• 한국유체기계학회 논문집
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• 제15권6호
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• pp.64-69
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• 2012

This paper deals with the study on repair case of journal shaft and bearing damage in 25MW industrial gas turbine caused by sudden blackout, operation mistake, and logic abnormal, etc. When a serious accident such as journal and bearing damage in a gas turbine occurs, the domestic local companies having the gas turbine are dependent on manufacturer for all maintenance and repair schedule until now. This case study shows that the damaged gas turbine is normally re-operated itself in domestic by establishing repair schedule in a short period of time, repairing damage journal shaft and tilting pad bearings, and performing rotating test for a reliability check. This paper can be regarded as the important case study of emergency test run experience of the refurbished 25MW gas turbine rotor.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2013년도 제46회 KOSCO SYMPOSIUM 초록집
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• pp.113-116
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• 2013

The Samsung Techwin has been developed the various types of combustor and fuel nozzle frontal devices for the aero engine and small scale industrial gas turbines. Currently, we have been developed the highly heat capacity and long-lived gas turbine combustor based on the short-lived combustor and fuel injector technologies. In this paper, the market trends and the information on the survey of an advanced gas turbine combustor were introduced for the development of large scale gas turbine combustor and fuel nozzle assembly.

• 대한안전경영과학회지
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• 제11권1호
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• pp.93-101
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• 2009

The use of the gas turbine for power supply is increasing recently. Accordingly, the operation and maintenance cost of the gas turbine is gradually increasing and the various efforts to cut the cost are needed. For an operation and maintenance cost saving of the gas turbine, reductions of the new purchasing charge and the reproduction repair cost of the hot gas parts are required through more effective operation and life management methods for the hot gas parts. The hot gas parts are the main parts of the gas turbine and they are replaced with the periodic. In this research, efficient operation and life management methods for the hot gas parts were presented with the cases. The methods were analyzed and verified based on real data and the cases for improving a lifetime were utilized in the field.

• 한국유체기계학회 논문집
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• 제6권3호
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• pp.36-43
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• 2003

Operating performance of industrial gas turbines in combined cycle power plants depends upon atmospheric conditions. Compressor fouling caused by airborne particles in the atmosphere and their adhesions on compressor blades is one of critical phenomena related to the performance degradation of industrial gas turbines. Compressor fouling provokes increase of pressure loss in inlet duct, decrease of mass flow rate of intake air and decrease of compressor stage efficiency. In this study, impacts of compressor fouling on the performance of an industrial gas turbine operating at design point condition are investigated analytically. As results, it is found that the reduction of produced power with decreased mass flow rate of intake air caused by narrowed flow area by the adhesion of airborne particles on compressor blades is the most dominant impact on the gas turbine performance by the compressor fouling phenomena.

• 한국유체기계학회 논문집
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• 제12권3호
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• pp.26-30
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• 2009

This paper predicts the critical speeds of a 5MW industrial gas turbine by using commercial rotordynamic tool, DYNAMICS 4.3. The gas turbine is operated at 12,975 rpm on squeeze film dampers. The stiffness of the squeeze film dampers are estimated. The critical speeds of the gas turbine rotor are calculated to have a sufficient separation margin (2%) from the 1st bending mode and pass over 2 rigid body modes below 4,000 cpm. This paper discussed the coupling effects on the dynamic response of the gas turbine.

• 한국연소학회:학술대회논문집
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• 대한연소학회 2003년도 제27회 KOSCO SYMPOSIUM 논문집
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• pp.265-272
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• 2003

Some catalytic reactors for industrial/generation gas turbines were reviewed and investigated to understand the current status and future prospect for ultra low NOx catalytic gas turbine combustor. Catalytic reactor which was applied to 1${\sim}$10MW class gas turbine has achieved the ultra low emission corresponding to less than 3ppm NOx and 10ppm CO. But the durability and sizing flexibility of catalyst is needed to improve the catalyst performance for commercial gas turbine operation.

• 한국추진공학회지
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• 제3권4호
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• pp.104-108
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• 1999

삼성항공(주)은 국내 유일의 가스터빈 전문업체로서 가스터빈과 터보기기 분야에서 다양한 사업들을 펼쳐왔다. 그 중에서 가스터빈 정비조립 사업, 부품제조 사업, 그리고 터보기기 사업의 현황과 생산, 기술, 개발 측면에서 현재의 능력과 수준을 조망해보고 향후의 사업 전개 방향에 대해서 간략히 소개하여 관련분야에 종사하는 분들에게 국내 가스터빈 산업의 현주소를 파악하는데 도움이 되고자 하였다.

• 한국유체기계학회 논문집
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• 제13권3호
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• pp.18-23
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• 2010

This paper predicts the unbalance and transient (start-up) response of a 5MW industrial gas turbine by using commercial rotordynamic tool, DYNAMICS 4.3. The gas turbine is operated at 12,975rpm on squeeze film dampers or tilting pad bearings. The stiffness and damping coefficients of the squeeze film dampers and tilting pad bearings are estimated. It is seen that the vibration amplitude of the gas turbine rotor is sufficiently small around the critical speeds and at the rated speed.

• 에너지공학
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• 제29권1호
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• pp.13-24
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• 2020

온실가스 배출을 감축하기 위한 각국의 노력이 활발해 지고 있으며, 그에 따라 석탄발전의 비중을 점차 줄이고 재생에너지 및 천연가스 발전의 비중을 높이려는 노력이 가시화되고 있다. 한국도 유사한 정책을 추구하고 있는데, 현재 LNG 발전 가치사슬 전체에 걸쳐 국산이 차지하는 부분은 매우 미미한 실정이어서 이러한 LNG 발전확대 정책이 국내 산업육성과 괴리는 있지 않은지 우려가 되는 상황이다. 따라서 본 논고에서는 LNG 발전에 사용되고 있는 가스터빈과 고온부품 산업의 국내외 현황을 살펴보고, 국내 가스터빈 산업의 Supply Chain 분석을 통해 국내 산업이 안고 있는 이슈와 문제점을 조사해 보았으며, 이를 기반으로 국내 가스터빈과 고온부품 산업의 활성화 및 국산화를 위한 전략을 제안하였다. 국내 가스터빈 산업육성 전략은 1) 가스터빈 얼라이언스 구성 등을 통한 국내 제조산업 생태계 조성, 2) 가스터빈 및 고온부품 국산화를 위한 전략적 기술개발 지원, 그리고 3) 국내 실증 테스트베드 구축 등 기술 사업화 촉진을 위한 환경 조성으로 요약될 수 있다.

• 한국연소학회지
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• 제9권1호
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• pp.11-17
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• 2004

The purposes of this study are to analyze nitrogen oxides(NOx) formation mechanism and to reduce abnormal NOx emissions in gas turbines. Industrial gas turbines emissions have potential to negative affect to the atmosphere in many different ways such as photochemical smog, acid rain and global warming. In conventional gas turbine combustors, one of the main pollutants such as nitrogen oxide(NOx) species, are principally formed from combustion process of fuel with oxygen in the primary combustion zone, and their emission levels are highly depend on peak temperatures in the combustor. In order to examine the characteristics and the effect of NOx formation, we used gas turbine of which commercial operating in Korea. From the examination, it has been found that NOx emissions are relatively high at low load(output) and during combustion mode change. Also, the effect of Air/Fuel ratio was considered. As the Air/Fuel ratio was increased in Lean-Lean mode, the NOx emission was decreased. The results of this study indicated that NOx emission levels are highly depend on peak temperature and pressure of combustion process in the combustor.