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An Introduction to Electrical Machines
P. Di Barba, University of Pavia, Italy Academic year 2011-2012
Contents
Transformer • 1. An overview of the device • 2. Principle of operation of a single-phase transformer • 3. Power (three-phase) transformer, signal transformer, autotransformer
Rotating electrical machines (REM) • 1. Ampère law, Faraday principle, Lorentz force • 2. An overview of REM • 3. Rotating magnetic field
Asynchronous machine: induction motor Synchronous machine: alternator DC machine: commutator motor, dynamo Permanent magnet motor Stepping motor
Transformer: static electrical machine operating in AC regime. It converts electric power into electric power, by varying the power factors (V,I) and keeping the power (approximately) constant.
1 : primary circuit (power in) 2 : secondary circuit (power out)
Single-phase
Three-phase
Applications Power transformer • Production systems operate at a reduced voltage in order to decrease dielectric material size • Transmission systems operate at a low current in order to decrease conducting material size • User systems operate at a low voltage in order to increase safety Signal (and power) transformer • Adapts the voltage of two systems to be connected • Adapts the impedance of two systems to be connected • Couples two systems, keeping them electrically disconnected
Step up transformer: increases V and decreases I Step down transformer: decreases V and increases I Power range: from 1 VA to 1000 MVA Voltage range: from 1 V to 400 kV
Basically, a transformer is composed of: • a magnetic circuit; • (at least) two magnetically-coupled electric circuits.
1 2
yoke
lim
b
2 1
low-voltage terminal
high-voltage terminal lamination package (core)
A>25 kVA forced cooling
A<25 kVA natural cooling
Single-phase power transformer (25 Hz < f < 400 Hz)
windings
a b c
1 2
Three-phase power transformer (f=50 Hz) : three pairs of windings
Signal transformer single phase 20 Hz < f < 20 kHz
open magnetic circuit (f>20 kHz, core made of Fe2O3)
closed magnetic circuit
Three primary windings 1a,1b,1c and three secondary windings 2a,2b,2c Used connections: star-delta, delta-delta, delta-star.
Operating principle (ideal case) Model assumptions: infinite core permeability, zero losses in the magnetic circuit and in the two electric circuits.
1: N1 turns
2: N2 turns
221121
21
2
112
IVIVAA
Ik
1I
N
Nk,V
k
1V
Transformer equations
1 1I
2
2I
Z
F
Transformer laws (ideal model) I No-load operation (I2=0) Let a sinusoidal voltage source v1(t) supply winding 1 Then, an infinitesimal magnetizing current I10 flows in winding 1 and gives rise to a magnetomotive force (mmf) Hopkinson law: magnetic flux
infinitesimal mmf infinitesimal reluctance non-infinitesimal sinusoidal flux
F101IN
Transformer laws (ideal model) II Flux F links both windings 1 and 2 Faraday-Lenz law: induced emf KVL v1=-e1 , v2=-e2 In phasor notation: In terms of RMS values, it turns out to be: transformer voltage law
dt
dNe
F 11
dt
dNe
F 22
kN
N
V
V
2
1
2
1
F 11 NjV F 22 NjV
F
2
1 10I
1
2
0EV
0EV
22
11
Kirchhoff voltage law
Terminal marking: currents entering the marked terminals originate like fluxes in the magnetic core.
I10 magnetizing current
Primary circuit: supplied by V1
Secondary circuit: open circuited
Transformer laws (ideal model) III On-load operation Current I2 is delivered by winding 2 to load Z mmf N2I2 originates a secondary flux F2 opposing the primary flux F1 = FM , but cannot vary due to the applied primary voltage V1
fN
VM
1
1
44.4F
Transformer laws (ideal model) IV Consequently, voltage source V1 is forced to deliver an additional current I1 to winding 1 in order to compensate the flux mismatch: N1I1-N2I2=N1I10=0 It turns out to be: transformer current law Finally, the complex power conservation holds:
kN
N
I
I 1
1
2
2
1
2211 IVIV
Vector diagram (Kapp diagram)
A resistive-inductive load is assumed
A more realistic model - 1
In a real transformer, power losses are not zero: P0=GV2 active power in the magnetic core (eddy current and hysteresis) Pc=RI2 active power in the electric circuits due to the Joule effect
Moreover, the finite magnetic permeability of the core causes a non-zero magnetizing power: Q0=BV2 reactive power in the magnetic circuit of main flux (inside the core) QC=XI2 reactive power in the magnetic circuit of stray flux (outside the core)
P0 and Q0 dominate in the no-load operation (measured in the open-circuit test)
Pc and Qc dominate in the on-load operation (measured in the short-circuit test)
A more realistic model - 2
As a consequence, in a real transformer: V1 is different from –E1 due to voltage drops caused by R and X of the windings F is not constant with respect to E1 because E1 varies with I1 for a given V1
V1 is different from kV2 due to on-load voltage drops I1 is different from I2/k due to no-load primary current A1 is different from A2 due to active and reactive power losses
Transformer equations based on the ideal model are valid as a first approximation only
A more realistic model - 3
stray flux main flux
power loss (eddy currents, hysteresis)
power loss (Joule effect)
Z R jX
Y G jB
21
2221
21
2221
121
212
BVXIQQ
GVRIPP
VYIk
1I
IZVk
1V
A more realistic model - 4
Primary winding admittance
Secondary winding impedance
A more realistic model - 5
Modified Kapp diagram
2
11
kZ
VI
Impedance adaption - 1
Problem: how to modify the value of an impedance Z to be connected at a terminal pair A-B ?
