• 제목/요약/키워드: vane angle

검색결과 164건 처리시간 0.024초

수직축 풍력터빈 성능개선에 관한 실험적 연구 (An Experimental Study on the Performance of the Vertical-Axis Wind Turbine)

  • 김병국;김영호;송우석;이승배;남상규;김사만
    • 한국유체기계학회 논문집
    • /
    • 제10권3호
    • /
    • pp.17-24
    • /
    • 2007
  • This paper presents the design procedure of a vertical wind turbine named jet-wheel-turbo turbine and the numerical and experimental verifications. The design parameters such as the rotor inlet angle, the diameter-to-hub ratio, the inlet guide outlet angle and the solidity were optimized to maximize the energy transfer, and to further increase the turbine efficiency by applying the side guide vane and the side opening to the rotor. The maximum power coefficient of 0.59, which is much higher than the ever-designed three-bladed horizontal turbines, was experimentally obtained when the optimal inlet- and side-guide vanes were installed and both sides of the rotor were 80% opened. The maximum power coefficients occur at the tip speed ratio ranging between 0.6 and 0.7. This vertical-axis turbine model can be applied to the large-scale power generation system with the speed and torque control algorithm for the specified wind characteristics.

카프란수차의 수력학적 성능특성 (Hydraulic Performance Characteristics of Kaplan Turbine)

  • 이철형;박완순
    • 한국신재생에너지학회:학술대회논문집
    • /
    • 한국신재생에너지학회 2005년도 춘계학술대회
    • /
    • pp.443-446
    • /
    • 2005
  • The Kaplan turbine model has been tested and analyzed. The blade angle and the guide vane opening of the turbine model were designed to be varied according to the best combination of guide vane and runner blade opening. When the changes in head and output were comparatively large, the efficiency drop were small, so the efficiency characteristics and stability of the entire operating condition were maintained in good condition. These results showed that the developed model in this study will be suitable for small hydro power stations with large changes in head and load.

  • PDF

저낙차 수자원활용을 위한 카프란수차 개발 (Development of Kaplan Type Turbine for Low Head Hydro Resources)

  • 이철형;박완순
    • 한국수자원학회:학술대회논문집
    • /
    • 한국수자원학회 2007년도 학술발표회 논문집
    • /
    • pp.1992-1996
    • /
    • 2007
  • The Kaplan turbine model has been tested and analized. The blade angle and the guide vane opening of the turbine model were designed to be varied according to the best combination of guide vane and runner blade opening. When the changes in head and output were comparatively large, the efficincy drop were small, so the efficiency characteristics and stability of the entire operating condition were maintained in good condition. These results showed that the developed model in this study will be suitable for small hydro power stations with large changes in head and load.

  • PDF

초고온 동압을 받는 제트 베인의 구조 안전성 평가에 대한 연구 (A study on structural safety evaluation of jet vane under very high temperature and dynamic pressure)

  • 박성한;이상연;박종규;김원훈;문순일
    • 한국추진공학회:학술대회논문집
    • /
    • 한국추진공학회 2005년도 제24회 춘계학술대회논문집
    • /
    • pp.99-105
    • /
    • 2005
  • 초고온($2700^{\circ}C$) 연소가스에 직접 노출된 상태에서 가스유동에 의한 동압을 받는 추력편향장치용 제트 베인의 열구조 안전성을 평가하기 위하여 내열합금의 초고온 인장시험 및 3차원 비선형 수치해석을 수행하였다. 고온 구조거동을 분석하여 제트 베인의 구조안전성을 평가하였으며 구조해석결과를 지상연소시험결과와 비교하였다. 구조 및 열 하중의 대부분은 제트 베인 축에 집중되었으며, 축은 $1400^{\circ}C$ 이하에서 구조적으로 안전한 것으로 밝혀졌다. 지상연소시험결과와 구조해석결과의 비교를 통하여 베인 하중과 축의 변위를 기준으로 구조안전계수를 평가하는 것이 등가응력에 의한 평가 기준보다 더 유용한 기준으로 판단되었다.

  • PDF

Influence of Guide Vane Setting in Pump Mode on Performance Characteristics of a Pump-Turbine

  • Li, Deyou;Wang, Hongjie;Nielsen, Torbjorn K.;Gong, Ruzhi;Wei, Xianzhu;Qin, Daqing
    • International Journal of Fluid Machinery and Systems
    • /
    • 제10권2호
    • /
    • pp.154-163
    • /
    • 2017
  • Performance characteristics in pump mode of pump-turbines are vital for the safe and effective operation of pumped storage power plants. However, the head characteristics are different under different guide vane openings. In this paper, 3-D steady simulations were performed under 13mm, 19mm and 25mm guide vane openings. Three groups of operating points under the three GVOs were chosen based on experimental validation to investigate the influence of guide vane setting on flow patterns upstream and downstream. The results reveal that, the guide vane setting will obviously change the flow pattern downstream, which in turn influences the flow upstream. It shows a strong effect on hydraulic loss (power dissipation) in the guide and stay vanes. It is also found that the hydraulic loss mainly comes from the flow separation and vortices. In addition, in some operating conditions, the change of guide vane opening will change the flow angle at the runner inlet and outlet, which will change the Euler momentum (power input). The joint action of Euler momentum and hydraulic loss results in the change of the head characteristics.

