• 한국신재생에너지학회:학술대회논문집
• /
• 2007.11a
• /
• pp.462-465
• /
• 2007

석탄가스화 수소생산 기술 분야는 석탄 등의 화석연료를 이용하여 고온, 고압하에서 반응가스(산소, 수증기, 수소)와의 화학적 반응을 통해 생산된 연소성 가스 ($H_2$, CO, $CO_2$ 등)를 전환반응(WGS) 및 분리반응을 거쳐 효율적으로 청정하게 수소를 생산해 내는 기술이다. 전력산업에서 석탄가스화 수소생산은 그 사용 방법(연료전지, 수소 터빈, 분산 이용 등)에 따라 발전시스템의 고효율화를 지향하고, zero-emission을 실현하는 첨단 발전 시스템의 종합 구현을 목표로 하고 있으며, 더불어, 도래하는 수소 경제로의 전이에 대비에 석탄을 이용한 중앙(Central) 수소생산 시스템을 구현하여 이송 및 전환을 통한 지역적 분산 이용을 가능케 하는 종합적인 인프라를 구축하는 기술이다. 본 기술에는 석탄가스화 기술, 수성가스 전환기술, 수소/$CO_2$ 분리기술, 이송용 연료 전환기술 등이 포함된다. 석탄가스화 수소생산 기술은 급등하는 오일 가격과 이의 수입사용 증가에 대응하기 위한 에너지 안보 대책 마련 및 효율 극대화의 필요성과 더불어, 전력산업에서 화력 발전시스템의 궁극적 실현 목표인 고효율, 초청정의 전력생산 시스템의 구현을 가능케 하여, 향후 화석 연료를 이용한 미래 발전 기술을 선도 할 것으로 기대된다. 더불어, 수소 경제로의 전환 시 수소 수요의 급팽창에 대비한 경제적인 대규모 수소생산 기술의 개발이 필요하며, 이에 기술 실현성이 가장 높은 석탄가스화 수소생산 기술의 개발 구현이 요구된다.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.38 no.5
• /
• pp.477-481
• /
• 2010

Some rotorcraft fuel tanks are required to be self-sealing and crashworthy for enhancing the survivability of crews. Self-sealing capability prevents the fuel leakage through contacting fuel with self-sealing material when the tank wall is penetrated by projectiles such as bullets. US army established MIL-DTL-27422D which specifies the detail requirements related to gunfire resistant fuel tank especially for military rotorcraft. The Fuel tanks for Korea Helicopter Program have been developed in accordance with MIL-DTL-27422D. The Self-sealing capability of the fuel tanks has been confirmed by the gunfire resistance test which specified on the MIL-DTL-27422D.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.38 no.8
• /
• pp.806-812
• /
• 2010

Fuel tanks for rotorcraft have a great influence on the survivability of crews. The philosophy of crashworthy rotorcraft design evolved from the long term effort of the US Army. US army established MIL-DTL-27422D for specifying detail requirements related to crash resistant fuel tank especially for military rotorcraft to prevent post crash fire which is the greatest threat to life in rotorcraft crash. Crashworthiness of the rotorcraft fuel tank could be guaranteed through the crash impact tests which are specified in the MIL-DTL-27422D. Fuel tanks for Korea Helicopter Program have been developed and tested according to MIL-DTL-27422D with minor modifications of flexible fittings. The present study shows some results of the mandatory crash impact tests of the fuel tanks to verify their performances.

• 한국신재생에너지학회:학술대회논문집
• /
• 2008.05a
• /
• pp.17-20
• /
• 2008

HYOSUNG manufactured and tested 1kW class PEFC systems to generate electrical and thermal energy for each residential usage. In particular, HYOSUNG developed power conditioning system that performs over 91% electrical conversion ratio specified in 1kW class PEFC systems. Prior to system integration, we tested each performances of components to derive control issues from it. In addition, we have been developing the adequate simulator to describe and predict system performance. In this paper, we verified HYOSUNG's 1kW class PEFC systems are valid for residential energy sources by testing the characteristics of systems and performances of main components.

