• 제목/요약/키워드: Impeller Shape

검색결과 161건 처리시간 0.026초

스플리터 형상최적화에 의한 양흡입 원심블로어 성능개선 (Performance Enhancement of Dual-Inlet Centrifugal Blower by Optimal Design of Splitter)

  • 이종성;장춘만
    • 대한기계학회논문집B
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    • 제38권12호
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    • pp.1065-1072
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    • 2014
  • 본 연구에서는 양흡입 원심블로어의 성능향상을 위하여 임펠러 스플리터의 형상 최적화 연구를 수행하였다. 두 개의 스플리터 형상 설계 변수(스플리터 코드 및 피치)를 선정하여 블로어 성능 및 내부 유동장 특성을 평가하였다. 수치해석에 의한 블로어 성능은 설계유량 조건에서 실험결과와 최대 4 % 이내로 잘 일치하였다. 스플리터 형상 최적화를 통하여 설계조건에서의 블로어 효율 및 압력은 기준 블로어 보다 3.65 % 및 1.14 % 각각 향상되었다. 스플리터 최적설계로 임펠러 날개 부압면의 유동박리를 억제시켜 익간 저속 유동에 의한 압력손실을 줄임으로써 블로어 전체의 성능이 향상되었다. 익간 내부유동 균일화는 임펠러 출구속도 분포에도 영향을 주어 볼류트케이싱 출구압력도 향상되었다.

일체형원자로 SMART 냉각재 순환펌프의 전산성능예측 (Computational Performance Prediction of Main Coolant Pump for the Integral Reactor SMART)

  • 김민환;이재선;박진석;김종인;김긍구
    • 한국전산유체공학회지
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    • 제8권3호
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    • pp.32-40
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    • 2003
  • CFD analyses of the three-dimensional turbulent flow in the impeller and diffuser of an axial flow pump including suction and discharge parts are presented and compared with experimental data. The purpose of the current study is to validate the CFD method for the performance analysis of the main coolant pump for SMART and to investigate the effect of suction and discharge shapes on the pump performance. To generate a performance curve, not only the design point but also the off-design points were computed. The results were compared with available experimental data in terms of head generated. At the design point, the analysis accurately predicts the experimental head value. In the range of the higher flow rates, the results are also in very good agreement with the experimental data, in magnitude but also in terms of slope of variation. For lower flow rates, the results shows that the analysis considering the suction and discharge well describe the typical S-shape performance curve of the axial pump.

치수효과를 고려한 횡류홴의 작동특성연구 (A Study on the Operational Characteristic with the Scale Effect of the Cross-Flow Fan)

  • 김형섭;김윤제
    • 한국유체기계학회 논문집
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    • 제8권3호
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    • pp.26-32
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    • 2005
  • One of noticeable features in the cross flow fan is that a working fluid passes through impeller blade twice without distinction between the inlet and exit angles. Also, it does produce higher circumferential velocity than other types of blade at the same flow rate in accordance with the application of the forward curved shape. However, a design theory for the cross-flow fall has not yet been formed owing to an eccentric vortex, which is the remarkable characteristics, occurred in a cross-flow fan. Furthermore, the eccentric vortex, which is difficult to control the size and position, is the important cause of performance decrease. In this study, experiments we carried out to estimate the similarity of the cross-flow fan with various scales and rotational velocity changes. Pressure coefficients to flow coefficients with various scales of the cross-flow fan are plotted to the application of the general similarity law of the turbomachinery in the cross-flow fan with Archimedes spiral, which is the important factor having an effect on it.

