ultra low head turbine

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    FINAL PRESENTATIONON

    Study of Ultra Low Head Turbine for N

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    NISCHAL POKHAREL (32102)

    PRADEEP PARAJULI(32098)PRATIK KOIRALA(32117)

    REJIT DULAL(32081)

    TEAMWOR

    K

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    Background

    Objectives

    Ultra low head(ULH) turbine : Introduction

    Scope of work

    Methodology

    Operational principle

    Work accomplished Problem faced

    Conclusion

    Project overview

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    BACKGROUND

    Hydropower Status of Nepal

    Problem and Solutions Small projec

    affordable c

    Project concern

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    OBJECTIVES

    Investigate the existing hydropower and identify core issues forvery low head hydropower

    Findings regarding the aesthetics of the ultra-low head turbiits reliability, functionality and selection of sites and future

    proceedings for the design.

    Design and the installations arrangementhe ultra-low head turbine

    Design of the test

    turbine and data a

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    Ultra low head(ULH) turbine : Introduct

    Ultra low-hea

    Head : lessthan 5 m

    Applicableeven natur

    man-marivers an

    canals wlittle or n

    water stor

    capacit

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    SCOPE AND LIMITATIONS

    Study of possibility of Ultralow

    head turbine and the possible area of installation(Terai and man made canals)

    Simple prototype design and design

    consideration of the canal required(no velocity

    triangle analysis)

    Electrical components (ge

    Study of metallurgical pro

    and hub material for turb

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    METHODOLOGY

    Literature review

    Consultation

    Web search

    Email

    Books

    Site visit

    Panauti canal

    (discharge

    measurement andposibility ofapplicationn)

    Model preparation

    First model

    Second model

    Third model

    Model testing

    Test at irrigation canearby roshi khola

    (panauti)

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    CONTD..

    = (

    ) F

    = (

    )

    Where, =(

    )

    which is drop in water level due to velocity.

    =

    Q= flow rate

    v2=(d1/d2)v1

    v2= downstream velocity

    V1= upstream velocity

    Counteracting force due

    acceleration

    Force due to pressure

    difference

    Thus power output,,

    = ( ) ( )

    And the efficiency, =

    =

    ()

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    WORKS ACCOMPLISHED

    Visit to Rossi kholaCanal

    Model preparation and testing

    (along design)

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    First Model

    Second Model

    Third Model

    CONTD..

    Fig :Successful modification of our model

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    Discharge and head measurement at RossiKholacanal Discharge obtained by Floatation method= 1.093 /

    Depth of canal= 1.305

    Both head (below 5 )and discharge ( 10 /) arewithin the required range for ULH turbine

    Concluded site to be favorable for it.

    Development of the model design

    First Model

    o Tested in Rossi kholacanal

    o Rotates in anticlockwise directionwith 20

    o But deviation in static pressuredifference principle due to lack ofhub

    Second Model

    o Deviation corrected byit and blades attached t

    o Expected to test it in frMechanics Lab and asstesting was done

    o But not tested

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    Testing of model :

    Consultation with Associate.Prof. Dr.

    Dimitar Kisliakov ,Dept. of Hydraulicengg,Bulgariaabout design parameter.

    Inability to test due to the problem of:

    1. Presence of side plate that block

    water passage.

    2. Inaccurate ratio of blade and the hub

    3. Also, leakage problem

    Fig Isometric view of second model

    Fig Assembly arrangement for second mod

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    Fig: Isometric view of third model Fig: Different views of

    Design of third Model:

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    CONTD.. Third Model:

    oSmall model was prepared with some design considerations

    oBoth hub and blades made up of PVC pipe

    oSlots was made on hub to attach blades to increase strength

    oSealing done by M-seal

    oGeometric specifications:

    Consists of 8 curved blades with a preferred angle of 20

    degrees. The blade depth, T = 10.6 cm

    The hub diameter, D =15.24 cm

    The projected blade length (L) parallel to the axis of hub=23 cm [to maintain the relation (L

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    CONTD..

    Also following assumptions are to be made while testing it

    Hub diameter = 1.2 to 1.25 times headdifference (to reduce the turbulence lossesduring blade entry upstream)

    d2= blade depth T but not less than 0.7 T (tomake significant efficiency)

    The projected blade length parallel to hub axis

    not less than 0.7 times the canal width to allowwater from sides.

    Fig: Top view of

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    jn

    Canal

    reservior

    pump

    Site Selected for testing

    Direction of flow of water

    In front of FluLab

    Closed loop w

    Pump (18 L/s

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    Failure of testing in the planned

    site at nearby fluid lab due toinsufficient discharge .

    Plannin

    own ca

    of testinearby

    THEN

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    CANAL SEPCIFICATION

    Use of wooden plank.

    Width of base of the canal= 35 cm

    Height of the side planks of the canal= 42 cm

    Length of each wooden planks= 220 cm

    Bearing (SKF 6205) was used to adjust the shaft(diamater 2.the canal wall

    Turbine fitted at distance of 150cm from intake.

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    TEST SETUPTURBINE HUB

    SHAFT

    TURBINE BLADESIDEWAYS LOSS BLOCKAGE

    INTAKE WATER

    LEVELOUTLET WATER

    LEVEL

    BEARING

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    MODEL TESTING AND RESULT

    Tested on the site nearby roshi khola .

    Discharge varied by varying the area of

    intake of canal.

    Upstream velocity noted

    Upstream height noted

    Rpm noted

    Efficiency and ideal pow

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    Data analysis

    v2 d1 H Q Fp Fa Po Pi efficiency

    0.65 0.14 0.07 0.016 12.8 5.2 5.0 11.00 45.14

    0.70 0.15 0.08 0.017 14.4 6.4 5.6 13.47 41.81

    0.75 0.16 0.09 0.018 16.0 7.7 6.2 16.15 38.48

    0.79 0.17 0.10 0.019 17.5 9.1 6.7 19.07 35.15

    0.84 0.18 0.11 0.021 19.0 10.6 7.1 22.20 31.82

    0.89 0.19 0.12 0.022 20.4 12.2 7.3 25.56 28.49

    0.93 0.2 0.13 0.023 21.7 13.9 7.3 29.15 25.16

    0.98 0.21 0.14 0.024 23.0 15.7 7.2 32.96 21.83

    1.03 0.22 0.15 0.025 24.3 17.6 6.8 36.99 18.50

    1 2 3 4

    Q 0.016 0.017 0.018 0.019 0

    Po 5.0 5.6 6.2 6.7

    0.000

    1.000

    2.000

    3.000

    4.000

    5.000

    6.000

    7.000

    8.000

    outputpower

    Graph showing thdischarge and ou

    T =gHQ

    = 39.71 Nm

    The torque calculated for the head difference of 12 cm is

    N= 12 rpm, H= 12 cm

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    Problems Faced

    Very few source ofinformation

    Insufficient discharge at theplanned cannel to test Solutio

    Design of own

    selecting the te

    Testing at the icanal near Ros

    GANTT CHART

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    GANTT CHARTS.N Activity March April May June

    1. Concept

    development

    2. Literature review

    3. Model preparationfor testing

    4. Site Selection for

    testing

    5. Progress report

    and midterm

    presentation

    6. Material

    collection and test

    rig preparation

    7. Testing of the

    model and data

    analysis

    8. Final

    Presentation

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    CONCLUSION AND RECOMENDAT

    Learned about design criteria of the ULH turbine

    Universal test rig needed to be prepared

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    THANK

    YOU