chapter2-2 types of dc motor

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    DC Motor - 2

    Muhamad Zahim

    Ext : 2312

    BEE2123

    ELECTRICAL MACHINES

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    Contents

    Overview of Direct Current Machines

    Construction Principle of Operation

    Types of DC Motor

    Power Flow Diagram

    Speed Control

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    DC motor principles

    DC motors consist of rotor-mountedwindings (armature) and stationarywindings (field poles). In all DC motors,

    except permanent magnet motors,current must be conducted to thearmature windings by passing currentthrough carbon brushes that slide overa set of copper surfaces called acommutator, which is mounted on the

    rotor. Parts of an electric motor

    The commutator bars are soldered to armature coils. The brush/commutatorcombination makes a sliding switch that energizes particular portions of thearmature, based on the position of the rotor. This process creates north andsouth magnetic poles on the rotor that areattracted to or repelled by northand south poles on the stator, which are formed by passing direct current

    through the field windings. It's this magnetic attraction and repulsion thatcauses the rotor to rotate.

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    The Advantages

    The greatest advantage of DC motors may be speed

    control. Since speed is directly proportional to armature

    voltage and inversely proportional to the magnetic flux

    produced by the poles, adjusting the armature voltage

    and/or the field current will change the rotor speed.

    Today, adjustable frequency drives can provide precise

    speed control for AC motors, but they do so at the

    expense of power quality, as the solid-state switching

    devices in the drives produce a rich harmonic spectrum.

    The DC motor has no adverse effects on power quality.

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    The drawbacks

    Power supply, initial cost, and maintenancerequirements are the negatives associated with DC

    motors Rectification must be provided for any DC motors

    supplied from the grid. It can also cause power qualityproblems.

    The construction of a DC motor is considerably morecomplicated and expensive than that of an AC motor,primarily due to the commutator, brushes, and armaturewindings. An induction motor requires no commutator orbrushes, and most use cast squirrel-cage rotor bars

    instead of true windings two huge simplifications.

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    Major types of dc motors

    Self excited dc motor Series dc motor

    Shunt dc motor

    Compound dc motor

    Separately excited dc motor

    Permanent magnet dc motor

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    Series motors

    Series motors connect

    the field windings in

    series with thearmature.

    Series motors lack good

    speed regulation, but

    are well-suited for high-

    torque loads like powertools and automobile

    starters because of their

    high torque production

    and compact size.

    Ea

    Rf

    M VT (dc

    supply)

    Raia

    )( faaaT RRiEV

    La iinote :

    aa IKKE 21

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    Series Motor Power Flow Diagram

    P

    Pout

    Pin= VTiL

    Pca=ia2Ra

    Pcf=ia2Rf

    Pm

    P is normally given

    Pin= Pout+ total losses

    Where,

    Pca =armature copper loss

    Pcf =field copper loss

    P=stray, mech etc

    in

    out

    mm

    oo

    P

    PEf f iciency

    N

    Ptorquemechanicalfor

    N

    Ptorqueloadoutputfor

    N

    P

    ,

    2

    60,

    2

    60,/

    2

    60

    Pm= Eaia

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    Series Motor (cont)

    Example 1:

    A dc machine in Figure 1 is

    consumed a 6.5kW when the12.5 A of armature current ispassing thru the armature andfield resistance of 3.3and 2.0respectively. Assume straylosses of 1.2kW. Calculate

    a) terminal voltage, VTb) back emf, Ea

    c) net torque if the speed is at3560rpm

    d) efficiency of the machine

    [520V, 453.75V, 12N-m, 68.8%]

    Ea

    Rf

    M VT (dc

    supply)

    Raia

    Figure 1

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    Series Motor (cont)

    Example 2:

    A 600V 150-hp dc machine inFigure 2 operates at its full rated

    load at 600rpm. The armature andfield resistance are 0.12and0.04respectively. The machinedraws 200A at full load. Assumestray losses 1700W. Determine

    a) the armature back emf at full load,

    Eab) developed/mechanical power anddeveloped/mechanical torque

    c) assume that a change in loadresults in the line current droppingto 150A. Find the new speed inrpm and new developed torque.

    {Hint: Ea=K1K2ia}

    Ea

    Rf

    M VT (dc

    supply)

    Raia

    Figure 2

    [568V, 113.6kW, 1808Nm, 811.27rpm, 1017Nm]

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    Shunt motors

    Shunt motors use high-resistance field windingsconnected in parallel with the

    armature. Varying the field resistance

    changes the motor speed.

    Shunt motors are prone toarmature reaction, a distortionand weakening of the fluxgenerated by the poles that

    results in commutationproblems evidenced by sparkingat the brushes.

    Installing additional poles, calledinterpoles, on the statorbetween the main poles wired inseries with the armature

    reduces armature reaction.

