ELECTRICAL MACHINES I - Fmcetfmcet.in/EEE/EE6401_uw.pdfi.e. LW V winding has no ohmic resistance, no...

ELECTRICAL MACHINES – I

Unit -I

INTRODUCTION

Hans Christian Oersted (1777 – 1851)

1822

In 1820 he showed that a current

produces a magnetic field.

X

André-Marie Ampère (1775 – 1836)

French mathematics professor who only

a week after learning of Oersted’s discoveries in Sept. 1820 demonstrated

that parallel wires carrying currents

attract and repel each other.

attract

repel

A moving charge of 1 coulomb

per second is a current of

1 ampere (amp).

Michael Faraday (1791 – 1867) Self-taught English chemist and physicist

discovered electromagnetic induction in

1831 by which a changing magnetic field

induces an electric field.

Faraday’s electromagnetic

induction ring

A capacitance of 1 coulomb per volt

is called a farad (F)

Joseph Henry (1797 – 1878) American scientist, Princeton University

professor, and first Secretary of the

Smithsonian Institution.

Discovered self-

induction

Built the largest

electromagnets of

his day

Unit of inductance, L, is the “Henry”

Magnetic Fields and Circuits

A current i through a coil produces a

magnetic flux, f, in webers, Wb.

BAf A

df B A

H = magnetic field intensity in A/m.

v

i

+

-

N

B = magnetic flux density in Wb/m2.

B H

= magnetic permeability

Ampere's Law: d i H l

Hl Ni

NiFMagnetomotive force fF R

reluctance

Magnetic Flux

Magnetic flux, f, in webers, Wb.

1v 2v

2i1i

+ +

- -

2N1N

11 flux in coil 1 produced by current in coil 1f




1 11 12 total flux in coil 1f f f

2 21 22 total flux in coil 2f f f

Current entering

"dots" produce

fluxes that add.

Faraday's Law

1v 2v

2i1i

+ +

- -

2N1N

1 1 1N f

Faraday's Law: induced voltage in coil 1 is

Sign of induced voltage v1 is such that the current i through

an external resistor would be opposite to the current i1 that

produces the flux f1.

Total flux linking coil 1:

1 11 1( )

d dv t N

dt dt

f

i

Example of Lenz's law Symbol L of inductance from Lenz

Mutual Inductance

1v 2v

2i1i

+ +

- -

2N1N

1 11 121 1 1 1( )

d d dv t N N N

dt dt dt

f f f

Faraday's Law

1 21 11 12( )

di div t L L

dt dt

In linear range, flux is proportional to current

self-inductance mutual inductance

Mutual Inductance

1v 2v

2i1i

+ +

- -

2N1N

1 21 11 12( )

di div t L L

dt dt

1 22 21 22( )

di div t L L

dt dt

12 21L L M Linear media

1 21 1( )

di div t L M

dt dt

1 22 2( )

di div t M L

dt dt

2 22L L1 11L LLet

Core losses

Hysteresis losses

Hysteresis losses

Eddy current losses

Eddy current losses

How do we reduce Eddy current losses

SOLID

LAMINATED

http://en.wikipedia.org/wiki/File:Hawkins_Electrical_Guide_-_Figure_292_-_Eddy_currents_in_a_solid_armature.jpg

http://en.wikipedia.org/wiki/File:Hawkins_Electrical_Guide_-_Figure_293_-_Armature_core_with_a_few_laminations_showing_effect_on_eddy_currents.jpg

Eddy current losses

Eddy current losses in windings

Can be a problem with thick wires

- Low voltage machines

- High speed machines

Force, torque and power

Universal modeling of terminal characteristic of electro-magnetic devices based on energy balance

Induced EMF

Induced emf could be classified into

two types

Dynamically induced EMF.

Statically induced EMF.

Statically induced emf

In statically induced emf, conductor is stationary with respect to the magnetic field.

Transformer is an example of statically induced emf. Here the windings are stationary,magnetic field is moving around

the conductor and produces the emf.

Statically induced emf

• The emf produced in a conductor due to the change in magnetic field is called statically induce emf .It could be classified

into two

• 1)self induced emf and 2)mutual induced emf

Dynamically induced emf

This is the EMF induced due to the motion of conductor in a magnetic field.

Mathematically

e = Blv volts

• e-induced emf

• B – flux density of magnetic field in Tesla

• l = length of conductor in meters

• v- velocity of conductor in m/s

Dynamically induced emf

If the conductor moves in an angle θ,the induced emf could be represented as

e= Blvsinθ

the direction of induced emf is given by

flemmings right hand rule.

Generator is an example of dynamically induced

emf.

UNIT - II

TRANSFORMERS

Introduction • A transformer is a static machines.

• The word ‘transformer’ comes form the word ‘transform’. • Transformer is not an energy conversion device, but is a device that

changes AC electrical power at one voltage level into AC electrical

power at another voltage level through the action of magnetic field,

without a change in frequency.

• It can be either to step-up or step down.

Generation Station

TX1 TX1

Distribution

s TX1

TX1

Transmission

System

33/13.5k

V

13.5/6.6kV

6.6kV/415

V Consumer

Transformer Construction

• Two types of iron-core construction: a) Core - type construction

b) Shell - type construction

• Core - type construction

Transformer Construction

• Shell - type construction

Ideal Transformer • An ideal transformer is a transformer which has no loses,

i.e. it’s winding has no ohmic resistance, no magnetic leakage, and therefore no I2 R and core loses.

• However, it is impossible to realize such a transformer in

practice.

• Yet, the approximate characteristic of ideal transformer will be used in characterized the practical transformer.

V1 V2

N1 : N2

E1 E2

I1 I2 V1 – Primary Voltage V2 – Secondary Voltage

E1 – Primary induced Voltage

E2 – secondary induced Voltage

N1:N2 – Transformer ratio

MZS

FKEE, UMP

Transformer Equation

• Faraday’s Law states that, – If the flux passes through a coil of wire, a voltage will be

induced in the turns of wire. This voltage is directly

proportional to the rate of change in the flux with respect

of time.

If we have N turns of wire,

dt

tdEmfV indind

)(

dt

tdNEmfV indind

)(

Lenz’s Law

MZS

FKEE, UMP


• For an ac sources,

– Let V(t) = Vm sint

i(t) = im sint

Since the flux is a sinusoidal function;

Then:

Therefore:

Thus:

tt m sin)(

tN

dt

tdNEmfV

m

mindind

cos

sin

mmindind fNNEmfV 2(max)

mmm

rmsind fNfNN

Emf

44.42

2

2)(

MZS

FKEE, UMP


• For an ideal transformer

• In the equilibrium condition, both the input power will be equaled to the

output power, and this condition is said to ideal condition of a transformer.