Impedance adaption - 2
Zk
V
k
1
Z
1
k
V
k
1
Z
V
k
1II
2
11221
Signal transformer: frequency response - 1
Xm Xc
Signal transformer: frequency response - 2
senjIIjXRVIjXRVVVk
22222201 cos)(1
V V20 V2
Voltage drop - 1
sincos 22220 XIRIVVV
Voltage drop - 2
Insulation transformer - 1
Measurement
Safety
Insulation transformer - 2
Insulation transformer - 3
Damping
kN
NN
V
V
2
12
2
1
k
1
NN
N
I
I
12
2
2
1
AAIVIVA 222111
212121 )()( VIIIVVAd
Auto-transformer
1A
Ad
Rotating Electrical Machine Basically, it consists of: • an electric circuit (inductor) originating the magnetic field; • a magnetic circuit concentrating the field lines; • an electric circuit (armature) experiencing electrodynamical force or electromotive force.
bi
Ampère law
e
Faraday law
transformer effect
b(t) e(t), i(t)
Faraday law
evb
(motional effect)
Fib
Lorentz force
stator
air-gap
rotor
inductor circuit
armature circuit
r
Bd
ld
i
B
n
Magnetic field of a circular coil
nr2
iB 0
1B
2B
j axis
r axis
B
1
2 Rotating magnetic field (two-phase) I
tr
Int
r
IB
cos
2cos
2
01
01
tsenr
Ijntsen
r
Int
r
IB
222cos
2
02
02
02
1B
2B
j axis
r axis
B
1
2
Rotating magnetic field (two-phase) II
tjer
Itsenjt
r
IBBB
2cos
2
0021
1
r axis
B
j axis
2
3
tjer
IB
22
3 0
Rotating magnetic field (three-phase): Ferraris field
10
1 cos2
ntr
IB
20
2
3
2cos
2nt
r
IB
30
3
3
4cos
2nt
r
IB
Three-phase asynchronous motor (induction motor)
graphic symbol
As a motor, it converts electric power into mechanical power
three-phase inductor circuit
ventilating fan
laminated stator and rotor
shaft
air gap
W
Squirrel-cage rotor Wound rotor
slip-ring commutator (single-phase)
end ring
bar
Induction motor: operating principle
• Inductor terminals are supplied by a three-phase symmetric voltage V1
• A three-phase balanced current I1 is delivered to inductor windings. • An induction field B1 rotating at speed N0 = 120 f p-1 is originated (f current frequency, p number of poles, speed in rpm). • In stator and rotor windings, subject to a sinusoidal magnetic flux F, electromotive forces E1=2.22 m1 f F and E2=2.22 m2 f F are induced, respectively. F max value of flux, E1,2 rms value of electromotive force m1,2 number of conductors in a winding
E2 three-phase balanced current I2 in the rotor windings
Magnetic effect of I2 : • a synchronous rotating field B2 (speed N0) is originated, which tends to decrease the inductor rotating field B1
• B1 depends on the applied voltage V1 and cannot vary • voltage source V1 is forced to deliver an additional current I3 to the inductor, such that rotating field B3 due to I3 compensates field B2
Mechanical effect of I2 : the axially-directed conductors placed in the radially-directed field B1
experience tangentially-directed forces Ft
The rotor experiences a torque C=2RFt: if unconstrained, it rotates.
Having defined the slip factor s=(N0-N)/N0
as the speed of the rotating field with respect to the rotor, the frequency of E2 and I2 is f2=sf
If the opposing torque is equal to zero then, the running torque CM=0 and f ≠ 0 I2=0 E2=0 f2=0 s=0 N=N0 the rotor is synchronous wrt the rotating field
If the opposing torque is different from zero then, the running torque CM≠0 and f ≠ 0 I2 ≠ 0 E2 ≠ 0 f2 ≠ 0 0<s<1 N<N0 the rotor is asynchronous wrt the rotating field (the rotor follows the field)
Torque-speed curve
Torque C is proportional to both flux F1 of the rotating field and real part of the armature current I2cos f2 (active component):
Current I2 and power factor cos f2 depend on emf E2 and armature circuit impedance:
On the other hand, electromotive force E2 depends on both relative rotor speed N0-N and flux F1
It turns out to be:
221 cosIkC F
2
2
2
22 LsRZ resistive-inductive impedance R2+jsL2
102 ' F NNkE
2
12
2
2
0
2
20
20
2
02
11
2
2
2
21 , VCNCC
LNNRN
RNNNk
Z
R
Z
EkC
FF
N N0 0
CR
CS
C
operating point
CM
Torque-speed curve
p
f120N0 synchronous speed (rpm)
self-starting Cs = k1F1
2 N0R2/(R22+2L2
2)
mechanical power Pm = CN electric power Pe = √3 VI cosf
Max torque CM = k1F1
2 N0/(2L2) when N = N0(1-R2/L2)
N
C
1
2
N
C
1
2
N
C
1
2
Speed control
increasing R2 (wound rotor only)
decreasing f decreasing V
Synchronous generator
turbine alternator
Three-phase output
Alternator structure
Three-phase armature circuit
DC inductor circuit (two-pole) In low-power alternators it can be replaced by a permanent magnet.
