• Aerospace Engineering and Technology
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• v.8 no.1
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• pp.162-171
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• 2009

Linear regulator for generating various voltages in satellite electronics is implemented with radiation harden regulator chips or simple linear regulator circuits. For implementing linear regulator circuits, the detail design can be various. But the worst case analysis method and interesting analysis items for the linear regulator circuits can be generalized. So this paper describes and summarizes the general worst case analysis method and interesting analysis items for the conventional linear regulator circuits.

• Transactions of the Korean Society of Mechanical Engineers
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• v.13 no.3
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• pp.554-560
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• 1989

An optimal design technique is used as a systematic approach to analyze the worst case of a circulating type ropeway for a given geometry and operating conditions. Worst case is meant here the case when the positions and weights of the cars are so conditioned that the minimum of all the reaction forces between the main rope and the towers is minimum. In the course of this study, a general theory for the deflections and tensions of the main rope were also derived taking into account of the variation of the weights and positions of the individual cars. And through an analysis of example ropeways, some general conditions for the worst case are deduced.

• Proceedings of the KIPE Conference
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• 2006.06a
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• pp.375-377
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• 2006

본 논문에서는 LLC 공진형 컨버터의 최적 설계를 위해, ZVS 영역에서 동작하는 LLC 공진형 컨버터의 최악의 상태에 대한 정상 상태 해석을 하였다. LLC 공진형 컨버터의 최악의 상태는 최소 입력 전압, 최대 부하 전류일 때 얻을 수 있는 최대 전압 이득을 의미한다. 설계 변수는 스위칭 주파수 범위와 공진 인덕터 비율로서, 각 설계 변수의 변화에 따른 공진 탱크 설계 값, 최악의 상태 출력 전압 그리고 최대 공진 캐패시터 전압을 보여주는 '최악의 조건 설계 표'를 나타내었으며, 설계된 특정 공진 탱크 값에 대한 시뮬레이션 결과와 실험 결과를 보였다.

• Bulletin of the Korean Space Science Society
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• 2003.10a
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• pp.73-73
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• 2003

인공위성은 발사체에 실려 임무궤도에 도달하는 동안 여러 과정을 겪고 이에 따른 우주 열환경에 노출되게 된다. 본 연구에서는 발사체의 페어링(Fairing)이 열리고 이후 인공위성이 임무궤도에 도달하는 동안까지 인공위성에 대한 열해석을 수치적인 방법을 이용하지 않고 해석해를 이용하여 수행하였다. 일반적으로 발사시 인공위성에 대한 열해석은 수치모델을 개발하여야 하는 시간과 노력이 많이 드는 작업이다. 그러나 수치 모델이 완성되기 전에 주요 부품에 대한 극한 환경에서의 온도 예측이 필요한 경우가 있다. 본 연구는 해석 기법을 이용하여 주요 부품의 온도를 비교적 간단한 방법으로 예측하는 것이다. 이를 위하여 열관련 지배방정식에 여러 가정을 적용하여 지배방정식을 최대한 단순화시켰다. 그 결과, 최종적으로 1차 미분 방정식 형태의 단순화된 지배방정식을 얻게 되었다. 또한 본 연구에서는 여러가지 조건에 대한 연구가 시도하였다. 즉 고려하는 대상의 질량이 일정하게 유지 되는 경우와 일정한 비율로 질량이 감소하는 경우, 인공위성이 최악의 고온환경과 최악의 저온환경에 처한 경우, 그리고 시간에 대한 변수항 때문에 약간의 수치작업이 필요한 경우가 연구되었다. 본 연구에서 제안된 해석해 기법은 적절한 우주 열환경 조건과 결합하게 되면 발사과정에 대한 완전한 수치모델이 완성되기전에 위성체 부품에 대한 열적 안정성을 검토하는데 유용하게 이용될 수 있을 것이다.

• Explosives and Blasting
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• v.37 no.3
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• pp.13-24
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• 2019

This paper was prepared to investigate the behavior of fragments in underwater torpedo explosion beneath a frigate or surface ship by using an explicit finite element analysis. In this study, a fluid-structure interaction (FSI) methodology, called the multi-material arbitrary Lagrangian-Eulerian (MM-ALE) approach in LS-DYNA, was employed to obtain the responses of the torpedo fragments and frigate hull to the explosion. The Euler models for the analysis were comprised of air, water, and explosive, while the Lagrange models consisted of the fragment and the hull. The focus of this modeling was to examine whether a worst-case fragment could penetrate the frigate hull located close (4.5 m) to the exploding torpedo. The simulation was performed in two separate steps. At first, with the assumption that the expanding skin of the torpedo had been torn apart by consuming 30% of the explosive energy, the initial velocity of the worst-case fragment was sought based on a well-known experimental result concerning the fragment velocity in underwater bomb explosion. Then, the terminal velocity of the worst-case fragment that is expected to occur before the fragment hit the frigate hull was sought in the second step. Under the given conditions, the possible initial velocities of the worst-case fragment were found to be very fast (400 and 1000 m/s). But, the velocity difference between the fragment and the hull was merely 4 m/s at the instant of collision. This result was likely to be due to both the tremendous drag force exerted by the water and the non-failure condition given to the frigate hull. Anyway, at least under the given conditions, it is thought that the worst-case fragment seldom penetrate the frigate hull because there is no significant velocity difference between them.

