• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.3
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• pp.58-63
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• 2009

The global restriction on pollutant emissions and the soaring of crude oil price are expected to result in the change of future transportation system. Hydrogen is considered to be the leading candidate as an alternative energy source before other new alternative energy sources emerge. Scientists anticipate that hydrogen fuel gas turbine engine and fuel cell will be the power plant of the aircraft in the near future. To realize the aircraft powered by fuel cell system in the future, the technologies such as fuel cell with higher energy density, compressed gas or liquid storage system of hydrogen fuel, and efficient and lightweight electric motor have to be developed first.

• 한국신재생에너지학회:학술대회논문집
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• 2011.05a
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• pp.189.2-189.2
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• 2011

매립가스(LFG)는 약 50v/v% 이상의 메탄가스로 이루어져 있어 LFG의 자원화 사업은 국내 신 재생에너지를 이용한 발전사업 중 태양광사업 다음으로 활발히 진행되고 있다. LFG의 대표적인 활용기술로는 가스엔진, 가스터빈 및 증기터빈을 이용한 발전과 중질가스 및 고질가스 형태의 연료로 생산하는 방식 등이 있으며 이러한 분야에 매립지가스를 적용하기 위해서는 장치 부식의 주 원인이 되는 황화수소 가스의 제거가 반드시 이루어져야 한다. 본 연구에서는 황화수소 제거를 위해 하이드레이트와 마찬가지로 동공을 형성하여 가스의 포집과 저장이 가능한 하이드로퀴논(HQ)을 이용하고자 한다. HQ은 $0^{\circ}C$ 부근에서 해리되는 하이드레이트와 달리 상온에서 고체 형태로 구조를 유지할 수 있어 가스의 포집 및 저장에 용이한 장점이 있다. 메탄, 이산화탄소, 황화수소 혼합가스에서 황화수소 90% 이상 제거를 목적으로 HQ와 반응시켜 동공 내에 이들 가스의 포집여부를 확인하였다.

• Journal of Aerospace System Engineering
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• v.17 no.6
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• pp.72-81
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• 2023

Hydrogen-fueled gas turbines are a promising technology that can resolve the carbon dioxide emission issue as future aviation propulsion engines and carbon-free power generations. To achieve high efficiency and stability of gas turbines using 100% hydrogen as fuel, an innovative design of combustor systems is necessary to consider the characteristics of hydrogen, which are different from those of conventional hydrocarbon fuels. Micromix is a combustor design method, which aims to terminate the reaction quickly by intense mixing of fuel and air, consequently reducing NOx and increasing the stability. In this paper, we examine the principles and design process of micromix combustors as a pure-hydrogen combustion technology, and we introduce a design of a 30 kW micromix hydrogen combustor for research.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.8
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• pp.805-811
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• 2009

An oxidizer pump of a turbopump for a 30-ton class gas generator cycle engine was tested in the medium of liquid oxygen. The turbine was driven by cold hydrogen gas in the test. The oxidizer pump was operated stably at both design and off-design conditions, satisfying the performance requirements. The pump head coefficient from the liquid oxygen test was 2~3% lower than that from the water test. The power required to run the oxidizer pump was well balanced with the power produced by the turbine.

• 한국신재생에너지학회:학술대회논문집
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• 2009.06a
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• pp.829-831
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• 2009

