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DC Machines
Dr. Mohammed H. Haque
School of Engineering
[email protected]
EEET 3032 – Electrical Machines 1
Topics
• Ideal electrical machines
• Induced voltage and torque equations
• Commutation and armature reaction
• Construction and operating principle
• Classification
• Equivalent circuit, power flow diagram, losses and efficiency
• Characteristics of various dc machines
• Speed control of dc motors
• Motor and load torque matching
• Dynamics of dc machines
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Electric Machines
An electric machine converts electrical energy into mechanical energy or mechanical
energy into electrical energy
Generator: Converts mechanical energy into electrical energy
Motor: Converts electrical energy into mechanical energy
Electromechanical energy conversion
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In Electrical System:
Primary quantities are voltage (V or E) and current (I)
In Mechanical System:
Primary quantities are torque (T) and speed (m or n)
AC Machines: Electrical system is AC
DC Machines: Electrical system is DC
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Coupling Magnetic Field
The coupling medium between the electrical and mechanical systems is magnetic
field and is essential in all electromechanical energy conversion processes
Coupling
Magnetic
Field
Mechanical
System
Electrical
System
E and I T and m
Coupling magnetic field between electrical & mechanical systems
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For an ideal (or lossless) machine
Electrical energy = Mechanical energy
 Electrical power = Mechanical power
Electrical power: Pe = EI (W) in DC circuit
Mechanical power: Pm = Tm (W)
 For an ideal machine
Pe = Pm  EI = Tm
Machine speed is usually measured (or given) in revolution per minute (rpm). However, in power
calculation, machine angular velocity (in radian/sec) is used. The relationship between speed n (in rpm)
and angular velocity m (in rad/sec) is
nm 