API 617 규격에 의거한 프로세스 가스 터보압축기의 로터다이나믹 해석 및 안정성 검토 (A Rotordynamic and Stability Analysis of Process Gas Turbo-Compressor in accordance with API 617 Standard)

  • 김병옥;이안성
    • 한국유체기계학회 논문집
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    • 제12권5호
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    • pp.47-53
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    • 2009
  • A rotordynamic and detailed stability analysis in accordance with API 617 standard were performed with a turbo-compressor, which is one of key rotating machinery in refinery, petroleum, and power plants. The system is composed of rotor shaft, impeller, sleeve hub, balance drum, and coupling hub. The rotor system is supported by tilting pad bearings, which has 5 pads and pad on loading condition. The rotordynamic analysis specified by API 617 includes the critical speed map, mode shape analysis, Campbell diagram, unbalance response analysis, and stability analysis. In particular, the specifications of stability analysis consist of a Level 1 analysis that approximates the destabilizing effects of the labyrinth seals and aerodynamic excitations, and Level 2 analysis that includes a detailed labyrinth seal aerodynamic analysis. The results of a rotordynamic analysis and stability analysis can evaluate the operating compressor health and can be utilized as a guide of its maintenance, repair and trouble solution.

해양광물자원 개발을 위한 사류형펌프의 내부유동 해석 (Internal Flow Analysis on a Mixed Flow Pump for Developing Marine Mineral Resources)

  • 이진우;최영도;이영호;윤치호;박종명
    • 한국유체기계학회 논문집
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    • 제13권5호
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    • pp.11-16
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    • 2010
  • The development of lifting pumps that lift minerals to a mining vessel are one of the vital parts of the commercial mining process. The purpose of this study is to investigate internal flow and its effect on the performance of a mixed flow pump in order to improve the pump's performance. Numerical analysis was performed by commercial code of ANSYS CFX-11 based on flow rate and length of flexible hose. The rated rotational speed of the impeller is 1750rpm. For taking into account the turbulence, k-$\omega$ SST model was selected to guarantee more accurate prediction of flow separation. The simulated results are in good agreement with the experimental results and showed that its efficiency and the head of the pump are related mainly to the flow rate and the length of flexible hose. A lesser flow rate caused more secondary flow through the guide vane passage. The length of flexible hose and flow rate exert much more influence on the pump's performance than the shape of the flexible hose.

The Channel Wall Confinement Effect on Periodic Cryogenic Cavitation from the Plano-convex Foil

  • Ito, Yutaka;Nagayama, Tsukasa;Yamauchi, Hiroshi;Nagasaki, Takao
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.383-390
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    • 2008
  • Flow pattern of cavitation around a plano-convex foil, whose shape is similar to the inducer impeller of the turbo-pumps in the liquid fuel rocket engine, was observed by using a cryogenic cavitation tunnel of blowdown type for visualization. Working fluids were liquid nitrogen and hot water. The parameter range to be varied was between 20 and 60mm for channel width, 20 and 60mm for foil chord, -1.8 and 13.2 for cavitation number, 3.7 and 19.5m/sec for averaged inlet velocity, $8.5{\times}10^4$ and $1.5{\times}10^6$ for Reynolds number, -8 and $8^{\circ}$ for angle of attack, respectively. Especially at positive angle of attack, namely, convex surface being downstream, the whole cavity or a part of the cavity on the foil surface departs periodically. Periodic cavitation occurs only in case of smaller cavitation size than twice foil chord. Cavitation thickness and length in 20mm wide channel are larger than those in 60mm due to the wall confinement effect. Therefore, periodic cavitation in 60mm wide channel easily occurs than that in 20mm. These results suggest that the periodic cavitation is controlled by not only the hydrodynamic effect of vortex shedding but also the channel wall confinement effect.

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Effect of the Blade Leading Edge on the Performance of a Centrifugal Compressor

  • Chu, Leizhe;Du, Jianyi;Zhao, Xiaolu;Xu, Jianzhong
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.168-172
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    • 2008
  • Three different geometry shapes of the blade leading edge in a centrifugal compressor were investigated in this paper. Numerical simulation was done to analyze the effect of the leading edge shape on the performance of the centrifugal compressor. The result shows that compared to the blunt leading edge, the circular leading edge will raise the chocking mass flow. The pressure ratio and efficiency will increase obviously. Using elliptical leading edge will get a further improvement on the performance than circular leading edge. The analysis of the flow field shows that the leading edge often causes flow separation near the inlet; using circular leading edge and elliptical leading edge will reduce the separation. What's more, using circular and elliptical leading edge will also reduce the wake loss near the outlet of the impeller. In a centrifugal compressor, using circular or elliptical leading edge on the splitter will improve the pressure loading distribution of main blade near the position of the splitter leading, which will increase the pressure ratio.