• From the ideal transformer circuit, note that,

•

m

m

fNE

fNE

22

11

44.4

44.4

1

2

2

1

2211 coscos

I

I

V

V

IVIV

poweroutputpowerInput

………………… (i)

2211 VEandVE

MZS

FKEE, UMP


aI

I

N

N

E

ETherefore

1

2

2

1

2

1,

Where, ‘a’ is the Voltage Transformation Ratio; which will

determine whether the transformer is going to be step-up

or step-down

E1 > E2 For a >1

For a <1 E1 < E2

MZS

FKEE, UMP

Transformer Rating

• Transformer rating is normally written in terms of

Apparent Power.

• Apparent power is actually the product of its rated

current and rated voltage. 2211 IVIVVA

Where,

I1 and I2 = rated current on primary and secondary winding.

V1 and V2 = rated voltage on primary and secondary winding.

Rated currents are actually the full load currents in

transformer

MZS

FKEE, UMP

Example

1. 1.5kVA single phase transformer has rated voltage of 144/240 V. Finds its full load current. Solution

AI

AI

FL

FL

6240

1500

45.10144

1500

2

1

Practical Transformer (Equivalent

Circuit)

V1 = primary supply voltage

V2 = 2nd terminal (load) voltage

E1 = primary winding voltage

E2 = 2nd winding voltage

I1 = primary supply current

I2 = 2nd winding current

I1’ = primary winding current

Io = no load current

V1 = primary supply voltage

V2 = 2nd terminal (load) voltage

E1 = primary winding voltage

E2 = 2nd winding voltage

I1 = primary supply current

I2 = 2nd winding current

I1’ = primary winding current

Io = no load current

V1

I1 R1 X1

RC

Ic

Xm

Im

Io

E1 E2 V2

I1’

N1: N2

R2 X2

Load

I2

Single Phase Transformer (Referred to

Primary) Actual Method

2

2

22

2

2

12 '' XaXORX

N

NX

2

2

22

2

2

12 '' RaRORR

N

NR

V1

I1 R1 X1

RC

Ic

Xm

Im

Io

E1 E2 V2

I2’ N1: N2

R2’

X2’

Load

I2

a

II

aVVORVN

NVE

22

222

2

1'

21

'

'

Single Phase Transformer (Referred to

Primary ) Approximate Method

2

2

22

2

2

12 '' RaRORR

N

NR

2

2

22

2

2

12 '' XaXORX

N

NX

V1

I1 R1 X1

RC

Ic

Xm

Im

Io

E1 E2 V2

I2’ N1: N2 R2

’ X2’

Load

I2

a

II

aVVORVN

NVE

22

222

2

1'

21

'

'

Example Problem

1. A 10 kVA single phase transformer 2000/440V has

primary resistance and reactance of 5.5 and 12

respectively, while the resistance and reactance of

secondary winding is 0.2 and 0.45 respectively.

Calculate:

i. The parameter referred to high voltage side and

draw the equivalent circuit

ii. The approximate value of secondary voltage at full

load of 0.8 lagging power factor, when primary

supply is 2000V

Example 1 (Cont)

Solution

R1=5.5 , X1=j12

R2=0.2 , X2=j0.45

i) Refer to H.V side (primary)

R2’=(4.55)2 (0.2) = 4.14,

X2’=j(4.55)20.45 = j9.32

Therefore,

R01=R1+R2’=5.5 + 4.13 = 9.64

X01=X1+X2’=j12 + j9. 32 = j21.32

V1 aV2

R01 X01

21.32 9.64

I1

Example 1 (Cont)

AV

VAIFL 5

2000

1010 3

1

Solution

ii) Secondary voltage

p.f = 0.8

Cos = 0.8

=36.87o

Full load,

From eqn

o

oo

oo

V

Vj

aVIjXRV

8.06.422

)55.4()87.365)(32.2164.9(02000

))((0

2

2

2101011

Transformer Losses

• Generally, there are two types of losses;

i. Iron losses :- occur in core parameters

ii. Copper losses :- occur in winding resistance

i. Iron Losses

ii Copper Losses

circuitopenccciron PRIPP 2)(

02

2

201

2

1

2

2

21

2

1

)()(,

)()(

RIRIPreferredifor

PRIRIPP

cu

circuitshortcucopper

Transformer Efficiency

• To check the performance of the device, by

comparing the output with respect to the input.

• The higher the efficiency, the better the system.

%100cos

cos

%100

%100,

22

22

cuc

lossesout

out

PPIV

IV

PP

P

PowerInput

PowerOutputEfficiency

%100cos

cos

%100cos

cos

2)(

)(

cuc

nload

cuc

loadfull

PnPnVA

nVA

PPVA

VA

Where, if ½ load, hence n = ½ ,

¼ load, n= ¼ ,

90% of full load, n =0.9 Where Pcu = Psc

Pc = Poc

Voltage Regulation

• The purpose of voltage regulation is basically to determine the percentage of voltage drop between no load and full load.

• Voltage Regulation can be determine based on 3 methods:

a) Basic Defination

b) Short – circuit Test

c) Equivalent Circuit

Voltage Regulation

(Basic Definition) • In this method, all parameter are being referred

to primary or secondary side.

• Can be represented in either

Down – voltage Regulation

%100.

NL

FLNL

V

VVRV

Up – Voltage Regulation

%100.

FL

FLNL

V

VVRV

Tap Changer

A transformer tap is a connection point along a transformer winding that allows a certain number of turns to be selected.

By this means, a transformer with a variable turns ratio is produced, enabling voltage regulation of the output. The tap selection is made via a tap changer mechanism.

http://en.wikipedia.org/wiki/Transformer

http://en.wikipedia.org/wiki/Voltage

Three Phase Transformers

3 single phase transformers connected together

1.Star/Delta winding arrangements

2. Easy to replace failed units

Common core device

1. Lighter and cheaper than 3 individual units

2. 6 rather than 12 external connections

3. Whole transformer must be replaced if single

winding fails .

For both cases analysis procedure identical!

UNIT-III

Electromechanical Energy

Conversion

Electromechanical Energy Conversion • The electromechanical energy conversion theory allows the representation of the electromagnetic force or torque

in terms of device variables, such as the currents and the displacement of the mechanical systems.

• An electromechanical system consists of an electric system, a mechanical system, and a means whereby the electric and mechanical systems can interact.

2

Electromechanical Energy Conversion

• Consider the block diagram depicted below.

3

Electric

System

Coupling

Field Mechanic

System

WE = We + WeL + WeS

Energy

supplied by

an electric

source

Energy transferred to

the coupling field by the

electric system

Energy losses of the

electric system.

Basically, I2R

Energy stored in the

electric o magnetic field


• The energy transferred to the coupling field can be represented by

4

WM = Wm + WmL + WmS Energy

supplied by a

mechanical

source


the coupling field from

the mechanical system

Energy losses of the

mechanical system


moving member and

compliance of the

mechanical system

WF = We + Wm

Total energy

transferred to

the coupling field


the coupling field by

the electric system

Energy transferred to the

coupling field from the

mechanical system

WF = Wf + WfL


electric system Energy dissipated as heat

(I2R)


• The electromechanical systems obey the law of conservation of energy.