• Transactions of the Korean Society of Automotive Engineers
• /
• v.11 no.3
• /
• pp.20-27
• /
• 2003

In this paper, the fuel transport characteristics during transient condition was studied by using a Fast Response Flame Ionization Detector(FRFID). The quantitative measurement method for the inducted fuel mass into cylinder is studied. The inducted fuel mass into the cylinder was estimated by using calculated air-fuel ratio by hydrocarbon concentration of cylinder and air flow model. In order to estimate the transportation of injected fuel from the intake port into cylinder, the wall wetting fuel model was used. The two coefficient $\alpha$,$\beta$) of the wall-wetting fuel model was determined from the measured fuel mass that was inducted into the cylinder at the first cycle after injection cut-off To reduce an air/fuel ratio fluctuation during rapid throttle opening, the appropriate fuel injection rate was obtain from the wall wetting model with empirical coefficients. Result of air/fuel ratio control, air/fuel excursion was reduced.

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.24 no.4
• /
• pp.512-518
• /
• 2000

A wall fuel-film flow model is developed to predict the effect of a wall-fuel-film on air-fuel ratio in an SI engine in transient conditions. Fuel redistribution in the intake port resulting from charge backflow and a simple liquid fuel behavior in the cylinder are included in this model. Liquid fuel film flow is calculated of every crank angle degree using the instantaneous air flow rate. The model is validated by comparing the calculated results and corresponding engine experiment results of a commercial 4 cylinder DOHC engine. The predicted results match well with the experimental results. To maintain the constant air-fuel ratio during transient operation. the fuel injection rate control can be obtained from the simulation result.

• Transactions of the Korean hydrogen and new energy society
• /
• v.22 no.4
• /
• pp.481-487
• /
• 2011

A fuel cell vehicle using a polymer electrolyte membrane fuel cell (PEM FC) as power source produces electric power by consuming the fuel, hydrogen. The unconsumed hydrogen is recirculated and reused to gain higer stack efficiency and to maintain the humidity in the anode side of the stack. So it is needed considering fuel efficiency to recirculated hydrogen. In this study, the indirect hydrogen recirculation flow rate measurement method for fuel cell vehicle is presented. By modeling of a convergent nozzle ejector and a hydrogen recirculation blower for the hydrogen recirculation of a PEM FC, the hydrogen recirculation flow rate was calculated by means of the mass balance and heat balance at Anode In/Outlet.

• Transactions of the Korean Society of Automotive Engineers
• /
• v.25 no.3
• /
• pp.326-335
• /
• 2017

It is known that diesel engines have the disadvantage of high emission levels of NOx and PM. Therefore, many combustion strategies have been developed to reduce these harmful NOx and PM emissions in a diesel engine. Among these strategies, HCCI(Homogeneous Charge Compression Ignition) and PCCI(Premixed Charge Compression Ignition) are the most popular as these can reduce NOx and PM simultaneously. However, when a single fuel like diesel is applied, it is difficult to control the combustion phase and this can lead to power reduction. In this study, premixed gasoline and pilot diesel were used to overcome the problems of controllability of the combustion phase and harmful emissions. We injected gasoline directly into the combustion chamber and the gasoline/air mixture was ignited with a pilot diesel fuel near the top dead center. The results showed that the combustion and emission characteristics of dual-fuel combustion were comparable to those of conventional diesel combustion. When we applied the dual-fuel PCCI combustion concept, more than 90 % of NOx and PM emission was reduced simultaneously without significant degradation of efficiency compared to conventional diesel combustion.

• 한국신재생에너지학회:학술대회논문집
• /
• 2005.11a
• /
• pp.553-553
• /
• 2005

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 2014.04a
• /
• pp.242-243
• /
• 2014