• 제목/요약/키워드: Steam Turbine Cycle

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2압, 증기분사 복합발전 사이클에 대한 성능해석 (A dual Pressure, Steam Injection Combined cycle Power Plant Performance Analysis)

  • 김수용;손호재;박무룡;윤의수
    • 연구논문집
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    • 통권27호
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    • pp.75-86
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    • 1997
  • Combined cycle power plant is a system where a gas turbine or steam turbine is used to produce shaft power to drive a generator for producing electrical power and the steam from the HRSG is expanded in a steam turbine for additional shaft power. Combined cycle plant is a one from of cogeneration. The temperature of the exhaust gases from a gas turbine ranges from $400^\circC$ to $600^\circC$, and can be used effectively in a heat recovery steam generator to produce steam. Combined cycle can be classed as a "topping(gas turbine)" and a "bottoming(steam turbine)" cycle. The first cycle, to which most of the heat is supplied, is called the topping cycle. The wasted heat it produces is then utilized in a second process which operates at a lower temperature level and is therefore referred to as a "bottoming cycle". The combination of gas/steam turbine power plant managed to be accepted widely because, first, each individual system has already proven themselves in power plants with a single cycle, therefore, the development costs are low. Secondly, the air as a working medium is relatively non-problematic and inexpensive and can be used in gas turbines at an elevated temperature level over $1000^\circC$. The steam process uses water, which is likewise inexpensive and widely available, but better suited for the medium and low temperature ranges. It, therefore, is quite reasonable to use the steam process for the bottoming cycle. Only recently gas turbines attained inlet temperature that make it possible to design a highly efficient combined cycle. In the present study, performance analysis of a dual pressure combined-cycle power plant is carried out to investigate the influence of topping cycle to combined cycle performance.

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3압 복합 발전 플랜트 사이클에 대한 성능해석 (Performance Analysis of a 3 Pressured Combined Cycle Power Plant)

  • Kim, S. Y.;K. S. Oh;Park, B. C.
    • 한국추진공학회지
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    • 제2권2호
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    • pp.74-82
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    • 1998
  • 복합발전 사이클은 가스터빈이나 스팀터빈으로부터의 출력을 이용하여 전개를 생산하기 위한 발전기를 구동시키고 배영회수기로부터 나온 증기를 스틸터빈에서 팽창시킴으로서 부가적인 동력을 얻는 장치를 가리킨다. 보통 가스터빈 배기로 부터의 온도는 $400{\sim}650^{\circ}C$정도로서 배열회수기에서 효과적으로 스팀을 생산할 수 있는 수준의 온도이다. 복합 사이클은 일반적으로 상부사이클과 하부사이클로 구분하는데 대부분의 열에너지 공급이 이루어지는 상부사이클을 브레이돈사이클 이라하며 브레이돈사이클에서 소비되는 에너지는 보다 낮은 온도 수준인 하부사이클에서 회수된다. 이러한 복합사이클은 최근 들어 더욱 보편적으로 적용되고 있는데 그 이유는 첫째, 가스터빈이나 스팀터빈이 독자적으로도 충분히 기술적인 검증을 받은 열기관으로서 초기에 비해 개발비가 저렴해졌다는 데 있고, 둘째, 작동유체인 공기가 $1000^{\circ}C$ 이상에서도 별다른 문제없이 적용될 수 있는 안전한 유체이고 비용이 전혀 들지 않는다는 점이다. 그 뿐 아니라 스팀터빈에 사용되는 물도 중저온에서 매우 저가로 공급할 수 있고 쉽게 공급이 가능하다는 이점으로 하부사이클에의 적용이 매우 양호하다는 점이다. 최근 소재기술의 개발에 따른 터빈입구온도의 향상은 이러한 복합발전 사이클의 기술적, 경제적 이점을 더욱 강화시켜 주고 있다. 본 연구에서는 3압에 의한 복합사이클에 대한 성능해석을 통하여 상부사이클이 전체 복합발전 성능에 미치는 영향을 조사하였으며 그 결과를 서인천 복합발전 인수 성능시험결과와 비교하였다. 본 연구결과는 현재 개념설계가 이루어지고 있는 장차 150~200MW수준의 산업용 가스터빈 개발에 중요한 방향제시를 할 수 있을 것으로 판단된다.