• Energy Balance in an Electromechanical System

5

WF = Wf + WfL = We + Wm

WE WeL

WeS

WfL WmL

Wf WmS

WM


• If the losses are neglected, we will obtain the following formula,

6

WF = We + Wm


the coupling field by

the electric system


the coupling field from

the mechanical system


• Consider the electromechanical system given below,

7

x

x0

N +

- ef

i L r

V

+

-

k

f

fe

D

m

f

Electromechanical Energy Conversion • The equation for the electric system is-

• The equation for the mechanical system is-

8

fedt

diLriV

fexxKdt

dxD

dt

dxmf )( 02

2

Electromechanical Energy Conversion • The total energy supplied by the electric source is -

• The equation for the mechanical system is-

9

dtdt

dxfdxfWM

dtie

dt

diLridtiVW fE


• Substituting f from the equation of motion-

10

dxfexxK

dt

dxD

dt

dxmdxfW

system mechanical

the from field couplingthe to dtransferre

energy Total

springthe in storedEnergy Potential

(Wall)friction the due

loss Heat

mass the in storedenergy Kinetic

E

)( 02

2


11

dxfidtedW

dxfidteW

WWeW

Recall

dxfW

eff

eff

Mf

eM

*


• If dx=0 is assumed, then

12

0

dxf

fEf

idW

dtidt

didteWW


• Recalling the normalized magnetization curve,

13

),( xi d

idW f

diWc

i


14

0

),(

),(),(

),(

dx

f diii

xiW

dxx

xidi

i

xid

xi


15

0

),(

),(),(

),(

dx

c dxi

diW

dxx

xid

xidi

xii


• From the previous relationship, it can be shown that for one coil,

16

01

*

0

*

0

)(

)(

dxj

jjf

i

f

i

f

diW

case, general a For

idxLiW

i xL diW

Electromechanical Energy Conversion • For two coupled coils,

• For the general case with n-coupled coils,

17

22

22211212

112

1

2

1iLiiLiLW f

n

p

n

qqppqf iiLW

1 12

1

Electromagnetic Force

• Recalling,

18

x

x0

N +

- ef

i L r

V

+

-

k

f

fe

D

m

f


19

dt

de

dWdWdxf

dxfidteW

WWeW

f

fee

eff

Mf


20

fe

fe

dWdidxf

didtidt

didtedW

dxx

xidi

i

xid

),(),(

dxx

xiWdi

i

xiWdW

ff

f

),(),(

Substituting for d and dWf in fedx=id dWf, it can be shown

fe dWx

ixif

,


• Recall,

21

d

idW f

diWc

i

x

W

xixif

x

W

xi

x

W

WiW

f

e

fc

fc

),(


22

x

Wxif

x

W

xi

xixif

x

W

xixif

WiWWWi

ce

ce

f

e

cfcf

),(

),(

),(

UNIT-IV

DC MACHINES

Introduction

• The direct current (dc) machine can be used as a motor or as a generator.

• DC Machine is most often used for a motor.

• The major advantages of dc machines are the easy speed and torque regulation.

• However, their application is limited to mills, mines and trains. As examples, trolleys and underground subway cars may use dc motors.

• In the past, automobiles were equipped with dc dynamos to charge their batteries.

Construction

Construction (cont.,)

• The stator of the dc motor has poles, which are excited by dc current to produce magnetic fields.

• In the neutral zone, in the middle between the poles, commutating poles are placed to reduce sparking of the commutator. The commutating poles are supplied by dc current.

• Compensating windings are mounted on the main poles. These short-circuited windings damp rotor oscillations. .

Construction (cont.,)

• The poles are mounted on an iron core that provides a closed magnetic circuit.

• The motor housing supports the iron core, the brushes and the bearings.

• The rotor has a ring-shaped laminated iron core with slots.

• Coils with several turns are placed in the slots. The distance between the two legs of the coil is about 180 electric degrees.

Construction (cont.,) • The coils are connected in

series through the commutator segments.

• The ends of each coil are connected to a commutator segment.

• The commutator consists of insulated copper segments mounted on an insulated tube.

• Two brushes are pressed to the commutator to permit current flow.

• The brushes are placed in the neutral zone, where the magnetic field is close to zero, to reduce arcing.

DC Machines

• The rotor has a ring-shaped laminated iron core with slots.

• The commutator consists of insulated copper segments mounted on an insulated tube.

• Two brushes are pressed to the commutator to permit current flow.

• The brushes are placed in the neutral zone, where the magnetic field is close to zero, to reduce arcing.

DC Machines

• The commutator switches the current from one rotor coil to the adjacent coil,

• The switching requires the interruption of the coil current.

• The sudden interruption of an inductive current generates high voltages .

• The high voltage produces flashover and arcing between the commutator segment and the brush.

DC Machine Construction

|

Shaft

Brush

Copper

segment

Insulation

Rotor

Winding

N S

Ir_dc

Ir_dc

/2

Rotation

Ir_dc

/2

Ir_dc

12

3

4

5

6

7

8

Pole

winding


Figure A. Details of the commutator of a dc motor.


Figure B. DC motor stator with poles visible.


Figure D. Cutaway view of a dc motor.

DC Generator

Operation

DC Generator Operation

• The N-S poles produce a dc magnetic field and the rotor coil turns in this field.

• A turbine or other machine drives the rotor.

• The conductors in the slots cut the magnetic flux lines, which induce voltage in the rotor coils.

• The coil has two sides: one is placed in slot a, the other in slot b.

30NS

Vdc

Bv

v

a

b

1

2

Ir_dc

(a) Rotor current flow from segment 1 to 2 (slot a to b)

30NS

Vdc

a

b

1

2

vv

B

Ir_dc

(b) Rotor current flow from segment 2 to 1 (slot b to a)


• The conductors in slot a are cutting the field lines entering into the rotor from the north pole,

• The conductors in slot b are cutting the field lines exiting from the rotor to the south pole.

• The cutting of the field lines generates voltage in the conductors.

• The voltages generated in the two sides of the coil are added.

30NS

Vdc

Bv

v

a

b

1

2

Ir_dc


30NS

Vdc

a

b

1

2

vv

B

Ir_dc



• The induced voltage is connected to the generator terminals through the commutator and brushes.

• The induced voltage in b is positive, and in a is negative.

• The positive terminal is connected to commutator segment 2 and to the conductors in slot b.

• The negative terminal is connected to segment 1 and to the conductors in slot a.

30NS

Vdc

Bv

v

a

b

1

2

Ir_dc


30NS

Vdc

a

b

1

2

vv

B

Ir_dc



• When the coil passes the neutral zone:

– Conductors in slot a are then moving toward the south pole and cut flux lines exiting from the rotor

– Conductors in slot b cut the flux lines entering the in slot b.

