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Design of Centrifugal Pump – Impeller

Apr 03, 2018

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Rajib Mandal
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    DESIGNOF CENTRIFUGAL PUMP IMPELLER

    Submitted by:

    Supriya Naha Biswas (09259007044)

    Sweta Sarkar (09259007049)

    Sandip Agarwal (09259007038)

    Under the Guidance of:

    Prof. Abhijit Chakrabarty.Deb Dulal Ganguly.

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    WORKING PRINCIPLE

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    PUMP ELEMENTS

    Stationary Elements

    Casing

    Stuffing box Bearings

    Packing

    Rotating Elements Impeller

    Impeller shaft

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    PUMP IMPELLER

    Rotating Component.

    Consists of a disc with blades mounted

    perpendicularly on its surface.

    Vanes may be of three different orientations,

    Radial

    Backward curved

    Forward curved

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    TYPESOF IMPELLER

    Impellers can be classified in terms of so many

    parameters, i.e. direction, stage, head, inlet angle,

    speed, position of shaft etc.

    In the axial flow impellers, the head is developed by

    the propelling or lift action of the vanes on the liquid

    which enters the impeller axially and discharges

    axially.

    In the radial flow impellers, the head is developed

    by the action of centrifugal force upon the liquid

    which enters the impeller axially at the centre and

    flows radially to the periphery.

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    BASIC PERSPECTIVESOF DESIGN

    Practical design

    Economical design

    Development of existing technology

    Consideration of manufacturing issues

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    DESIGN DATAAND FORMULAE

    Head = 60 ft.

    Discharge = 2500 gal / min

    Speed = 1500 rpm

    Important formula

    Water horsepower,

    Break horsepower,

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    DESIGN CONSIDERATIONS

    Specific Speed,

    Classification of specific speed

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    DESIGN CONSIDERATIONS

    Speed ratio = 1.15

    Flow ratio = 0.170

    Diameter ratio = 0.65

    Width ratio = 0.25

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    DESIGN CONSIDERATIONS

    The selection of outlet vane angle (2) depends on the type of

    head capacity characteristics desired. For optimum efficiency,

    usually a value of about 25 is taken for all specific speeds.

    The inlet vane angle is selected so that inlet absolute velocity

    may be radial. The radius of curvature of vanes is selected

    depending on the inlet and outlet blade angles, so that a

    smooth, separation free flow is obtained in the impeller

    passage.

    The number of vanes in an impeller depends on the pump

    size, the speed ratio, the vane load and the outlet blade angle.

    With low values of outlet blade angle, usually six or eight

    vanes are adopted.

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    CALCULATEDVALUE

    Impeller outlet diameter, D2 = 0.91 ft

    Impeller inlet diameter, D1 = 0.59 ft

    Impeller outlet width, B2 = 0.23ft

    Impeller inlet width, B1= 0.35 ft

    Impeller outlet blade angle = 22.71

    Impeller inlet blade angle = 14.01

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    CENTRIFUGAL PUMP PERFORMANCE CURVE

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    INLET VELOCITY TRIANGLE

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    OUTLET VELOCITY TRIANGLE

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    IMPELLER DIMENSION

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    CONCLUSION

    Energyefficientdesign ofany machineis the

    ultimatesuccess ofthis era.

    We remainthankful to

    our Guide,HOD andeveryonewho arehelping us inthis project.

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    REFERENCES1. Ahuja, V., Hosangadi, A., Ungewitter, R. and Dash, S. M., A Hybrid Unstructured Mesh Solver for Multi-Fluid Mixtures, AIAA 99-3330,

    14th Computational Fluid Dynamics Conference, Norfolk, VA, June, 1999.

    2. Chen, Y., Heister, S.D. (1994) Two-Phase Modeling of Cavitated Flows,ASME FED-Vol. 190, pp.299-307.

    3. Gridgen User Manual, Version 13.3, Pointwise, 1999.

    4. Hirschi, R., Dupont, Ph., Avellan, F., Favre, J.-N., Guelich, J.-

    F., Parkinson, E. (1998) Centrifugal Pump Performance Drop Due to Leading Edge Cavitation: Numerical Predictions Compared With Model

    Tests,ASME Journal of Fluids Engineering, Vol. 120, No. 4, pp. 705-711,

    5. Jorgenson, P.C.E., Chima, R.V. (1989) "Explicit Runge-Kutta Method for Unsteady Rotor-Stator Interaction," AIAA Journal, Vol. 27, No. 6, pp.

    743-749.

    6. Kunz, R.F., Boger, D.A., Stinebring, D.R., Chyczewski, T.S., Gibeling, H.J., Govindan, T.R. (1999) "Multi-phase CFD Analysis of Natural and

    Ventilated Cavitation About Submerged Bodies,ASME Paper FEDSM99-7364.

    7. Kunz, R.F., Boger, D.A., Stinebring, D.R., Chyczewski, T.S., Lindau, J.W., Gibeling, H.J., Venkateswaran, S., Govindan, T.R. (2000) APreconditioned Navier-Stokes Method for Two-Phase Flows with Application to Cavitation Predication,Computers and Fluids, Vol. 29, No.

    8, pp. 849-875.

    8. Kunz, R.F., Lindau, J.W., Billet, M.L., Stinebring, D.R. (2001) Multiphase CFD Modeling of Developed and Supercavitating Flows, VKI

    Special Course on Supercavitating Flows, February.

    9. Lindau, J.W., Kunz, R.F., Gibeling, H.J. (2000) Validation of High Reynolds Number, Unsteady Multi-Phase CFD Modeling for Naval

    Applications, presented at the 23rd Symposium on Naval Hydrodynamics, Val de Reuil, France.

    10. Merkle, C.L., Feng, J.Z. and Buelow, P.E.O. (1998) Computational Modeling of the Dynamics of Sheet Cavitation, 3rd

    InternationalSymposium on Cavitation, Grenoble, France.

    11. Meyer, R.S., Yocum, A.M. (1993) Pump Impeller Performance Evaluation Tests for a Parametric Variation of Geometric Variables, ARL

    Technical Memorandum 93-125.

    12. Nakamura, S., Ding, W., Yano, K. (1998) A 2.5D Single Passage CFD Model for Centrifugal Pumps,ASME Paper FEDSM98-4858.

    13. Song, C., He, J. (1998) "Numerical Simulation of Cavitating Flows by Single-phase Flow Approach, 3rd International Symposium on

    Cavitation, Grenoble, France.

    14. Taylor, L.K., Arabshahi, A., Whitfield, D.L. (1995) Unsteady Three-Dimensional Incompressible Navier-Stokes Computations for a ProlateSpheroid Undergoing Time-Dependent Maneuvers,AIAA Paper 95-0313.

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    THANK YOU