    Ea VT (dc

    supply)

    Raia

    if

    RfM

    iL

    )( aaaT RiEV

    ffT

    faL

    RiV

    iiinote

    :

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    Shunt Motor (power flow diagram)

    PPout

    Pin=VTiL

    Pca=ia2Ra

    Pcf=if2Rf

    Pm

    P is normally given

    Pin= Pout+ total losses

    Where,

    Pca =armature copper loss

    Pcf =field copper loss

    P=stray, mech etc

    in

    out

    mm

    oo

    P

    PEf f iciency

    N

    Ptorquemechanicalfor

    NPtorqueloadoutputfor

    N

    P

    ,

    2

    60,

    260,/

    2

    60

    Pm= Eaia

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    Shunt Motor

    Example :

    A voltage of 230V is applied to armature of amachines results in a full load armature currents

    of 205A. Assume that armature resistance is

    0.2. Find the back emf, net power and torque by

    assuming the rotational losses are 1445W at full

    load speed of 1750rpm.

    [189V, 37.3kW, 203.5Nm]

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    Compound motors

    the concept of the

    series and shunt

    designs arecombined.

    Ea VT (dc

    supply)

    Raia

    if

    Rf1M

    iLRf2

    )(2faaaT

    RRiEV

    1

    :

    ffT

    faL

    RiV

    iiinote

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    Compound motor (power flow diagram)

    P is normally given

    Pin= Pout+ total losses

    Where,

    Pca =armature copper loss

    Pcf =field copper loss

    P=stray, mech etc

    in

    out

    mm

    oo

    P

    PEf f iciency

    N

    Ptorquemechanicalfor

    NPtorqueloadoutputfor

    N

    P

    ,

    2

    60,

    260,/

    2

    60

    Pm= Eaia

    PPoutPin=VTiL

    Pca=ia2Ra

    Pcf1=if2Rf1

    Pm

    Pcf2=ia2Rf2

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    Separately Excited Motor

    There is no direct connection between the

    armature and field winding resistance

    DC field current is supplied by an

    independent source

    (such as battery or another generator or prime

    movercalled an exciter)

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    Separately Excited Motor (Cont)

    nKniKC

    pnZ

    E fffa 60

    2

    fff RiV

    aaaT RiEV

    Where p= no of pole pair

    n= speed (rpm)

    Z=no of conductor

    =Flux per pole (Wb)C= no of current/parallel path

    =2p (lap winding)

    =2 (wave winding)

    KVL:

    Circuit analysis:

    La iinote :

    Ea

    Ra Laia

    M

    Rf

    VTVfLf

    If

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    Permanent Magnet motors

    PMDC is a dc motor whose poles are made of

    permanent magnets.

    Do not require external field circuit, no copper losses

    No field winding, size smaller than other types dc

    motors

    Disadvantage: cannot produce high flux density,

    lower induce voltage

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    Speed Control for shunt motor and

    separately excited dc motor

    Torquespeed characteristic for shunt and separately

    excited dc motor

    a

    ff

    a

    ff

    a

    a

    a

    aa

    aa

    R

    nIK

    R

    IVK

    excitedseparatelyassame

    nE

    REV

    n

    IE

    IEtorqueDeveloped

    22

    ,

    2

    2

    ,

    22

    a

    ff

    R

    IVKc

    2

    Starting

    torque

    a

    ff

    R

    nIK

    slope 2

    22

    nNLnn

    m

    =0

    n=0

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    Speed Control for shunt motor and

    separately excited dc motor

    By referring to the Torquespeed characteristic for shunt andseparately excited dc motor

    note that, there are three variables that can influence the speed of

    the motor, VIf

    Ra Thus, there are three methods of controlling the speed of the

    shunt and separately excited dc motor,

    i. Armature terminalvoltage speed control

    ii. Field speed control

    iii. Armature resistance speed control

    a

    ff

    a

    ff

    RnIK

    RIVK

    22

    22

    Variables

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    Speed Control for shunt motor and

    separately excited dc motor

    i. Armature resistance speed control

    - Speed may be controlled by changing Ra

    - The total resistance of armature may be varied by means of a

    rheostat in series with the armature

    - The armature speed control rheostat also serves as a starting

    resistor.

    - From -n characteristic,

    a

    ff

    a

    ff

    start

    R

    nIKslope

    R

    IVKc

    2

    2

    22 Will be changed

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    Speed Control for shunt motor and

    separately excited dc motor

    Torquespeed characteristic

    Ra1

    nNL nn1

    m

    Ra2

    Ra3

    Ra1 < Ra2< Ra3

    n2n3

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    Speed Control for shunt motor and

    separately excited dc motor

    Advantages armature resistance speed control:

    i. Starting and speed control functions may be combined in one

    rheostat

    ii. The speed range begins at zero speed

    iii. The cost is much less than other system that permit control

    down to zero speed

    iv. Simple method

    Disadvantages armature resistance speed control :

    i. Introduce more power loss in rheostat

    ii. Speed regulation is poor (S.R difference nLoaded& nno loaded)

    iii. Low efficiency due to rheostat

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    Speed Control for shunt motor and

    separately excited dc motor

    ii. Field Speed Control

    - Rheostat in series with field winding (shunt or separately ect.)

