• 제목/요약/키워드: gas-turbines

검색결과 247건 처리시간 0.028초

조속기 시험 시스템의 자동화 (Automation of Governor Performance Test System)

  • 이일영;김지웅;강만곤
    • 동력기계공학회지
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    • 제9권4호
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    • pp.155-161
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    • 2005
  • Governors control the revolution speed of heat engines such as diesel engines, steam turbines and gas turbines. Precise and prompt tests for the control performances of governors are essential both in governors' manufacturing processes and in governors' maintenance processes. In the conventional governor test systems controlled by analog type electronic controllers, the incorporation of heat engine's dynamics to the test system have been considered very difficult to realize. This study suggests a new governor test system controlled by a digital controller using a personal computer. The application of the digital controller to the test system instead of the analog type electronic controller have brought about the following advancements; (1) heat engine's dynamics could be implemented easily in the test system, (2) automatic test data acquisition both in steady state and in transient state enables us to save test time and to enhance the reliability of the tests.

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빌딩 내 최대 풍력발전설비 연계를 위한 소형풍력발전원 구성에 관한 연구 (A Study on Configuration of Small Wind Turbines for Maximum Capacity of Wind Power Systems Interconnected With a Building)

  • 이여진;김성열
    • 전기학회논문지
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    • 제66권4호
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    • pp.605-612
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    • 2017
  • One of the biggest environmental issues that our world has been facing is climate change. In order to cope with such environmental issues, the world is putting a great deal of effort into energy conservation. The building sector, in particular, consumes 36% of the energy consumed worldwide and emits considerable amount of greenhouse gases. Therefore, introduction of renewable energies in the building sector is highly recommended. Renewable energy sources that can be utilized in the building sector include sunlight, solar heat, geothermal heat, fuel cells and wind power. The wind power generation system which converts wind energy into electrical energy has advantages in that wind is an unlimited and pollution-free resource. It is suitable to be connected to existing buildings because many years of operational experience and the enhanced stability of the system have made it possible to downsize the electrical generator. In case of existing buildings, it is necessary to consider the live loads of the buildings to connect the wind power generation system. This paper, through the connection of the wind power generation with existing buildings, promotes reduction of greenhouse gas emissions and energy independence by reducing energy consumption in the building sector. In order to connect the wind power generation system with an exciting building, the live load of the building and the area of the rooftop should be considered. The installable model is selected by comparing the live load of the building and the load of the wind power generation system. The maximum number of the wind turbines that can be installed is obtained by considering the separation distance between the wind turbines within the area of the rooftop. Installations are divided into single installations and multiple installations of two different types of wind turbines. After determining the maximum installable number, the optimal model that can achieve the maximum annual power generation will be selected by comparing the respective total annual amount of the power generation of different models.

국내 가스터빈연소기 LNG열량변화에 따른 대응방향 연구 (Action Plan for the Effects of Variation of Fuel Gas Composition on Domestic Gas Turbines)

  • 이중성;하종만;한정옥
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2014년도 제49회 KOSCO SYMPOSIUM 초록집
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    • pp.115-118
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    • 2014
  • Since 1st July 2012, the our Goverment and KOGAS have been adopting a calorific value range system from the standard calorific value system. Domestic power plant companies and KOGAS have asked GT manufacture about the effects of the reduction of the calorific value. We received GT manufacture's answer to the question on April 12.2011. Gas components of some GT models were limited to no more than 9% of the C2+ content. Now some of GTs remain under debating whether effects on variation of gas heating or not.

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마이크로 가스터빈 설계 및 운전 성능 분석 : 제1부 - 성능해석 프로그램 (Analysis of Design and Operation Performance of Micro Gas Turbine : Part 1 - Performance Analysis Program)

  • 김정호;강도원;김동섭
    • 한국유체기계학회 논문집
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    • 제18권4호
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    • pp.22-29
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    • 2015
  • In this study, an in-house program to predict steady state operation of micro gas turbines is constructed using MATLAB. The program consists of two parts: design and off-design simulations. The program is fully modular in its structure, and performance of each component (compressor, combustor, turbine, recuperative heat exchanger and pipe elements) is calculated in a separate calculation module using mass and energy balances as well as models for off-design characteristics. The off-design modules of compressor and turbine use performance maps, which are program inputs. The off-design operation of a micro gas turbine under development was predicted by the program. The prediction results were compared with those by commercial software, and the validity of the in-house program was confirmed.

Gas Turbine Data Acquisition and Monitoring System for Combined Cycle Power Plant

  • Kang, Feel-Soon
    • Journal of information and communication convergence engineering
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    • 제6권4호
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    • pp.405-410
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    • 2008
  • This paper presents a data acquisition and monitoring system for a gas turbine. The proposed system entitled C-Tune DAS plays an important role to make an analysis of the real-time operation of the gas turbine under maintenance. The designed LabVIEW based software is divided into three parts according to their original functions, i.e., data acquisition, data analysis with display, and data storage. The data acquisition part receives data from a PMS (Plant Management System) server and two cFPs (Compact-Field Point). To verify the validity of the developed system, it is applied to gas turbines in the combined cycle power plant in Korea.