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이산요소해석에 기초한 블레이드 형상에 따른 숏볼의 투사속도 예측 (Prediction of Velocity of Shot Ball with Blade Shapes based on Discrete Element Analysis)

  • 김태형;이승호;정찬기
    • 한국기계기술학회지
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    • 제20권6호
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    • pp.844-851
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    • 2018
  • In this study, the regression equation was suggested to predict of the shot ball velocity according to blade shapes based on discrete element (DE) analysis. First, the flat type blade DE model was used in the analysis, the validity of the DE model was verified by giving that the velocity of the shot ball almost equal to the theoretical one. Next, the DE analyses for curved and combined blade models was accomplished, and their analytical velocities of shot ball were compared with the theoretical one. The velocity of combined blade model was greatest. From this, the regression equation for velocity of shot ball according to the blade shape based on the DE analysis was derived. Additionally, the wind speed measurement experiment was carried out, and the experimental result and analytical one were the same. Ultimately, it was confirmed that the prediction method of the velocity of shot ball based on DE analysis was effective.

후드겸용 전자레인지 시로코홴의 유동 및 소음특성에 관한 연구 (A study on the flow and aeroacoustic characteristics of the sirocco fan of OTR (Over The Range))

  • 전완호;류호선;송성배;손상범
    • 한국유체기계학회 논문집
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    • 제7권1호
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    • pp.17-23
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    • 2004
  • Aeroacoustic characteristics of sirocco fan used in Over-The-Range (OTR) has been analyzed in this paper. A microwave hood combination over the gas range is short for the OTR. The flow phenomena of the double-sided sirocco fan was analyzed numerically and experimentally by using commercial code and three dimensional PIV for flow visualization. Also, microphone array is used in order to understand acoustic characteristics of OTR. Two dimensional unsteady flow and acoustic simulation is tried to qualitatively estimate the effects of tonal noise and broadband noise on the overall sound pressure level. It is found that tonal sound is generated from the strong interaction between the impeller and cutoff while broadband sound is generated from the strong secondary flows along the scroll surface. To reduce the noise level, the V-shape cut-off was applied to improve the sound quality by reducing tonal noise. So the peak noise at BPF (Blade Passing Frequency) was almost reduced. The shape of flow-guide to suppress the secondary flow over the scroll surface was carefully checked. It is found that this affects flow pattern at the fan exit and reduces the broad band noise. Through this numerical and experimental study, the sound pressure level was lowered by 4dBA compared to that of the previous fan at the operating point.

흄드실리카로부터 제조된 실리카졸의 분산인자 상관성 연구 (Correlation Research of Dispersion Factors on the Silica Sol Prepared from Fumed Silica)

  • 박민경;김훈;임형미;최진섭;김대성
    • 한국재료학회지
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    • 제26권3호
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    • pp.136-142
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    • 2016
  • To study the dispersion factors of silica sol prepared from fumed silica powder, we prepared silica sol under an aqueous system using a batch type bead mill. The dispersion properties of silica sol have a close relationship to dispersion factors such as pH, milling time and speed, the size and amount of zirconia beads, the solid content of fumed silica, and the shape and diameter of the milling impellers. Especially, the silica particles in silica sol were found to show dispersion stability on a pH value above 7, due to the electrostatic repulsion between the particles having a high zeta potential value. The shape and diameter of the impellers installed in the bead mill for the dispersion of fumed silica was very important in reducing the particle size of the aggregated silica. The median particle size ($D_{50}$) of silica sol obtained after milling was also optimized according to the variation of the size and amount of the zirconia beads that were used as the grinding medium, and according to the solid content of fumed silica. The dispersion properties of silica sol were investigated using zeta potential, turbiscan, particle size analyzer, and transmission electron microscopy.