=
60
2

That is m and n are linearly related and the proportionality constant is 2/60
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Electromagnetic Energy Conversion
Two basic electromagnetic phenomena are:
• A moving conductor in a magnetic field induces voltage. This is called
generator action.
• A current carrying conductor in a magnetic field produces force. This
is called motor action.
In all electric machines, both actions/effects are taken place simultaneously
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Induced Voltage
The induced voltage or emf (e) in a moving conductor in the presence of a magnetic
field is given by
e = BLv (V) when B, L and v are mutually perpendicular
B = magnetic flux density, T or Wb/m2
L =conductor length in magnetic field, m
v = relative velocity between field and conductor, m/s
The polarity or direction of induced voltage (e)
can be determined by the Right Hand Rule (RHR)
as shown in the figure
Electric machines are designed in such a way that
B, L and v are mutually perpendicular
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A Simple Generator
Consider a coil rotates in a magnetic field produced by two poles (N and S) as shown in
the figure. Coil ends are connected to two rotating slip rings. Stationary brushes are
placed on the rotating slip rings to extract the internal induced voltage. External load is
connected between the stationary brushes.
The resultant voltage appears
between the slip rings A and
B is alternating (but not DC).
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Generation of Unidirectional Voltage
• Commutators are used to convert the internal AC induced voltage into unidirectional
output voltage.
• Commutators can be considered as mechanical rectifier.
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Commutator
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• Coil sides and commutators change position simultaneously because they are on the
same structure
• Connection between brushes and commutators changes whenever the polarity of the
induced voltage is revered
• Thus, the polarity of output (or load) voltage remains unchanged. The output voltage
is unidirectional but pulsating as shown in the figure. It has high ripples.
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How to Reduce Ripples?
Ripples can be reduced by using a large number of armature coils connected in series
• First consider that only two coils A-B and C-D are placed at right angle and
connected in series
• The phase shift between EAB and ECD is 90
0 and the resultant voltage ER is EAB + ECD
as shown in the following figure
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Comparison of Output Voltage
(a) 1-coil;
(b) 2-coil;
(c) 8-coil
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Construction of DC Machines
Stator: Provides the physical support and magnetic poles
Rotor: The main winding (where the voltage is induced) is placed in the rotor. The rotor
of a DC machine is also called armature
Three essential elements in DC machines are
• Production of magnetic field or flux. Usually electromagnets are used
• Rotating coils/conductors where the voltage is induced
• Brush-commutator arrangement (to convert AC voltage to DC voltage)
Field coil on a pole piece A complete armature
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Field Windings and Representation
There are two sets of field windings
• Shunt field winding: Consists of a large number of turns with fine wire and
carries less current (usually a few % of rated current). It has high resistance
• Series field winding: Consists of less number of turns with heavy wire and carries
large current (usually the load current). It has low resistance
To produce magnetic field, it is not necessary to use both field windings simultaneously.
Representation of Field Windings
A field winding is represented by a coil as shown in schematic diagram. It consists of
resistance (R) and inductance (L). For steady state analysis, L is ignored and thus only R
is considered.
Schematic diagram Electrical equivalent circuit
R
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Representation of Armature
Armature consists of a large number of conductors where voltage is induced. For
steady state analysis, the armature inductance (L) is ignored and thus its equivalent
circuit consists of induced voltage E and the resistance Ra. Note that E is not
constant.
E
R
a
Brush
Schematic
diagram
Electrical
equivalent circuit
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Classification of DC Machines
The characteristic of a DC machine depends on the field winding(s) used (series or
shunt) to produce flux. Classification of DC machines is based on mutual connection
between the armature and field windings.
(a) Separately excited
The shunt field winding is connected to a separate
DC source Vf. The series field winding is not used. V
t
E
Shunt field
V
f
(b) Self-excited
The armature induced voltage/current is used to excite the field circuit(s). A separate
DC source is not required. Self-excited machines can further be classified into three
categories (i) Shunt, (ii) Series and (iii) Compound
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(i) Shunt: The shunt field winding is connected in parallel
with the armature. The armature terminal voltage is the
same as the shunt field voltage. Series field winding is
not used in a shunt machine.
VtE
S
h
u
n
t
fi
e
ld
(ii) Series: The series field winding is connected in
series with the armature. Thus, the armature current is
the same as the series field current. Shunt field winding
is not used in a series machine
V
t
E
Series field
(iii) Compound: In compound machines, both series and shunt field windings are
used. There are two possible connections of compound machines (1) short-shunt and
(2) long-shunt.
Vt
E
Series field
S
h
u
n
t
fi
e
ld Vt
E
Series field
S
h
u
n
t
fi
e
ld
(1) Short-shunt (2) long-shunt
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DC Generators
EMF or Induced Voltage Equation
The emf or induced voltage in the armature of a DC machine is directly proportional
to the flux  produced by the poles and the angular velocity m of the rotor or
armature. The induced voltage (E) can be expressed as
E = kφωm Volt
Here k is a constant and it depends on the rotor or armature of the machine.
Induced voltage (E) depends on the following three factors:
• Flux  produced by the poles
• Angular velocity m of the rotor or armature
• Constant k representing the size of the machine
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This is called voltage equation or EMF equation
Magnetization Curve
The flux is usually produced by passing current through the field winding(s). The flux
induces voltage in the armature when it rotates. The variation of induced voltage
against the field winding current (at constant speed) is called magnetization curve.
The procedure of generating the magnetization curve is as follows
• Run the machine at a constant speed (rated speed)
as a separately excited generator without any load
(or open circuit condition)
• Measure the terminal voltage Vt for different values
of fields current If. Note that at no load, the
armature current is zero and thus the internal
voltage E is the same as the terminal voltage Vt
VtE
If
Rf
Rrh
Vf
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• Plot the induced voltage E against the field current If and is called the magnetization
curve of the machine
• The magnetization curve is also known as Open Circuit Characteristic (OCC) or no-
load (NL) characteristic
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Magnetization Curve
Magnetization curve has three
distinct regions:
• Linear region (E is directly
proportional to If, i.e. E = k1If)
• Transition region (relationship
between E & If is nonlinear)
• Saturation region (E  constant,
independent of If)
Magnetization curve or OCC or no-load characteristic
Residual Voltage
The induced voltage E for If = 0 is
called residual voltage. The residual
voltage is the induced due to residual
flux in the poles and is usually very
small (about 5% of rated value)
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Effects of Speed and Flux on Voltage
Voltage equation: E = km
The ratio of the voltage (for two different conditions, say ‘1’ and ‘2’) is given by












=











=
2
1
2
1
2
1
2
1
2
1
2
1
n
n
E
E
E
E
m
m





 This is a general equation and valid
for all DC machines
(a) For a Shunt Machine
Flux  is produced by the shunt field current If
Thus,  = f(If)
In the linear region:  = kf If (kf is a constant).
Thus, the ratio of flux  is the same as ratio of If
VtE
S
h
u
n
t
fi
e
ld















=














=
2
1
2
1
2
1
2
1
2
1
2
1
n
n
I
I
E
E
or
I
I
E
E
f
f
m
m
f
f


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(b) For a series machine
Flux  is produced by the series field current Is which is the
same as armature current Ia
Thus,  = f(Is) or  = f(Ia)
In the linear region:  = ksIs or  = ksIa (ks is a constant).
Thus, the ratio of flux  is the same as ratio of Ia
V
t
E
Series field












