of components and parts with high-risk, hence the design for reliability to put the satellite in to the target orbit safely has been performed.

• Proceedings of the KIEE Conference
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• 2008.11a
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• pp.187-188
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• 2008

본 논문은 지중송전케이블 사고 시 수반되는 고장전류가 케이블에 미치는 전자력 영향에 대한 내용을 다룬다. 지중송전선로는 도심지 및 인구밀집 지역의 안정적 전력공급에 필수불가결한 송전방식이나 전력구 등의 제한된 설치 공간으로 인하여 최대한 밀집배치 되므로 고장 시 고장전류에 의한 전자력의 상호작용이 가공선로에 비하여 매우 커서 이에 대한 면밀한 검토가 필요하다. 본 문에서는 전력구내 포설 형태와 고장상황에 따른 케이블 상호간 작용 전자력에 대하여 심층적으로 분석하여, 향후 전자력 영향 감소 및 해소를 위한 지지용 금구류 등의 개선 및 개발을 위한 기본 자료로 활용하고자 한다.

• Transactions of the Korean hydrogen and new energy society
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• v.31 no.1
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• pp.65-72
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• 2020

In this study, the purpose is to identify the risks of the facilities of packaged hydrogen stations. As a risk identification method, failure mode & effect analysis (FMEA), a qualitative risk assessment, was used to analyze failure mode and effects of component of each facility. The analysis criteria were used to derive the risk priority number (RPN) using the 5-point method according to severity, incidence, and detectability. The study analyzed a total of 141 components of 23 types that can be identified on the design of the packaged hydrogen filling station. As a result, 683 types of failures and their causes and effects were identified. and the RPN was number of a total of 1,485. Of these, 10 failure types with a RPN value of 40 or more were deemed necessary. In addition, a list of failure types with a severity score of 5 was identified and analyzed.

• Journal of the Korean Society for Railway
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• v.13 no.1
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• pp.58-64
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• 2010

As a modem urban train is getting complex in terms of high-technology in its systems and components, the failure management should be performed with scientific and systematic technique. FMEA is a technique to analyze the failure trends of component parts and influences to the higher level system in order to discover the design incompleteness and potential defects, which is for improving reliability. Especially, FMECA (Failure Mode Effects, and Criticality Analysis) is used in case that the criticality that has an immense influence to the system is important. In case of urban train, in its design and manufacturing steps, FMEA is frequently used as an analysis technique to meet the safety objectives and eliminate potential hazards/failures since the concepts of reliability of train is introduced these days. Though, FMEA technique in the maintenances steps lacks in its investigation and applications yet. FMEA is also not applied to the trains operated by Seoul metro in the design and manufacture steps excepts the newest trains. In this paper, through analyzing the failures/maintenance data of the belt-type door systems used in trains operated in Seoul metro Line 1, which is accumulated in RIMS (Rolling-stock Information Maintenance System), FMEA procedures to the belt-type door engines are proposed. Especially, an effort is made, to approach the detailed FMECA procedures to the door magnet valve and switch and door engine devices which vastly influences the customer safety and satisfaction.

• Transactions of the Korean Society of Automotive Engineers
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• v.22 no.3
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• pp.68-74
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• 2014

As the number of ECUs (Electronic control units) are increasing, reliability and functional stability of a software in an ECU is getting more important. Therefore the application of functional safety standards ISO 26262 is making the software more reliable. Software fault injection test (SFIT) is required as a verification technique for the application of ISO 26262. In case of applying SFIT, an artificial error is injected to inspect the vulnerability of the system which is not easily detected during normal operation. In this paper, the basic concept of SFIT will be examined and the application of SIFT based on ISO26262 will be described.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.17 no.1
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• pp.24-28
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• 2009

The reliability assessment is performed for Pressure Control Regulator of Aircraft Fuel System using reliability procedure which consists of the reliability analysis and the Failure Modes and Effects Analysis(FMEA). The target reliability as MTBF(Mean Time Between Failure) is set to 5000hr. During the reliability analysis process, the system is categorized by Work Breakdown Structure(WBS) up to level 3, and a reliability structure is defined by schematics of the system. Since the components and parts that have been collected through EPRD/NPRD. The predicted reliability to meet mission requirements and operating conditions is estimated as 4375.9hr. To accomplish the target reliability, the components and parts with high RPN have been identified and changed by analyzing the potential failure modes and effects. By changing the configuration design of components and parts with high-risk, the design is satisfied target reliability.

• Proceedings of the KIEE Conference
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• 2009.07a
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• pp.1698_1699
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• 2009

핵폭발 등에서 방출되는 과도펄스(Transient pulse) 형태의 방사선이 반도체 소자에 조사되면 소자 내부에서는 짧은 시간에 다량의 전하가 생성된다. 이 전하들이 일정방향으로 증폭된 광전류가 소자의 고장과 오동작을 유발하거나 극단적으로 소진(Burn out)되는 원인이 된다. 본 연구에서는 과도방사선 펄스가 입사하였을 때 pMOSFET 소자 내에 생성되는 전자 정공 쌍(EHP)으로 인해 형성되는 광전류가 소자의 방사선 피해로 나타나는 과정 및 영향을 연구하기 위해 반도체 공정 시뮬레이터를 이용해 전하들의 거동과 광전류 크기를 시뮬레이션하고, 전자가속기에서 실측시험을 병행하였다. 가속기 주변의 전자장을 인한 큰 잡음으로부터 가속기 펄스신호에 의해 pMOSFET에서 발생된 소신호의 광전류를 측정하기 위해서 정밀 신호처리 회로를 구성하였다. 시뮬레이션과 실측시험에서의 결과 비교/분석에서 두 광전류 파형은 유사한 형태를 확인할 수 있었다.