• Title/Summary/Keyword: Stream turbine

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Development of Hydrodynamic Capacity Evaluation Method for a Vertical-Axis Tidal Stream Turbine (수직축 조류발전 터빈의 유체공학적 용량 산정기법 개발)

  • Lee, D.H;Hyun, B.S.;Lee, J.K.;Kim, M.C.;Rhee, S.H.
    • Journal of the Korean Society for Marine Environment & Energy
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    • v.15 no.2
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    • pp.142-149
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    • 2012
  • This study deals with the investigation of the scale effect for the vertical-axis tidal stream turbine by evaluating the hydrodynamic efficiency of turbine rotors of different diameters at different flow conditions. Numerical analyses are made for the turbine rotors with a same shape, but different sizes obtained using the diameter evaluation equation suggested in this paper. It is shown that the performance of turbine is clearly dependent upon the rotor size and inflow velocity, i.e. Reynolds number dependency of different-scaled turbines showing better efficiency with increasing Reynolds number. The sudden decrease of efficiency is also noticed around the transition region of Reynolds number. The hydrodynamic capacity evaluation method needed at initial stage of turbine design is suggested and exercised with some test cases. It is recommended that the method is expected to be useful for turbines with demanding powers between 10 kW and 300 kW.

A Study of Performance estimate and Flow Analysis of the 100kW Counter-Rotating Marine Current Turbine by CFD

  • Kim, Mun-Oh;Kim, Chang-Goo;Lee, Young-Ho
    • 한국신재생에너지학회:학술대회논문집
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    • 2011.05a
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    • pp.166.1-166.1
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    • 2011
  • The rotor design is fundamental to the performance and dynamic response of the Counter-rotating marine tidal current turbine. The wind industry has seen significant advancement single rotor blade technology, offering considerable knowledge and making it easy to transfer to tidal stream energy converters. In this paper, 3D flow and performance an alysis on a 100 kW counter-rotating marine current turbine blade was carried out by using the 3-D Navier-Stokes commercial solver(ANSYS CFX-11.0) to provide more efficient design techniques to design engineers. The front and rear rotor diameter is 8m and the rotating speed is 24.72rpm. Hexahedral meshing was generated by ICEM-CFD to achieve better quality of results. The rated power and its approaching stream velocity for design are 100 kW and 2 m/s respectively. The pressure distribution on the blade's suction side tells us that the pressure becomes low at the leading edge of the airfoil as it moves from the hub to the tip.

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Tidal Farming Optimization around Jangjuk-sudo by Numerical Modelling

  • Nguyen, Manh Hung;Jeong, Haechang;Kim, Bu-Gi;Yang, Changjo
    • The KSFM Journal of Fluid Machinery
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    • v.19 no.4
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    • pp.54-62
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    • 2016
  • This study presents an approach of tidal farming optimization using a numerical modelling method to simulate tidal energy extraction for 1MW scale tidal stream devices around Jangjuk-sudo, South Korea. The utility of the approach in this research is demonstrated by optimizing the tidal farm in an idealized scenario and a more realistic case with three scenarios of 28-turbine centered tidal array (named A, B and C layouts) inside the Jangjuk-sudo. In addition, the numerical method also provides a pre-processing calculation helps the researchers to quickly determine where the best resource site is located when considering the position of the tidal stream turbine farm. From the simulation results, it is clearly seen that the net energy (or wake energy yield which includes the impacts of wake effects on power generation) extracted from the layout A is virtually equal to the estimates of speed-up energy yield (or the gross energy which is the sum of energy yield of each turbine without wake effects), up to 30.3 GWh/year.

Effects of Combustor-Level High Free-Stream Turbulence on Blade-Surface Heat/Mass Transfer in the Three-Dimensional Flow Region near the Endwall of a High-Turning Turbine Rotor Cascade

  • Lee Sang Woo;Kwon Hyun Goo;Park Byung-Kyu
    • Journal of Mechanical Science and Technology
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    • v.19 no.6
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    • pp.1347-1357
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    • 2005
  • Effects of combustor-level high free-stream turbulence on the blade-surface heat/mass transfer have been investigated in the three-dimensional flow region near the endwall within a high-turning turbine rotor cascade passage. Free-stream turbulence intensity and integral length scale in the high turbulence case are 14.7 percents and 80 mm, respectively. The result shows that there is no considerable discrepancy in the blade heat/mass transfer near the endwall between the low and high turbulence cases. As departing from the endwall, however, the deviation between the two cases becomes larger, particularly in the region where flow separation and re-attachment occur. Under the high turbulence, flow disturbances such as boundary-layer separation and re-attachment seem to be suppressed, which makes the blade heat/mass transfer more uniform. Moreover, there are some evidences that endwall vortices tend to be weakened under the high turbulence.

A Spray Characteristics of Dual Orifice Injector with Different Fuel Properties (연료 종류에 따른 이중 오리피스 노즐의 분무 특성 연구)

  • Lee, D.H.;Choi, S.M.;Park, J.B.
    • Journal of ILASS-Korea
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    • v.8 no.2
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    • pp.7-15
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    • 2003
  • The effects of fuel density and fuel viscosity on spray characteristics were investigated under two different gas turbine fuels and various fuel supply pressure conditions through measurement of SMD, number density and volume flux by using PDPA system in dual orifice injector for gas turbine engines. In this study, we found out that the droplet size and spray structure are strongly depend on fuel density for dual orifice injector. The spray characteristics of high density fuel in dual orifice injector are similar with the characteristics of low density fuel in single orifice injector. The shear region between primary main fuel stream and secondary main fuel stream is examined in low density fuel condition but not exist in high density fuel condition, then this shear region is very important in quality of gas turbine spray. There are worth consideration for the effect of fuel density on spray characteristics in frontal device design to improve combustion efficiency.

