• 산업기술연구
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• 제26권B호
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• pp.145-155
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• 2006

High level of reliability in facility operation is specifically required these days. The goal of this study is to secure a methodology for reliability analysis of hydro-power plant so that an appropriate decision for operation and investment can be made. Fault tree analysis of water supply system within hydro-power plant has been performed in this study. We briefly examined the electric power generation facility and water supply system. We then developed fault tree for the water supply system based on failure modes and effects analysis. We conclude this study and provided future research areas.

• 기계와재료
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• 제23권3호
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• pp.190-198
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• 2011

하이브리드 굴삭기는 에너지 재생 및 연비향상을 위하여 기존의 유압부품들 중 일부를 전기부품으로 대체하여 시스템을 구성하고 있다. 따라서, 하이브리드 굴삭기의 신뢰성을 평가하고 보장하기 위해서는 기계적인 부하와 전기적인 부하가 복합적으로 영향을 미쳐 발생되는 고장모드를 고려하여 신뢰성평가기법을 개발하여야 한다. 특히 하이브리드 굴삭기는 가혹한 실외 환경조건에서 운용되므로 새롭게 개발되는 부품들에 대하여 설계 결함을 조기에 발견하기 위한 복합 내환경 시험과 초가속 수명시험이 수행되어야만 한다. 본 연구에서는 FMEA, FMECA, FTA 및 HALT 등의 다양한 신뢰성 기법을 사용하여 하이브리드 굴삭기의 신뢰성평가기법을 개발하였고, 개발대상 하이브리드 굴삭기의 주요 동력전달 파트인 선회구동 시스템에 대한 신뢰성평가장비를 개발하고 구축하였다. 본 연구에서 개발된 하이브리드 굴삭기 신뢰성평가기법은 하이브리드 자동차의 부품들에 대한 신뢰성평가에도 유용하게 사용될 수 있을 것으로 기대된다.

• 한국항공우주학회지
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• 제38권2호
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• pp.169-179
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• 2010

3중 비행제어시스템이 종래의 4중 비행제어시스템과 유사한 수준의 시스템 신뢰성과 이중 결함시의 안전한 운용성능을 제공하기 위해서는 기존의 고전적인 다중화 설계기법에 많은 변경과 수정이 필요하다. 이에 따라 국내에서 개발된 고등훈련기급의 3중 비행제어시스템 다중화 설계기법은 4중 시스템과 동일한 수준의 생존성을 확보하기 위해서 3중 시스템의 핵심인 비행제어컴퓨터의 입출력 프로세서와 메인 프로세서를 기능적으로 분리시켜 상호 고장에 대한 영향성을 최소화키고, 시스템의 치명적인 결함을 검출하기 위해서 특별한 고장 분석 기법과 격리 알고리즘을 적용하여 비행제어시스템의 안정성과 신뢰도가 보장되도록 설계하였다. 본 논문은 이러한 다중 시스템 구조와 고장관리 설계기법을 소개하고 설계된 3중 비행제어시스템의 손실율 분석을 통해서 기존 신뢰성 요구도가 만족됨을 해석적으로 입증하였으며, 또한 3중 비행제어시스템의 각종 고장모드에 대한 시스템 영향성 및 안정성 시험을 통해서 그 성능을 검증하였다.

• 한국기계가공학회지
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• 제20권9호
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• pp.35-41
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• 2021

A rotor is a crucial component in various mechanical assemblies. Additionally, high-speed and high-efficiency components are required in the automotive industry, manufacturing industry, and turbine systems. In particular, the failure of high-speed rotating bearings has catastrophic effects on auxiliary systems. Therefore, bearing reliability and fault diagnosis are essential for bearing maintenance. In this work, we performed failure mode and effect analysis on bearing rotors and determined that corrosion is the most critical failure type. Furthermore, we conducted experiments to extract vibration characteristic data and preprocess the vibration data through principle component analysis. Finally, we applied a machine learning algorithm called support vector machine to diagnose the failure and observed a classification performance of 98%.