=











=
2
1
2
1
2
1
2
1
2
1
2
1
n
n
I
I
E
E
or
I
I
E
E
a
a
m
m
a
a


Example: The induced voltage E in a separately excited DC generator is found to be 150
V at 1450 rpm when the field current is adjusted to 2.8 A. Find the induced voltage E
(a) for a field current of 3.0 A at 1600 rpm.
(b) for a field current of 2.2 A at 1300 rpm.
Assume that the field flux  is directly proportional to the field current If.
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Solution:
Induced voltage equation
E = km ; Here  = kfIf (kf = constant)
Therefore, E= k(kfIf)m Volts
Thus, the voltage ratio is given by 














=














=
2
1
2
1
2
1
2
1
2
1
n
n
I
I
I
I
E
E
f
f
m
m
f
f


Here E1 = 150 V, If1 = 2.8 A and n1 = 1450 rpm
VE
E
34.177
1600
1450
0.3
8.2150
2
2
=











=
VE
E
66.105
1300
1450
2.2
8.2150
2
2
=











=
(a)
(b)
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Voltage Build-up in a Shunt Generator
In a shunt generator, the armature induced voltage is used to excite the field circuit.
Only under certain conditions, the generator will build up voltage. The process of
building up voltage in a shunt generator is described below
• Assume that the field switch SW is initially opened and the
armature is driven at a constant speed
• A small voltage Ear will induce due to residual pole flux
• When the switch SW is closed, the field circuit is connected to the
armature circuit. A small field current If1 will flow due to Ear and
that will produce an additional field flux
• If the additional field flux is in the same direction of the residual
flux, the resultant flux and hence the induced voltage will increase
(to Ea1)
• Higher voltage causes higher If and . This in turns induces more
voltage.
• The above voltage build-up process continues until the voltage
reaches the steady state operating point ‘P’
VtE
SWIf
Rf
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At no-load, E = (Rf + Ra)If  RfIf (because
Rf >> Ra). Thus, E ≈ Vt = RfIf and it is
represented by a straight line as shown
in the figure. Since the armature and
field are in parallel, they must have the
same voltage and which can be
obtained from the point of intersection
of E vs. If curve and E ≈ Vt = RfIf line.
Effect of speed on induced voltage
For a given field current If, the induced
voltage E is directly proportional to
speed n or m (as shown)
n1 > n2 > n3 > n4 > n5
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Adjustment of No-Load Voltage
The no-load voltage can be adjusted by changing the
point of intersection ‘P’. That is, by changing the slope of
the line or field resistance. This can be achieved by
adding a variable resistance in series with the shunt field
circuit and is called field rheostat. The total field circuit
resistance Rft is the sum of field winding resistance Rf and
field rheostat resistance Rrh → (Rft = Rf + Rrh). The no-load
voltage decreases when the field circuit resistance is
increased
Critical Field Circuit Resistance (Rfcr)
When the field circuit resistance line coincides with the
linear part of the magnetization curve, the voltage
become unstable and the corresponding field circuit
resistance is called the critical field circuit resistance Rfcr
VtE
If
Rf
Rrh
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When
Rft < Rfcr : Voltage will build-up (normal operation)
Rft > Rfcr : Voltage will not build-up (only up to Vt4)
Rft = Rfcr : Unstable situation
Conditions to be Satisfied to Build-up Voltage in Shunt Generators
• Existence of residual flux
• Flux produced by the field current must be in the same direction
of the residual flux
• Total field circuit resistance must be less than the critical field
circuit resistance Rfcr
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In a DC Generator
The internal voltage E is always greater than the terminal voltage Vt. The difference
between E and Vt is called armature voltage drop (AVD). Thus
(E – Vt) = AVD; or E = (Vt + AVD)
At no-load, the load current is zero and thus the AVD is zero or negligible.
Note that in a DC generator, E is the source of electrical power.
For analysis, write appropriate equations for various connections of the machine
(using KVL and KCL)
V
t
E
Shunt field
V
f
In a Separately Excited Generator
The field circuit is isolated from the armature
circuit. The field current If can be adjusted
independently. The induced voltage E depends on If
and which can directly be obtained from the
magnetization curve
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Load Characteristic
When the load current is increased, the load voltage or
terminal voltage decreases because of AVD. Variation
of load voltage (VL) or terminal voltage (Vt) against load
current (IL) is called load characteristic
Causes of voltage drop
• Armature circuit resistance drop or AVD
• Armature reaction voltage drop
• Cumulative effects (for self excited generators)
Armature Reaction
• When the armature delivers current, it produces another flux called armature flux
• The interaction of field flux and armature flux is called armature reaction (AR)
• The AR reduces the resultant flux and hence E
• The AR can be minimized/cancelled by using compensating windings connected in
series with the armature
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Voltage Regulation (VR)
The voltage regulation (VR) is defined as
%100%100 

