• Title/Summary/Keyword: 터빈 최적 직경

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A Study of Optimum Design of Impulse Turbine for 500kW Class OWC-type Wave Energy Conversion (500kW급 OWC형 파력발전장치 설계를 위한 임펄스터빈 최적 직경 산출에 대한 연구)

  • Moon, Jae-Seung;Hong, Key-Yong;Shin, Seung-Ho;Hyun, Beom-Soo;Kim, Gil-Won
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2007.12a
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    • pp.123-124
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    • 2007
  • 파력발전은 파랑에너지를 이용하여 유용한 에너지를 얻어내는 것인데, 본 논문에서는 그 가운데 진동수주 (Oscillating Water Column)형을 연구 대상으로 취하였다. 이는 외해에서의 파랑에너지를 공기실에 유입 집중시켜 공기실 내 수면의 승강운동을 증폭시키고 이로 인해 발생한 공기실 내의 공기 흐름을 터빈의 구동력으로 사용하는 것을 말한다. 적지 선정과정에서 채택된 곳의 설계파고를 바탕으로 원하는 정격출력인 500kW를 얻어낼 수 있도록 유량과 임펄스 터빈의 최적 직경을 산출하고자 하였는데 개념설계된 파력발전장치의 덕트가 쌍동형 형태를 취하고 있으므로 한 터빈당 250kW급을 목표 발전용량으로 하였다. 지난 연구를 통해서 기 작성된 터빈 성능도표를 활용하여, 본 연구에서는 1차적으로 임펄스 터빈의 개략적인 직경 및 유량을 구하고, 터빈의 자기 기동 특성을 고려하여 최종적인 형상을 구체적으로 도출하였다.

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Design of 3MW class outer rotor type PMSG for wind turbine (풍력 발전용 3MW급 외전형 영구자석 동기발전기 설계)

  • Kim, Taehun;Kim, Geohwa;Kim, Dongeun;Chung, Chinhwa;Park, H.C.
    • 한국신재생에너지학회:학술대회논문집
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    • 2010.11a
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    • pp.179.1-179.1
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    • 2010
  • 포항공과대학교 풍력특성화대학원에서는 3MW급 외전형 영구자석 동기발전기 설계를 진행하고 있다. 여기서 외전형이란 RFPM 발전기에서 회전자가 바깥에서 회전하는 형태로 기존의 RFPM 발전기와 비교하여 같은 공극직경에 더 많은 자석을 채택할 수 있고, 회전자와 터빈 블레이드를 직접 연결이 가능하다. 또한, 회전자를 외부에 노출 시킬 수 있으므로 냉각에 유리한 면이 있다. 설계 변수 중 출력과 회전수를 고정시키고 각 극수와 공극 직경, 전압을 변화함에 따른 전기적 특성을 비교하고, 그 중 최적의 모델을 선택한다. 선택된 모델의 전자기장 해석, 손실 계산, 열분석을 수행한다. 본 논문에서는 각 경우에 따른 결과를 비교하고 최적 모델에 대한 해석 결과에 대해 요약한다.

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Optimum Design of Dual Orifice Fuel Nozzle (이중 오리피스 연료 노즐 최적설계)

  • Lim, O-Kaung;Choi, Eun-Ho;Kim, Sung-Sub
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.20 no.4
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    • pp.407-416
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    • 2007
  • Fuel spray nozzle has a critical effect on combustion characteristics. Mass flow rate and SMD(sauter mean diameter) were selected as design variables by using the experiment data of various types of duplex fuel nozzles for the swirl atomizers. The sensitivity of each design variable on the mass flow rate and SMD was analyzed and the uniformity of mass flow rate was investigated through the shape optimization of duel-orifice-type swirl atomizers. The design variables that have a little effect on the optimum design were excluded using the DOE(design of experiments) method, which enabled the optimization of sensitive design variables on mass flow rate and limit tolerance. The SMD of the research spray nozzle that was used in this study was found to be most similar to that of the calculation results using the Jasuja's SMD relationship. This study showed the specific characteristics of duel orifice type swirl atomizers and the optimization of these kinds of nozzle. This study provided the optimization design of mass flow rate and its allowable tolerance.

Parametric Numerical Study on the Performance of Helical Tidal Stream Turbines (헬리컬 터빈의 설계인자에 따른 성능 연구)

  • Han, Jun-Sun;Choi, Da-Hye;Hyun, Beom-Soo;Kim, Moon-Chan;Rhee, Shin-Hyung;Song, Mu-Seok
    • Journal of the Korean Society for Marine Environment & Energy
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    • v.14 no.2
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    • pp.114-120
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    • 2011
  • The characteristics of a helical turbine to be used for tidal stream energy conversion have been numerically studied with varying a few design parameters. The helical turbines were proposed aiming at mitgating the well known poor cut-in characteristics and the structural vibration caused by the fluctuating torque, and the basic concept is introducing some twisting angle of the vertical blade along the rotation axis of the turbine. Among many potential controling parameters, we focused, in this paper, on the twisting angle and the height to diameter ratio of the turbine, and, based on the numerical experiment, We tried to propose a configuration of such turbine for which better performance can be expected. The three-dimensional unsteady RANS equations were solved by using the commercial CFD software, FLUENT with k-${\omega}$ SST turbulence model, and the grid was generated by GAMBIT. It is shown that there are a range of the twisting angle producing better efficiency with less vibration and the minimum height to diameter ratio above which the efficiency does not improve considerably.

