Renewable Energy(Wind)

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    RENEWABLE

    ENERGY(WIND)

    Dr. Biswajit Basu

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    Topics

    1. Introduction Wind Turbine2. Wind Characteristics and Resources

    General, Atmospheric Boundary Layer, Wind data

    analysis, resource estimation, statistical techniques,measurement and instrumentation

    3. Aerodynamics

    1-D momentum and Betz limit, Ideal HAWT, Bladeelement theory, Blade shape, rotor design simplifiesHAWT rotor performance calculation, Drag, advancedtopics

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    Introduction

    Important factors for re-emergence of windenergy

    NeedNeed; finiteness of fossil fuel

    Potential; wind exists everywhere in the world TechnologyTechnology; other fields applied to wind turbine

    VisionVision; a new way to use

    Political willPolitical will; support research, testing, provideregulatory reform, interconnection withnetworks, incentive

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    Modern Wind Turbines

    Difference between wind mill are wind turbine capacity

    small ~ 10 kW to ~ 50 kW to 2 MW

    Aerodynamic force of lift => net positive torque on rotating

    shaft => mechanical power => electricity in a generator

    Not possible to store ~responds to wind immediately

    available

    Variability/Fluctuation

    Not transportable

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    Modern Wind Turbine

    Horizontal Axis Wind Turbine ( HAWT)

    HAWT ROTOR CONFIURATION

    OptionsOptions

    Number of Blades ( 2 or 3)

    Rotor Orientation

    Blade material, Profile

    Hub Design Power Control =>Aerodynamic control ( STALL)

    => Variable Pitch Blade ( Pitch Control)

    Fixed or Variable Rotor Speed Orientation by self aligning ( Free Yaw) or direct control

    (Active Yaw)

    Gearbox or Direct drive Generator

    Synchronous or Induction Generator

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    Rotor

    Hub and Blades (important from performance

    and cost)

    Most turbines up wind with 3 blades

    Fixed blade pitch with stall control ( intermediate

    size), Increased pitch control ( larger size)

    Materials; composites- fiber glass reinforcedplastics (GRP), wood/epoxy laminates

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    Drive Train

    Rotating parts

    Low speed shaft (rotor side), gear box, high speed shaft

    (generator side)

    Supporting bearings, couplings, brakes, rotating parts ofgenerator

    Types of gearbox: parallel shaft, planetary larger

    machines (planetary gearbox) Unique loading: fluctuating wind and dynamics of large

    rotors

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    Generator

    Induction or Synchronous

    Induction more popular (50 Hz, 1500 rpm)

    Induction: more rugged, inexpensive, easy toconnect to network

    Variable speed wind turbine( less wear andtear, more efficiency)

    Hardware: variable speed; power electronicscomponent; suitable power electronicconverters

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    Nacelle and Yaw System Wind turbine housing, machine bed plate or maintenance

    and yaw orientation system Mainframe: mounting and alignment

    Nacelle: Protection from weather

    Yaw system : align rotor with wind direction (bearingconnecting mainframe to tower)

    Active: Contain motors which drive pinion gear against a bullgear attached to the yaw bearing

    Sensor: On Nacelle

    Yaw Brakes

    Free yaw in down wind machine

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    Tower and Foundation

    Tower structure and foundation

    Free standing; stand tubes; lattice or concrete

    For smaller turbines, guyed towers

    Tower height is typically 1 to 1.5 times rotordiameter

    Possibility of coupled tower/rotor vibration

    For down wind rotors, effect of tower shadow

    causes complex tower dynamics, power

    fluctuations, noise generation

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    Controls

    Sensor speed, position, temperature,flow, current

    Controller mechanical, electrical,

    computer Power amplifiers switches, electrical

    amplifiers, hydraulic pumps, valves

    Actuators motors, pistons, magnetsand solinoids

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    Aim:

    Upper bound on torque and power

    experienced by drive train

    Maximizing fatigue life of rotor drive train

    and structural components

    Maximize energy production

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    Balance of Electrical Systems

    Cables, switchgear, transformer

    Power electronic converters, power

    factor correction capacitors

    Yaw, pitch motors

    Interconnection with network

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    Wind Characteristics

    Mechanics of wind motion

    Spatial variation in heat transfer to the earths atmosphere

    create variations in the atmospheric pressure field

    Cause: Air movement from high to low pressureFour atmospheric forces

    1. Pressure forces

    2. Coriolis force (rotation)

    3. Inertial forces (large scale circular motion)

    4. Frictional forces

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    Wind Characteristics (contd)