• This changes the polarity of the induced voltage in the coil.

• The voltage induced in a is now positive, and in b is negative.

30NS

Vdc

Bv

v

a

b

1

2

Ir_dc


30NS

Vdc

a

b

1

2

vv

B

Ir_dc



• The simultaneously the commutator reverses its terminals, which assures that the output voltage (Vdc) polarity is unchanged.

– the positive terminal is connected to ommutator segment 1 and to the conductors in slot a.

– The negative terminal is connected to segment 2 and to the conductors in slot b.

30NS

Vdc

Bv

v

a

b

1

2

Ir_dc


30NS

Vdc

a

b

1

2

vv

B

Ir_dc


UNIT-V

DC Motor

DC Motor Operation

• In a dc motor, the stator poles are supplied by dc excitation current, which produces a dc magnetic field.

• The rotor is supplied by dc current through the brushes, commutator and coils.

• The interaction of the magnetic field and rotor current generates a force that drives the motor

|

Shaft

Brush

Copper

segment

Insulation

Rotor

Winding

N S

Ir_dc

Ir_dc

/2

Rotation

Ir_dc

/2

Ir_dc

12

3

4

5

6

7

8

Pole

winding

DC Motor Operation

• The magnetic field lines enter into the rotor from the north pole (N) and exit toward the south pole (S).

• The poles generate a magnetic field that is perpendicular to the current carrying conductors.

• The interaction between the field and the current produces a Lorentz force,

• The force is perpendicular to both the magnetic field and conductor


Vdc

30NS

Bv

v

a

b

1

2

Ir_dc


30NS V

dc

a

b

1

2

B

v v

Ir_dc

DC Motor Operation

• The generated force turns the rotor until the coil reaches the neutral point between the poles.

• At this point, the magnetic field becomes practically zero together with the force.

• However, inertia drives the motor beyond the neutral zone where the direction of the magnetic field reverses.

• To avoid the reversal of the force direction, the commutator changes the current direction, which maintains the counterclockwise rotation. .


Vdc

30NS

Bv

v

a

b

1

2

Ir_dc


30NS V

dc

a

b

1

2

B

v v

Ir_dc

8.2.1 DC Motor Operation

• Before reaching the neutral zone, the current enters in segment 1 and exits from segment 2,

• Therefore, current enters the coil end at slot a and exits from slot b during this stage.

• After passing the neutral zone, the current enters segment 2 and exits from segment 1,

• This reverses the current direction through the rotor coil, when the coil passes the neutral zone.

• The result of this current reversal is the maintenance of the rotation.


Vdc

30NS

Bv

v

a

b

1

2

Ir_dc


30NS V

dc

a

b

1

2

B

v v

Ir_dc

EMF equation

Let

• Ø= flux/pole in Wb Z = total number of armature conductors P = number of poles A = number of parallel paths = 2 … for wave winding = P … for lap winding N = speed of armature in r.p.m. Eg= e.m.f. of the generator = e.m.f./parallel path

EMF equation

Armature Resistance (Ra)

• The resistance offered by the armature

circuit is known as armature resistance (Ra) and includes: (i) resistance of armature winding (ii) resistance of brushes The armature resistance depends upon the construction of machine. Except for small machines, its value is generally less than 1Ω.

Back EMF

• When the armature of a d.c. motor rotates under the influence of the driving torque, the armature conductors move through the magnetic field and hence e.m.f. is induced in them as in a generator The induced e.m.f. acts in opposite direction to the applied voltage V(Lenz’s law) and in known as back or counter e.m.f. Eb. The back e.m.f. Eb (= P Φ ZN/60 A) is always less than the applied voltage V, although this difference is small when the motor is running under normal conditions.

• Consider a shunt wound motor shown in Fig. (4.2). When d.c. voltage V is applied across the motor terminals, the field magnets are excited and armature conductors are supplied with current. Therefore, driving torque acts on the armature which begins to rotate. As the armature rotates, back e.m.f. Eb is induced which opposes the applied voltage V. The applied voltage V has to force current through the armature against the back e.m.f. Eb . The electric work done in overcoming and causing the current to flow against Eb is converted into mechanical energy developed in the armature. It follows, therefore, that energy conversion in a d.c. motor is only possible due to the production of back e.m.f. Eb.

Back EMF

• Net voltage across armature circuit = V – Eb

• If Ra is the armature circuit resistance, then, Ia = (V – Eb)/ Ra

• Since V and Ra are usually fixed, the value of Eb will determine the current drawn by the motor. If the speed of the motor is high, then back e.m.f. Eb (= P Φ ZN/60 A) is large and hence the motor will draw less armature current and viceversa.

Significance of Back E.M.F.

• The presence of back e.m.f. makes the d.c. motor a self-regulating machine i.e., it makes the motor to draw as much armature current as is just sufficient to develop the torque required by the load.

• Armature current,Ia = (V – Eb)/ Ra

• (i) When the motor is running on no load, small torque is required to overcome the friction and windage losses. Therefore, the armature current Ia is small and the back e.m.f. is nearly equal to the applied voltage. (ii) If the motor is suddenly loaded, the first effect is to cause the armature to slow down. Therefore, the speed at which the armature conductors move through the field is reduced and hence the back e.m.f. Eb falls. The decreased back e.m.f. allows a larger current to flow through the armature and larger current means increased driving torque. Thus, the driving torque increases as the motor slows down. The motor will stop slowing down when the armature current is just sufficient to produce the increased torque required by the load. (iii) If the load on the motor is decreased, the driving torque is momentarily in excess of the requirement so that armature is accelerated. As the armature speed increases, the back e.m.f. Eb also increases and causes the armature current Ia to decrease. The motor will stop accelerating when the armature current is just sufficient to produce the reduced torque required by the load.

• It follows, therefore, that back e.m.f. in a d.c. motor regulates the flow of armature current i.e., it automatically changes the armature current to meet the load requirement

Armature Reaction

• In a d.c. generator, the purpose of field winding is to produce magnetic field (called main flux) whereas the purpose of armature winding is to carry armature current. Although the armature winding is not provided for the purpose of producing a magnetic field, nevertheless the current in the armature winding will also produce magnetic flux (called armature flux). The armature flux distorts and weakens the main flux posing problems for the proper operation of the d.c. generator. The action of armature flux on the main flux is called armature reaction.

• It was hinted that current in the coil is reversed as the coil passes a brush. This phenomenon is termed as commutation. The criterion for good commutation is that it should be sparkless. In order to have sparkless commutation, the brushes should lie along magnetic neutral axis.