Optimal Design and Combustion Analysis of Fuel-rich Gas Generator for Liquid Rocket Engine Based on RP-1 fuel (RP-1연료를 사용한 농후연소 가스발생기의 최적설계 및 연소해석)

  • 권순탁;이창진
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2003.05a
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    • pp.258-261
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    • 2003
  • The optimal design and combustion analysis of the gas generator for Liquid Rocket Engine (LRE) were performed. A fuel-rich gas generator in open cycle turbopump system was designed for 101on1 in thrust with RP-1/LOx combination. The optimal design was done for maximizing specific impulse of main combustion chamber with constraints of combustion temperature and power matching in turbopump system. Results of optimal design show the dimension of length, diameter, and contraction ratio of gas generator. The configuration of the gas generator and the condition for performance which can maximize the objective function were determined and found to meet the design constraints. Also, the combustion analysis was conducted to evaluate the performance of designed chamber and injector of gas generator. And the effect of the turbulence ring was investigated on the mixing enhancement in the chamber.

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A Study on Performance Characteristics of Horizontal Axis Tidal Turbine Considering Nose Shape, Angle of Inflow and Tower Structure (수평축 조류발전 터빈의 노즈 형상 및 유입각도, 타워 구조물의 영향을 고려한 터빈 성능특성 분석)

  • Heo, Man-Woong;Kim, Dong-Hwan;Yi, Jin-Hak
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.32 no.1
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    • pp.17-25
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    • 2020
  • In this study, three-dimensional fluid flow analyses have been performed in order to investigate the performance characteristics of a horizontal axis tidal turbine (HATT) by solving three-dimensional Reynolds-averaged Navier-Stokes equations utilizing the shear-stress-transport turbulence model. The computational domain for the flow analysis has been composed of hexahedral grids, and the grid dependency test has been carried out so as to determine the optimum grid size. Performance characteristics of the HATT have been investigated in consideration of the effects of hub nose geometry, inflow angle, and the tower. It has been found that the power output can be enhanced along with an increase of the ratio of the length to the diameter of the turbine nose, and the power of HATT has been reduced by approximately 10% when the primary fluid flow had an inflow angle of 15°. The power output of downstream HATT is found to be lower than that of the upstream HATT by about 1%.

Experimental Study of Micro hydropower with Vortex Generation at Lower Head Water (저낙차에서 와류발생부를 구비한 마이크로 소수력에 관한 실험 연구)

  • Choi, In-Ho;Kim, Jong-Woo;Chung, Gi-Soo
    • Journal of Wetlands Research
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    • v.22 no.2
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    • pp.121-129
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    • 2020
  • This paper described a laboratory investigation of micro hydropower at lower head water in a free vortex flow. The vortex height, turbine rotation and torque for straight blade with inner curved edge, twisted blade and curved blade were investigated at the flow rate of 0.0069 ㎥/s in the inlet channel. The results showed that the optimum vortex strength occurred within the range of the diameter of basin to the outlet diameter ratios of 0.17~18.5. The power output and efficiency of straight blade were higher as compared to other blades. The highest amount of generated energy was 12.33 W, the torque was 0.91 N·m and the highest efficiency by considering effective head was 29.5 %, whereas the highest efficiency by considering vortex height was 80.5 % at the rotational speed of 132 rpm. The water vortex velocity of straight blade was about 2.8 times larger than the mean velocity in the inlet channel.

Study on the Design and Operation Characteristics of Ejector System (이젝터 시스템의 설계 및 작동 특성에 관한 연구)

  • NamKoung, Hyuck-Joon;Han, Poong-Gyoo;Kim, Young-Soo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.627-630
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    • 2009
  • Ejector system can induce the secondary flow or affect the secondary chamber pressure by both shear stress and pressure drop which are generated in the primary jet boundary. Ejectors are widely used in a range of applications such as a turbine-based combined-cycle propulsion system and a high altitude test facility for rocket engine, pressure recovery system, desalination plant and ejector ramjet etc. The primary interest of this study is to set up an configuration and operating conditions for an ejector in the condition of sonic and subsonic. Experimental and theoretical investigation on the sonic and subsonic ejectors with a converging-diverging diffuser was carried out. Numerical simulation was adopted for an optimal geometry design and satisfying the required performance. Also, some ejectors with a various of nozzle throat and mixing chamber diameter were manufactured precisely and tested for the comparison with the calculation results.

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Aerodynamic Retrofit of Bridge and Energy Harvesting by Small Wind Turbines (소형 풍력발전기를 이용한 교량의 공력성능 개선 및 에너지 생산)

  • Kwon, Soon-Duck;Lee, Seongho;Lee, Hankyu
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.30 no.1A
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    • pp.27-33
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    • 2010
  • This study addresses a methodology to use small wind turbines for dual purposes, improving aerodynamic performance of flexible bridges and wind energy harvesting. A way to proper placement of small wind turbines on flexible bridges were proposed according on the analogy of conventional aerodynamic appendages. From the wind tunnel tests, it was found that the wind turbine attached like fairing was effective to reduce the vortex-induced vibration of bridge and the optimal spanwise interval of the wind turbine was 3-4.5 time of turbine diameter. Moreover the aerodynamic coefficients of the bridge were improved after installation of the wind turbines. Present results showed the general availability of wind turbine for improvement of aerodynamic performance and energy supply of flexible bridges although the capacity of wind power generation was strongly dependent on wind characteristics of the bridge site.