• Title/Summary/Keyword: Impeller design

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Design of a Pump-Turbine Based on the 3D Inverse Design Method

  • Chen, Chengcheng;Zhu, Baoshan;Singh, Patrick Mark;Choi, Young-Do
    • The KSFM Journal of Fluid Machinery
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    • v.18 no.1
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    • pp.20-28
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    • 2015
  • The pump-turbine impeller is the key component of pumped storage power plant. Current design methods of pump-turbine impeller are private and protected from public viewing. Generally, the design proceeds in two steps: the initial hydraulic design and optimization design to achieve a balanced performance between pump mode and turbine mode. In this study, the 3D inverse design method is used for the initial hydraulic impeller design. However, due to the special demand of high performance in both pump and reverse mode, the design method is insufficient. This study is carried out by modifying the geometrical parameters of the blade which have great influence and need special consideration in obtaining the high performance on the both modes, such as blade shape type at low pressure side (inlet of pump mode, outlet of turbine mode) and the blade lean at blade high pressure side (outlet of pump mode, inlet of turbine mode). The influence of the geometrical parameters on the performance characteristic is evaluated by CFD analysis which presents the efficiency and internal flow results. After these investigations of the geometrical parameters, the criteria of designing pump-turbine impeller blade low and high sides shape is achieved.

Effects of the Impeller Inlet Tip Clearance on the Flow and Performance of Airfoil Fans (임펠러 흡입구 간극이 원심형 에어포일 송풍기의 성능에 미치는 영향)

  • Kang, Shin-Hyoung;Kim, Young-Jae
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.23 no.8
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    • pp.957-968
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    • 1999
  • Performance tests of an airfoil fan and measurement of flow fields at the impeller exit are carried out to investigate the effects of the tip clearance between the rotor and inlet casing on the impeller performance. The impeller is twelve bladed of NACA 65-810 airfoils and tested with 3 different size of gap; 1, 2, 4mm. The relative decrease of pressure rising performance of the fan is 15 percent for the design flow rate when the gap size is 1 percent of the impeller diameter. The reduction of performance becomes large as the flow rate increases. The leakage flow through the clearance affects the through flow of the impeller, which results in decrease of the slip factor as well as the impeller efficiency. The data base obtained in the present study can be used for the design and flow analysis of the airfoil fans.

Internal Defect Minimization of Die Cast Impeller Blade Using Taguchi's Design of Experiment (다구치 실험계획법을 이용한 임펠러 블레이드 다이캐스팅의 내부 결함 최소화)

  • Kim, D.;Choo, I.H.;Lee, Y.S.;Kim, S.W.
    • Transactions of Materials Processing
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    • v.19 no.3
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    • pp.173-178
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    • 2010
  • A die cast impeller blade has been developed in the effort on cost reduction in marine equipment industry. The purpose of this work is to optimize the die casting process using Taguchi's design of experiment for minimizing the internal defect of the die cast impeller blade. The experiments were preformed using the numerical simulation based on the L18 orthogonal array. As a results, the internal defect size of the die cast impeller blade for optimal design was controlled less than 1mm.

Flow characteristics at the Impeller Exit of a Centrifugal Pump (원심펌프의 회전차 출구 유동 특성)

  • Hong, Soon-Sam;Kang, Shin-Hyoulg
    • 유체기계공업학회:학술대회논문집
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    • 2000.12a
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    • pp.36-44
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    • 2000
  • The flow at the impeller exit is important to validate engineering design and numerical analysis of pumps. We installed axisymmetric collector instead of the volute casing, so there is no interaction between the impeller and casing. A hot-film probe and a high response pressure transducer are used to investigate the flow at impeller exit and vaneless diffuser region for design and off design flow rate. For a single suction centrifugal pump of low specific speed, the flow field such as velocity, flow angle, and total pressure are measured by traversing the probe across the vaneless diffuser. These data can be used for performance prediction, design, and numerical analysis of pumps.

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A study on a design for a centrifugal pump impeller shape (원심펌프 회전차 형상 설계에 대한 연구)

  • 김진환
    • Journal of Ocean Engineering and Technology
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    • v.11 no.4
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    • pp.213-220
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    • 1997
  • In this study, a design for a shape of centrifugal pump impeller has been performed using a p.c. under a Windows environment. Interaction between a user and a computer has been easily established using the Visual Basic. In determining an outer diameter of an impeller, steps are divided into two, a basic computational step and a refinment step. In this way user can enter his/her experience at the refinment step and hence can expect to lessen the nonlinear nature inherent to the design. In determining a shape of a side view of an impeller, the Bezier cubic curve has been used, and it can be seen that the Bezier cubic curves are well suited in the shape design under a Windows environment. By simply manipulating the four control points, one can generate various cubic curves among which one is selected. Also, a simple method, which can determine the curved position of an impeller vane, has been developed. These data can be used for final CAD drawings.

