• JOURNAL OF ELECTRICAL WORLD
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• s.287
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• pp.54-55
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• 2000

• Journal of Energy Engineering
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• v.20 no.1
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• pp.13-20
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• 2011

The high fuel flexibility of Micro Gas Turbine(MGT) has boosted their use in a wide variety of applications. Recently, the demand for biogas generated from the digestion of organic wastes and landfill as a fuel for gas turbines has increased. We researched the influence of firing landfill gas(LFG) on the performance and operating characteristics of a micro gas turbine combined heat and power system. $CH_4$ and $CO_2$ simultaneous recovery process has been developed for field plant scale to provide an isothermal, low operating cost method for carrying out the contaminants removal in Land Fill Gas(LFG) by liquid phase catalyst for introduce into the green house for the purpose of $CO_2$ rich cultivation of the plants. Methane purification and carbon dioxide stripping by muti panel autocirculation bubble lift column reactor utilizing Fe-EDTA was conducted for evaluate optimum conditions for land fill gas. Based on inflow rate of LFG as 0.207 $m^3$/min, 5.5 kg/$cm^2$, we designed reactor system for 70% $CH_4$ and 27% $CO_2$ gas introduce into MGT system with $H_2S$ 99% removal efficiency. A green house designed for four different carbon dioxide concentration from ambient air to 1500 ppm by utilizing the exhaust gas and hot water from MGT system.

• JOURNAL OF ELECTRICAL WORLD
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• s.300
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• pp.78-83
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• 2001

미쓰비시電機가 제안하는 에너지솔루션은, 고객의 에너지절약, 코스트절약 및 환경개선의 파트너로서 현장에 밀착하여 에너지의 종합엔지니어링력(力)(에너지 발생$\cdot$공습$\cdot$이용기술)과 IT를 구사하여, 고객의 에너지와 관련된 여러 가지 과제(부분적인 과제에서 고객 전체의 에너지과제까지)에 대하여 에너지절약 컨설테이션, 설계시공, 설비리스, O&M, 에너지 공급, 에너지운용관리까지 폭넓게 고객과 함께 해결해 오고 있다. 그 일환으로서 동사는 마이크로 가스터빈의 코제너레이션 시스템''마이크로 에코터보 MTG-28''을 분산전원의 레퍼터리로서 제품화하고 동시에 분산전원에 의한 전$\cdot$열공급 서비스사업을 적극적으로 전개하고 있다. 동사는 Capstone사 제품인 28kW 마이크로 가스터빈을 이용하여 열이용을 포함한 코제너레이션 패키지를 개발하고 또한 고객의 큰 관심사항인 메인터넌스에 대해서도 24시간 원격감시하는 시스템을 실용화하여 애프터서비스 체제를 정비하고 있다.

• The KSFM Journal of Fluid Machinery
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• v.18 no.4
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• pp.30-35
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• 2015

This study analyzed the variations in the performance and operation of a 200 kW class micro gas turbine according to performance degradation of compressor and turbine. An in-house code, developed by the present authors and presented in the first part of these series of papers, were used for the analysis. The degradation of compressor and turbine were simulated by modifications in the their performance maps: mass flow rate, pressure ratio and efficiency were decreased from the reference values. Firstly, the variations in the operating conditions (air flow rate, pressure ratio) were predicted for the full load condition. Then, the same analysis were performed for a wide partial load operating range. The change in engine's performance (power output and efficiency) due to the component degradation was predicted. In addition, the change in the compressor surge margin, which is an important indicator for safe engine operation, was evaluated.

• 열병합발전
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• s.29
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• pp.29-31
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• 2002

• KIPE Magazine
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• v.8 no.3
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• pp.35-38
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• 2003

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.30 no.1
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• pp.46-50
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• 2001

• JOURNAL OF ELECTRICAL WORLD
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• s.291
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• pp.43-45
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• 2001

• 유체기계공업학회:학술대회논문집
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• 2001.11a
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• pp.354-360
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• 2001

Hybrid energy system of fuel cell and gas turbine is discussed as the system to be used in the distributed power generation. Discussion is first directed to the distributed power generation system which is expected to be more popularly introduced both in urban and isolated areas. In the next some characteristic features of fuel cell and micro gas turbine are shortly described. In the last discussion is turn to the fuel cell and micro gas turbine hybrid system. In particular, performance characteristics of a representative SOFC/MGT hybrid system are investigated through the concept design at various power capacity levels.

• Journal of the Korea Institute of Military Science and Technology
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• v.14 no.6
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• pp.1207-1214
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• 2011

Design of 500W class UMGT(Ultra Micro Gas Turbine) for power generation is conducted. Basic design parameters are obtained by cycle analysis. Off-design performances are predicted by 1D aerodynamic design and 1D performance analysis of compressor and turbine. 3D impellers are designed and 3D performance analysis is carried out to predict the performance characteristics of UMGT. 1D and 3D performance analysis show similar results. Structure analysis is conducted to select materials. Titanium Alloy is proposed for structural stability.