• Journal of Navigation and Port Research
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• v.44 no.4
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• pp.283-290
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• 2020

BOG (Boil Off Gas) generation is unavoidable in the liquefied hydrogen carrier, and proper measures are necessary to prevent pressure problems inside the cargo tank. The BOG can be used as propulsion fuel for ships, and the remaining parts used for propulsion must be effectively managed, such as in the form of reliquefying or burning. This study proposes an BOG reliquefaction system optimized for a 160,000 m3 liquefied hydrogen carrier with a hydrogen propulsion system. The system comprises a hydrogen compression and helium refrigerant section, and increases the efficiency by effectively using the cold energy of the BOG discharged from the cargo tank. In this study, the system was evaluated through the exergy efficiency and SEC (Specific Energy Consumption) analysis according to the rate of the reliquefaction of the BOG while the hydrogen BOG with a supply temperature of -220℃ entered the reliquefaction system. As a result, it showed SEC of 4.11 kWh/kgLH2 and exergy efficiency of 60.1% at the rate of reliquefaction of 20%. And the parametric study of the effects of varying the hydrogen compression pressure, inlet temperature of the hydrogen expander, and the feed hydrogen temperature was conducted.

• Applied Chemistry for Engineering
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• v.31 no.2
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• pp.153-163
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• 2020

Compared to gaeous hydrogen, liquid hydrogen has approximately 1/800 volume, 800 times higher volumetric energy density at the same pressure, and the advantage of lower explosion risk and easier transportation than gaseous hydrogen. However, hydrogen liquefaction requires larger scale facility investment than simple compression storage method. Therefore, the research on energy-saving hydrogen liquefaction processes is highly necessary. In this study, helium/neon (mole ratio 80 : 20) refrigeration cycle was investigated as the main refrigeration process for hydrogen liquefaction. Process simulation for less energy consumption were carried out using PRO/II with PROVISION V10.2 of AVEVA. For hydrogen liquefaction, energy consumption was compared in three cases: Using a helium/neon refrigerant cycle, a SMR+helium/neon refrigerant cycle, and a C3-MR+helium/neon refrigerant cycle. As a result, the total power consumptions of compressors required to liquefy 1 kg of hydrogen are 16.3, 7.03 and 6.64 kWh, respectively. Therefore, it can be deduced that energy usage is greatly reduced in the hydrogen liquefaction process when the pre-cooling is performed using the SMR process or the C3MR process, which have already been commercialized, rather than using only the helium/neon refrigeration cycle for the hydrogen liquefaction process.

• Journal of Power System Engineering
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• v.11 no.1
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• pp.76-81
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• 2007

The objective of this study is to find the optimum design of a snubber using CFD analysis. Several dimensions such as snubber height(H), snubber diameter(D), buffer width and buffer angle are considered in this study. The present study shows that the CFD can be applied to study the pressure characteristics inside the snubber. The objective of the snubber design optimization are to minimize a pressure loss and the pulsation ratio. Numerical results such as particle track, pressure distribution and turbulent kinetic energy are used to analyze the critical area and pressure behavior inside the snubber. As a result, snubber model with H/D ratio of 3.23 and buffer angle of $40^{\circ}$ has a minimum pressure loss. On the other hand, snubber model with H/D ratio 4.41 and buffer angle $10^{\circ}$ has a minimum pulsation ratio.

• Journal of Hydrogen and New Energy
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• v.17 no.1
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• pp.1-7
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• 2006

The free-piston hydrogen fueled engine is estimated as the next generation power system which can obtain high efficiency and low emission, simultaneously. In order to develop the free-piston hydrogen fueled engine, it is necessary to stable the combustion. The engine combustion, backfire and knock phenomenons were studied by using RICEM for researching combustion characteristics of free-piston engine. As the results, backfire occurrence was not observed in the free-piston engine under limited experimental condition. And knocking occurred in case of higher cylinder wall temperature.

• Journal of Hydrogen and New Energy
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• v.17 no.2
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• pp.227-233
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• 2006

A free-piston hydrogen fueled engine is considered as one of the next power systems which is able to obtain high efficiency and low emission, simultaneously. In this study, in order to ensure the possibility as the next generation power system, the combustion characteristics and the performance of the free-piston hydrogen fueled engine are analyzed by using the linear RICEM for the change of injection pressure and equivalence ratio. As the results, in-cylinder maximum pressure is shown at injection pressure $P_{inj}$=6bar. Backfire phenomenon is not observed under experimental condition and knock occurs over ${\Phi}=0.8$. The thermal efficiency is the highest at injection pressure, $P_{inj}$=6bar and equivalence ratio, ${\Phi}=0.7$, respectively.

• Elastomers and Composites
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• v.44 no.1
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• pp.76-83
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• 2009

The purpose of this study was to investigate the effects of combined use of several types of silicone polymers on the physical properties of the dental polyvinylsiloxane impression materials (PVS). Four types of silicone prepolymers having different molecular weight and vinyl group position, and two types of cross-linkers having differently located silyl hydride functional groups were used in various combinations for the formulation. The samples containing bimodal or trimodal prepolymers showed higher tensile strength, elongation at break, and elastic deformation than those containing only one type of prepolymer. The samples using CR210 cross-linker which has side- and terminal-silyl hydride groups showed higher elastic deformation and elongation at break than those using CR101 cross-liker which has side-only silyl hydride group. High vinyl content prepolymer having side vinyl group delayed setting even though it enhanced tensile strength. Further studies are needed to clarify the specific role of this component on setting time and to find appropriate controlling methods for making improved PVS with optimum workability.

