Title: Lecture 1 - EE743
1SYNCHRONOUS MACHINES
Two-pole,3-phase,wye-connected,salient-pole
synchronous machine
2SYNCHRONOUS MACHINES
- In abc reference frame, voltage equations can be
written as
3SYNCHRONOUS MACHINES
4SYNCHRONOUS MACHINES
- Referring all rotor variables to the stator
windings
5SYNCHRONOUS MACHINES
- Referring all rotor variables to the stator
windings
6SYNCHRONOUS MACHINES
- Referring all rotor variables to the stator
windings
7SYNCHRONOUS MACHINES
- TORQUE EQUATION IN MACHINE VARIABLES
8SYNCHRONOUS MACHINES
9SYNCHRONOUS MACHINES
- Stator Voltage Equations in Arbitrary
Reference-frame Variables
- The rotor voltage equations are expressed only in
the rotor reference frame
10SYNCHRONOUS MACHINES
- The flux linkage equations may be expressed as
- The sinusoidal terms are constant, independent
of ? and ?r only if ? ?r
11SYNCHRONOUS MACHINES
- Therefore, the time-varying inductances are
eliminated from the voltage equations only if the
reference frame is fixed in the rotor.
- Voltage Equations In Rotor Reference-frame
variables park's Equations
12SYNCHRONOUS MACHINES
13SYNCHRONOUS MACHINES
- Park's voltage equations are often written in
expanded form
- Flux linkages in expanded form
14SYNCHRONOUS MACHINES
- The Equivalent q-axis Circuits
15SYNCHRONOUS MACHINES
- The Equivalent d-axis Circuits
16SYNCHRONOUS MACHINES
- The Equivalent 0-axis Circuits
17SYNCHRONOUS MACHINES
- It is often convenient to express the voltage
and flux linkage equations in terms of reactances
rather than inductances
18SYNCHRONOUS MACHINES
- Also, it is convenient to define
19SYNCHRONOUS MACHINES
- If we select the currents as independent
variables
20SYNCHRONOUS MACHINES
- If we select the flux linkages per second as
independent variables
21SYNCHRONOUS MACHINES
- Torque Equations in Substitute Variables
22SYNCHRONOUS MACHINES
it is convenient to relate the position of the
rotor of a synchronous machine to a voltage or to
the rotor of another machine.
The electrical angular displacement of the rotor
relative to its terminal voltage is defined as
the rotor angle,
The rotor angle is the displacement of the rotor
generally referenced to the maximum positive
value of the fundamental component of the
terminal voltage of phase a
23SYNCHRONOUS MACHINES
It is important to note that the rotor angle is
often used as the argument in the transformation
between the rotor and synchronously rotating
reference frames
The rotor angle is often used in relating torque
and rotor speed (if ?e is constant)
24SYNCHRONOUS MACHINES
PER UNIT SYSTEM
- Base voltage
- the rms value ofthe rated phase voltage for
the abc variables - the peak value for the qd0 variables.
- Base power
- When considering the machine separately, the
power base is selected as its volt-ampere rating. - When considering power systems, a system
power base (system base) is selected
- Once the base quantities are established, the
corresponding base current and base impedance may
be calculated.
- Base torque is the base power divided by the
synchronous speed of the rotor
25SYNCHRONOUS MACHINES
- The torque expressed in per unit
26SYNCHRONOUS MACHINES
- ANALYSIS OF STEADY-STATE OPERATION
For balanced conditions the 0s quantities are
zero. ?r is constant and equal to ?e the rotor
windings do not experience a change of flux
linkages the current is not flowing in the
short-circuited damper windings the time rate of
change of all flux linkages neglected
27SYNCHRONOUS MACHINES
- ANALYSIS OF STEADY-STATE OPERATION
For balanced conditions
28SYNCHRONOUS MACHINES
- ANALYSIS OF STEADY-STATE OPERATION
Hence
and if it is noted that
Then
29- ANALYSIS OF STEADY-STATE OPERATION
It is convenient to define the last term on the
right-hand side as (excitation voltage)
if rs is neglected, the expression for the
balanced steady-state electromagnetic torque in
per unit can be written as
30DYNAMIC PERFORMANCE DURING A SUDDEN CHANGE IN
INPUT TORQUE
31DYNAMIC PERFORMANCE DURING A SUDDEN CHANGE IN
INPUT TORQUE
Dynamic performance of a hydro turbine generator
during a step increase in input torque from zero
to rated
32DYNAMIC PERFORMANCE DURING A SUDDEN CHANGE IN
INPUT TORQUE
Torque versus rotor angle characteristics
33DYNAMIC PERFORMANCE DURING A SUDDEN CHANGE IN
INPUT TORQUE
34DYNAMIC PERFORMANCE DURING A SUDDEN CHANGE IN
INPUT TORQUE
Dynamic performance of a steam turbine generator
during a step increase in input torque from zero
to 50 rated.
35DYNAMIC PERFORMANCE DURING A SUDDEN CHANGE IN
INPUT TORQUE
Torque versus rotor angle characteristics
36DYNAMIC PERFORMANCE DURING A 3 PHASE FAULT AT THE
MACHINE TERMINALS
a hydro turbine generator
37DYNAMIC PERFORMANCE DURING A 3 PHASE FAULT AT THE
MACHINE TERMINALS
Torque versus rotor angle characteristics
38DYNAMIC PERFORMANCE DURING A 3 PHASE FAULT AT THE
MACHINE TERMINALS
a steam turbine generator
39DYNAMIC PERFORMANCE DURING A 3 PHASE FAULT AT THE
MACHINE TERMINALS
Torque versus rotor angle characteristics
40COMPUTER SIMULATION
Simulation in Rotor Reference Frame
Where
41COMPUTER SIMULATION
Simulation in Rotor Reference Frame
42COMPUTER SIMULATION
Simulation of Saturation
43COMPUTER SIMULATION
Simulation of Saturation