=

=
t
t
FL
FLNL
V
VE
V
VV
VR
VNL : No-load voltage
VFL = Full load voltage
At no-load, Vt ≈ E (because of no or negligible AVD)
Example
A DC shunt generator has a field circuit resistance of 50 . The internal induced
voltage E is 274.6 V when it delivers an output power of 50 kW at a terminal voltage
of 250 V. Neglect the armature reaction.
(a) Determine the armature resistance
(b) Determine the internal voltage when it delivers an output power of 30 kW at a
terminal voltage of 250 V.
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Solution
(a) Here Rf = 50 , Vt = 250 V,
E = 274.6 V, and Pout = 50 kW
Load current IL = Pout/Vt
= 50,000/250 =200 A
Field current If = Vt/Rf
= 250/50 = 5 A
Armature current Ia = (IL + If)
= (200 + 5) = 205 A
But E = (Vt + IaRa)
 274.6 = (250 + 205Ra)  Ra = 0.12 
(b) Load current IL = Pout/Vt = 30,000/250 =120 A
Field current If = Vt/Rf = 250/50 = 5 A
Armature current Ia = (IL + If) = (120 + 5) = 125 A
But E = (Vt + IaRa)= (250 + 1250.12) = 265 V
VtE
ILIa
If
Rf Load
Vt
IL
IaIf
Rf Ra
E
Load
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Losses and Efficiency
The efficiency () of a generator is the ratio of output power to input power
%100%100
powerInput
powerOutput
==
in
out
P
P

But input power = output power + losses  Pin = (Pout + Ploss)
Pin = Input power to the generator is mechanical power and is given by = Tinm W.
Pout = Output power of the generator is electrical power and is given by = VLIL W
Note: For a separately excited machine, field circuit electrical input power is VfIf W
Losses
There are two major components of losses:
Mechanical or rotational losses (Prot)
It consists of bearing and brush frictions, and windage losses. The iron losses are also considered in
the rotational losses. The rotational losses Prot are usually considered as constant losses.
Electrical or copper losses (Pcu)
Copper losses are I2R loss in various windings (armature, series field and shunt field). The electrical
losses depend on current and hence load. Thus, the electrical losses are considered as variable losses.
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Power Flow Diagram
The input power to a generator is mechanical power and the output power is electrical
power. The portion of mechanical power which is converted into electrical power is
called developed power (Pd). It is the internal power of the machine.
Efficiency:
%100=
in
out
P
P

Pin = (Pd + Prot)
Pd = (Pout + Pcu)
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Example: A shunt generator operates at an efficiency of 85% when delivers 50 A of load
current at 110 V. The rotational losses are 480 W and shunt field resistance is 65 .
Calculate the armature resistance.
Solution:
Output power Pout = Vt IL
= 110  50 = 5500 watts
Input power Pin = Pout/
= 5500/0.85 = 6470.6 watts
Total losses = (Pin – Pout)
= (6470.6 – 5500) = 970.6 watts
Electrical losses = (total losses – rotational losses)
= (970.6 – 480) = 490.6 watts
Shunt field current If = Vt/Rf = 110/65 =1.69 A
Armature current Ia = (IL + If) = (50 + 1.69) = 51.69 A
VtE
ILIa
If
Rf Load
Vt
IL
IaIf
Rf Ra
E
Load
Therefore
Electrical losses =
ffaa RIRI
22 +
 490.6 = 51.692Ra + 1.69
265
 Ra = 0.114 
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Construction wise, a DC motor is similar to a DC generator. The same machine can be
operated either as a generator or as a motor. However the direction of power flow is
opposite.
In generators:
Mechanical power is supplied to the armature. E > Vt; power
flows from E to Vt; E act as a source; E = (Vt + AVD); terminal
voltage Vt is the same as load voltage VL
In motors:
Armature delivers mechanical power. E < Vt; power flows from
Vt to E; E act as a load; E = (Vt – AVD); or Vt = (E + AVD);
terminal voltage Vt is the same as input voltage Vin
Motor induced voltage (E) is usually called back emf
DC Motors
Pm
Generator
E
Ra
Ia
Motor
Pm E
Ra
Ia
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Developed Force
The force developed in a current carrying conductor in the
presence of a magnetic field is given by
Force F = BLI Netwon
The direction of the force can be determined by the Left Hand
Rule (LHR)
Applications of DC Motors
DC motors are widely used for accurate control of speed, position, torque, etc.
Typical applications are:
• Vehicles (starter, wiper, fan and other accessories)
• Machine tools, robots, etc.
• Applications that require high starting torque
Classification of DC Motors
Classification of DC motors is exactly the same as described for DC generatorsEEET 3032/M. H. Haque/2019 37
Torque Equation
For an ideal or lossless machine, the power at the
electrical port is the same as at the mechanical port.
Thus, EIa = Tdm
a
m
am
m
a
d Ik
IkEI
T 