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Analysis of Design and Part Load Performance of Micro Gas Turbine/Organic Rankine Cycle Combined Systems

  • Lee, Joon-Hee;Kim, Tong-Seop
    • Journal of Mechanical Science and Technology
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    • 제20권9호
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    • pp.1502-1513
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    • 2006
  • This study analyzes the design and part load performance of a power generation system combining a micro gas turbine (MGT) and an organic Rankine cycle (ORC). Design performances of cycles adopting several different organic fluids are analyzed and compared with performance of the steam based cycle. All of the organic fluids recover greater MGT exhaust heat than the steam cycle (much lower stack temperature), but their bottoming cycle efficiencies are lower. R123 provides higher combined cycle efficiency than steam does. The efficiencies of the combined cycle with organic fluids are maximized when the turbine exhaust heat of the MGT is fully recovered at the MGT recuperator, whereas the efficiency of the combined cycle with steam shows an almost reverse trend. Since organic fluids have much higher density than steam, they allow more compact systems. The efficiency of the combined cycle, based on a MGT with 30 percent efficiency, can reach almost 40 percent. hlso, the part load operation of the combined system is analyzed. Two representative power control methods are considered and their performances are compared. The variable speed control of the MGT exhibits far better combined cycle part load efficiency than the fuel only control despite slightly lower bottoming cycle performance.

초임계 이산화탄소 사이클을 이용한 연료 재순환 MCFC의 폐열회수 (Waste heat recovery of recirculated MCFC using supercritical carbon dioxide power cycle)

  • 이재윤;안지호;김동섭
    • 플랜트 저널
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    • 제15권2호
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    • pp.42-45
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    • 2019
  • 용융탄산염 연료전지는 폐열의 온도가 높아 하부 사이클을 구성하여 효율을 높일 수 있다. 이러한 목적으로 연료를 재순환하는 용융탄산염 연료전지에 하부 사이클로 증기 터빈 사이클을 적용한 선행 연구가 있었다. 본 연구는 하부 사이클을 증기 터빈 사이클에서 초임계 이산화탄소 사이클로 대체하는 것을 고려하였다. 그리고 출력을 비교하여 하부 사이클을 대체하는 것에 대한 검토를 하였다. 그 결과 현재 개발 단계의 초임계 이산화탄소 사이클의 출력은 증기 터빈 사이클보다 낮지만, 이론적으로 증기 터빈 사이클보다 출력이 더 커질 수 있음을 확인하였다. 만약 초임계 이산화탄소 사이클이 터빈의 등엔트로피 효율을 89%, 압축기의 등엔트로피 효율을 83%, 복열기의 유용도를 0.9의 수준으로 향상 시킨다면 증기 터빈 사이클과 동등한 출력을 낼 수 있다.

복합화력발전소 증기터빈 동익 손상 원인분석 (Root Cause Analysis on the Steam Turbine Blade Damage of the Combined Cycle Power Plant)

  • 강명수;김계연;윤완노;이우광
    • 동력기계공학회지
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    • 제12권4호
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    • pp.57-63
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    • 2008
  • The last stage blade of the low pressure steam turbine remarkably affects turbine plant performance and availability Turbine manufacturers are continuously developing the low pressure last stage blades using the latest technology in order to achieve higher reliability and improved efficiency. They tend to lengthen the last stage blade and apply shrouds at the blades to enhance turbine efficiency. The long blades increase the blade tip circumferential speed and water droplet erosion at shroud is anticipated. Parts of integral shrouds of the last stage 40 inch blades were cracked and liberated recently in a combined cycle power plant. In order to analyze the root cause of the last stage blades shroud cracks, we investigated operational history, heat balance diagram, damaged blades shape, fractured surface of damaged blades, microstructure examination and design data, etc. Root causes were analyzed as the improper material and design of the blade. Notches induced by erosion and blade shroud were failed eventually by high cycle fatigue. This paper describes the root cause analysis and countermeasures for the steam turbine last stage blade shroud cracks of the combined cycle power plant.

