• Journal of the Korea Academia-Industrial cooperation Society
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• v.19 no.8
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• pp.239-245
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• 2018

The importance of reliability in the development of weapons systems and reliability tests has been emphasized recently. Therefore, this study evaluated a reliability test design method of a bladder type accumulator and proposed a process for reliability test design. To design the reliability test of the accumulator, the main failure modes and failure mechanisms were investigated, and the main stress factors were analyzed to select the appropriate acceleration model. A steady - state reliability test was designed according to the number of samples, and the reliability level and accelerated life test time were calculated according to the acceleration factor computed using the selected acceleration model.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.29 no.1A
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• pp.45-52
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• 2009

In conventional structural design, deterministic optimization which satisfies codified constraints is performed to ensure safety and maximize economical efficiency. However, uncertainties are inevitable due to the stochastic nature of structural materials and applied loads. Thus, deterministic optimization without considering these uncertainties could lead to unreliable design. Recently, there has been much research in reliability-based design optimization (RBDO) taking into consideration both the reliability and optimization. RBDO involves the evaluation of probabilistic constraint that can be estimated using the RIA (Reliability Index Approach) and the PMA(Performance Measure Approach). It is generally known that PMA is more stable and efficient than RIA. Despite the significant advancement in PMA, RBDO still requires large computation time for large-scale applications. In this paper, A new reliability-based design optimization (RBDO) method is presented to achieve the more stable and efficient algorithm. The idea of the new method is to integrate a response surface method (RSM) with PMA. For the approximation of a limit state equation, the moving least squares (MLS) method is used. Through a mathematical example and ten-bar truss problem, the proposed method shows better convergence and efficiency than other approaches.

• 전기의세계
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• v.44 no.2
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• pp.15-20
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• 1995

1995년도는 한국 유일의 원자력발전소 플랜트 종합설계 회사인 한국전력기술주식회사가 기술자립 목표를 달성하는 해로서, 이번 기회에 울진원자력 3,4호기의 플랜트 종합설계(Architect Enginering:A/E)에서는 원자력발전소의 안전성과 신뢰성 확보와 증진을 위하여 어떻게 설계를 개선하고, 노력하고 있는 지를 소개하므로써, 원자력발전소의 안전성과 신뢰성 이해에 도움을 주고자 한다.

• Journal of the Korean Geotechnical Society
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• v.30 no.8
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• pp.5-11
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• 2014

The objective of this paper is to develop a rational reliability analysis procedure for the LRFD design provisions of bridge substructures. A bridge abutments is considered in this study. The reliability analysis is applied to determine the relationship between the major design parameters for bridge abutment and reliability index. The considered load components include dead load, vertical and horizontal earth pressure, earth surcharge, and vehicle live load. Several limit states are considered: foundation bearing capacity, sliding, and overturning. The analysis results show that the most important parameter in the reliability analysis is the effective stress friction angle of the soil. The reliability indices are calculated using Monte Carlo simulations for a selected bridge abutment. The results of the sensitivity analysis indicate that reliability index is most sensitive with regard to resistance factor and horizontal earth pressure factor.

• 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.

• Journal of Korea Society of Industrial Information Systems
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• v.3 no.1
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• pp.1-11
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• 1998

본 논문에서는 "실행 프로세서 " , "대기 프로세서" 그리고 "프로세서 절체"와 같은 향상된 개념과 기법을 사용하여 실시간 시스템에 의한 이중화 구조를 설계하고 신뢰성을 평가한다. 이중화구조는 동일한 두 개의 하드웨어 요소로 구성되며, 신속한 결함검출과 결함분리를 위한 유용한 여러 복구단계로 구성되었기 때문에 하드웨어와 소프트웨어의 부가로 인한 시스템의 부담을 최소화 시키고, 시스템이 연속성을 유지하도록한다. 기존의 결함허용 기법과 비교해서, 제안한 구조는 삼중화 구조(TMR) 보다 신뢰성이 향상됨을 보인다. 삼중화 구조(TMR) 보다 신뢰성이 향상됨을 보인다.