    - If field current, If is varied, hence flux is also varied

    - Not suitable for series field

    - Refer to -n characteristic,

    - Slope and nNLwill be changed

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    Speed Control for shunt motor and

    separately excited dc motor

    Torquespeed characteristic

    If1 < If2< If3

    1< 2< 3

    nNL3 nn1

    m

    n2 n3 nNL2

    nNL1Base speed

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    Speed Control for shunt motor and

    separately excited dc motor

    Advantages field speed control:

    i. Allows for controlling at or above the base speed

    ii. The cost of the rheostat is cheaper because Ifis small value

    Disadvantages field speed control :

    i. Speed regulation is poor (S.R difference nLoaded& nno loaded)

    ii. At high speed, flux is small, thus causes the speed of themachines becomes unstable

    iii. At high speed also, the machines is unstable mechanically,

    thus there is an upper speed limit

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    Speed Control for shunt motor and

    separately excited dc motor

    iii. Armature terminal voltage speed control

    - Use power electronics controller

    - AC supplyrectifier

    - DC supplychopper

    - Supply voltage to the armature is controlled

    - Constant speed regulation

    - From -n characteristic,- C and nNLwill be change

    - Slope constant

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    Speed Control for shunt motor and

    separately excited dc motor

    Torquespeed characteristic

    nNL1nn1

    m

    V3< V2< V1

    n2n3 nNL2

    nNL3

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    Speed Control for shunt motor and

    separately excited dc motor

    Advantages armature terminal voltage speed control:

    i. Does not change the speed regulation

    ii. Speed is easily controlled from zero to maximum safe speed

    Disadvantages armature terminal voltage speed

    control :

    i. Cost is higher because of using power electronic controller

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    FACTORS AFFECTING THE

    PERFORMANCE OF DC MACHINE

    There are two factors affecting the

    performance of dc machine

    1. Armature reaction

    2. Armature inductance

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    Armature Reaction

    Definition of armature reaction:1. It is the term used to describe the effects of the armature

    mmf on the operation of a dc machineas a "generator" nomatter whether it is a generator or motor.

    2. It effects both the flux distribution and the flux magnitude inthe machine.

    3. The distortion of the flux in a machineis called armaturereaction

    Two effects of armature reaction:1. Neutral Plane Shift

    2. Flux Weakening

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    Armature Reaction

    Effect on flux distribution:Neutral plane shift

    When currentis flowing inthe field winding, hence aflux is producedacross themachine which flows from

    the North pole to the Southpole.

    Initially the pole fluxisuniformly distributed andthe magnetic neutral planeis vertical

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    Armature Reaction

    Effect on flux distribution:

    Neutral plane shift

    effect by the air gapon the

    flux fieldcauses the

    distribution of flux is no longer

    uniform across the rotor.

    There are two points on the

    periphery of the rotor where

    B= 0.

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    Armature Reaction

    Effect on flux distribution:Neutralplane shift

    when a load connected to themachines a resulting magneticfield produced in the armature

    If the armatureis rotated at aspeed by an external torqueeach armature coil experiences

    a change in flux t as itrotates.

    A voltage is generatedacrossthe terminals of each windingaccording to the equation e =t

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    Armature Reaction

    Effect on flux distribution:Neutral plane shift

    Both rotor and pole fluxes (fluxproduced by the field windingand the flux produced by thearmature winding) are addedand subtracted togetheraccordingly

    The fields interact to produce adifferent flux distribution in therotor.

    Thus, the flux on the middleline, between the two field

    poles, is no longer zero.

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    Armature Reaction

    Effect on flux distribution:Neutral planeshift

    The combined flux in the machinehasthe effect of strengthening or weakeningthe flux in the pole.Neutral axis istherefore shifted in the direction ofmotion.

    The result is current flow circulatingbetween the shorted segments and largesparks at the brushes. The ending resultis arcing and sparking at the brushes.

    Solution to this problem:

    placing an additional poles on theneutral axis or mid-point that willproduce flux density component,which counter-acts that produced bythe armature.

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    Armature Reaction

    Effect on flux magnitude:FluxWeakening

    Most machine operate at saturationpoint

    When the armature reaction happen,at location pole surface:

    The add of rotor mmf to pole mmfonly make a small increase in flux

    The subtract of rotor mmf frompole mmf make a large decreasein flux.

    The result is the total average fluxunder entire pole face isdecreased.

    This is called Flux Weakening

    dflux decrease under subtracting section of poles

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    Armature Inductance

    When rotor turns, thus we have inductance value, e1= L(di/dt). Let say current ia1.

    That means, we have ability to store energy If the machine is turn off, thus, e1will decreased.

    This will affect the current as well. Say ia2. When the machine is turn on again, it will produce

    e2while e1is still inside. The current now is reverseddirection from previous (decreasing) current.

    Thus, it will cause sparking resulting the sameaching problem caused by neutral plane shift.