• Journal of the Korean Institute of Gas
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• v.18 no.1
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• pp.25-30
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• 2014

Mixture of hydrogen and natural gas HCNG mixing equipment production and refueling experiment were performed for supply and product. Hydrogen and CNG in 30 : 70 ratio is mixing of HCNG was performed using ratio control. HCNG refueling method was calculated after reading the pressure of tank for full refuel, amount refuel. Both full refuel and amount refuel results mixed ratio 30 : 70 in the error limits of $H_2{\pm}2%$ met the criterion. HCNG composition analysis result in refueling tank using gas chromatography is satisfying the error limits in refuel tank 30 : 70 ratio were confirmed.

• Journal of the Korean Institute of Gas
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• v.4 no.3 s.11
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• pp.53-58
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• 2000

It was carried out consequence analysis(CA) of CNG (compressed natural gas) service station and we compared the results of CA of CNG service station with LPG service station which was installed by high Pressure gas law. The results of CA were that distance of CNG LFL was 1.5 times than the length of LPG LFL. Thermal radiation effect about CNG may not be showed damage of process facilities, but in the case of LPG, it was enough to have an large damage effect on a downtown. The thermal radiation of 37.5 $kw/m^2$ extended 12.6 m. Also, in the case of 12.5 $kw/m^2$ which was able to burn wood, the radiation effect of LPG is 3 times than CNG.

• Proceedings of the KIPE Conference
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• 2015.07a
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• pp.528-529
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• 2015

본 논문은 DC-DC 플라이백 컨버터 회로를 바탕으로, 고전압 입력으로부터 다채널의 절연된 저전압을 출력하는 고압 SMPS에 관한 것이다. 제안된 토폴로지는 고전압을 분배하는 커패시터와 MCU 전용의 커패시터를 직렬로 구성하고, 각 커패시터에 분배된 전압을 입력으로 다중여자 방식의 플라이백 컨버터 구조로 되어있다. 직렬 커패시터 구조는 고압환경에서의 소자들의 절연 및 전압스트레스를 저감할 수 있으며, MCU 전용의 커패시터는 시스템의 초기구동을 위한 자가충전(Self-Power) 및 Black-Start의 시스템 안정화 구조이다. 또한 다중여자방식은 변압기의 단일 코어를 사용하여 스위칭 전류를 흘려줌으로서 커패시터의 전압불균형을 막을 수 있는 장점을 가지고 있다. 제안된 토폴로지는 시뮬레이션을 통하여 타당성을 검증하였다.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.153.1-153.1
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• 2012

조립 후 발사대로 이송된 추진기관(또는 발사체)는 지상시험 및 비행시험을 위한 충전을 하게 되는데, 추진제 및 고압가스 등 추진기관 구성품의 운용절차는 하드웨어의 설계 단계에서 그 개념이 수립되어야 한다. 다시 말해, 발사체 및 추진기관 설계 단계에서 연료와 산화제의 충전/배출, 시험 취소시의 운용절차 개념이 수립되어 있어야 추진기관 구성품들의 설계, 지상인터페이스 구성품의 설계에 그 내용이 반영될 수 있다. 따라서, 본 논문에서는 발사체 및 추진기관 운용와 관련된 일반적인 충전/배출 절차와 지연 또는 취소시의 작업절차의 주요개념을 다루었고, 추진기관 운용에 필요한 각종 지상설비에 요구되는 주요 기능을 검토하였다. 또한, 추진제 충전 이후 발사 대기시까지의 업무와 발사 전에 수행되어야 하는 추진기관 운용 업무(Pre-Launch Operation)도 다루었다. 특히 다단 발사체의 경우에는 운용과 관련된 준비 업무량이 단수에 비례하여 늘어나므로, 효율적으로 모든 시험 준비 업무를 마치기 위해, 지상에서의 추진기관 운용절차는 각 단별로 유기적으로 진행되어야 한다. 즉, 각 단별 하드웨어에 대한 사전 검사, 충전, 대기 등의 운용시간 설계 및 그 절차가 중요하다. 한국형 발사체 및 추진기관의 운용 개념설계를 수행하는데에는 기 확보된 운용기술을 활용하였다.

• Journal of Korea Foundry Society
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• v.24 no.4
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• pp.238-248
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• 2004

고압 다이캐스팅에서 요구되고 있는 고품질의 주조를 위해, 비교적 간단한 개선 방안으로 용탕 주입 방법의 개선이 실험적으로 시도 되었으며, 그로 인해 많은 경우에 긍정적인 결과가 관찰 되었다. 특히, 냉가압 다이캐스트에서, 금형내 용탕의 예충전을 유도하는 용탕 주입의 속도 및 플렌저의 위치제어를 통해 기공율의 저하 및 그로 인한 기계적 강도의 개선 효과를 확인 할 수 있었다. 본 논문은, 그 원인과 결과 대한 연구를 위해, 상용 해석 도구인 Flow3D를 이용, 금형내 용탕의 흐름을 모델링을 통해 가시화하여 용탕의 주입속도 및 위치의 변화가 주물의 품질에 미치는 영향을 조사하였다. 용탕 주입을 위한 플런저의 속도 및 위치 제어의 변수로, 1) 금형내에 용탕의 예충전 유도를 위한 용탕 고속 주입 지연 정도, 2) 플런저의 저속운행에서 고속으로의 가속도, 3) 용탕의 예충전 동안의 플런저 속도를 선택, 그로 인한 영향을 연구 분석 하였고, 그 결과로 플런저의 속도 및 위치 조절을 통하여 금형내 갇힌 공기의 양이 줄어 들 수 있음을 알 수 있었다.