===
)(
ad IkT = This is called torque equation
Expression of induced voltage or back emf (E) of a motor is exactly the same as
that for a generator ( E = km)
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Speed Equation
Consider a separately excited motor is running at a
speed of n (or m) while taking an armature current of Ia
KVL in the armature circuit
Vin = (E + AVD) = (km + AVD)
Pm
Vin
Iin
Rf
If
Vf


k
AVDVin
m

= This is called speed equationThus,
Speed Regulation (SR)
Speed regulation (SR) of a motor is very similar to the voltage regulation of a generator
%100%100 

=

=
mFL
mFLmNL
FL
FLNL
n
nn
SR


NL  No-load and FL  Full-load
Speed adjustment should not be
considered in the regulation
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Power Flow Diagram
The input power to a motor is electrical while the output power is mechanical. The
portion of electrical power which is converted into mechanical power is called
developed power. This is the internal power of the machine.
Efficiency:
%100=
in
out
P
P

Pin = (Pd + electrical losses)
Pd = (Pout + rotational losses)
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For a separately excited
machine, field circuit electrical
input power is VfIf W
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How to Find Rotational Losses?
The technique of determining the rotational losses is given below
• Run the motor at no-load (NL) condition and measure the input voltage Vin
and the input current Iin
• At no-load, output power Pout is zero and thus the input power Pin (= VinIin) is
the total losses in the machine
Pin = (rotational losses + copper losses)  Pin = Prot + Pcu
Calculate Pcu and subtract it from Pin to get the rotational losses
Prot = (Pin – Pcu)
• From power flow diagram
(Pin – Pcu) = Pd = EIa = Prot (at no load or when Pout = 0)
The above calculations is to be done at no-load condition to get Prot.
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Example: A 250-V shunt motor has Ra = 0.25  and Rf = 125 . At no-load, Iin = 5 A and
n = 1200 rpm. At full-load, Iin = 52 A. (a) Find the rotational losses (b) Also find speed,
speed regulation, developed torque and efficiency of the motor at full load.
Solution
(a) At no-load
Here If = Vin/Rf = 250/125 = 2 A
Armature current Ia1 = (Iin – If) = (5 - 2) = 3 A
Induced voltage E1 = (Vin – Ia1Ra) = (250 – 3  0.25) = 249.25 V
Rotational losses Prot = Pd = EIa = 249.253 = 747.75 W
Speed n1 = 1200 rpm (given)
Pm
Vin
Iin
Rf
If
Ia
Iin
Rf
Vin
Ia If
Ra
E
(b) At full-load
Ia2 = (Iin – If) = (52 - 2) = 50 A
E2 = (Vin – Ia2Ra) = (250 – 50  0.25) = 237.5 V
Speed n2 is unknown
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But rpmn
nn
n
E
E
1143
1200
1
5.237
25.249
2
22
1
2
1
2
1 ===


(Note that for the same field current, the ratio of flux is 1)
Speed Regulation %5%100
1143
11431200
=

Developed power Pd = EIa = 237.550 = 11,875 watts
Nm
P
T
m
d
d 2.99
)60/1143(2
875,11
===

Pout = (Pd – Prot) = (11,875 – 747.75) = 11,127.25 Watts
Pin = VinIin = 25052 = 13,000 Watts
%6.85%100
000,13
25.127,11
%100 ===
in
out
P
P

Torque-Speed Characteristic
EEET 3032/M. H. Haque/2019 44
The torque-speed characteristic of a DC motor can be derived from the speed and
torque equations
Td = kIa This is called torque eqn. (or Td–Ia characteristic)


k
AVDVin
m

= This is called speed eqn. (or m–Ia characteristic)
For a Shunt Motor
AVD = IaRa; flux  depends on shunt field current If;  =
f (If);  = kfIf (in the linear region). If the input voltage
Vin and field circuit resistance Rf are constant, the field
current If and hence flux  is also constant
Pm
Vin
Iin
Rf
If
Ia
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For a Series Motor
AVD = Ia(Ra+Rs); flux  depends on series field current which is
the same as the armature current Ia;  = f (Ia);  = ksIa (in the
linear region). The flux  depends on the armature current which
in turn depends on load. Thus,  of a series motor is not
constant.
Vin
Iin
Pm
Rs
To get the torque speed characteristic, plug in the value of Ia from torque equation into
the AVD term of the speed equation
Example: A 400 V series motor has Ra = 0.35  and Rs = 0.15 . When Iin = 44 A, n =
650 rpm. (a) Find the motor speed n for Iin = 36 A. (b) Obtain the speed-current
characteristic and find the speed n for Iin = 36 A from the characteristic. Assume
that the motor operates in the linear part of magnetization curve.
EEET 3032/M. H. Haque/2019 46
Solution
When Iin = Ia = 44 A
E1 = Vin – Ia (Ra + Rs) = 400 – 44  (0.35 +0.15) = 378 V
n1 = 650 rpm m1 = 2n1/60 = 68.07 rad/sec
(a) When Iin = Ia = 36 A
E2 = Vin – Ia (Ra + Rs) = 400 – 36  (0.35 +0.15) = 382 V
But E = km
For a series motor  = f(Ia) = ksIa
Therefore, E = k(ksIa)m
Vin
Iin
Pm
Rs Iin
Vin Ra
E
Rs
rpmn
nn
n
I
I
E
E
a
a
85.802
650
36
44
382
378
2
22
1
2
1
2
1
=