폐기물, 석탄 등 다양한 시료의 가스화 반응을 통해서 발생되는 합성가스는 CO, $H_2$, $CO_2$가 주성분으로 가스엔진, 가스터빈 등의 연료로 사용하여 발전하거나 합성반응을 통해 다양한 화학원료로의 전환이 가능하다. 또한 폐기물, 석탄 등의 다양한 원료의 가스화 반응에 의해 발생한 합성가스로부터 F-T(Fischer-Tropsch) 합성을 통한 인조합성석유, Non F-T 합성을 통한 메탄올, DME(Dimethyl Ether) 등을 제조할 수 있으며, 메탄화 반응을 통해 대체천연가스(SNG, Substitute Natural Gas)로 제조하여 활용하는 방안도 가능하다. 또한 현재 상업용 규모의 수소 제조 방법 중에서 가장 경제적인 방법으로 천연가스를 개질하여 CO, $H_2$가 주성분인 합성가스를 만든 다음 수성가스 전환, PSA(Pressure Swing Adsorption)통해 $CO_2$와 $H_2$를 분리하여 생산하고 있으나, 천연가스 가격의 상승 및 다양한 시료로부터 향후 경제성 확보가 가능한 수소 제조 방법에 대한 연구가 진행되고 있으며, 석탄 가스화 및 폐기물 가스화를 통해 얻어진 합성가스로부터의 수소 제조 공정이 개발 및 상업화 추진되고 있다. 본 연구에서는 폐기물 가스화를 통해 발생한 합성가스에 대하여 수성가스 전환 반응을 통한 수소 생산 특성 및 수성가스 전환 반응의 공간속도 변화 및 스팀주입량 변화에 따른 반응 특성을 고찰하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.3
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• pp.20-26
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• 2009

Turbopump test for a 30-ton-thrust liquid rocket engine was carried out using real-propellant. Liquid oxygen, kerosene, cold hydrogen gas were used for the oxidizer pump, the fuel pump, and the turbine, respectively. The turbopump was reliably operated at the design and off-design conditions and the performance requirements were satisfied, which implies that the turbopump development at the engine subsystem level is successfully accomplished in the point of performance validation. This paper presents the results of a test where the turbopump was run for 75 seconds at three operating modes. In terms of performance characteristics of pumps and turbine, the results of turbopump assembly test using real-propellant showed a good agreement with those of the turbopump component tests using simulant working fluid.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.11a
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• pp.359-365
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• 2008

Turbopump test for a 30-ton-thrust liquid rocket engine was carried out using real-propellant. Liquid oxygen, kerosene, cold hydrogen gas were used for the oxidizer pump, the fuel pump, the turbine, respectively. The turbopump was run stably at the design and off-design conditions and the performance requirements were satisfied, which implies that the turbopump development at the engine subsystem level is successfully accomplished in the point of performance validation. This paper presents the results of a test where the turbopump was run for 75 seconds at three operating modes. In terms of performance characteristics of pumps and turbine, the results from turbopump assembly test using real-propellant showed a good agreement with those from the turbopump component tests using simulant working fluid.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.20 no.12
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• pp.804-815
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• 2019

Due to the depletion and environmental problems of fossil fuel, biomass has arisen as an alternative energy source. Biomass is a renewable and carbon-neutral source. However, it is moister and has lower energy density. Therefore, biomass needs thermal chemical conversion processes like gasification, and it does not only produce a flammable gas, called 'syngas', which consists of CO, H2, and CH4, but also some unwanted byproducts such as tars and some particulates. These contaminants are condensed and foul in pipelines, combustion chamber and turbine, causing a deterioration in efficiency. Thus this work attempted to find a method to remove tars and particles from syngas with a filter which adopts a pre-coating technology for preventing blockage of the filter medium. Hydrated limestone powder and activated carbon(wood char) powder were used as the pre-coat materials. The removal efficiency of the tars was 86 % and 80 % with activated carbon(wood char) coating and hydrated limestone coating, respectively.

• Journal of the Korean Applied Science and Technology
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• v.34 no.4
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• pp.717-726
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• 2017

The current allowable cross-contamination level of fatty acid methyl esters (FAME) in aviation turbine fuel (AVTUR) is 50 mg/kg, due to that the presence of FAME in AVTUR can significantly impact the fuel supply system and jet engine. It has been difficult to analyze the level of FAME in AVTUR, since it is consisted of a lot of hydrocarbons. In this study, thus, a new method using multi-dimensional GC-MS (MDGC-MS) was proposed in order to determine the FAME level in AVTUR effectively. Applying to MDGC-MS with Deans switching system enabled us to detect and quantify the FAME with low carbon numbers such as those derived from coconut oil and palm kernel oil. The matrix effect of MDGC-MS method, which could shift the FAME peaks to slightly longer retention times, was reduced by 20 times compared with that of 1-dimensional GC-MS reference method. This developed method could be suitable for qualitative and quantitative analyses to determine the contamination level of trace FAME in AVTUR.