the main objective of the use of wind turbine is generating electricity

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    NEED FOR CONTROL SYSTEM.

    .The main objective of the use of WINDturbine is generating electricity.

    .The power output P, from a wind turbine

    is given by the epression!

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    . Electrical energy generated form a

    wind turbine varies as the cube of

    wind speed.

    .The power _ wind velocity contains

    four regions:

    1) Wind speed < cut _ in speed:

    at this region the eciency is not

    accepted.

    !) Wind speed "cut _in speed:at this region the wind turbine

    starting to wor#.

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    $) Wind speed "rated speed :

    at this speed the generator wor#ing

    at speci%ed rated power.

    &) Wind speed '" cut _out _speed:

    that may causes damage the wind

    turbine

    and causes the damage of the

    generator.

    . (o we need to control system for:

    1) capture rated power.

    !) *rotect the wind turbine from high

    wind turbine.

    $) When generator disconnected

    suddenly prevent the rotor from

    runaway.

    &) +irection control.

    Drag & lift forces

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    .,ift is de%ned to be the component

    of this force that is perpendicular to

    the oncoming -ow direction.

    .+rag is de%ned to be the

    component of this force that is in thesame direction the oncoming -ow

    direction.

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    "ngle of attac# is the angle between the

    lifting body$s reference line and theoncoming %ow.

    . The critical angle of attac# is the angle

    of attac# which produces maimum lift

    coe&cient.

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    Power control

    . y far the most e/ective way of

    in-uencing the aerodynamic angle

    of attac# and thus the input

    power is by mechanically

    ad0usting the rotor blade pitch

    angle for this purpose in general

    the rotor blade is turned about its

    longitudinal ais with the aid of

    actively controlled actuators.

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    .*ower control by changing the

    aerodynamic angle of attac# of

    the rotor can be achieved by two

    methods:

    2) the conventional approach is by

    ad0usting the angle of attac# of

    the blade to a smaller angle in

    order to reduce power input.

    3onversely increasing the angleof attac# increases the power

    input.

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    . 22) The other possibility is to

    change the blade pitch angle to a

    larger angle of attac# up to theso4called critical aerodynamic

    angle of attac# at which point the

    air-ow separates at the surface of

    the rotor blades thus limiting the

    aerodynamic power input.

    . This e/ect is #nown as a stall.

    Active itc! control

    . 2n general the rotor blade is

    turned about its longitudinal ais

    with the aid of

    actively controlled actuators..There is two types of active pitch

    control.

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    2) F"ll#san itc! control$ rotating

    all each blade about its ais in

    the direction which reduces the

    angle of attac#.22) Partial#san itc! control$ %

    a'("sting t!e itc! of onl )*

    to +,- of t!e %la'e lengt! is

    sucient from the point of

    view of aerodynamic eciency.

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    la'e itc!ing 'rive

    The main distinguishing feature of

    blade pitching systems is the type of

    drive.

    .there is two types:

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    2) 5ydraulic drives 22) electrical

    drives

    /'ra"lic la'e Pitc!

    Sste0s

    .(upply of the actuators is commonly

    housed at a %ed location in thenacelle so that the supply lines must

    be routed through the gearbo and

    the hollow rotor shaft into the hub.

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    . To reach the rotating hub from the

    stationary nacelle a sealed hydraulic

    rotary transmissionlead through is re6uired.

    .Three hydraulic actuators are

    installed outside the rotor hub. The

    hydraulic supply and return lines for

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    the actuators are routed through the

    hollow rotor shaft and through the

    gearbo into the rear part of thenacelle to the pressure supply

    system located there which consists

    of a motor4driven pump and pressure

    accumulators.

    . The actuators are controlled by

    means of control valves via a change

    in mass -ow or control pressure.

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    . To avoid having to use a rotary lead

    through one can either locates the

    entire hydraulic system in therevolving hub or the actuators have

    to be installed in a %ed position in

    the nacelle.

    2n the latter case the pitch

    ad0ustment motion must be

    transmitted into the revolving hub

    by means of mechanical transmission

    elements

    .for eample a connecting rod The

    hydraulic actuator wor#s against astrong spring so that in a

    brea#down involving the complete

    loss of system pressure the rotor

    blades are forced into the feathered

    position by the spring thus causing

    the rotor to stop.