=











=
(b) Speed-current characteristic
E = k(ksIa)m  378 = kks4468.07  kks = 0.1262
Speed equation is
as
saainin
m
Ikk
RRIV
k
AVDV )( +−
=

=


sec/96.3
6.3169
1262.0
)15.035.0(400
rad
I
I
I
a
m
a
a
m






−=

+−
=


When Ia = 36 A, m = (3169.6/36) – 3.96 = 84.08 rad/sec
or, n = 802.8 rpm (same as obtained in part (a)).
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Example: A 240-V DC shunt motor has Ra = 0.15  and Rf = 120 . At full load, Iin = 100 A
and n = 1150 rpm. Derive the torque-current, speed-current and torque-speed
characteristics of the motor. Also find Td and n when Iin = 50 A.
Solution
At full load current of Iin = 100 A
n = 1150 rpm  m = 120.43 rad/sec
If = Vin/Rf = 2 A
Ia = (Iin – If ) = (100 – 2) = 98 A
E = (Vin–IaRa)=(240 - 980.15) = 225.3 V
But E = km  k = E/m
= 225.3/120.43 = 1.87
For a shunt machine, field current
If and hence  is constant
Pm
Vin
Iin
Rf
If
Ia
Iin
Rf
Vin
Ia If
Ra
E
Torque-current characteristic
Td = kIa  Td = 1.87Ia
sec/)0802.034.128(
87.1
15.0240
radI
I
k
IRV
am
aaain
m
−=

=

=



Speed-current characteristic
EEET 3032/M. H. Haque/2019 48
Torque-speed characteristic
87.1
15.0)87.1/(240)/( −
=

=

= dadinaainm
T
k
RkTV
k
RIV




 m = (128.34 – 0.0429Td) rad/sec
At 50 A of input current
Iin = 50 A; Ia = (Iin – If) = 48 A
Td = 1.87Ia = 1.8748 = 89.76 Nm
m = (128.34–0.0802Ia) = (128.34–0.080248) =124.5 rad/sec
 n = 1189 rpm
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Speed Control
EEET 3032/M. H. Haque/2019 49
The speed equation of a DC motor is 

k
AVDVin
m

=
Three possible methods of speed control are:
(a) Armature resistance or AVD control; (b) Field or flux control; (c) Input voltage control
(a) Armature Resistance or AVD Control
Add a variable external resistance Rext in series with the
armature circuit to change the armature voltage drop Ia(Ra+Rext)
and hence to change the speed. Here AVD = Ia(Ra+Rext)
Main Features
• Speed can only be decreased
• Ineffective at no load (when Ia  0)
• Higher losses and lower efficiency
Vin
Iin
Rf
If
Ia
Rext
EEET 3032/M. H. Haque/2019 50
(b) Field Control
Add a field rheostat Rrh in series with the shunt field circuit to
reduce the field current If (or ) and hence to increase the speed.
Vin
Iin
Rf
IfIa
Rrh
frh
in
f
RR
V
I
+
= ;  = f(If)
Main Features
• Speed can only be increased
• Speed can be controlled at all load levels
(c) Input Voltage Control
Connect a variable voltage source to the armature and a fixed
voltage source to the field circuit (separately excited)
Main Features
• Speed can only be decreased (because Vin < Vrated)
• Speed can be controlled at all load levels
Iin
Rf
If
Vf
Variable
voltage
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In many cases, it is required to control the speed over a
wide range (below and above the normal speed). For such
a case, a combination of field and input voltage controls
can be used.
Iin
Rf
If
Vf
Rrh
Variable
voltage
Combination of field and voltage controls
Control of dc motor by
Power Electronics
EEET 3032/M. H. Haque/2019 52
Example: A 240-V shunt motor has Ra = 0.05  and Rf = 60 . At no-load, Iin = 7 A and
n = 1120 rpm. At full load, Iin = 46 A. The motor operates in the linear part of
magnetization curve. Find the motor speed at full load input current (a) without any
extra resistance; (b) with an extra field resistance of 20 , and (c) with an extra
armature resistance of 1  and no extra field resistance.
Solution
At no load
If = 240/60 = 4 A;
Ia = (Iin – If) = (7 – 4) = 3 A
E = (Vin–IaRa) = (240 – 30.05) = 239.85 V
Pm
Vin
Iin
Rf
If
Ia
2
1
2
1
2
1
2
1
2
1
n
n
I
I
I
I
E
E
f
f
m
m
f
f
==