Armature Reaction

• So far we have assumed that the only flux acting in a d.c. machine is that due to the main poles called main flux. However, current flowing through armature conductors also creates a magnetic flux (called armature flux) that distorts and weakens the flux coming from the poles. This distortion and field weakening takes place in both generators and motors. The action of armature flux on the main flux is known as armature reaction. The phenomenon of armature reaction in a d.c. generator is shown in Fig. (2.1). Only one pole is shown for clarity. When the generator is on no-load, a smal1 current flowing in the armature does not appreciably affect the main flux Φ1 coming from the pole [See Fig 2.1 (i)]. When the generator is loaded, the current flowing through armature conductors sets up flux Φ1. Fig. (2.1) (ii) shows flux due to armature current alone. By superimposing Φ1 and Φ2, we obtain the resulting flux Φ3 as shown in Fig. (2.1) (iii). Referring to Fig (2.1) (iii), it is clear that flux density at; the trailing pole tip (point B) is increased while at the leading pole tip (point A) it is decreased. This unequal field distribution produces the following two effects: (i) The main flux is distorted. (ii) Due to higher flux density at pole tip B, saturation sets in. Consequently, the increase in flux at pole tip B is less than the decrease in flux under pole tip A. Flux Φ3 at full load is, therefore, less than flux Φ1 at no load. As we shall see, the weakening of flux due to armature reaction depends upon the position of brushes.

Armature Reaction

Geometrical and Magnetic

Neutral Axes • (i) The geometrical neutral axis (G.N.A.) is the axis that

bisects the angle between the centre line of adjacent poles [See Fig. 2.2 (i)]. Clearly, it is the axis of symmetry between two adjacent poles.

• (ii) The magnetic neutral axis (M. N. A.) is the axis drawn perpendicular to the mean direction of the flux passing through the centre of the armature. Clearly, no e.m.f. is produced in the armature conductors along this axis because then they cut no flux. With no current in the armature conductors, the M.N.A. coincides with G, N. A. as shown in Fig. [2.2(ii)]. In order to achieve sparkless commutation, the brushes must lie along M.N.A.


Neutral Axes • With no current in armature conductors, the M.N.A. coincides with G.N.A. However,

when current flows in armature conductors, the combined action of main flux and armature flux shifts the M.N.A. from G.N.A. In case of a generator, the M.N.A. is shifted in the direction of rotation of the machine. In order to achieve sparkless commutation, the brushes have to be moved along the new M.N.A. Under such a condition, the armature reaction produces the following two effects: 1. It demagnetizes or weakens the main flux. 2. It cross-magnetizes or distorts the main flux. Let us discuss these effects of armature reaction by considering a 2-pole generator (though the following remarks also hold good for a multipolar generator). (i) Fig. (2.3) (i) shows the flux due to main poles (main flux) when the armature conductors carry no current. The flux across the air gap is uniform. The m.m.f. producing the main flux is represented in magnitude and direction by the vector OFm in Fig. (2.3) (i). Note that OFm is perpendicular to G.N.A. (ii) Fig. (2.3) (ii) shows the flux due to current flowing in armature conductors alone (main poles unexcited). The armature conductors to the left of G.N.A. carry current “in” (x) and those to the right carry current “out” (•). The direction of magnetic lines of force can be found by cork screw rule. It is clear that armature flux is directed downward parallel to the brush axis. The m.m.f. producing the armature flux is represented in magnitude and direction by the vector OFA in Fig. (2.3) (ii).

http://electricalandelectronics.org/2008/09/13/field-poles/


Neutral Axes • (iii) Fig. (2.3) (iii) shows the flux due to the main poles and that due

to current in armature conductors acting together. The resultant m.m.f. OF is the vector sum of OFm and OFA as shown in Fig. (2.3) (iii). Since M.N.A. is always perpendicular to the resultant m.m.f., the M.N.A. is shifted through an angle θ. Note that M.N.A. is shifted in the direction of rotation of the generator. (iv) In order to achieve sparkless commutation, the brushes must lie along the M.N.A. Consequently, the brushes are shifted through an angle θ so as to lie along the new M.N.A. as shown in Fig. (2.3) (iv). Due to brush shift, the m.m.f. FA of the armature is also rotated through the same angle θ. It is because some of the conductors which were earlier under N-pole now come under S-pole and vice-versa. The result is that armature m.m.f. FA will no longer be vertically downward but will be rotated in the direction of rotation through an angle θ as shown in Fig. (2.3) (iv). Now FA can be resolved into rectangular components Fc and Fd.


Neutral Axes


Neutral Axes • (a) The component Fd is in direct opposition to the m.m.f. OFm due to main poles. It

has a demagnetizing effect on the flux due to main poles. For this reason, it is called the demagnetizing or weakening component of armature reaction.

• (b) The component Fc is at right angles to the m.m.f. OFm due to main poles. It distorts the main field. For this reason, it is called the crossmagnetizing or distorting component of armature reaction.

• It may be noted that with the increase of armature current, both demagnetizing and distorting effects will increase.

• Conclusions (i) With brushes located along G.N.A. (i.e., θ = 0°), there is no demagnetizing component of armature reaction (Fd = 0). There is only distorting or crossmagnetizing effect of armature reaction. (ii) With the brushes shifted from G.N.A., armature reaction will have both demagnetizing and distorting effects. Their relative magnitudes depend on the amount of shift. This shift is directly proportional to the armature current. (iii) The demagnetizing component of armature reaction weakens the main flux. On the other hand, the distorting component of armature reaction distorts the main flux. (iv) The demagnetizing effect leads to reduced generated voltage while crossmagnetizing effect leads to sparking at the brushes

http://electricalandelectronics.org/2009/05/08/armature-reaction/

Demagnetizing and cross

magnetizing conductors • With the brushes in the G.N.A. position, there is only cross-magnetizing effect of

armature reaction. However, when the brushes are shifted from the G.N.A. position, the armature reaction will have both demagnetizing and crossmagnetizing effects. Consider a 2-pole generator with brushes shifted (lead) θm mechanical degrees from G.N.A. We shall identify the armature conductors that produce demagnetizing effect and those that produce cross-magnetizing effect. (i) The armature conductors θ°m on either side of G.N.A. produce flux in direct opposition to main flux as shown in Fig. (2.4) (i). Thus the conductors lying within angles AOC = BOD = 2θm at the top and bottom of the armature produce demagnetizing effect. These are called demagnetizing armature conductors and constitute the demagnetizing ampere-turns of armature reaction (Remember two conductors constitute a turn).

• ii) The axis of magnetization of the remaining armature conductors lying between angles AOD and COB is at right angles to the main flux as shown in Fig. (2.4) (ii). These conductors produce the cross-magnetizing (or distorting) effect i.e., they produce uneven flux distribution on each pole. Therefore, they are called cross-magnetizing conductors and constitute the cross-magnetizing ampere-turns of armature reaction.