    Pressure force 1p

    p

    F n

    =

    = density of air, p = pressure ( n is the direction

    normal to the lines of constant pressure)

    Coriolis Force Fc= fu, u = wind speed,

    f = Coriolis parameter = 2 sinw

    = Latitude, = angular rotation of earthw

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    Variation in time

    Inter-annual:> 1 year, long term

    30 years data required, average (annual) over 5years

    Prediction at 90% confidence levelAnnual: Significant seasoned variations;

    monthly average wind speeds

    Diurnal: Large wind variations on a daily scaledue to differential heating of earths surfaceduring the daily radiation cycle

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    Short-term:

    Short term wind speed variation induce

    turbulence and gust over mean

    Usually mean variation over 10 min or

    less sampled at 1 sec. Stochastic character represent

    turbulence Gust is a discrete event

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    Atmospheric boundary layer

    Lapse rate dp = -gdzp = pressure, = density,z = elevation measured positive upward

    1st Law of ThermodynamicsHeat transferred, dq = du + pdv

    = dh dp

    =CpdT 1/ dpT = temperature, u = internal energy, h = enthalpy,= Specific heat, Cp =constant pressure specific heat

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    Atmospheric boundary layer

    (contd)

    For adiabatic pressure, dq = 0

    Therefore, CpdT = 1/ dp = -g/Cpwhich gives

    g = 9.81 m/s2; Cp= 1.005 KJ/kgKThis is important for atmospheric stability and generation of

    turbulence

    0 . 0 0 9 8

    a d i a b a t i c

    d T K

    d z m

    =

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    Turbulence

    Turbulence Intensity ( TI)

    Velocity,_

    u U U= +

    0

    1, 10min

    t

    U udt t

    t

    = =

    _

    U=mean, U =fluctuating

    Sampled form,1

    1i

    is

    U uN =

    = sN

    , . ,s st N t N No of samples t Sampling time = = =

    uTI

    U

    =

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    Turbulence (contd)

    where, standard deviation

    ( )2

    1

    1

    1

    sN

    u i

    is

    u UN

    =

    =

    Normally, TI = 0.1 to 0.4, depends on site terrain

    features and surface conditions

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    Wind Velocity Profile

    Log law

    ( )*

    0

    lnU zU zk z

    =

    z0= Surface roughness, K = Von Karman constant = 0.4U*=friction velocity

    0*ln( ) ( ) ln( )

    K

    z U z zU

    = + Also,

    Z0 is a function of terrain

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    Wind Velocity Profile (contd)

    Power law (simple)0

    0

    ln

    ( )( ) ln rr

    z

    zU zzU z

    z

    =

    ( )( )r r

    U z zU z z

    =

    = function of elevation, time of day, season, terrain, temperature

    ( )( )

    0.37 0.088ln,

    1 0.088 ln 10

    ref

    ref

    Uvelocity height

    z

    =

    ( )2

    10 0 10 00.096log 0.016 log 0.24z z= + +(surface

    roughness)

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    Wind Speed Measurement

    Cup anemometers: Based on rotation

    Propeller anemometers: Three

    dimensional measurement of velocity

    components Kite anemometers: At heights greater

    than towers; at areas of high turbulenceAcoustic Doppler sensors (SODAR)

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    Advanced Topics

    Application of stochastic processes

    Fatigue Model field data with historical datae

    Turbulence

    Load Structured excitation

    Fatigue

    Control Power Quality

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    Advanced Topics (contd)

    CFD for flow characterization

    Numerical modelling of complex flow Micrositing

    Resource assessment tool to determine exactposition

    CFD models or micrositing models

    Statistically based resource assessment Alternative of physical models

    MCP approach (Measure-Correlate-Predict)

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    1-D Momentum Theory and Betz

    Limit

    Idealized rotor turbine

    Actuator disk model of WT

    Assumptions: Homogeneous, incompressible, steady state flow

    No frictional drag

    Infinite number of blades

    Uniform thrust over disk

    A non rotating wake

    Static pressure for upstream and for downstream of the

    rotor is equal to the undisturbed air pressure

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