• Journal of the Korean Institute of Gas
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• v.21 no.2
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• pp.58-63
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• 2017

Currently, the safety monitoring process in a complex plant environment is proceeded by human. Sometimes, human error that may occur in a filed causes an severe problem. This paper introduces new method of safety monitoring system using sound information and fuzzy theory that is one of intelligent theories, in order to recognize the status of plant environment. In this paper, the filling station of high pressure gas will be used as a test plant. The result system will be widely applied for more complex plant environments.

• Journal of Hydrogen and New Energy
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• v.33 no.2
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• pp.158-163
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• 2022

The test method on the Type II high-pressure hydrogen storage tanks made of the metal wire hoop winding is a complex and high risk. Also closeup on the tank being test is difficult. In this study, we studied a mechanical test method for a high-pressure hydrogen tanks. This method must be simple, risk-free and possible to observe the change in microscopic behavior of a metal wire on a liner. As the results, it was possible to observe the microscopic behavior on the metal wire by the mechanical test method. Also, a simple and risk-free test was possible compared to the conventional test method for high pressure hydrogen tanks.

• Journal of the Korean Institute of Gas
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• v.14 no.2
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• pp.1-6
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• 2010

The strength safety of high pressure gas cylinder has been analyzed by using a finite element method. In this study, the internal gas pressures of a steel bombe include a service charging pressure of $9kg/cm^2$, high limit charging pressure of $18.6kg/cm^2$, high limit of safety valve operation pressure $24.5kg/cm^2$, and hydraulic testing pressure of $34.5kg/cm^2$. The computed FEM results indicate that the strength safety for a service charging pressure of $9kg/cm^2$ and high limit charging pressure of $18.6kg/cm^2$ is safe because the stress of a gas cylinder is within yield strength of steel. But the stress for a hydraulic testing pressure of $34.5kg/cm^2$ sufficiently exceeds the yield strength and remains under the tensile strength. If the hydraulic testing pressures frequently apply to the gas cylinder, the bombe may be fractured because a fatigue residual stress is accumulated on the lower round end plate due to a plastic deformation. The computed results show that the concentrated force in which is applied on a skirt zone does not affect to the lower round end plate, and the most weak zone of a bombe is a middle part of a lower round end plate between a bombe body and a skirt for a gas pressure. Thus, the FEM results show that the profile of a lower round end plate is an important design parameter of a high pressure gas cylinder.

• Journal of Hydrogen and New Energy
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• v.32 no.3
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• pp.163-171
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• 2021

Securing energy sources is a key element essential to economic and industrial development in modern society, and research on renewable energy and hydrogen energy is now actively carried out. This research was conducted through experiments and analytical methods on the hydrogen filling process in the hydrogen storage tank of the hydrogen charging station. When low-temperature, high-pressure hydrogen was injected into a high-pressure tanks where hydrogen is charged, the theoretical method was used to analyze the changes in temperature and pressure inside the high-pressure tanks, the amount of hydrogen charge, and the charging time. The analysis was conducted in the initial vacuum state, called the First Cycle, and when the residual pressure was present inside the tanks, called the Second Cycle. As a result of the analysis, the highest temperature inside the tanks in the First Cycle of the high-pressure tank increased to 442.11 K, the temperature measured through the experiment was 441.77 K, the Second Cycle increased to 397.12 K, and the temperature measured through the experiment was 398 K. The results obtained through experimentation and analysis differ within ±1%. The results of this study will be useful for future hydrogen energy research and hydrogen charging station.

• Journal of the Korean Institute of Gas
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• v.27 no.4
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• pp.78-84
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• 2023

Recently, the world's countries are tightening regulations on CO2 and air pollutants emission to solve them. In addition, eco friendly vehicles is increasing to replace automobiles in internal combustion engine. The government is supporting the expansion of hydrogen refueling infrastructure according to the hydrogen economy road map. In particular, refueling station is important to secure the safety that supplies high-pressure hydrogen with a wide LFL range. This paper is on guidelines for the determination safety distances to ensure worker safety from accident as jet fire. The safety distance is set according to the procedure of the EIGA doc 075/21. For accident frequency is upper 3.5E-05 per annum, safety distance is decided via consequence analysis where the risk of harm is below individual harm exposure threshold.