But
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EEET 3032/M. H. Haque/2019 53
Pm
Vin
Iin
Rf
If
Ia
(a) At full load (without any extra resistance)
If = 240/60 = 4 A; Ia = (Iin – If) = (46 – 4) = 42 A
E = (Vin – IaRa) = (240 – 420.05) = 237.9 V
rpmn
n
1111
1120
4
4
9.237
85.239
2
2
==
(b) At full load (with 20  extra resistance in field circuit)
If = 240/(60+20) = 3 A;
Ia = (Iin – If) = (46 – 3) = 43 A
E = (Vin–IaRa) = (240 – 430.05) = 237.85 V
Vin
Iin
Rf
IfIa
Rrh
rpmn
n
1481
1120
3
4
85.237
85.239
2
2
==
(c) At full load (with 1.0  extra resistance in armature circuit)
Here If = 4 A and Ia = 42 A
E = 240 – 42(0.05+1.0) = 195.9 V
rpmn
n
915
1120
4
4
9.195
85.239
2
2
==
Vin
Iin
Rf
If
Ia
Rext
Starting of DC Motors
EEET 3032/M. H. Haque/2019 54
KVL in the armature circuit is
Vin =(E + IaRa) 
a
in
a
R
EV
I

=
At starting; n = 0
 E = 0 (because E = km)
 Ia (start) = Vin / Ra  Starting current is extremely high
Pm
Vin
Iin
Rf
If
Ia
Consequences
• Armature is subject to a severe mechanical shock
• Blow fuses
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Starting of DC Motors
EEET 3032/M. H. Haque/2019 55
How to overcome high current?
Add an external variable resistance in series with
the armature and is called starter
startera
in
a
RR
V
I
+
=start)(
Power Electronics
Power electronics devices can also be used to reduce the starting current. This
can be achieved by applying reduced voltage to armature at starting. Most of the
modern dc motors use this technique.
Motor and Load Torque Matching
EEET 3032/M. H. Haque/2019 56
Torque-speed characteristic of a motor and
a load can be expressed as
Motor: Td = f1(ωm) (1)
Load: TL = f2(ωm) (2)
Decelerating
Torque
Accelerating
Torque
Speed
T
o
rq
u
e
Motor torque
Load torque
Equilibrium
point
For steady state operation (when Prot = 0)
Motor developed torque = Load torque
 Td = TL
Steady state operating condition (m & T) can be
obtained
• By solving eqns. (1) and (2) simultaneously
• From the point of intersection of eqns. (1) &
(2)
When Td > TL : motor accelerates
When Td < TL : motor decelerates
Torque-speed characteristic of motor and load
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Example: A 120 V DC shunt motor has Ra = 0.1 , Rf = 120  and Prot = 0. When Iin = 119.4
A, the motor runs at 1100 rpm.
(a) Find the developed torque
(b) Establish the torque-speed characteristic
(c) Estimate the no-load speed and starting torque
(d) Find the speed when the load torque is
(e) Calculate Td, Ia and  for the load condition of part (d)
mLT 2778.6=
Solution:
(a) Here Ra = 0.1 , Rf = 120 , and n = 1100 rpm when Iin = 119.4 A
m = 2n/60 = 115.2 rad/sec
If = Vin/Rf = 120/120 = 1A
Ia = (Iin – If) = (119.4 - 1) = 118.4 A
E = (Vin – IaRa) = (120 – 118.40.1) = 108.16 V
Pd = EIa = 108.16118.4 = 12.8 kW
But Pd = Tdm  Td = Pd/m = 111.2 Nm
Also E = km  k = E/m = 0.939
Pm
Vin
Iin
Rf
If
Ia
Iin
Rf
Vin
Ia If
Ra
E
EEET 3032/M. H. Haque/2019 58
(b) Speed equation: d
ainadinaain
m T
k
R
k
V
k
RkTV
k
RIV
2)(
)/(



 −=

=

=
ddm TT 1134.08.127
939.0
1.0
939.0
120
2
−=−=
Therefore, the torque-speed characteristic of the motor is:
NmTor
radT
md
dm
)82.81127(,
sec/)1134.08.127(