• Proceedings of the Korean Reliability Society Conference
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• 2005.06a
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• pp.379-384
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• 2005

신뢰성 보증을 위한 인증시험(reliability qualification test)이나 수락시험(reliability acceptance test)에 있어서 가장 널리 사용되는 시험방식 중의 하나가 무고장 시험방식(zero-failure test)이다. 무고장 시험방식이 선호되는 이유는 요구수명을 주어진 신뢰수준으로 보장하는 시험방식들 중에서 적용이 비교적 수월하며 상대적으로 시험기간이나 시료수를 줄일 수 있다는 점 때문이다. 그러나 무고장 시험의 경우, 시험을 의뢰하는 입장에서는 고장이 하나라도 발생하면 불합격 된다는 부담감을 가질 수 있으며 생산자 위험이 커진다는 단점도 가지고 있다. 본 연구에서는 이러한 문제를 보완한 2단계 시험방식을 설계, 제안하고 시험시간, OC곡선 등 시험방식의 특성을 무고장 시험방식과 비교, 분석하였다.

• Journal of Korean Society of Coastal and Ocean Engineers
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• v.22 no.6
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• pp.415-422
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• 2010

Development of the reliability-based design program in the GUI environment is inadequate for engineers familiar with the deterministic design to deal with the international design criterion based on the probabilistic design. In this study, the design program based on the GUI environment is developed in order to more efficiently input the design factor and more easily carry out the design works. The GUI environment is the GUIDE (Graphic User Interface Development Environment) tool supported by the latest MATALB version 7.1. In order to test the model reliability, the probabilities of failure (POF) on the breakwater armor block (AB) and gravity quay-wall (QW) in the sliding mode are computed using the model in the Level II and Level III. The POF are 55.4~55.7% for breakwater AB and 0.0006~0.0007% for gravity QW. A non-GUI environment program results of the POF are 55.6% for breakwater AB and 0.0018% for gravity QW. In comparison, the POF difference is negligible for breakwater AB because the exact input design parameters are available, whereas the large POF difference, but within the same order, for gravity QW can be explained by the difference of the input design factors because of the poor input data information.

• Proceedings of the Korea Water Resources Association Conference
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• 2020.06a
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• pp.90-90
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• 2020

상수관망시스템은 관할 지역 내 생활 및 공업용수를 공급하기 위한 사회기반시설물로써, 비상시에도 사용자의 용수 수요를 충족하기 위한 안정적인 성능이 요구된다. 이러한 상수관망시스템의 용수공급능력은 비상시 용수공급가능량, 공급수압 등 여러 가지 수리해석 결과를 통해 판단할 수 있다. 그러나, 시스템의 설계 및 운영 과정에서 다양한 성능들을 시간·공간적으로 모두 고려하는 것은 매우 복잡한 과정을 거치므로, 복합적인 용수공급 성능을 집약적으로 평가하기 위한 신뢰도 지수들이 개발되었다. 여기서 신뢰도 지수들은 각각의 이론적 접근방법에 따라 시스템의 특정 성능에 다소 편중된 평가 결과를 갖는 것으로 알려져 있으며, 따라서 상수관망시스템의 설계 및 운영 시, 목적과 특성에 맞는 적합한 신뢰도 지수를 선정하고, 적용하기 위한 분석이 필요하다. 본 연구에서는 상수관망시스템의 구조적 특성 및 핵심 성능에 따른 신뢰도 지수별 적용성을 평가하기 위해, 다양한 형태의 네트워크에서 몇 가지 공급부하 시나리오를 바탕으로 수리해석 결과와 신뢰도 지수 간의 상관성을 분석하였다. 또한, 다기준 분석기법을 통해 종합적인 시스템 핵심 성능에 대한 신뢰도 지수의 상관성을 분석함으로써, 시스템 전반에 대한 신뢰도 지수별 적용성을 함께 평가하였다. 본 연구 결과는 향후 상수관망시스템의 설계 또는 기존 시스템의 보강 및 운영계획 수립 등을 위한 연구에서 폭넓게 활용할 수 있을 것으로 기대된다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.5
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• pp.438-447
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• 2008

This study is focused on reliability based design optimization (RBDO) using moving least squares. A response surface is used to derive a limit-state equation for reliability based design optimization. Response surface method (RSM) with least square method (LSM) or Kriging will be used as a response surface. RSM is fast to make the response surface. On the other hand, RSM has disadvantage to make the response surface of nonlinear equation. Kriging can make the response surface in nonlinear equation precisely but needs considerable amount of computations. The moving least square method (MLSM) is made of both methods (RSM with LSM+Kriging). Numerical results by MLSM are compared with those by LMS in Rosenbrock function and six-hump carmel back function. The RBDO of engine duct of smart UAV is pursued in this paper. It is proved that RBDO is useful tool for aerospace structural optimal design problems.