• Journal of Korean Society of Steel Construction
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• v.11 no.1 s.38
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• pp.23-31
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• 1999

The concept models are used for the analysis of joints because they are simple to use and accurate. The modeling parameters of concept models are estimated using the results of experiments performed on the joints. The concept joint models accurately describe the behavior of joints under the loads which are used in the experiments for the estimation of parameters. However, they may not be accurate under the loads which are not used in the experiments. The accuracy can be dependent on the loads which are used in the evaluation of accuracy. In this study, antioptimization is presented to find the worst possible loads, under which the accuracy of concept joint models can be evaluated. The procedure was applied to the accuracy evaluation of concept joint models in an isolated 3-D joint and 2-D joints of a vehicle structure.

• Journal of the Korean Society of Manufacturing Process Engineers
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• v.16 no.1
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• pp.102-111
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• 2017

An automobile ball joint is the element for connecting the control arm and the knuckle arm, allowing rotational motion. The ball joint consists of the stud, plug, socket, and seat. These components are assembled through the caulking process that consists of plugging and spinning. In the existing research, the pull-out strength and gap stiffness were calculated, but we did not consider the uncertainties due to the numerical analysis and production. In this study, the uncertainties of material property and tolerance are considered to predict the distributions of pull-out strength and gap stiffness. Also, pull-out strength and gap stiffness are predicted as the a distribution rather than one deterministic value. Furthermore, a robust design applying the Taguchi method is suggested.

• The Transactions of the Korean Institute of Power Electronics
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• v.10 no.4
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• pp.403-410
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• 2005

This Paper Presents development of solar may shunt switching unit with a fully regulated Power regulation for Geostationary Earth Orbit(GEO) satellite. This shunt switching unit comprises the solar may shunt modules that regulate the solar array power. These solar array shunt modules connect/disconnect the solar array segments to/from the bus through switching actions. And that is also possible simply extension to an existing design by FPGA control logic changing. In order to verify the proposed design, the control logic and worst case analysis are analyzed and the simulation and experimental results we shown.

• Proceedings of the KIPE Conference
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• 2012.11a
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• pp.243-244
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• 2012

ITER 초전도자석 전원공급장치에서 고장의 종류는 단락, 단락 외 컨버터 내부고장 그리고 여러 외부요인에 의한 고장 크게 세 가지로 구분된다. 여기서 단락 외 컨버터 내부고장과 외부요인에 의한 고장은 보호시스템 및 장치의 동작으로 인해 피해가 축소된다. 하지만 단락시에는 보호시스템이 동작하더라도 단락전류가 매우 커 큰 피해를 줄 수 있다. 또한 ITER 초전도자석 전원공급장치는 운전 중 발생 가능한 부하의 단락으로부터 초전도자석 및 다른 장치 등을 보호하기 위하여 ITER에서 요구하고 있는 FSC(Fault Suppression Capability: 고장 억제 능력) 조건을 만족해야 한다. FSC 조건에서 전원공급장치는 출력에서 300 kA의 단락전류가 흐를 경우에도 80 ms(50 Hz, 4주기)동안 전기적 고장 없이 견뎌야 한다. 본 논문에서는 전원공급장치에서 발생될 수 있는 주요 단락 항목을 소개하고, 최악의 조건에서 단락전류에 의한 전원공급장치의 고장해석을 통해 FSC 요건을 만족하는 소자 선정 및 구조설계의 적합성을 검증한다.

• Journal of the Korean Institute of Gas
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• v.24 no.6
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• pp.83-90
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• 2020

This study conducted a risk assessment using the HyKoRAM program created by international joint research. Risk assessment was conducted based on accident scenarios and worst-case scenarios that could occur in the facility, reflecting design specifications of major facilities and components such as compressors, storage tanks, and hydrogen pipes in the hydrogen charging station, and environmental conditions around the demonstration complex. By identifying potential risks of hydrogen charging stations, we are going to derive the worst leakage, fire, explosion, and accident scenarios that can occur in hydrogen storage tanks, treatment facilities, storage facilities, and analyze the possibility of accidents and the effects of damage on human bodies and surrounding facilities to review safety.