• 전기학회논문지
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• 제63권1호
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• pp.184-190
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• 2014

Fuel cell power system, unlike conventional energy sources, converts chemical energy into electrical energy through electrochemical reaction of hydrogen and oxygen. In recent years, railway field as well as mobile fuel cell power system is being studying actively with development of hydrogen storage technologies. This paper presents the feasibility study on small-scale prototype electric railway vehicle application using fuel cell generation system. it is confirmed that proposed fuelcell-battery hybrid system shows good response characteristic about speed and torque based on design of parameter on system. Also as results of response for proposed system modeling, it show that powering mode and braking mode of system is controlled by switching devices of converters.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2007년도 춘계학술대회 논문집
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• pp.727-728
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• 2007

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2005년도 연구개발 발표회 논문집
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• pp.684-689
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• 2005

Parametric calculation were conducted to estimate performance of variable geometry of hydrogen recirculation blower for fuel cell vehicle. The pressure rise and efficiency are effected by change of the geometric parameter of impeller and casing, and stripper clearance under various mass flow. Hydrodynamic performance were evaluated, and also the inner flow fields were investigated by CFD. Calculated results show good coincidence with experimental test results of total pressure performance. Performance of model designed by parametric calculations satisfied experimental data of verification model.

• 한국수소및신에너지학회논문집
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• 제19권1호
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• pp.26-34
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• 2008

This study presents an aerodynamic design and an experimental performance test of a turbo air compressor consisted of mixed-flow impeller and curved diffuser for the PEM fuel cell vehicle application. Many studies compare the efficiency, cost or noise level of high-pressure and low-pressure operation of PEM fuel cell systems. Pressure ratio 2.2:1 is considered as design target The goal of compressor design is to enlarge the flow margin of compressor from surge to choke mass flow rate to cover the operational envelope of FCV. Large-scale rig test is performed to evaluate the compressor performance and to compare the effects of compressor exit pipe volume to stall or surge characteristics. The results show that the mixed-flow compressor designed has large flow margin, and the flow margin of compressor configuration with small exit volume is larger than that with large exit volume.

• 한국수소및신에너지학회논문집
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• 제25권5호
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• pp.516-524
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• 2014

Proper discharge of nitrogen gas and water condensate is required in a conventional fuel cell system for performance, stability and durability of fuel cell stacks. Present study covers the development of integrated unit and its functioning logic for simultaneous nitrogen gas purge and water condensate drainage in a fuel cell vehicle system. Configuration of condensate drainage pipe, purge valve and level sensor is considered and optimized in physical integration. As a key factor, discharge time is considered and optimized based on the test result of constant-current operation with various operating temperature in logic development. Consequently, derived optimal values are applied and verified in actual vehicle drive mode test. Increase of system design flexibility, weight reduction and cost reduction are anticipated with this study. Additional study for physical and logical improvement is currently being implemented.

• 에너지공학
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• 제23권3호
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• pp.132-145
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• 2014

수소연료전지자동차(FCV)의 냉온기동, 가속, 주행성능, 수소연료충전시간, 및 항속거리 등의 기술 항목들은 2015-2020년경의 수요자요구를 충족하는 것으로 보인다. 그러나 짧은 내구성, 높은 가격 및 부족한 수소공급인프라 등은 본격적인 FCV 상용화를 위하여 극복해야 할 과제이다. 가격저감 및 내구성 향상 등 연료전지자동차의 상용화를 위하여 개발되고 있는 기술과제들을 중심으로 수소연료전지자동차의 기술동향을 분석한다.

• Advances in aircraft and spacecraft science
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• 제9권1호
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• pp.17-37
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• 2022

This paper discusses an improved unmanned aerial vehicle, UAV, configuration characterized by telescopic booms to optimize the flight mechanics and fuel consumption of the aircraft at various loading/flight conditions.The starting point consists of a full-composite smaller UAV which was derived by a general aviation ultralight motorized aircraft ULM. The present design, named ToBoFlex, extends the two-booms configuration to a three tons aircraft. To adapt the design to needs relevant to different applications, new solutions were proposed in aerodynamic fields and materials and structural areas. Different structural solutions were reported. To optimize aircraft endurance, the innovative concept of Telescopic Tail Boom was considered along with two different tails architecture. A new structural configuration of the fuselage was proposed. Further consideration of hydrogen fuel cell electric propulsion is now being studied in collaboration between the Polytechnic of Turin and Prince Mohammad Bin Fahd University which could be the starting point of future investigations.

• 한국수소및신에너지학회논문집
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• 제14권3호
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• pp.236-246
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• 2003

This paper focuses on developing a model of a PEM fuel cell stack and to integrate it with realistic model of the air supply system for fuel cell vehicle application. The fuel cell system model is realistically and accurately simulated air supply operation and its effect on the system power and efficiency using simulation tool Matlab/Simulink. The Peak performance found at a pressure ratio of 3, and it give a 15mV increase per cell. The limit imposed is a minimum SR(Stoichiometric Ratio) of 2 at low fuel cell load and 2.5 at high fuel cell load.

• 한국터널지하공간학회 논문집
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• 제23권1호
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• pp.47-60
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• 2021

수소는 차세대 에너지원으로서 수소경제 활성화 로드 맵에 따라 수소를 안정적으로 생산·저장·운송하기 위한 산업과 더불어 수소차의 보급이 급속도로 이루어질 것으로 예상된다. 이에 따라 터널과 같은 반밀폐공간에서의 수소차의 사고에 대비한 안전대책이 요구되고 있다. 본 연구에서는 도로터널에서 수소차량의 안전성을 확보하기 위한 연구의 일환으로 터널 내 수소차 사고에 따른 다양한 위험요인 중 가스 누출에 따른 화재와 폭발의 위험성에 대한 기초적인 조사·연구를 수행하였으며, 다음과 같은 결과를 얻었다. 수소차 사고 시 가스누출속도는 TPRD의 오리피스직경에 의존하며, 가스가 점화되는 경우에 최대화재강도는 오리피스직경에 따라 3.22~51.36 MW (오리피스직경: 1~4 mm)에 도달하나 지속시간이 짧기 때문에 화재로 인한 위험의 가중은 거의 없는 것으로 분석되었다. 등가 TNT방법에 의해서 폭발에 따른 과도압력을 계산하였으므로 폭발수율을 0.2적용하는 경우, 안전한계 거리는 대략 35 m 정도로 분석되고 등가사망자는 보수적인 관점에서 수십 명 정도에 달할 것으로 예측된다.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2007년도 추계학술대회 논문집
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• pp.165-168
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• 2007

The objective of this study is to demonstrate and commercialized for on-board fuel storage system for the hydrogen fuel cell vehicles. Type3 composite cylinder is consisting of the full wrapped composites on a seamless aluminum liner. Especially, the seamless aluminum liner has been commercialized with development of fabrication through this study. The key technologies, including design, analysis and the optimized filament winding process for 350bar composite cylinder, were established and verified with design qualification test in accordance with international standard. And the facilities for fabrication and design qualification test have been constructed.