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냉매증기터빈에 의해 구동되는 냉동사이클의 해석 (Analysis of a Refrigeration Cycle Driven by Refrigerant Steam Turbine)

  • 정진희
    • 설비공학논문집
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    • 제14권10호
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    • pp.801-810
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    • 2002
  • We have analyzed a combined cycle employing refrigerant Rankine cycle and simple refrigeration cycle with one working fluid. Although this cycle shows promising aspects such as simplicity, it does not have a good efficiency to compete with the other existing technologies because of high temperature at the exit of the turbine. However, by introducing a recuperator, it is found that the cycle efficiency can be improved up to the level much higher than other technology's efficiency.

가스터빈 열 회수 증기 발생기의 난류연소 해석과 배기가스 예측 및 검증 (Numerical Analysis of Turbulent Combustion and Emissions in an HRSG System)

  • 장지훈;한가람;박호영;이욱륜;허강열
    • KEPCO Journal on Electric Power and Energy
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    • 제5권2호
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    • pp.103-111
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    • 2019
  • The combined cycle plant is an integration of gas turbine and steam turbine, combining the advantages of both cycles. It recovers the heat energy from gas turbine exhaust to use it to generate steam. The heat recovery steam generator plays a crucial role in combined cycle plants, providing the link between the gas turbine and the steam turbine. Simulation of the performance of the HRSG is required to study its effect on the entire cycle and system. Computational fluid dynamics has potential to become a useful to validate the performance of the HRSG. In this study a solver has been implemented in the open source code, OpenFOAM, for combustion simulation in the heat recovery steam generator. The solver is based on the steady laminar flamelet model to simulate detailed chemical reaction mechanism. Thereafter, the solver is used for simulation of HRSG system. Three cases with varying fuel injections and gas turbine exhaust gas flow rates were simulated and the results were compared with measurements at the system outlet. Predicted temperature and emissions and those from measurements showed the same trend and in quantitative agreement.

복합화력발전 하부시스템의 성능설계해석 (Performance Design Analysis of the Bottoming System of Combined Cycle Power Plants)

  • 이봉렬;김동섭;노승탁;신흥태;전용준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집D
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    • pp.738-743
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    • 2001
  • A computer program, capable of performing thermal design analysis of the triple pressure bottoming system of combined cycle power plants, was developed. The program is based on thermal analysis of the heat recovery steam generator and estimation of its size and steam turbine power. The program is applicable to various parametric analyses including optimized design calculation. This paper presents examples of analysis results for the effects of arrangement of heat exchanger units, steam pressures and deaerating sources on design performance indices such as steam turbine power and the size of heat recovery steam generator.

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吸氣冷却-蒸氣噴射 가스터빈 사이클에 관한 열역학적 연구 (A Thermodynamic Study on Suction Cooling-Steam Injected Gas Turbine Cycle)

  • 박종구;양옥룡
    • 대한기계학회논문집
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    • 제16권1호
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    • pp.77-86
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    • 1992
  • 본 연구에서는 사이클은 터빈 출구로 부터 배출되는 폐열을 최대한 회수하여 얻은 증기를 연소기내에 분사시킴으로써 부가적인 압축기 및 비출력의 상향을 기할수 있다.아울러 폐열이용 암모니아 흡수기 냉동기를 구동하여 압축기 입구 온도를 낮 춤에 의해 열효율 및 비출력의 증대는 물론 대기온도 변화에 따른 기관 성능의 변동을 감소시킬 수 있다.

열회수 증기발생기와 증기터빈 시스템의 동적 거동 해석 (Analysis of Dynamic Behavior of a Heat Recovery Steam Generator and Steam Turbine System)

  • 박형준;김동섭;노승탁
    • 대한기계학회논문집B
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    • 제24권7호
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    • pp.994-1001
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    • 2000
  • The dynamic behavior of a single-pressure heat recovery steam generator and turbine system for the combined cycle power plant is simulated on the basis of one-dimensional unsteady governing equations. A water level control and a turbine power control are also included in the calculation routine. Transient response of the system to the variation of gas turbine exit condition is simulated and effect of the turbine power control on the system response is examined. In addition, the effect of the treatment of inertia terms(fluid inertia and thermal inertia of heat exchanger metal) on the simulated transient response is investigated.