시편의 열화에 따른 가스터빈 로터볼트 기계적 강도평가 (Evaluation for mechanical hardness of gas turbine rotor bolt according to deterioration of specimen)

  • 길두송;안연식;박상기
    • 동력기계공학회지
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    • 제15권4호
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    • pp.19-24
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    • 2011
  • The operational efficiency of domestic gas turbine is about 25% and it is now in the trend of the gradual growth in spite of the severe temperature, frequent starting and shutdown according to the environmental management and the energy-efficient use. Rotor bolts of gas turbine in power plants have been the cause of defects because these gas turbines have been operated for a long time under the high pressure and temperature environment experiencing the aging change and stress concentration of the bonded part. The connection parts of the bolt revealed various failure shape and these parts were elongated under very low pressure when operated in the relaxed condition. The cause is in the lack of the metal distribution in the bottle lack area and the cap screw of the bolt is broken totally in case that the nut is fastened in most cases. Gas turbine rotor bolts are connected to the rotor wheel and these bolts caused the vibration, the bulk accident of the rotor in the event that the coupling power among these bolts was relaxed. Therefore, we would like to evaluate the soundness of the main part of the gas turbine rotor bolt through the measurement of the inner condition change along with the mechanic deterioration and temperature, stress in the gas turbine rotor material.

플랜트의 구성을 고려한 IGCC용 가스터빈의 성능해석 (Performance Analysis of a Gas Turbine for IGCC Considering Plant Configuration)

  • 김영식;이종준;김동섭;손정락;주용진
    • 대한기계학회논문집B
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    • 제32권9호
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    • pp.704-711
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    • 2008
  • Integrated gasification combined cycle (IGCC) is an environment friendly method of using coal. Several commercial IGCC plants have been built worldwide during the past decade, and a domestic development project has also been launched recently. Operation and performance characteristics of a gas turbine in the IGCC plant deviates from those of original gas turbines due to several factors such as increased amount of fuel supply and integration with other components. In this study, performance of a gas turbine in the IGCC plant is analyzed considering its integration with the air separation unit (ASU). Influence of the degree of integration (split of air supplies to ASU from the auxiliary compressor and the gas turbine compressor) on the system performance is investigated. In addition, effect of modulating nitrogen return flow from the gasifier to the gas turbine on the operating characteristics of the gas turbine is examined.

발전용 소형가스터빈의 축류터빈 공력설계 (Axial Turbine Aerodynamic Design of Small Heavy-Duty Gas Turbines)

  • 김중석;이우상;류제욱
    • 대한기계학회논문집B
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    • 제37권4호
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    • pp.415-421
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    • 2013
  • 본 논문은 두산중공업(주)에서 개발 중인 소형 가스터빈의 축류 터빈 설계 과정을 기술하였다. 축류터빈의 설계 과정은 크게 유로설계, 익형설계, 3D 성능 계산의 세 단계로 구성되며. 최적의 유로를 설계하기 위해 자오면의 형상, 평균 반경, 블레이드간 간격, 유로 형상각 등 여러 형상 변수에 대해 통과유동계산 및 손실계산을 수행한다. 익형 설계는 유로 설계시 스팬 방향으로 계산된 입출구 유동각을 기준으로 실험상관식을 적용하여 최적의 블레이드 개수를 결정한 후 2D 익형 단면을 설계하며 2D NS 계산을 통해 캐스케이드 유동구조를 검토하여 설계한 단면의 설계적정성을 평가한다. 설계된 2D 익형 단면을 스팬방향으로 적층하여 3D 익형을 생성하고, 다단 Euler 계산, 단익렬, 다단 NS 계산을 수행하여 3D 유동 특성을 고찰한다.

연구용 30 kW 수소 전소 마이크로믹스 연소기 개발 (Development of a 30 kW Hydrogen-Fueled Micromix Combustor for Research)

  • 옥서준;김민수;박수현
    • 항공우주시스템공학회지
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    • 제17권6호
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    • pp.72-81
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    • 2023
  • 수소 가스터빈은 미래 항공 추진 기관과 무탄소 발전 동력원으로 이산화탄소 배출 문제에 대응할 수 있는 유망한 기술이다. 100% 수소를 연료로 사용하는 가스터빈을 위해서는 기존 탄화수소 연료와 다른 수소의 특성을 고려하여 효율과 안정성이 높은 혁신적인 연소기 시스템을 설계할 필요가 있다. 마이크로믹스는 연료와 공기를 강하게 혼합하여 반응이 빠르게 종료되도록 함으로써 질소산화물을 저감하고 안정성을 높이도록 하는 연소기 설계 방식이다. 본 논문에서는 수소 전소 기술로서 마이크로믹스 방식 연소기의 원리와 설계 방법을 살펴보고, 연구용 30 kW 마이크로믹스 수소 연소기 설계안을 소개한다.

Review on Advanced Health Monitoring Methods for Aero Gas Turbines using Model Based Methods and Artificial Intelligent Methods

  • Kong, Changduk
    • International Journal of Aeronautical and Space Sciences
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    • 제15권2호
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    • pp.123-137
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    • 2014
  • The aviation gas turbine is composed of many expensive and highly precise parts and operated in high pressure and temperature gas. When breakdown or performance deterioration occurs due to the hostile environment and component degradation, it severely influences the aircraft operation. Recently to minimize this problem the third generation of predictive maintenance known as condition based maintenance has been developed. This method not only monitors the engine condition and diagnoses the engine faults but also gives proper maintenance advice. Therefore it can maximize the availability and minimize the maintenance cost. The advanced gas turbine health monitoring method is classified into model based diagnosis (such as observers, parity equations, parameter estimation and Gas Path Analysis (GPA)) and soft computing diagnosis (such as expert system, fuzzy logic, Neural Networks (NNs) and Genetic Algorithms (GA)). The overview shows an introduction, advantages, and disadvantages of each advanced engine health monitoring method. In addition, some practical gas turbine health monitoring application examples using the GPA methods and the artificial intelligent methods including fuzzy logic, NNs and GA developed by the author are presented.