    2n wind turbines with partial blade

    pitching

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    the pitch mechanism must be

    installed in the outer blade area.

    Electrical la'e Pitc!

    Sste0s

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    .The power supply for emergencypitch ad0ustment consists of two

    batteries which are also located in

    the rotor hub.

    The %rst one of these was Enercon

    where each rotor blade on theirmedium4si7ed range of turbines 8E4

    &9) has its own electric pitch motor

    mounted on the outside -ange ring

    8igs. ;.1). =ther manufacturers

    place the electric pitching drivecompletely inside the rotor hub

    Stall control

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    .a stall is a reduction in the lift

    coecient generated by an airfoil as

    angle of attac# increases.. This occurs when the critical angle

    of attac# of the airfoil is eceeded.

    . Where the angle of attac# increases

    beyond a certain point such that the

    lift begins to decrease.

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    . low separation %eginsto occur atsmall angles of attac# while attac!e'

    -ow over the wing is still dominant.

    >s angle of attac# increases the

    separated regions on the top of the

    wing increase in si7e and hinder thewing?s ability to create lift.

    >t the critical angle of attac#

    separated -ow is so dominant that

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    further increases in angle of attac#

    produce lesslift and vastly more

    drag.

    Yaw sste0

    .@aw system has been used with all

    hori7ontal ais wind turbines toorient the nacelle and the rotor as.

    Aertical ais wind turbines do not

    need a yaw system since their

    vertical rotors can face the wind

    from any direction.

    .The wind direction changes.

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    F"nction

    .the @aw system has two main

    functions:

    1)orienting the rotor and

    the nacelle into the wind.

    !) (ome turbines also

    use active yaw as a means of power

    control.

    . @awing the rotor with respect to the

    wind direction it reduces the

    e/ective swept area with respect to

    the wind direction.

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    1ariations in win'

    'irection

    .variations of wind direction in time

    can be divided into the following

    categories:

    . 2nter4annual

    . >nnual.+iurnal

    .(hort4term 8gusts and turbulence).

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    . 2nter4annual:2nter4 annual

    variations in wind direction occur

    over time scales greater than oneyear.

    . >nnual:(igni%cant variations in

    seasonal or monthly.

    . +iurnal 8time of day):large wind

    variations also can occur on a

    diurnal or daily time scale.

    . (hort4term:(hort4 term wind

    direction variations of interest

    include turbulence and gusts.

    2in' 'irectioninstr"0entation

    .due to continuous change at wind

    direction (o we need a winddirection sensor.

    . Wind direction is normally

    measured via

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    the use of a wind vane.

    . Wind vanes usually produce signals

    bycontact closures or by

    potentiometers.

    .=ne type of wind that the use of

    self4synchronous motors.

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    .The transmitter T is mechanically

    connected to a wind vane while the

    receiver B is connected to a pointer

    on an indicating instrument.

    .oth rotors are connected to thesame source of ac.

    .When the induced voltages are the

    same and opposing each other

    there will be no current -ow and no

    rotor tor6ue.

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    . When the transmitter rotor is

    moved voltage magnitudes become

    unbalanced causing currents to -owand a tor6ue to be produced on the

    receiver rotor.

    . This causes the receiver rotor to

    turn until it again is in alignment

    with the transmitter rotor.

    .=ther type of wind vane which

    wor#s well for digital data system.

    .2t consists of potentiometer a

    voltage source A and an analog to

    digital converter.

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    . The potentiometer is oriented so

    the output voltage Advalue is

    changes due to wind directionchanges.

    . The >C+ converter converts Adto a

    digital form for recording.

    .Each digital number represents a

    range of wind direction.

    Tes

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    'a

    wTy

    pe

    'a

    wTy

    pe

    y aw i n

    gb yf a n (t a i l

    w he e l

    y aw i n

    gb yf a n (t a i l

    w he e l

    awing % fan#tailw!eels

    .@awing with the help of a fan4tail is

    the simplest method.. @awing with the aid of a fan4tail

    wheel can still be found in some

    smaller turbines.

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    .the fantail in the cap of the turbine.

    . the fantail parallel to the air-ow

    at this case it did not turn ..if the wind shifted it would begin to

    turn the fantail .

