• Title/Summary/Keyword: Heavy Duty Gas Turbine

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EGR Effects on Exhaust Gas of Heavy-Duty Turbo Charge Engine with Low Pressure Route System (저압방식을 적용한 대형과급기관의 배기가스에 관한 EGR효과)

  • 오용석
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.3 no.1
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    • pp.58-62
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    • 2002
  • The efforts of EGR on performance and emissions were investigated in this study. The engine used for the tests was a six-cylinder, 11 liter, and turbo-charged, heavy-duty diesel engine with a low pressure route ECR system. The volume of recirculated gas was controlled by a manually operated valve which was installed between the turbine outlet and compressor inlet. The experiments were performed at various engine speeds and loads while the ECR rates were set at 4% and 8%. Exhaust emissions with EGR system were compared with the baseline emissions.

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Analysis of Start-Up Characteristics of Gas Turbines for Power Generation (발전용 가스터빈의 시동특성 해석)

  • Kim, Jae-Hwan;Song, Tae-Won;Kim, Tong-Seop;Ro, Sung-Tack
    • Proceedings of the KSME Conference
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    • 2000.11b
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    • pp.662-667
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    • 2000
  • A simulation procedure for a full transient analysis of the start-up of heavy-duty gas turbines for power generation is constructed. Compressor stages are grouped into three categories (front, mid, rear) and three different stage characteristic curves are applied to consider the different low-speed operating characteristics. Start-up behavior of a typical single-shaft gas turbine for power generation is simulated. The predicted transient behavior shows a good agreement with the field data. Special attention is paid to the effects of the modulation of VIGV on start-up characteristics, which play a key role in the stable operation of gas turbines.

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Program Development for Design and Part Load Performance Analysis of Single-Shaft Gas Turbines (단축가스터빈의 설계점 및 부분부하 성능해석 프로그램 개발)

  • Kim, Dong-Seop;No, Seung-Tak
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.20 no.7
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    • pp.2409-2420
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    • 1996
  • This paper describes the development of a general program for the design and part load performance analysis of single-shaft-heavy-duty gas turbines. Efforts are made to fully represent the real component features by the characteristic models and special emphasis is put on the modeling of cooled turbine stages. The design analysis routine is applied to simulate the performance of current gas turbines and its appropriateness for system analysis is validated. Meanwhile, the component parameters of real engines which describe the technology level are obtained. The program is extended to predicting the part load operation of gas turbines with the aid of models for the off-design characteristics of compressor, turbine and other main components. Part load simulation can be carried out only with limited numbers of input data. It is demonstrated that the program accurately estimates the part load characteristics of real turbines.

Spray characteristics and performance of pressure swirl simplex injector for heavy duty industrial gas turbines (대형가스터빈용 단일 압력 선회식 연료분사기의 분무 특성 및 성능 평가)

  • Seok, Jungmin;Jeong, Hanjin;Choi, Inchan;Kim, Jaiho;Lee, Sanghoon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.892-895
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    • 2017
  • As a component development of heavy duty industrial gas turbine combustor development program, pressure swirl simplex injector was designed and tested to figure out spray characteristics and performance. Injector flow rate as a function of pressure drop was measured and compared to the design target. Also spray shape was analyzed qualitatively and spray cone angle was measured from spray visualization image using shadowgraph. The flow test result showed that the injector was designed and manufactured correctly according to the design target and spray cone angle was measured from shadowgraph result. As a next step, PDA (Phase Doppler Anemometry) measurement is planned to figure out more specific spray performance and characterization.

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

  • Kim, S. Y.;K. S. Oh;Park, B. C.
    • Journal of the Korean Society of Propulsion Engineers
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    • v.2 no.2
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    • pp.74-82
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    • 1998
  • Combined cycle power plant is a system where a gas turbine or a 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. The temperature of the exhaust gases from a gas turbine ranges from $400{\sim}650^{\circ}C$, and can be used effectively in a heat recovery steam generator to produce steam. Combined cycle can be classed as a topping and bottoming cycle. The first cycle, to which most of the heat is supplied, is a Brayton gas turbine cycle. The wasted heat it produces is then utilized in a second process which operates at a lower temperature level is a steam turbine cycle. The combined gas and steam turbine power plant have been widely accepted because, first, each separate system has already proven themselves in power plants as an independent cycle, therefore, the development costs are low. Secondly, using the air as a working medium, the operation is relatively non- problematic and inexpensive and can be used in gas turbines at an elevated temperature level over $1000^{\circ}C$. 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. Recently gas turbine attained inlet temperature that make it possible to design a highly efficient combined cycle. In the present study, performance analysis of a 3 pressured combined cycle power plant is carried out to investigate the influence of topping cycle to combined cycle performance. Present calculation is compared with acceptance performance test data from SeoInchon combined cycle power plant. Present results is expected to shed some light to design and manufacture 150~200MW class heavy duty gas turbine whose conceptual design is already being undertaken.

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