−=
−=
(1)
(c) At NL: Td = 0; m = 127.8 rad/sec (or n =1220.4 rpm)
At starting: n = 0 (or m = 0);  Td = 1127 Nm
(d) The torque-speed characteristic of the load is
mLT 2778.6= (2)
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At steady state: Td = TL  (1127 – 8.82m) m2778.6=
016.16327062.2562 =+− mm 
Therefore, m = 136.08 rad/sec or 119.98 rad/sec.
Consider m = 119.98 rad/sec  n = 1145.7 rpm
(m = 136.08 rad/sec provides negative value of Td and thus not feasible)
(e) From eqn. (1): Td = (1127 – 8.82119.98) = 68.78 Nm
Also, Td = kIa  Ia = Td/ k = 68.78/0.939 = 73.25 A
Pd = Tdm = 68.78119.98 = 8252.2 W = Pout (note Prot = 0)
If = Vin/Rf = 120/120 = 1A
Iin = (Ia + If) = (73.25 + 1) = 74.25 A
Pin =Vin Iin = 12074.25 = 8910 watts
%62.92%100
8910
5.8252
Input
Output
===
in
out
P
P
Efficiency =
Dynamics of Armature Voltage Controlled DC Motors
EEET 3032/M. H. Haque/2019 60
Consider the armature of a separately excited dc motor is connected to a voltage
source through a switch ‘S’ as shown in the following figure.
Sudden application of armature voltage would
cause a transient whose duration is governed by
the parameters of the machine and the load.
Assume that the field circuit has already reached
the steady state condition and its current remains
constant. Under this case, the variation of
armature current can be represented by the
following first order differential equation
)(
)(
)( 1 tk
dt
tdi
LtiRV m
a
aaas ++=
Note that the back emf E = (kφ)ωm =
k1ωm (for a constant value of field
current If or φ)
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The torque equation of the motor under transient condition can be expressed by the
following first order differential equation.
dt
td
JtDTtikT m
mLad
)(
)()(
1

 ++==
Here TL = load torque
D = viscous friction coefficient of rotating members
J = inertia of the rotating members
k1 = kφ
The above two equations can be written in the following form
 
 saam
a
a
Lam
m
VtiRtk
Ldt
tdi
TtiktD
Jdt
td
+−−=
−+−=
)()(
1)(
)()(
1)(
1
1



EEET 3032/M. H. Haque/2019 62



















+

















−−

=










s
L
a
a
m
a
a
a
a
m
V
T
L
J
ti
t
L
R
L
k
J
k
J
D
dt
tdi
dt
td
1
0
0
1
)(
)(
)(
)(
1
1


The above equation can be rearrange in matrix form as
In general form: BUAXX +=
Here X is the state variable X = [ωm(t) ia(t)]
T and U is the input variables U = [TL Vs]
T
Solutions of the above equation would provide the variation of motor speed ωm(t)
and armature current ia(t) as function of time.
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Block Diagram of a Separately Excited DC Motor
EEET 3032/M. H. Haque/2019 63
Dynamic equations:
 
 saam
a
a
Lam
m
VtiRtk
Ldt
tdi
TtiktD
Jdt
td
+−−=
−+−=
)()(
1)(
)()(
1)(
1
1



Laplace Transform of the above equations with zero initial condition
 
 )()()(1)(
)()()(
1
)(
1
1
sVsIRsk
L
ssI
sTsIksD
J
ss
saam
a
a
Lamm
+−−=
−+−=
EEET 3032/M. H. Haque/2019 64
The above equations can be represented by the following block diagram in Matlab/Simulink
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+
-
+
-
k1
k1
Vs(s)
TL(s)
Ωr(s)Td(s)Ia(s)
s
1
s
1
aL
1
J
1
aR D
- -
The combined block diagram is
EEET 3032/M. H. Haque/2019 66
Typical variation of armature current under no-load condition
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Typical variation of speed under no-load condition
Acknowledgement
The figures and diagrams of this lecture note are taken from
the following sources:
• B. S. Guru and H. R. Hiziroglu, “Electric Machines and Transformers”, 3rd
Edition, Oxford University Press, 2001.
• G. B. Shrestha and M. H. Haque, “AC Circuits and Machines”, Pearson
Prentice Hall, 2006.
• P. C. Sen, “Principles of Electric Machines and Power Electronics”, 2nd
Edition, John Wiley & Sons, 1997.
• P. F. Ryff, D. Platnick and J. A. Karnas, “Electrical Machines and
Transformers”, Prentice Hall, 1987.
EEET 3032/M. H. Haque/2019 68
67
68
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