• Title/Summary/Keyword: 혼합 날개

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Evaluation of Convective Heat Transfer Performance of Twist-Vane Spacer Grid in Rod Bundle Flow (봉다발 유동 내 비틀림 혼합날개 지지격자의 대류열전달 성능 평가)

  • Lee, Chi Young
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.40 no.3
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    • pp.157-164
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    • 2016
  • The performance of convective heat transfer in rod bundle flow was experimentally evaluated using a twist-vane spacer grid. A $4{\times}4$ square-arrayed rod bundle was prepared as the test section, with a pitch-to-diameter ratio(P/D) of ~1.35. To check the convective heat transfer performance, the circumferential and longitudinal variations in rod-wall temperatures were measured downstream of the twist-vane spacer grid. In the circumferential measurements, the rod-wall temperature toward the twist-vane tip showed the lowest value, which might be due to the deflected water flow caused by the twist-vane. On the other hand, the wall temperature of the longitudinal measurements near the twist-vane spacer grid decreased dramatically, which implies that the convective heat transfer performance was enhanced. A heat transfer enhancement of ~35 % was achieved near downstream of the twist-vane spacer grid, as compared with the upstream value. Based on the present experimental data, a correlation for predicting the heat transfer performance of a twist-vane spacer grid was proposed.

Numerical Analysis of Flow Distribution Inside a Fuel Assembly with Split-Type Mixing Vanes (분할 형태 혼합날개가 장착된 연료집합체 내부유동 분포 수치해석)

  • Lee, Gong Hee;Cheong, Ae Ju
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.40 no.5
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    • pp.329-337
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    • 2016
  • As a turbulence-enhancing device, a mixing vane, which is installed at a spacer grid of the fuel assembly, plays an important role in improving convective heat transfer by generating either swirl flow in the subchannels or cross flow between the fuel rod gaps. Therefore, both the geometric configuration and the arrangement pattern of a mixing vane are important factors in determining the performance of a mixing vane. In this study, in order to examine the flow-distribution features inside a $5{\times}5$ fuel assembly with split-type mixing vanes, which was used in the benchmark calculation of the OECD/NEA, we conduct simulations using the commercial computational fluid dynamics software, ANSYS CFX R.14. We compare the predicted results with measured data obtained from the MATiS-H (Measurement and Analysis of Turbulent Mixing in Subchannels-Horizontal) test facility. In addition, we discuss the effect of the split-type mixing vanes on the flow pattern inside the fuel assembly.

Effect of Vane Angle of Swirl Type Mixer on Flow Mixing and Pressure Drop in Marine Selective Catalytic Reduction Systems (선박용 SCR 시스템에서 스월형 혼합기의 날개 각도가 유동혼합 및 압력강하에 미치는 영향)

  • Park, Taewha;Sung, Yonmo;Kim, Taekyoung;Choi, Cheolyong;Kim, Duckjool;Choi, Gyungmin
    • Journal of Advanced Marine Engineering and Technology
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    • v.39 no.4
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    • pp.443-448
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    • 2015
  • A swirl type mixer was developed to improve the flow mixing performance of a marine selective catalytic reduction system. In this study, the swirl type mixer and a multi-staged swirl type mixer, in which the angle of the vanes at each stage is controllable were considered to provide the optimal region of angles for the mixers. The effects of the vane angles in both mixers on the uniformity index and pressure drop were investigated using a computational fluid dynamics simulation. In the swirl type mixer, the optimal conditions for the flow mixing performance were observed at vane angles from 30 to 60 degrees when vane angles could be adjusted between 10 to 80 degrees, however, the pressure drop increased continually with increasing vane angle of the mixer. On the other hand, control of the individual staged angles of the multi-staged mixer showed that it is possible to keep enhancing flow mixing performance while reducing the pressure drop.

Examination of Forced Convection Heat Transfer Performance of a Twist-Vane Spacer Grid for a Dual-Cooled Annular Fuel Assembly (이중냉각 환형핵연료 집합체를 위한 비틀림 혼합날개 지지격자의 강제대류열전달 성능 검토)

  • Lee, Chi Young
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.41 no.1
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    • pp.53-62
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    • 2017
  • The forced convection heat transfer performance of a twist-vane spacer grid for a dual-cooled annular fuel assembly was examined experimentally. The twist-vane spacer grid was uniquely designed to enhance mixing inside subchannels and mixing between adjacent subchannels. For testing, a $4{\times}4$ square-arrayed rod bundle with narrow gaps between rods was prepared as the dual-cooled annular fuel assembly to be simulated. The pitch-to-rod diameter ratio of simulated dual-cooled annular fuel assembly was 1.08. The experiments were performed under the following conditions: axial bulk velocity, 1.5 m/s and heat flux, $26kW/m^2$. With regard to the circumferential temperature distribution, the lowest rod-wall temperatures upstream and downstream were measured at the subchannel center and the position toward the tip of twist-vane, respectively. With regard to the axial temperature distribution, behind the twist-vane spacer grid, the rod-wall temperature decreased drastically, and the Nusselt number was enhanced by up to 56 %. The present measured data indicate that the twist-vane spacer grid can effectively improve the forced convection heat transfer in the dual-cooled annular fuel assembly with narrow gaps.

Viscous Flow Analysis around a Wind Turbine Blade with End Plate and Rake (풍력터빈 날개의 끝판과 레이크 효과에 대한 점성유동장 해석)

  • Kim, Ju-In;Kim, Wu-Joan
    • Journal of the Korean Society for Marine Environment & Energy
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    • v.14 no.4
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    • pp.273-279
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    • 2011
  • Turbulent flow analysis around a wind turbine blade was performed to evaluate the power performance of offshore wind turbine. Fluent package was utilized to solve the Reynolds-averaged Navier-Stokes equations in non-inertial rotating coordinates. The realizable k-$\varepsilon$ model was used for turbulence closure and the grid system combining structured and unstructured grids was generated. In the first, lift and drag forces of 2-D foil section were calculated and compared with existing experimental data for the validation. Then torque and thrust of the wind turbine blade having NACA 4-series sections were calculated with fixed pitch angle and rpm. Tip speed ratio was varied by changing wind speed. In the next, three kinds of end plate were attached at the tip of blade in order to increase the power of the wind turbine. Among them the end plate attached at the suction side of the blade was found to be most effective. Furthermore, performance analysis with tilt angle and rake was also performed.

Turbulent Heat Transfer with Mixing Vane in Nuclear Fuel Assembly (핵연료 봉다발내 혼합날개에 의한 난류열전달 해석)

  • Jung, Sang-Ho;Kim, Kwang-Yong
    • The KSFM Journal of Fluid Machinery
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    • v.10 no.4
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    • pp.9-14
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    • 2007
  • The purpose of present work is to analyze the convective heat transfer downstream of mixing vane in subchannel of nuclear reactor with three-dimensional Navier-Stokes equations. SST model is selected as a turbulence closure by comparing the performances of two different turbulent closures. Three different shapes of mixing vane are tested. And, thermal-hydraulic performances of these vanes are discussed. The results show that twist of the vane improves the heat transfer performance far downstream of the vane.