• 제목/요약/키워드: Turbine Load Set

검색결과 29건 처리시간 0.025초

Improved Suter Transform for Pump-Turbine Characteristics

  • Dorfler, Peter K.
    • International Journal of Fluid Machinery and Systems
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    • 제3권4호
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    • pp.332-341
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    • 2010
  • Standard dimensionless parameters cannot simultaneously represent all operation modes of a pump-turbine. They either have singularities at E=0 and multiple values in the 'unstable' areas, or else get singular at n=0. P. Suter (1966) introduced an alternative set of variables which avoids singularity and always remains unique-valued. This works for non-regulated pumps but not so well for regulated machines. A modification by C.S. Martin avoids distortion at low load. The present paper describes further improvements for the representation of torque, and for closed gate (where Suter's concept does not work). The possibility to interpolate across all operation modes is likewise useful for representing other mechanical parameters of the machine. Practical application for guide vane torque and pressure pulsation data is demonstrated by examples.

Long-term simulation of wind turbine structure for distributed loading describing long-term wind loads for preliminary design

  • Ibrahimbegovic, Adnan;Boujelben, Abir
    • Coupled systems mechanics
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    • 제7권2호
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    • pp.233-254
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    • 2018
  • In order to reduce the dependency on fossil fuels, a policy to increase the production capacity of wind turbine is set up. This can be achieved with increasing the dimensions of offshore wind turbine blades. However, this increase in size implies serious problems of stability and durability. Considering the cost of large turbines and financial consequences of their premature failure, it is imperative to carry out numerical simulations over long periods. Here, an energy-conserving time-stepping scheme is proposed in order to ensure the satisfying computation of long-term response. The proposed scheme is implemented for three-dimensional solid based on Biot strain measures, which is used for modeling flexible blades. The simulations are performed at full spatial scale. For reliable design process, the wind loads should be represented as realistically as possible, including the fluid-structure interaction (FSI) dynamic effects on wind turbine blades. However, full-scale 3D FSI simulations for long-term wind loading remain of prohibitive computation cost. Thus, the model to quantify the wind loads proposed here is a simple, but not too simple to be representative for preliminary design studies.

50KW 터보제너레이터용 가스터빈 엔진의 설계점/ 탈설계/과도성능해석 (On/Off-Design/Transient Analysis of a 50KW Turbogenerator Gas Turbine Engine)

  • 김수용;박무룡;조수용
    • 연구논문집
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    • 통권27호
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    • pp.87-99
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    • 1997
  • Present paper describes on/off design performance of a 50KW turbogenerator gas turbine engine for hybrid vehicle application. For optimum design point selection, relevant parameter study is carried out. The turbogenerator gas turbine engine for a hybrid vehicle is expected to be designed for maximum fuel economy, ultra low emissions, and very low cost. Compressor, combustor, turbine, and permanent-magnet generator will be mounted on a single high speed (82,000 rpm) shaft that will be supported on air bearings. As the generator is built into the shaft, gearbox and other moving parts become unnecessary and thus will increase the system's reliability and reduce the manufacturing cost. The engine has a radial compressor and turbine with design point pressure ratio of 4.0. This pressure ratio was set based on calculation of specific fuel consumption and specific power variation with pressure ratio. For the given turbine inlet temperature, a rather conservative value of $1100^\circK$ was selected. Designed mass flow rate was 0.5 kg/sec. Parametric study of the cycle indicates that specific work and efficiency increase at a given pressure ratio and turbine inlet temperature. Off design analysis shows that the gas turbine system reaches self operating condition at N/$N_{DP}$ = 0.53. Bleeding air for turbine stator cooling is omitted considering low TIT and for a simple geometric structure. Various engine performance simulations including, ambient temperature influence, surging at part load condition. Transient analysis were performed to secure the optimum engine operating characteristics. Surge margin throughout the performance analysis were maintained to be over 80% approximately. Validation of present results are yet to be seen as the performance tests are scheduled by the end of 1998 for comparison.