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Blade Shape Design of Mixed-flow Pump Impellers and Diffusers in a Fixed Meridional Geometry (자오면 고정 형상에서 사류펌프 임펠러 및 디퓨져 날개형상 설계)

  • Kim, Sung;Choi, Young-Seok;Lee, Kyoung-Yong
    • Proceedings of the SAREK Conference
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    • 2009.06a
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    • pp.1203-1208
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    • 2009
  • In this paper, the flow characteristics of the mixed-flow pump impellers and diffusers were numerically predicted by commercial CFD software and DOE(design of experiments). We also discussed how to improve the performance of the mixed-flow pump by designing the impeller and diffuser in the mixed-flow pump. Geometric design variables were defined by the vane plane development which indicates the blade-angle distributions and length of the impeller and the diffusers. Firstly, the design optimization of the defined impeller geometric variables has been done. After that, the flow characteristics were analyzed in the point of incidence angle at the diffuser leading edge for the optimized impeller. Then design of the defined diffuser shape variables has been performed. The reason for the performance improvement was discussed by examining the flow characteristics through the diffuser.

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A study on the design of cross-section of impeller for 3-lobes blower (나선형 3엽 블로어의 임펠러 단면설계)

  • Lee, H.S.
    • Proceedings of the KSME Conference
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    • 2001.06c
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    • pp.77-82
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    • 2001
  • The 3-lobes blower has been conventionally made by constructing the impeller with the cross-section of simple arc, and has several problems such as noise, vibration and the oscillation of torque. These are caused by the variation of clearance between both impellers rotating in geared. In the present study, an approach for the design of cross-section of impeller has been proposed to prevent the above problems. The whole cross-section is divided into the concave and convex part. The concave zone is designed by simple arc and the convex zone is modified by the condition that some part of convex zone is always in contact with the other impeller during rotating. A sample design has been carried out and it can be seen that the clearance between both impellers is always uniform and the validity of present work has been verified.

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Impeller Redesign of Multi-stage Centrifugal Pumps (다단 원심펌프 임펠러의 개량 수력설계)

  • Oh, JongSik;Kim, DongSoo
    • 유체기계공업학회:학술대회논문집
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    • 2001.11a
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    • pp.177-184
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    • 2001
  • For two kinds of the multi-stage centrifugal pump with diffuser vanes and return channel vanes the meanline performance prediction is applied to get information of hydraulic performance at each internal flow station, because only flange-to-flange test curves are available. As a first step of redesign fur higher efficiency, the impeller geometry is numerically investigated in the present study. Quasi-3D inviscid loading distributions are obtained, for the two impellers, using the state-of-the-art method of impeller 3D design, which provides a guide to optimal redesign. Full 3D turbulent flow fields are thereafter analyzed, using the specialized CFD code, to confirm the redesign results. The inherent limitation of the traditional graphic method of impeller design, which most of domestic pump manufacturers are now employing, is found.

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Effect of impeller geometrical parameter on the performance of a centrifugal (임펠러 형상변수가 원심펌프 성능에 미치는 영향)

  • Kim, Sung;Choi, Young-Seok;Kim, Joon-Hyung;Yoon, Joon-Yong
    • Proceedings of the SAREK Conference
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    • 2008.06a
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    • pp.1303-1308
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    • 2008
  • This paper presents effects of impeller geometrical parameters on the performance of a centrifugal pump impeller. The effects of meridional parameters and vane plane development parameters on the performance of the impeller were numerically studied using a commercial CFD code and DOE(design of experiments) software. Geometrical parameters in a method of meridional view and vane plane development were selected and defined to generate the 3D impeller shape. The response variables are defined in a total head and efficiency curve with flow rate. The influences of selected design variables on the various objective functions were examined as a result of the calculation using 2k factorial.

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A Study on the Performance Characteristics of the 2-D Centrifugal Turbomachinery (2차원 원심식 터보기계의 성능특성에 관한 연구)

  • 최민선;김춘식;이영호
    • Journal of Advanced Marine Engineering and Technology
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    • v.18 no.3
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    • pp.43-51
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    • 1994
  • The design technique of turbo pumps has been developed due to an increasing demand from related industrial fields. But infant stage of turbomachinery in the domestic industry needs more fundamental design method. Among various types of pumps, centrifugal pump was chosen because of its wide industrial application. It is difficult to decide the correct specification of centrifugal impeller, because of its complex flow analysis at the inlet, passage and outlet. This study is limited on the impeller blade design and its related performance analysis.

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