• Title/Summary/Keyword: Bottoming Cycle

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Analysis of the Influence of CO2 Capture on the Performance of IGCC Plants (가스화 복합화력발전 플랜트에서 CO2제거가 성능에 미치는 영향 해석)

  • Cha, Kyu-Sang;Kim, Young-Sik;Lee, Jong-Jun;Kim, Tong-Seop;Sohn, Jeong-L.;Joo, Yong-Jin
    • The KSFM Journal of Fluid Machinery
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    • v.13 no.1
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    • pp.9-16
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    • 2010
  • In the power generation industry, various efforts are needed to cope with tightening regulation on carbon dioxide emission. Integrated gasification combined cycle (IGCC) is a relatively environmentally friendly power generation method using coal. Moreover, pre-combustion $CO_2$ capture is possible in the IGCC system. Therefore, much effort is being made to develop advanced IGCC systems. However, removal of $CO_2$ prior to the gas turbine may affect the system performance and operation because the fuel flow, which is supplied to the gas turbine, is reduced in comparison with normal IGCC plants. This study predicts, through a parametric analysis, system performances of both an IGCC plant using normal syngas and a plant with $CO_2$ capture. Performance characteristics are compared and influence of $CO_2$ capture is discussed. By removing $CO_2$ from the syngas, the heating value of the fuel increases, and thus the required fuel flow to the gas turbine is reduced. The resulting reduction in turbine flow lowers the compressor pressure ratio, which alleviates the compressor surge problem. The performance of the bottoming cycle is not influenced much.

Influence of Precooling Cooling Air on the Performance of a Gas Turbine Combined Cycle (냉각공기의 예냉각이 가스터빈 복합발전 성능에 미치는 영향)

  • Kwon, Ik-Hwan;Kang, Do-Won;Kang, Soo-Young;Kim, Tong-Seop
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.2
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    • pp.171-179
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    • 2012
  • Cooling of hot sections, especially the turbine nozzle and rotor blades, has a significant impact on gas turbine performance. In this study, the influence of precooling of the cooling air on the performance of gas turbines and their combined cycle plants was investigated. A state-of-the-art F-class gas turbine was selected, and its design performance was deliberately simulated using detailed component models including turbine blade cooling. Off-design analysis was used to simulate changes in the operating conditions and performance of the gas turbines due to precooling of the cooling air. Thermodynamic and aerodynamic models were used to simulate the performance of the cooled nozzle and rotor blade. In the combined cycle plant, the heat rejected from the cooling air was recovered at the bottoming steam cycle to optimize the overall plant performance. With a 200K decrease of all cooling air stream, an almost 1.78% power upgrade due to increase in main gas flow and a 0.70 percent point efficiency decrease due to the fuel flow increase to maintain design turbine inlet temperature were predicted.

Design and Construction of a Bottoming Organic Rankine Cycle System for an Natural Gas Engine (가스엔진용 유기랭킨사이클의 설계 및 제작)

  • Lee, Minseog;Baek, Seungdong;Sung, Taehong;Kim, Hyun Dong;Chae, Jung Min;Cho, Young Ah;Kim, Hyoungtae;Kim, Kyung Chun
    • Journal of the Korean Institute of Gas
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    • v.20 no.6
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    • pp.65-72
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    • 2016
  • ORC system was designed and constructed for utilizing the heat of the exhaust gas and coolant released from the gas engine which was modified to use natural gas as a fuel. In this paper the components of the ORC system were designed and manufactured based on measured data of the gas engine. The components are composed of two plate heat exchanger, the 5kW-class expander and multi stage centrifugal pump. The thermodynamic performance of the ORC system was analyzed by using the electric heater. Also, the developed ORC system was implemented to modified natural gas engine. Two gas engines were used to supply heat to the ORC system. As a result of test bench, when the heat source temperature is $110^{\circ}C$ expander shaft power, the pressure ratio and cycle efficiency is 5.22kW, 7.41, 9.09%. As a result of field test, when the heat source temperature is $86^{\circ}C$ expander shaft power, the pressure ratio and cycle efficiency is 2kW, 3.75, 6.45%.