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IEC 61400 풍력표준을 적용한 제주도 김녕 난류강도 특성분석 (Analysis on Turbulence Intensity Characteristics at Gimnyeong, Jejudo by Applying IEC 61400 Wind Turbine Standards)

  • 김현구;정태윤;장문석
    • 한국태양에너지학회 논문집
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    • 제30권6호
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    • pp.59-65
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    • 2010
  • Analysis on turbulence intensity profile depending on wind speed is an important process to set up design condition of wind turbine in terms of fatigue load. This paper tests goodness of fit of turbulence intensity empirical equations suggested by the IEC 61400 Standards with Jejudo Gimnyeong met-tower measurement, which is erected at a seashore. Therefore sea breeze and land breeze coexist. Sea breeze case showed apparent increasing trend of turbulence intensity in a high wind speed regime due to increase of sea surface roughness. However, neither inland wind turbine standard IEC 61400-1 nor offshore wind turbine standard IEC 61400-3 fit such a trend adequately. On the other hand, the modified empirical equation of turbulence intensity of IEC 61400-3 derived from Germany FINO1 application study by considering turbulence intensity behavior in a high wind speed regime showed good agreement with the measurement. Therefore, we can reconfirm and conclude that IEC 61400-3 Ed.1 legislated in 2009 needs to be modified.

WFMS 모의를 위한 풍력발전단지 모델 구성 연구 (Study of Wind Farm Model Configuration for WFMS simulation)

  • 김현욱;정승민;황평익;유연태;송성윤;장길수
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2015년도 제46회 하계학술대회
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    • pp.247-248
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    • 2015
  • Wind turbines causes instabilities on the grid as their penetration increase. To mitigate harmful effects from wind turbines, transmission system operator(TSO) set up some requirements to obligate for wind generation operator for grid connection. So wind farm management system(WFMS) has important role to follow requirement from TSO, WFMS calculates available real power by considering wake effects, and dispatches real power order to each wind turbine in wind farm to optimize for decreasing load fatigue. To verify operation of WFMS, real-time simulator(RTS) is necessary. This paper deals with RTS configuration to verify WFMS operation. RTS includes wind farm model and power flow code. Normally, wind farm equivalent simple model makes wind turbines in wind farm to one wind turbine mode which cannot verify power flow in wind farm and WFMS operation. Thus, this paper makes wind farm model using simple wind turbine model with transfer function. Matlab is used for make power flow code and wind farm model to impose RTS and those model is certified by PSCAD/EMTDC.

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H-Bridge VSC with a T-Connected Transformer for a 3-Phase 4- Wire Voltage and Frequency Controller of an Isolated Asynchronous Generator

  • Kasal, Gaurav Kumar;Singh, Bhim
    • Journal of Power Electronics
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    • 제9권1호
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    • pp.43-50
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    • 2009
  • This paper deals with a novel solid state controller (NSSC) for an isolated asynchronous generator (IAG) feeding 3-phase 4-wire loads driven by constant power prime movers, such as uncontrolled pico hydro turbines. AC capacitor banks are used to meet the reactive power requirement of the asynchronous generator. The proposed NSSC is realized using a set of IGBTs (Insulated gate bipolar junction transistors) based current controlled 2-leg voltage source converters (CC- VSC) and a DC chopper at its DC bus, which keeps the generated voltage and frequency constant in spite of changes in consumer loads. The neutral point of the load is created using aT-configuration of the transformers. The IAG system is modeled in MATLAB along with Simulink and PSB (power system block set) toolboxes. The simulated results are presented to demonstrate the capability of the isolated generating system consisting of NSSC and IAG driven by uncontrolled pico hydro turbine and feeding 3-phase 4-wire loads.