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Mathematical Model for the Effect of Blade Friction on the Performance of Pelton Turbine

  • Atthanayake, Iresha Udayangani;Sugathapala, Thusitha;Fernando, Rathna
    • International Journal of Fluid Machinery and Systems
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    • v.4 no.4
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    • pp.396-409
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    • 2011
  • Water turbines have been used in electricity generation for well over a century. Hydroelectricity now supplies 19% of world electricity. Many hydro power plants are operated with Pelton turbines, which is an impulse turbine. The main reasons for using impulse turbines are that they are very simple and relatively cheap. As the stream flow varies, water flow to the turbine can be easily controlled by changing the number of nozzles or by using adjustable nozzles. Scientific investigation and design of turbines saw rapid advancement during last century. Most of the research that had been done on turbines were focused on improving the performance with particular reference to turbine components such as shaft seals, speed increasers and bearings. There is not much information available on effects of blade friction on the performance of turbine. The main focus in this paper is to analyze the performance of Pelton turbine particularly with respect to their blade friction.

Measurements of Endwall Heat(Mass) Transfer Coefficient in a Linear Turbine Cascade Using Naphthalene Sublimation Technique (나프탈렌승화법을 이용한 터빈 익렬 끝벽에서의 열(물질)전달계수 측정)

  • Lee, Sang-U;Jeon, Sang-Bae;Park, Byeong-Gyu
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.25 no.3
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    • pp.356-365
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    • 2001
  • Heat (mass) transfer characteristics have been investigated on the endwall of a large-scale linear turbine cascade. Its profile is based on the mid-span of the first-stage rotor blade in a industrial gas turbine. By using the naphthalene sublimation technique, local heat (mass) transfer coefficients are measured for two different free-stream turbulence intensities of 1.3% and 4.7%. The results show that local heat (mass) transfer Stanton number is widely varied on the endwall, and its distribution depends strongly on the three-dimensional vortical flows such as horseshoe vortices, passage vortex, and corner vortices. From this experiment, severe heat loads are found on the endwall near the blade suction side as well as near the leading and trailing edges of the blade. In addition, the effect of the free-stream turbulence on the heat (mass) transfer is also discussed in detail.

Experimental Study on Power Improvement of a Flapping Tidal Stream Turbine by Mimicking a Manta-Ray (쥐가오리 모방 진동식 조류 터빈의 출력향상에 대한 실험적 연구)

  • Ko, Jin Hwan;Kim, Jihoon
    • Ocean and Polar Research
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    • v.39 no.4
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    • pp.293-300
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    • 2017
  • Various approaches have been tried in an effort to improve the power performance of a flapping tidal stream turbine after it was introduced as an alternative to conventional rotary turbines. Among the different approaches, researches on mimicking the morphology and behavior of animals have been conducted. In this study, we utilized a flapper to mimic the multi-joint pectoral fin of a Manta-ray and investigated its effect on power generation. Experiments were conducted by a dual flapping apparatus with rigid and flexible flappers in a towing tank facility. First, in order to determine the conditions that can produce high power generation, the performances of the dual rigid flappers were compared when input arm angles and frequencies are changed, and the two conditions $40^{\circ}$, 0.2 Hz and $40^{\circ}$, 0.3 Hz for the input arm angle, frequency were selected. When the mimicked flexible flapper was used instead of the front rigid flapper and the rear one, the power was improved by an average of 22% and 38% in the experimental conditions, respectively. Moreover, it was recognized from the apparent camber observed during the experiment that the flexible flapper had been successfully applied. If the feasibility of the Manta-Ray mimicked flapper is improved through subsequent researches, the flapping tidal turbine can be a viable alternative to rotary turbines in the near future.

Experimental Study on Stream Turbine Cascade Flow (증기터빈 익렬유동에 관한 실험적 연구)

  • 권순범;윤의수;김병지
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.8
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    • pp.2177-2183
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    • 1994
  • The rapid expansion or condensible gas such as moist air of steam gives rise to nonequilibrium condensation. As a result of irreversibility of condensation process in the supersonic cascade flow of low pressure steam turbine, the entropy of the flow is increased, and the efficiency of the turbine is decreased. In the present study, to investigate the flow of moist air in 2-dimensional cascade made as the configuration of the tip section of the last actual steam turbine moving blade, the static pressure at both sides of pressure and suction of blade are measured by static pressure taps and the distribution of Mach number on both surfaces of the blade are obtained by using the measured static pressure. Also, the flow field is visualized by a schlieren system. From the experimental results, the effects of the stagnation temperature and specific humidity on the flow properties in a 2-dimensional stationary cascade of a practical steam turbine blade are clearly identified.

Study for Dynamic Stall Characteristics of Vertical Axis Wind Turbine Airfoil (수직형 풍력터빈 익형의 동특성 분석)

  • Kim, Cheol-Wan;Cho, Tae-Whan
    • 한국신재생에너지학회:학술대회논문집
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    • 2009.11a
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    • pp.478-481
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    • 2009
  • As a first step for aerodynamic analysis of vertical axis wind turbine, dynamic stall characteristics of airfoil was investigated. Dynamic stall of wind turbine airfoil is caused by severe variation of angle of attack and relative velocity of flow around airfoil. Angle of attack and relative velocity can be expressed with tip speed ratio. Variation of angle of attack is strongly dependent on the tip speed ratio. For tip speed ratio, 1.4 and free stream velocity, 15m/s, dynamic stall characteristics of wind turbine airfoil is compared with those of oscillating airfoil having same angle of attack variation.

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