• 제목/요약/키워드: Turbine Rotor Blade

검색결과 342건 처리시간 0.029초

노즐과 로터가 장착된 초음속 충동형 터빈의 전산유동해석 (Numerical Flow Analysis of a Supersonic Impulse Turbine with Nozzles and Rotor blades)

  • 박편구;이은석;정은환;김진한
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
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    • pp.445-451
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    • 2004
  • Four design candidates for a 1.4MW class partial admission turbine have been chosen from a Preliminary design process. Their performance were estimated through the 3-D numerical analyses using a frozen rotor method. In order to select the optimum design, each flow analysis result was compared with others. Flow characteristics in the passages and some types of losses induced by shocks and wakes were found from calculation results. Based on these calculations, a new rotor blade was redesigned and compared with previous one through flow analysis.

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풍력 터빈 허브의 피로강도 평가 (Fatigue Strength Evaluation of Wind Turbine Hub)

  • 이현주;고장욱;오시덕
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.1033-1038
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    • 2003
  • A wind turbine obtains its power input by converting the force of the wind into a torque (turning force) acting on the rotor blades. The amount of energy which the wind transfers to the rotor depends on the density of the air, the rotor area, and the wind speed. Because it has long term operating life and very complex load condition, the fatigue strength of each component must be considered. In this paper, we calculated the load condition by wind using a combined blade elemental theory and a FEM based analytical approach was use to evaluate the fatigue strength of a Hub of wind turbine. The effect of tensile mean stress was taken into account by the modified Goodman diagram. Using this approaches, we evaluated the fatigue strength of hub and main shaft and improved the design.

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1단 축류터빈 로터의 후류에서 비정상 전압력 측정에 관한 연구 (Measurement of Unsteady Total Pressure downstream of an 1-Stage Axial Turbine)

  • 강정식;차봉준;양수석;이대성
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2005년도 연구개발 발표회 논문집
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    • pp.318-323
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    • 2005
  • To evaluate the accurate performance of turbomachinery, it is important to measure the unsteady flow phenomena downstream of the rotor blade. This paper presents the development of the fast-response total pressure probe for the measurement of the total pressure field at the exit of rotor and the result of measurement in a 1-stage axial turbine. The fast-response total pressure probe was fabricated by installing a fast-response pressure sensor near the head of a Kiel probe. And it measured the phase-lock averaged total pressure downstream of an 1-stage axial turbine. The developed probe successfully measured the accurate total pressure distribution at rotor exit and made possible to evaluate the loss distribution and the accurate performance of turbomachinery.

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새로운 방식의 소형 풍력발전기 시스템 고찰 (Research of New Type Small Wind Turbine System)

  • 김영민;황종선;김종만;김병욱;김동용
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2005년도 춘계학술대회 논문집
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    • pp.130-134
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    • 2005
  • The objectives of this study are to improve the aerodynamics performance on the down-wind blade system with folding type blade which consists of the folding type rotor blade, wind vane yawing stabilizer and a bevel gearbox. The aerodynamics performance for the new wind turbine system are compared with those of the conventional up-wind blade system. In addition to, a novel multi voltage inverter system is applied for reductions of harmonic.

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10 kW급 수평축 풍력 터빈 로터 블레이드의 공력 설계 (Aerodynamic Design of 10 kW-level HAWT Rotor Blades)

  • 장세명;이장호
    • 한국항공우주학회지
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    • 제35권10호
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    • pp.884-890
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    • 2007
  • 10 kW급 수평축 풍력 터빈의 로터를 개발하기 위해 블레이드의 공력 설계 절차를 체계적으로 연구하고 실행하였다. 운동량 이론과 깃 요소법에 근거한 역 설계 방법을 확립하고, 이를 이용하여 주어진 공력 분포에 따른 근사 최적 형상을 설계하였다. 설계된 형상은 공군사관학교의 풍동에서 검증되었고, 본 설계를 통하여 실제로 제작된 로터로부터 실측 데이터를 취득하여 비교하였다. 본 연구를 통하여 저자들은 풍력 터빈 블레이드의 설계 방법에 대한 체계적 기술을 축적하고, 나아가 같은 방법을 중대형 시스템으로 확장하기 위한 기술적 노하우를 취득하였다.

Numerical Predictions of Roughness Effects on the Performance Degradation of an Axial-Turbine Stage

  • Kang Young-Seok;Yoo Jae-Chun;Kang Shin-Hyoung
    • Journal of Mechanical Science and Technology
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    • 제20권7호
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    • pp.1077-1088
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    • 2006
  • This paper describes a numerical investigation on the performance deteriorations of a low speed, single-stage axial turbine due to use of rough blades. Numerical calculations have been carried out with a commercial CFD code, CFX-Tascflow, by using a modified wall function to implement rough surfaces on the stator vane and rotor blade. To assess the stage performance variations corresponding to 5 equivalent sand-grain roughness heights from a transition ally rough regime to a fully rough regime, stage work coefficient and total to static efficiency were chosen. Numerical results showed that both work coefficient and stage efficiency reduced as roughness height increased. Higher surface roughness induced higher blade loading both on the stator and rotor which in turn resulted in higher deviation angles and corresponding work coefficient reductions. Although, deviation angle changes were small, a simple sensitivity analysis suggested that their contributions on work coefficient reductions were substantial. Higher profile loss coefficients were predicted by higher roughness heights, especially on the suction surface of the stator and rotor. Furthermore sensitivity analysis similar to the above, suggested that additional profile loss generations due to roughness were accountable for efficiency reductions.