Demagnetizing and cross

magnetizing conductors

Calculation of Demagnetizing

Ampere-Turns Per Pole

(ATd/Pole) • It is sometimes desirable to neutralize the demagnetizing

ampere-turns of armature reaction. This is achieved by adding extra ampere-turns to the main field winding. We shall now calculate the demagnetizing ampere-turns per pole (ATd/pole). Let Z = total number of armature conductors I = current in each armature conductor = Ia/2 … for simplex wave winding = Ia/P … for simplex lap winding θm = forward lead in mechanical degrees Referring to Fig. (2.4) (i) above, we have, Total demagnetizing armature conductors= Conductors in angles AOC and BOD = 4θm/360 × Z

Calculation of Demagnetizing

Ampere-Turns Per Pole

(ATd/Pole)

• Since two conductors constitute one turn, Therefore Total demagnetizing ampere-turns =

Demagnetising ampere-turns Per Pole

(ATd/Pole)

Demagnetising ampere-turns Per Pole

(ATd/Pole) • Note. When a conductor passes a pair of poles, one cycle of voltage is

generated. We say one cycle contains 360 electrical degrees. Suppose there are P poles in a generator. In one revolution, there are 360 mechanical degrees and 360 ×P/2 electrical degrees.

Cross-Magnetizing Ampere-Turns Per

Pole (ATc/Pole)

• Demagnetizing ampere-turns per pole is given by


Pole (ATc/Pole)

since two conductors make one turn)

Demagnetizing ampere-turns per pole is given by


Pole (ATc/Pole)

• Therefore Cross-magnetizing ampere-turns/pole are

COMMUTATION

• Fig. (2.6) shows the schematic diagram of 2-pole lap-wound generator. There are two parallel paths between the brushes. Therefore, each coil of the winding carries one half (Ia/2 in this case) of the total current (Ia) entering or leaving the armature. Note that the currents in the coils connected to a brush are either all towards the brush (positive brush) or all directed away from the brush (negative brush). Therefore, current in a coil will reverse as the coil passes a brush. This reversal of current as the coil passes & brush is called commutation.

COMMUTATION

COMMUTATION

• The reversal of current in a coil as the coil passes the brush axis is called commutation. When commutation takes place, the coil undergoing commutation is shortcircuited by the brush. The brief period during which the coil remains shortcircuited is known as commutation period Tc. If the current reversal is completed by the end of commutation period, it is called ideal commutation. If the current reversal is not completed by that time, then sparking occurs between the brush and the commutator which results in progressive damage to both.

http://electricalandelectronics.org/2008/09/15/commutator/

Ideal commutation

• Let us discuss the phenomenon of ideal commutation (i.e., coil has no inductance) in one coil in the armature winding shown in Fig. (2.6) above. For this purpose, we consider the coil A. The brush width is equal to the width of one commutator segment and one mica insulation. Suppose the total armature current is 40 A. Since there are two parallel paths, each coil carries a current of 20 A. (i) In Fig. (2.7) (i), the brush is in contact with segment 1 of the commutator. The commutator segment 1 conducts a current of 40 A to the brush; 20 A from coil A and 20 A from the adjacent coil as shown. The coil A has yet to undergo commutation.

Ideal commutation

Ideal commutation

• (ii) As the armature rotates, the brush will make contact with segment 2 and thus short-circuits the coil A as shown in Fig. (2.7) (ii). There are now two parallel paths into the brush as long as the short-circuit of coil A exists. Fig. (2.7) (ii) shows the instant when the brush is one-fourth on segment 2 and three-fourth on segment 1. For this condition, the resistance of the path through segment 2 is three times the resistance of the path through segment 1 (since contact resistance varies inversely as the area of contact of brush with the segment). The brush again conducts a current of 40 A; 30 A through segment 1 and 10 A through segment 2. Note that current in coil A (the coil undergoing commutation) is reduced from 20 A to 10 A.

Ideal commutation

• iii) Fig. (2.7) (iii) shows the instant when the brush is one-half on segment 2 and one-half on segment 1. The brush again conducts 40 A; 20 A through segment 1 and 20 A through segment 2 (since now the resistances of the two parallel paths are equal). Note that now. current in coil A is zero. (iv) Fig. (2.7) (iv) shows the instant when the brush is three-fourth on segment 2 and one-fourth on segment 1. The brush conducts a current of 40 A; 30 A through segment 2 and 10 A through segment 1. Note that current in coil A is 10 A but in the reverse direction to that before the start of commutation. The reader may see the action of the commutator in reversing the current in a coil as the coil passes the brush axis. (v) Fig. (2.7) (v) shows the instant when the brush is in contact only with segment 2. The brush again conducts 40 A; 20 A from coil A and 20 A from the adjacent coil to coil A. Note that now current in coil A is 20 A but in the reverse direction. Thus the coil A has undergone commutation. Each coil undergoes commutation in this way as it passes the brush axis. Note that during commutation, the coil under consideration remains shortcircuited by the brush.

Ideal commutation

• Fig. (2.8) shows the current-time graph for the coil A undergoing commutation. The horizontal line AB represents a constant current of 20 A upto the beginning of commutation. From the finish of commutation, it is represented by another horizontal line CD on the opposite side of the zero line and the same distance from it as AB i.e., the current has exactly reversed (- 20 A). The way in which current changes from B to C depends upon the conditions under which the coil undergoes commutation. If the current changes at a uniform rate (i.e., BC is a straight line), then it is called ideal commutation as shown in Fig. (2.8). Under such conditions, no sparking will take place between the brush and the commutator

Commutation Practical difficulties

• This is illustrated in Fig. (2.9). The straight line RC represents theThe ideal commutation (i.e., straight line change of current) cannot be attained in practice. This is mainly due to the fact that the armature coils have appreciable inductance. When the current in the coil undergoing commutation changes, self-induced e.m.f. is produced in the coil. This is generally called reactance voltage. This reactance voltage opposes the change of current in the coil undergoing commutation. The result is that the change of current in the coil undergoing commutation occurs more slowly than it would be under ideal commutation whereas the curve BE represents the change in current when self-inductance of the coil is taken into account. Note that current CE (= 8A in Fig. 2.9) is flowing from the commutator segment 1 to the brush at the instant when they part company. This results in sparking just as when any other current carrying circuit is broken. The sparking results in overheating of commutatorbrush contact and causing damage to both.

• Fig. (2.10) illustrates how sparking takes place between the commutator segment and the brush. At the end of commutation or short-circuit period, the current in coil A is reversed to a value of 12 A (instead of 20 A) due to inductance of the coil. When the brush breaks contact with segment 1, the remaining 8 A current jumps from segment 1 to the brush through air causing sparking between segment 1 and the brush.

Commutation Practical difficulties

Calculation of Reactance Voltage

• Reactance voltage = Coefficient of self-inductance × Rate of change of current When a coil undergoes commutation, two commutator segments remain shortcircuited by the brush. Therefore, the time of short circuit (or commutation period Tc) is equal to the time required by the commutator to move a distance equal to the circumferential thickness of the brush minus the thickness of one insultating strip of mica.