As a generator, it converts mechanical power into electric power.
• The inductor circuit is supplied by a DC current IE
• A magnetic flux FR sinusoidally distributed in the air-gap is originated
• A speed W is applied to the rotor shaft
• In the armature circuit a three-phase symmetric electromotive force
E = kWFR at an angular frequency = Wp/2 is induced • If the armature circuit is on load, a three-phase (balanced) current I is delivered, so providing an active power P = 3EI cos f
• An equal amount of mechanical power must be supplied to the shaft
• Current I generates a synchronous rotating field (speed ), which originates a flux FS opposing flux FR
• In order to keep E constant, excitation current IE must be increased
Alternator operating principle
I I
2
pW
Two-pole DC winding Four-pole DC winding
number of poles electric frequency
rotor speed
DC machine
graphic symbol
From electric to mechanical power: motor From mechanical to electric power: dynamo
ventilating fan
laminated stator and rotor
shaft sliding brushes with commutator
armature
inductor
salient pole
air gap
DC machine - Principle of operation I
MOTOR Inductor circuit is supplied by DC voltage VE
Current IE is originated Magnetic field B, and so flux F, take place Armature circuit is supplied by DC current IA Armature conductors, carrying axial current IA and placed in radial field B, are subject to tangential force F Main effect F C N Pm = CN Secondary effect Due to the rotor motion, in the armature conductors an AC emf is induced, which is subsequently rectified by the multi-sector commutator. Therefore, a back emf E = kNF appears at the commutator terminals. It turns out to be: E = V (V voltage across armature terminals) Pe = EIA = CN = Pm (power balance)
DC machine - Principle of operation II
DYNAMO Inductor circuit is supplied by DC voltage VE Current IE is originated Magnetic field B, and so flux F, take place Rotor is given speed N, externally applied to the shaft In the armature conductors, an AC emf is induced At the commutator terminals a rectified emf E = kNF is available Main effect If armature terminals are connected to a resistive load E IA Pe = EIA
Secondary effect Armature conductors, carrying axial current IA and placed in radial field B, are subject to tangential force F opposing the motion F C N Pm = CN To maintain the motion, power Pm must be supplied to the shaft (Pm = Pe) .
+
B
A
b
a
B
A
b
a
t t1
a b
t2
t
VAB
t
VAB
Multi-sector commutator: principle of operation
As a result, the original AC signal is mechanically transformed into a DC signal, and viceversa.
with two conductors/sectors
with several conductors/sectors
The polarity of each sector is reversed when crossing the A-B line joining the brushes (orthogonal to the pole axis).
Each armature conductor is electrically connected to a sector.
The voltage VAB between brushes exhibits always the same polarity.
MVE
I
Series excitation (motors for traction) When Cres varies, both N and C vary in such a way that CN const (constant power motor)
MVE
IE IA
VA
Independent excitation
MV
IE IA
Derived excitation
When Cres varies, excitation current IE varies N const (constant speed motor)
DC motor excitation schemes
F kNE
AA
R
EV'kI'kC
FF
EIFF
Equivalent circuit of the DC motor (with independent excitation)
k voltage constant
k’ torque constant
Induced emf (rectified)
Excitation flux
inductor circuit
armature circuit (Ra resistance of armature conductor)
Torque
F F(IE )
F
k
VN0
AS
R
V'kC F
Torque-speed curve (independent-excitation motor)
self-starting
NCkNVR
kC
A
FF
'
Speed control
Ideal diode: current-voltage curve
AC to DC conversion - 1
iR i1 i2
R RiR
Transformer + single phase rectifier
AC to DC conversion - 2
Single-phase rectifier (full-wave): principle of operation
AC to DC conversion - 3
A rectified voltage vR is originated: non-zero average value
Wound synchronous motor
Excitation
windings
Permanent magnet synchronous motor
Magnets
Magnets
SPM IPM
Synchronous motor: torque-speed curve
Reference signal Rotor position sensor (Hall probe)
feedback Control system
Three-phase inverter
Brushless DC motor: principle of operation
Stepping motor: principle of operation
Permanent-magnet stepping motor
Variable-reluctance stepping motor