• 한국철도학회논문집
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• 제14권6호
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• pp.515-525
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• 2011

도시형 자기부상열차 실용화사업에 적용된 유도무선루프방식 열차제어시스템에 대하여 최상위 레벨에서 전체 시스템에 대한 시스템 분류, 기능 분석을 시행하고 차상신호설비, 지상신호설비로 나누어 신뢰도, 가용도, 유지보수도 및 안전도를 수식을 통하여 분석한 결과를 제시하였다. RAM 분석은 신뢰도 블록도(RBD)를 각 장치별로 적용하여 시스템 서비스 가용도를 산출하였고, 안전도 분석은 PHA(예비위험원 분석), FMEA (고장모드영향분석), HAZOP을 통한 각각의 정상사상(Top Event)의 FTA(고장트리분석)을 시행하고 그 결과를 제시하여 RAMS 목표 값에 도달함을 수식을 통하여 증명하였다.

• 한국항공운항학회지
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• 제24권4호
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• pp.26-34
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• 2016

In this study, reliability prediction of the ignition system of hybrid rocket is performed. The FMECA is preceded to the reliability prediction. To this end, the ignition system is divided into 5 components and 19 potential failure modes. The failure cause and effects are identified and criticality analysis is carried out for each failure mode, in which the criticality number is estimated using the failure rate databases. Among the numbers, the failure modes and components with higher criticality and severity are chosen and allocated with higher weighting factor. The reliability predictions are performed using the failure rate databases, from which the current ignition system is found to satisfy the target reliability.

• 한국신뢰성학회지:신뢰성응용연구
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• 제10권2호
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• pp.123-135
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• 2010

Failure mode and effects analysis (FMEA) is a widely used technique to assess or to improve reliability of products or processes at early stage of development. Traditionally, the prioritization of failures for corrective actions is performed by evaluating risk priority numbers (RPN). In practice, due to insufficient evaluation criteria specific to related products and processes, RPN is not always evaluated properly. This paper reestablishes an effective methodology for prioritization of failure modes in FMEA procedure. Revised evaluation criteria of RPN are devised and a refined FMEA sheet is introduced. To verify the proposed methodology, it is applied to inspection processes of PCB products.

• 한국수소및신에너지학회논문집
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• 제34권6호
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• pp.682-688
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• 2023

In this paper, analyzes the type of failure and its effect on the hydrogen fueling nozzle used in hydrogen station. Failure of hydrogen fueling nozzle was analyzed using a qualitative risk assessment method, failure mode and effect analysis. The failure data of hydrogen fueling nozzles installed in domestic hydrogen stations are collected, and the failure types are classified, checked the main components causing the failure. Criticality analysis was derived based on frequency and severity depending on the failure mode performed. A quality function is developed by a performance test evaluation item of the hydrogen fueling nozzle, and the priority order of design characteristics is selected. Through the analysis results, the elements to improve the main components for enhancing the quality and maintenance of the hydrogen fueling nozzle were confirmed.

• 유공압시스템학회논문집
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• 제2권2호
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• pp.1-7
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• 2005

For the reliability evaluation of the track drive unit(TDU), firstly, we analyzed the major failure modes through FMEA(failure mode & effects analysis), FTA(failure tree analysis), and 2-stage QFD(quality function deployment), and then quantitatively determined the priority order of test items. The Minitab analysis was also performed for prediction of life distribution and parameters of TDU by use of field failure data collected from 430 excavators for two years. In addition, we converted the fluctuation load in field conditions into the equivalent load, and for evaluation of the accelerated lift by the cumulative fatigues, the equivalent load is again divided into the fluctuation load by reference of test time. And then, by use of the test method in this paper, the acceleration factor(AF) of needle bearing inside planetary gear which is the most weakly designed part of TDU is achieved as 5.3. This paper presents the quantitative selection method of test items for reliability evaluation, the determination method of the accelerated life test time, and the method of non-failure test time based on a few of samples. And, we proved the propriety of the proposed methods by experiments using a TDU for a 30 ton excavator.

• 한국군사과학기술학회지
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• 제21권6호
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• pp.894-903
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• 2018

In the case of helicopters, the development of parts technology is rapidly changing, and the complexity is rapidly increasing. Particularly, the surge of various electric and electronic systems is recognized as a problem that is directly related to the safety of the helicopter. Due to these problems, there is a growing interest in reliability evaluation in the face of the problem of confirming and certifying the reliability of parts in the development stage. In this paper, the analysis of the failure mechanism of the wiper system was carried out, and the priority and importance of each failure mode were checked by using the results, and major stress factors were derived and the corresponding acceleration model was selected. Also, the accelerated lifetime test time was calculated according to the life test time, acceleration status and acceleration level of the steady state by using the selected acceleration model and characteristic values.