• Let Wb = brush width in cm,Wm = mica thickness in cm,v = peripheral speed of commutator in cm/s Commutation period, Tc = ( Wb – Wm )/v seconds The commutation period is very small, say of the order of 1/500 second.

• Let the current in the coil undergoing commutation change from + I to – I (amperes) during the commutation. If L is the inductance of the coil, then reactance voltage is given by;

• Reactance Voltage,(for linear commutation)

Methods of improving commutation

• mproving commutation means to make current reversal in the short-circuited coil as sparkless as possible. The following are the two principal methods of improving commutation: (i) Resistance commutation (ii) E.M.F. commutation We shall discuss each method in turn.

http://electricalandelectronics.org/2009/05/10/commutation/

Resistance Commutation

• Resistance Commutation The reversal of current in a coil (i.e., commutation) takes place while the coil is short-circuited by the brush. Therefore, there are two parallel paths for the current as long as the short circuit exists. If the contact resistance between the brush and the commutator is made large, then current would divide in the inverse ratio of contact resistances (as for any two resistances in parallel). This is the key point in improving commutation. This is achieved by using carbon brushes (instead of Cu brushes) which have high contact resistance. This method of improving commutation is called resistance commutation. Figs. (2.11) and (2.12) illustrates how high contact resistance of carbon brush improves commutation (i.e., reversal of current) in coil A. In Fig. (2.11) (i), the brush is entirely on segment 1 and, therefore, the current in coil A is 20 A. The coil A is yet to undergo commutation. As the armature rotates, the brush shortcircuits the coil A and there are two parallel paths for the current into the brush. Fig. (2.11) (ii) shows the instant when the brush is one-fourth on segment 2 and three-fourth on segment 1. The equivalent electric circuit is shown in Fig. (2.11) (iii) where R1 and R2 represent the brush contact resistances on segments 1 and 2.

http://electricalandelectronics.org/2008/09/15/armature/

Resistance Commutation

Resistance Commutation • A resistor is not shown for coil A since it is assumed that the coil resistance

is negligible as compared to the brush contact resistance. The values of current in the parallel paths of the equivalent circuit are determined by the respective resistances of the paths. For the condition shown in Fig. (2.11) (ii), resistor R2 has three times the resistance of resistor R1. Therefore, the current distribution in the paths will be as shown. Note that current in coil A is reduced from 20 A to 10 A due to division of current in (he inverse ratio of contact resistances. If the Cu brush is used (which has low contact resistance), R1 R2 and the current in coil A would not have reduced to 10 A. As the carbon brush passes over the commutator, the contact area with segment 2 increases and that with segment 1 decreases i.e., R2 decreases and R1 increases. Therefore, more and more current passes to the brush through segment 2. This is illustrated in Figs. (2.12) (i) and (2.12) (ii), When the break between the brush and the segment 1 finally occurs [See Fig. 2.12 (iii)], the current in the coil is reversed and commutation is achieved. It may be noted that the main cause of sparking during commutation is the production of reactance voltage and carbon brushes cannot prevent it. Nevertheless, the carbon brushes do help in improving commutation. The other minor advantages of carbon brushes are: (i) The carbon lubricates and polishes the commutator. (ii) If sparking occurs, it damages the commutator less than with copper brushes and the damage to the brush itself is of little importance.

EMF commutation • In this method, an arrangement is made to neutralize the reactance voltage by

producing a reversing voltage in the coil undergoing commutation. The reversing voltage acts in opposition to the reactance voltage and neutralizes it to some extent. If the reversing voltage is equal to the reactance voltage, the effect of the latter is completely wiped out and we get sparkless commutation. The reversing voltage may be produced in the following two ways: (i) By brush shifting (ii) By using interpoles or compoles (i) By brush shifting In this method, the brushes are given sufficient forward lead (for a generator) to bring the short-circuited coil (i.e., coil undergoing commutation) under the influence of the next pole of opposite polarity. Since the short-circuited coil is now in the reversing field, the reversing voltage produced cancels the reactance voltage. This method suffers from the following drawbacks:

• (a) The reactance voltage depends upon armature current. Therefore, the brush shift will depend on the magnitude of armature current which keeps on changing. This necessitates frequent shifting of brushes. (b) The greater the armature current, the greater must be the forward lead for a generator. This increases the demagnetizing effect of armature reaction and further weakens the main field. (ii) By using interpoles or compoles The best method of neutralizing reactance voltage is by, using interpoles or compoles.

Interpoles or Compoles

• The best way to produce reversing voltage to neutralize the reactance voltage is by using interpoles or compoles. These are small poles fixed to the yoke and spaced mid-way between the main poles (See Fig. 2.13). They are wound with comparatively few turns and connected in series with the armature so that they carry armature current. Their polarity is the same as the next main pole ahead in the direction of rotation for a generator (See Fig. 2.13). Connections for a d.c. generator with interpoles is shown in Fig. (2.14).

Interpoles or Compoles

Functions of Interpoles • The machines fitted with interpoles have their brushes set on geometrical

neutral axis (no lead). The interpoles perform the following two functions: (i) As their polarity is the same as the main pole ahead (for a generator), they induce an e.m.f. in the coil (undergoing commutation) which opposes reactance voltage. This leads to sparkless commutation. The e.m.f. induced by compoles is known as commutating or reversing e.m.f. Since the interpoles carry the armature current and the reactance voltage is also proportional to armature current, the neutralization of reactance voltage is automatic. (ii) The m.m.f. of the compoles neutralizes the cross-magnetizing effect of armature reaction in small region in the space between the main poles. It is because the two m.m.f.s oppose each other in this region.

• Fig. (2.15) shows the circuit diagram of a shunt generator with commutating winding and compensating winding. Both these windings are connected in series with the armature and so they carry the armature current. However, the functions they perform must be understood clearly. The main function of commutating winding is to produce reversing (or commutating) e.m.f. in order to cancel the reactance voltage. In addition to this, the m.m.f. of the commutating winding neutralizes the crossmagnetizing ampere-turns in the space between the main poles. The compensating winding neutralizes the cross-magnetizing effect of armature reaction under the pole faces.

Functions of Interpoles

DC Generator Equivalent circuit

• The magnetic field produced by the stator poles induces a voltage in the rotor (or armature) coils when the generator is rotated.

• This induced voltage is represented by a voltage source.

• The stator coil has resistance, which is connected in series.

• The pole flux is produced by the DC excitation/field current, which is magnetically coupled to the rotor

• The field circuit has resistance and a source

• The voltage drop on the brushes represented by a battery


• Equivalent circuit of a separately excited dc generator.

Rf

Ra

Vbrush

VdcE

agV

f

max

If

Iag

Load

Mechanical

power in

Electrical

power out


• The magnetic field produced by the stator poles induces a voltage in the rotor (or armature) coils when the generator is rotated.