터보펌프 터빈의 열구조적 적합성 검증을 위한 터빈로터-파이로시동기 연계시험 (Turbine Rotor-Pyrostarter Coupled Test for the Verification of Thermo-Structural Suitability of a Turbopump Turbine)

  • 정은환;강상훈;홍문근;이항기;이수용;김진한
    • 한국추진공학회지
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    • 제18권1호
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    • pp.65-72
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    • 2014
  • 터보펌프 터빈로터의 열구조적 적합성 검증을 위한 터빈로터-파이로시동기 연계시험을 수행하였다. 새로운 추진제를 적용한 파이로시동기와 열응력 경감 설계 및 터빈 동익 표면 건전성 향상을 위한 후 가공 공정이 적용된 터빈로터시편이 시험에 사용되었다. 시험은 75톤급 엔진시동을 위한 파이로 시동기의 연소가스를 터보펌프 터빈로터와 동일한 형상의 시편에 분사하는 방식으로 이루어졌다. 터빈에 가해지는 열 부하는 운용 설계점에서 극한 조건까지 세 종류로 구분하여 시험을 진행하였으며 모든 시험에서 터빈로터의 손상은 발견되지 않았다.

굽힘 및 비틀림 연성 효과를 고려한 대형 풍력 터빈 블레이드의 강제 진동 및 하중 해석 (Forced Vibration and Loads Analysis of Large-scale Wind Turbine Blades Considering Blade Bending and Torsion Coupling)

  • 김경택;박종포;이종원
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2008년도 추계학술대회논문집
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    • pp.256-263
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    • 2008
  • The assumed modes method is developed to derive a set of linear differential equations describing the motion of a flexible wind turbine blade and to propose an approach to investigate the forced responses result from various wind excitations. In this work, we have adopted Euler beam theory and considered that the root of the blade is clamped at the rigid hub. And the aerodynamic parameters and forces are determined based on Blade Element Momentum (BEM) theory and quasi-steady airfoil aerodynamics. Numerical calculations show that this method gives good results and it can be used fur modeling and the forced vibration analysis including the coupling effect of wind-turbine blades, as well as turbo-machinery blades, aircraft propellers or helicopter rotor blades which may be considered as straight non-uniform beams with built-in pre-twist.

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ANALYSIS OF A LAMINATED COMPOSITE WIND TURBINE BLADE CHARACTERISTICS THROUGH MATHEMATICAL APPROACH

  • CHOI, YOUNG-DO;GO, JAEGWI;KIM, SEOKCHAN
    • Journal of the Korean Society for Industrial and Applied Mathematics
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    • 제23권4호
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    • pp.367-380
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    • 2019
  • A 1kW-class horizontal axis wind turbine (HAWT) rotor blade is taken into account to investigate elastic characteristics in 2-D. The elastic blade field is composed of symmetric cross-ply laminated composite material. Blade element momentum theory is applied to obtain the boundary conditions pressuring the blade, and the plane stress elasticity problem is formulated in terms of two displacement parameters with mixed boundary conditions. For the elastic characteristics a fair of differential equations are derived based on the elastic theory. The domain is divided by triangular and rectangular elements due to the complexity of the blade configuration, and a finite element method is developed for the governing equations to search approximate solutions. The results describe that the elastic behavior is deeply influenced by the layered angle of the middle laminate and the stability of the blade can be improved by controlling the layered angle of laminates, which can be evaluated by the mathematical approach.

Tidal Current Power Generation by a Darrieus Type Water Turbine at the Side of a Bridge Pier

  • Kyozuka, Yusaku;Wakahama, Hisanori
    • 한국해양공학회:학술대회논문집
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    • 한국해양공학회 2006년 창립20주년기념 정기학술대회 및 국제워크샵
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    • pp.99-104
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    • 2006
  • There are several advantages to make use of a bridge pier for the tidal power generation. Current velocity increases near the pier, therefore the tidal power generation becomes more efficient because the power is proportional to the cubic of the current velocity. The pier is convenient for access and maintenance of the hydraulic turbine and the power unit. The project is now underway at the Ikitsuki Bridge in Tatsuno-Seto Strait of Nasasaki Prefecture, where the tidal current was measured by the bottom mount ADCP for almost one year. Model experiments for a Darrieus water turbine with two and three straight blades were carried out in the circulating water channel, in which the power coefficients of the turbine were obtained as a function of blade section and the attaching angle of a blade to the rotor. Those experimental results are discussed to obtain an optimum Darrieus turbine for tidal power generation.

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