초고온 동압을 밭는 제트 베인의 구조 안전성 평가에 대한 연구 (A Study on Structural Safety Evaluation of let Vane under very High Temperature and Dynamic Pressure)

  • 박성한;이상연;박종규;김원훈;문순일
    • 한국추진공학회지
    • /
    • 제9권3호
    • /
    • pp.18-24
    • /
    • 2005
  • 초고온(2700$^{\circ}C$ ) 연소가스에 직접 노출된 상태에서 가스유동에 의한 동압을 받는 추력편향장치용 제트 베인의 열구조 안전성을 평가하기 위하여 내열합금의 초고온 인장시험 및 3차원 비선형 수치해석을 수행하였다. 고온 구조거동을 분석하여 제트 베인의 구조안전성을 평가하였으며 구조해석결과를 지상 연소시험결과와 비교하였다. 구조 및 열 하중의 대부분은 제트 베인 축에 집중되었으며, 축은 1400$^{\circ}C$ 이하에서 구조적으로 안전한 것으로 밝혀졌다. 지상연소시험결과와 구조해석결과의 비교를 통하여 베인 하중과 축의 변위를 기준으로 구조안전계수를 평가하는 것이 등가응력에 의한 평가기준보다 더 유용한 기준으로 판단되었다.

축류펌프 안내 깃 최적화 설계를 위한 전산 유동해석 (CFD Analysis for Optimization of Guide Vane of Axial-Flow Pump)

  • 윤정의
    • 대한기계학회논문집B
    • /
    • 제40권8호
    • /
    • pp.519-525
    • /
    • 2016
  • 펌프 성능 관점에서 바라보면 회전날개의 충격손실을 최소화하는 것은 매우 중요하다. 본 연구는 회전날개의 충격손실에 직접적으로 영향을 미치는 흡입 케이싱 내에 설치되는 안내깃의 형상 및 설치 각 변화가 축류 펌프의 성능에 미치는 효과를 수치 해석 방법을 통해 살펴보았다. 그리고 주어진 운전조건에서 흡입 케이싱 내에 설치되는 안내깃의 최적형상 및 설치 각을 최적화 기법을 사용하여 최적화하였다.

극저비속도 원심펌프의 불안정성능개선 및 소형화에 관한 연구 (Improvement of Performance Instability and Miniaturization of Very Low Specific Speed Centrifugal Pump)

  • 최영도;쿠로카와준이치
    • 한국유체기계학회 논문집
    • /
    • 제10권4호
    • /
    • pp.21-28
    • /
    • 2007
  • The ratio of disk friction loss in a centrifugal pump is very large for the total pump loss in the range of very low specific speed. Therefore, impeller radius should be shortened to increase the pump efficiency because the disk friction loss is proportional to the fifth power of impeller radius. In order to compensate the decreased head by the shortened impeller radius, vane angle at impeller outlet should be increased. However, as the vane angle at impeller outlet becomes larger, performance instability occurs at low flow rate regions. In this study, J-Groove is adopted to suppress the performance instability and detailed examination is performed for the influence of the J-Groove on the pump performance. The results show that J-Groove gives good effect on the suppression of performance instability. Moreover, as J-Groove increases pump head considerably, the pump size can be smaller for head requirements.

디퓨저 깃배치각의 변화에 따른 원심압축기의 공력성능 특성에 관한 수치 연구 (NUMERICAL INVESTIGATION OF THE EFFECT OF THE STAGGER ANGLE ON THE AERODYNAMIC PERFORMANCES IN THE VANED DIFFUSER OF A CENTRIFUGAL COMPRESSOR)

  • 박태규;정인수;정희택;박준영;김세미;백제현
    • 한국전산유체공학회:학술대회논문집
    • /
    • 한국전산유체공학회 2010년 춘계학술대회논문집
    • /
    • pp.131-135
    • /
    • 2010
  • In the present study, the effects of the stagger angles on the aerodynamic performances in the vaned centrifugal compressor has been investigated by CFD methods. The diffuser vane angles were vane angles were varied in the range of ${\pm}10$ deg. from the intial-design points. The commercial Navier-Stokes solver, ANSYS-CFX were applied to solve the impeller-diffuser flowfields. Through the numerical results, the desirable setting angles were proposed to fit the best performance to the variation of the operating conditions.

  • PDF