• The dc field current of the poles generates a magnetic flux

• The flux is proportional with the field current if the iron core is not saturated:

fag IK1


• The rotor conductors cut the field lines that generate voltage in the coils.

• The motor speed and flux equations are :

vBNE grag 2

2

gDv ggag DB


• The combination of the three equation results the induced voltage equation:

• The equation is simplified.

agrggr

g

grgrag NDBND

BNvBNE

222

fmfragrag IKIKNNE 1


• When the generator is loaded, the load current produces a voltage drop on the rotor winding resistance.

• In addition, there is a more or less constant 1–3 V voltage drop on the brushes.

• These two voltage drops reduce the terminal voltage of the generator. The terminal voltage is;

brushaagdcag VRIVE

DC Motor Equivalent circuit

• Equivalent circuit of a separately excited dc motor

• Equivalent circuit is similar to the generator only the current directions are different

Rf

Ra

Vbrush

VdcE

amV

f

max

If

Iam

Mechanical

power out

Electrical

power in

DC Power

supply


• The operation equations are:

• Armature voltage equation

brushaamamdc VRIEV

The induced voltage and motor speed vs angular

frequency

fmam IKE mn 2


• The operation equations are:

• The combination of the equations results in

The current is calculated from this equation. The output

power and torque are:

mamdcamfm RIVEIK

amamout IEP famm

out IIKP

T

Excitation methods

• There are four different methods for supplying the dc current to the motor or generator poles:

– Separate excitation;

– Shunt connection

– Series connection

– Compound


• Equivalent circuit of a shunt dc motor

DC Power

supply

Vdc

Eam

Iam

max R

f

If

Ra

Vbrush

Im

Pout


• Equivalent circuit of a series dc motor

Vdc

Eam

Rf

Ra

Vbrush

Im

max

DC Power

supply

Pout


• Equivalent circuit of a compound dc motor

Vdc

Eam

Rfs

Ra

Vbrush

Im

max

DC Power

supply

Rfp

Iam

Ifp

Pout

Generator characteristics

• The following are the three most important characteristics of a d.c. generator: 1. Open Circuit Characteristic (O.C.C.) This curve shows the relation between the generated e.m.f. at no-load (E0) and the field current (If) at constant speed. It is also known as magnetic characteristic or no-load saturation curve. Its shape is practically the same for all generators whether separately or self-excited. The data for O.C.C. curve are obtained experimentally by operating the generator at no load and constant speed and recording the change in terminal voltage as the field current is varied. 2. Internal or Total characteristic (E/Ia) This curve shows the relation between the generated e.m.f. on load (E) and the armature current (Ia). The e.m.f. E is less than E0 due to the demagnetizing effect of armature reaction. Therefore, this curve will lie below the open circuit characteristic (O.C.C.). The internal characteristic is of interest chiefly to the designer. It cannot be obtained directly by experiment. It is because a voltmeter cannot read the e.m.f. generated on load due to the voltage drop in armature resistance. The internal characteristic can be obtained from external characteristic if winding resistances are known because armature reaction effect is included in both characteristics

• 3. External characteristic (V/IL) This curve shows the relation between the terminal voltage (V) and load current (IL). The terminal voltage V will be less than E due to voltage drop in the armature circuit. Therefore, this curve will lie below the internal characteristic. This characteristic is very important in determining the suitability of a generator for a given purpose. It can be obtained by making simultaneous measurements of terminal voltage and load current (with voltmeter and ammeter) of a loaded generator.

http://electricalandelectronics.org/2009/05/08/armature-reaction/

Parallel operation of dc

generators • In a d.c. power plant, power is usually supplied from several generators of small ratings connected

in parallel instead of from one large generator. This is due to the following reasons: (i) Continuity of service If a single large generator is used in the power plant, then in case of its breakdown, the whole plant will be shut down. However, if power is supplied from a number of small units operating in parallel, then in case of failure of one unit, the continuity of supply can be maintained by other healthy units. (ii) Efficiency Generators run most efficiently when loaded to their rated capacity. Electric power costs less per kWh when the generator producing it is efficiently loaded. Therefore, when load demand on power plant decreases, one or more generators can be shut down and the remaining units can be efficiently loaded. (iii) Maintenance and repair Generators generally require routine-maintenance and repair. Therefore, if generators are operated in parallel, the routine or emergency operations can be performed by isolating the affected generator while load is being supplied by other units. This leads to both safety and economy. (iv) Increasing plant capacity In the modern world of increasing population, the use of electricity is continuously increasing. When added capacity is required, the new unit can be simply paralleled with the old units. (v) Non-availability of single large unit In many situations, a single unit of desired large capacity may not be available. In that case a number of smaller units can be operated in parallel to meet the load requirement. Generally a single large unit is more expensive.

Speed Control for shunt motor and separately excited dc motor

• Torque –speed characteristic for shunt and separately excited dc motor

a

ff

a

ff

a

a

a

aa

aa

R

nIK

R

IVK

excitedseparatelyassame

n

E

R

EV

n

IE

IEtorqueDeveloped

22

,

2

2

,

22

a

ff

R

IVKc

2

Starting torque

a

ff

R

nIKslope

2

22

nNL n n

m

=0 n=0


• By referring to the Torque –speed characteristic for shunt and separately excited dc motor

• note that, there are three variables that can influence

the speed of the motor, V

If Ra

• Thus, there are three methods of controlling the speed of the shunt and separately excited dc motor,

i. Armature terminal – voltage speed control

ii. Field speed control

a

ff

a

ff

R

nIK

R

IVK

22

22

Variables


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


• Torque –speed characteristic

Ra1

nNL n n1

m

Ra2

Ra3

Ra1 < Ra2 < Ra3

n2 n3


• 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. 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 nNL will be changed



If1 < If2 < If3

1 < 2 < 3

nNL3 n n1

m

n2 n3 nNL2

nNL1 Base speed


• Advantages field speed control:

i. Allows for controlling at or above the base speed

ii. The cost of the rheostat is cheaper because If is 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 the machines becomes unstable

iii. At high speed also, the machines is unstable


iii. Armature terminal – voltage speed control

- Use power electronics controller

- AC supply rectifier

- DC supply chopper

- Supply voltage to the armature is controlled

- Constant speed regulation

- From -n characteristic, - C and nNL will be change

- Slope constant



nNL1 n n1

m

V3 < V2 < V1

n2 n3 nNL2 nNL3


• 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

ELECTRICAL MACHINES I - Fmcetfmcet.in/EEE/EE6401_uw.pdfi.e. LW V winding has no ohmic resistance, no...

Documents

Transcript of ELECTRICAL MACHINES I - Fmcetfmcet.in/EEE/EE6401_uw.pdfi.e. LW V winding has no ohmic resistance, no...