풍력전단지의 계통 연계 운전에 따른 보호 계전기 설정치 정정에 관한 고찰 (The Study on Correction of Protective Relaying Set Value for the Power Electric Network Paralleled with Wind Farm)

  • 장성일;최돈만;최정환;김광호;오종률;김주열
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2002년도 하계학술대회 논문집 A
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    • pp.487-490
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    • 2002
  • Wind farm paralleled with electric power network can supply the power into a power network not only the normal conditions, but also the fault conditions of distribution network. If the fault happened in the power line with wind farm, the fault current level measured in a relaying point might be lower than that of distribution network without wind turbine generator. Consequently, it is difficult to detect the fault happened in the distribution network connected with wind generator. This paper describes the influence of wind turbine generator on the protective relaying system for detecting the fault occurred in a power line network. Simulation results shows that the fault current depends on the fault impedance, location, and the capacity of wind farm and distribution network load.

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유연핀을 적용한 2.5MW급 풍력발전기용 기어박스의 동응답 해석 (Dynamic Response Analysis of 2.5MW Wind Turbine Gearbox with Flexible Pins)

  • 조진래;정기용
    • 한국전산구조공학회논문집
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    • 제29권1호
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    • pp.37-44
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    • 2016
  • 본 연구는 2.5MW급 풍력발전기용 기어박스의 동특성 분석에 관한 것으로서, 유연핀(flexible pin) 채용에 따른 유성기어축의 미스얼라인먼트(misalignment) 개선여부와 충격하중에 따른 기어박스의 동응답 특성을 유한요소해석을 통해 고찰하였다. 내부의 복잡한 기어시스템의 하중전달을 정확하게 그리고 효과적으로 반영하기 위해 치접촉을 등가 치강성계수를 갖는 스프링요소와 물림률을 이용하여 모델링하였다. 기어의 등가 치강성계수는 기어치에 대한 변형해석을 통해 계산하였으며, 동특성 분석을 위해 기어박스 입력단에 충격 토오크를 부과하였다. 수치실험을 통해 등가 치강성모델의 타당성을 검증하였으며, 양단 그리고 일단 고정축과의 상대 비교를 통해 유연핀 적용에 따른 유성기어축의 미스얼라인먼트 개선여부를 확인할 수 있었다.

터보프롭엔진(PT6A-62)의 성능저하 진단을 위한 최적 계측 변수 선정에 관한 연구 (A Study on Optimal Parameter Selection for Health Monitoring of Turboprop Engine (PT6A-62))

  • 공창덕;기자영;장현수;오성환
    • 한국추진공학회지
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    • 제4권4호
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    • pp.87-97
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    • 2000
  • 국내에서 최초로 개발된 기본훈련기 KT-1의 추진기관인 터보프롭 엔진(PT6A-62)을 위한 정상상태 성능모사 덴 진단 프로그램을 개발하였다. 개발된 정상상태 성능해석 프로그램의 검증을 위해 해석 결과를 엔진 제작사에서 제공한 성능 데이터 및 가스터빈 엔진의 성능 모사 프로그램으로 잘 알려진 GASTURB와 비교하였다. 개발된 정상상태 성능해석 프로그램의 검증을 위해 해석 결과를 엔진 제작사에서 제공한 성능 데이터 및 가스터빈 엔진의 성능 모사 프로그램으로 잘 알려진 GASTURB와 비교하였다. 개발된 프로그램의 유용성을 검증하기 위해 다양한 고도, 비행마하수, 부분부하에서의 성능을 해석하였다. GPA(Gas Pess Analysis) 방법은 엔진의 성능 저하를 구성품 효율의 저하와 공기유량의 변화량으로 나타내는 방법이다. 오염, 부식, 침식과 같은 물리적 손상을 탐지하기 위한 최적의 계측변수 선정을 위해 GPA 방법은 유용하다. 본 연구에서는 최적의 계측변수를 선정하기 위해 2가지 방법을 이용하였다 하나는 독립변수의 수를 다르게 하여 계측기 수가 진단에 미치는 영향을 알아보았으며 다음 종속변수의 종류가 미치는 영향을 살펴보았다. 해석 결과에 따르면 압축기 입구 온도 및 압력, 압축기 터빈 입구 온도 및 압력, 동력 터빈 입구의 온도 및 압력과 축마력, 연료유량 등을 측정하여 진단에 이용하는 것이 가장 오차가 적었다.

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