    .this would turn a shaft running from

    the fantail

    +own to wheels or a gear bo whichwould turn the turbine bac# into the

    wind .

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    This has the advantage of not

    re6uiring a separate power source

    or controls.

    free Yaw te

    . Turbines with free yaw are normally

    downwind machines..2f the rotor is positioned downwind

    the point of attac# of the total

    aerodynamic force of the rotor is

    located behind the ais of rotation of

    the tower head.

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    .the yaw ais so that with the cross

    wind force the aerodynamic forces

    produce a restoring moment on the

    rotor within a very wide yaw angle

    range.

    .2n turbines with free yaw the yaw

    system is normally much simpler.

    . =ften there is nothing more than

    the yaw bearing..ree yaw machines sometimes

    incorporate yaw dampers to limit the

    yaw rate.

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    Active Yaw te

    . Dpwind turbines normally have

    some type of active yaw control.

    . This usually includes:

    . =ne or more yaw motors gears

    .bra#e to #eep the turbine stationaryin yaw when it is properly aligned.

    . The speed must be reduced so that

    the yaw rate is slow and so that

    ade6uate tor6ue can be suppliedfrom a small motor.

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    Yaw %earing. Begardless of the type of yaw system

    all hori7ontal ais wind turbines have

    some type of yaw bearing.

    .The primary component is a large

    bearing that connects the main frame tothe tower.

    . 2t serves as a rotatable connection

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    between the tower and the nacelle of

    the wind turbine.

    .2n a turbine with active yaw theyaw bearing includes gear teeth

    around its circumference.

    .@aw damping is desirable even during

    the yawing in order to avoid unwanted

    yawing oscillations.

    .These re6uirements can be met both by

    a

    conventional roller bearing.

    Yaw %ra3es

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    .yaw bra#e system comprising:

    . +is# bra#e.

    .ra#e caliper.

    . 3aliper actuator 8hydraulic).

    .When not yawing the machinery is

    positively loc#ed by means of several

    yaw bra#e calipers acting on a bra#e

    disc.

    .dis# bra#e is a device for slowing or

    stopping the rotation of while it is in

    motion.

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    'a

    wdr

    ive

    hy

    drau

    l icsy

    ste

    )l e

    ct ri ca l

    syst

    em

    . To stop the wheel friction material

    in the form of bra#e pads is forced

    mechanically hydraulicallypneumatically or electromagnetically

    against both sides of the disc.

    The bra#e caliper is the assembly

    which houses the bra#e pads and

    pistons.

    Yaw 'rive

    . The yaw drive is the name given to

    the mechanism used to rotate the

    nacelle with in order to #eep theturbine facing into the wind.

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    . The two choices for the yaw drive

    are hydraulic or electrical

    components.the hydraulic system name lower

    costs smaller si7e and also higher

    tor6ue as advantages.

    . Each yaw drive consists of powerful

    electric or hydraulic motor with its

    electric drive and

    a large gearbo which increases the

    tor6ue.

    Yaw Control. There are two aims of control

    system:

    .1) the deviation of the rotor from

    the wind direction the yaw angle is

    supposed to be as small as possible

    to avoid power loss.

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    .!) The yaw control system must not

    respond too sensitively to avoid

    continuous small yaw movementswhich would reduce the life of the

    mechanical components.

    . The yaw motion in an active yaw

    system is controlled using yaw erroras an input.

    .@aw error is monitored by means of

    a wind vane mounted on the turbine.

    . When the yaw error is outside the

    allowed range for some period oftime the drive system is activated

    and the turbine is moved in the

    appropriate direction.

    . The problem is to %nd a practicable

    compromise as it is not possible toset up a general rule.

    . The situation relating to theW>4F9

    turbine will be given as an eample.

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    . The wind measuring system of the

    turbine provides a mean value of the

    wind direction over a period of tenseconds.

    .2f the deviation remains below $

    degrees the yaw control system willnot be activated.

    . 2f the yaw angle determined is

    above this value the time until

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    correction is determined in

    accordance with a pre4programmed

    function..2f the wind speed eceeds $F mCs

    the rotor will not be yawed.

    References

    1_ Wind Turbines: undamentals Technologies>pplications Economics GErich5auH

    !_ Wind Energy 5andboo# GTonyurtonH

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    *+"PT) -*NT/

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