• Journal of Hydrogen and New Energy
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• v.27 no.6
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• pp.651-659
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• 2016

Korea Institute of Machinery & Materials (KIMM) has developed a high efficient Stirling cryocooler with moving magnet linear compressor for precooling hydrogen liquefier and cooling high temperature superconductor (HTS) devices, such as superconductor cable and superconductor fault current limiters. Hydrogen liquefier and HTS electric devices require cryocooler with cooling capacity of hundred watts to kilowatts at 77 K. The compressor in the Stirling cryocooler uses opposed moving magnet linear motors to drive opposed pistons. High efficient Stirling cryocooler is designed by SAGE-software, manufactured and tested systematically. A cooling capacity of 1 kW at 77 K with an electric input power of 9.6 kW has been analyzed. But prototype test results of the Stirling cryocooler have the cooling capacity of 0.65 kW at 76.8 K with an electric input power of 8.1 kW. And then, 21.5% Carnot COP (Coefficient of performance) of the prototype Stirling cryocooler is achieved. The comparison analysis between SAGE-model and experimental results has shown the direction for further design optimization of the Stirling cryocooler.

• Proceedings of the Korean Vacuum Society Conference
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• 1999.07a
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• pp.46-46
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• 1999

터보분자펌프(turbomolecular pump, TMP)는 각종 연구장비, 반도체 제조장치, 가속기, 핵융합 실험 장치 등 여러 분야에서 가장 널리 쓰이는 고진공 펌프로서 자리잡고 있다. 이런 TMP의 광범위한 사용에도 불구하고 성능평가에 관한 통일된 규격이 마련되어 있지 않다. 국제 규격협회(ISO)의 터보분자펌프 성능평가방법 시안을 토대로 제정중인 KS 규격은 아직 실험적인 근거를 자체적으로 가지고 있지 못하므로 앞으로 각 항목들에 대한 많은 실험이 수행되어야 한다. TMP의 성능을 나타내 주는 항목들 중 배기속도(pumping speed)와 압축비(compression ratio)는 가장 중요한 것들로서 다른 고진공 펌프 및 TMP 상호간의 성능을 비교할 수 있는 기본 항목이라 할 수 있다. 본 실험에서는 종래의 단순 TMP와 큰 기체유량에서도 안정된 배기속도를 유지하는 복합터보분자펌프(compound molecular pump, CMP)의 배기속도와 압축비 및 임계배압(critical backing pressure)을 KS 규격안대로 시험 평가하여 안의 평가방법과 기준의 타당성을 검토하고, 두 가지 다른 방식의 펌프에 적용할 수 있는지를 검토하였다. TMP 및 CMP 흡기구에 표준용기를 부착하고 수소 및 질소 기체를 사용하여 흡기구 압력을 변화시키면서 배기속도 및 압축비를 측정하고 배기구 압력을 변호시키면서 최대압축비 및 임계배압을 측정하였다. 흡기구의 압력측정에는 인출형 전리진공계(EG)를 사용하였고, 배기구의 압력측정은 전기용량의 격막진공계(CDG)와 피라니 진공계로 측정하였다. 진공계는 모두 회전식 점성진공계(SRG)로 교정한 후 사용하였다.

• 기계와재료
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• v.24 no.1
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• pp.26-35
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• 2012

가스액화플랜트는 질소, 산소, 헬륨 등 고순도의 가스를 효율적으로 저장 및 운송을 위해 가스를 액체로 변환하는 플랜트로, 대표적인 플랜트로는 질소, 산소, 아르곤 등의 가스를 생산하는 공기분리플랜트, 헬륨액화플랜트, 수소액화플랜트, 천연가스액화플랜트 등이 있다. 질소, 산소, 수소 등의 가스는 산업의 전반적인 분야에서 널리 사용되고 있으며, 국내의 경우 철강, 반도체, 디스플레이제조산업 등 가스 다소비 분야의 비약적인 발전에 따라 급격하게 수요가 증가하고 있는 상황이다. 대용량의 가스액화플랜트는 원료로부터 불순물을 제거하고, 팽창 또는 열교환 과정을 통해 가스를 액체로 변환하는 극저온기술로 주로 구성되며, 이와 같은 과정은 압축기, 열교환기, 증류탑, 팽창터빈, 콜드박스 등의 구성요소에 의해 구현된다. 따라서 가스액화플랜트에서 효율적인 극저온의 생성 및 유지는 플랜트의 경제성 제고를 위해 핵심적인 요소이다.

• Journal of Hydrogen and New Energy
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• v.15 no.3
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• pp.175-186
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• 2004

In this paper, we developed the dynamic model of a fuel cell system suitable for controller design and system operation. The transient phenomena captured in the model include the flow characteristics and inertia dynamics of the compressor, the intake manifold filling dynamics, oxygen partial pressures and membrane humidity on the fuel cell voltage. In the simulations, we paid attention to the transient behavior of stack voltage and compressor pressure, stoichiometric ratio. Simulation results are presented to demonstrate the model capability. For load current following, stack voltage dynamic characteristics are plotted to understand the Electro-chemistry involved with the fuel cell system. Compressor pressure and stoichiometric ratio are strongly coupled, and independent parameters may interfere with each other, dynamic response, undershoot and overshoot.