% M-file: prob5_4e.m % M-file to calculate and plot the terminal voltage % of a synchronous generator as a function of load % for power factors of 0.8 lagging, 1.0, and 0.8 leading... As
Trang 1(a) This generator is Y-connected, so I L=I A At rated conditions, the line and phase current in this generator is
1000 kVA
251 A
L
P
V
The phase voltage of this machine is Vφ =V T/ 3=1328 V The internal generated voltage of the machine
is
1328 0 0.15 251 36.87 A 1.1 251 36.87 A
E
1537 7.4 EA= ∠ °V
The input power to this generator is equal to the output power plus losses The rated output power is
OUT 1000 kVA 0.8 800 kW
2
CU 3 A A 3 251 A 0.15 28.4 kW
F&W 24 kW
core 18 kW
stray (assumed 0)
IN OUT CU F&W core stray 870.4 kW
OUT IN
800 kW
870.4 kW
P P
(b) If the generator is loaded to rated kVA with lagging loads, the phase voltage is Vφ=1328 0 V∠ ° and the internal generated voltage is EA=1537 7.4 V∠ ° Therefore, the phase voltage at no-load would be
1537 0 V
Vφ = ∠ ° The voltage regulation would be:
1537 1328
1328
−
(c) If the generator is loaded to rated kVA with leading loads, the phase voltage is Vφ=1328 0 V∠ ° and the internal generated voltage is
1328 0 0.15 251 36.87 A 1.1 251 36.87 A
1217 11.5 EA= ∠ ° V
The voltage regulation would be:
1217 1328
1328
−
(d) If the generator is loaded to rated kVA at unity power factor, the phase voltage is
1328 0 V
V and the internal generated voltage is
Trang 2116
1328 0 0.15 251 0 A 1.1 251 0 A
1393 11.4 EA= ∠ ° V
The voltage regulation would be:
1393 1328
1328
−
(e) For this problem, we will assume that the terminal voltage is adjusted to 2300 V at no load
conditions, and see what happens to the voltage as load increases at 0.8 lagging, unity, and 0.8 leading power factors Note that the maximum current will be 251 A in any case A phasor diagram representing the situation at lagging power factor is shown below:
I
A
V φ
E
A
θ
δ
θ
θ
I
A
R
A
jX
S I
A
By the Pythagorean Theorem,
2
E = Vφ+R I θ+X I θ + X I θ−R I θ
2
Vφ = E − X I θ−R I θ −R I θ−X I θ
A phasor diagram representing the situation at leading power factor is shown below:
I
A
V φ
E
A
θ
θ
I
A
R
A
jX
S I
A
By the Pythagorean Theorem,
2
E = Vφ+R I θ−X I θ + X I θ+R I θ
2
Vφ = E − X I θ+R I θ −R I θ+X I θ
A phasor diagram representing the situation at unity power factor is shown below:
I
E
A
δ
I
A
R
A
jX
S I
A
Trang 3By the Pythagorean Theorem,
E =Vφ + X I
2
Vφ = E − X I
The MATLAB program is shown below takes advantage of this fact
% M-file: prob5_4e.m
% M-file to calculate and plot the terminal voltage
% of a synchronous generator as a function of load
% for power factors of 0.8 lagging, 1.0, and 0.8 leading
% Define values for this generator
EA = 1328; % Internal gen voltage
I = 0:2.51:251; % Current values (A)
R = 0.15; % R (ohms)
X = 1.10; % XS (ohms)
% Calculate the voltage for the lagging PF case
VP_lag = sqrt( EA^2 - (X.*I.*0.8 - R.*I.*0.6).^2 )
- R.*I.*0.8 - X.*I.*0.6;
VT_lag = VP_lag * sqrt(3);
% Calculate the voltage for the leading PF case
VP_lead = sqrt( EA^2 - (X.*I.*0.8 + R.*I.*0.6).^2 )
- R.*I.*0.8 + X.*I.*0.6;
VT_lead = VP_lead * sqrt(3);
% Calculate the voltage for the unity PF case
VP_unity = sqrt( EA^2 - (X.*I).^2 );
VT_unity = VP_unity * sqrt(3);
% Plot the terminal voltage versus load
plot(I,abs(VT_lag),'b-','LineWidth',2.0);
hold on;
plot(I,abs(VT_unity),'k ','LineWidth',2.0);
plot(I,abs(VT_lead),'r-.','LineWidth',2.0);
title ('\bfTerminal Voltage Versus Load');
xlabel ('\bfLoad (A)');
ylabel ('\bfTerminal Voltage (V)');
legend('0.8 PF lagging','1.0 PF','0.8 PF leading');
axis([0 260 1500 2500]);
grid on;
hold off;
The resulting plot is shown below:
Trang 4118
5-5 Assume that the field current of the generator in Problem 5-2 has been adjusted so that it supplies rated
voltage when loaded with rated current at unity power factor (You may ignore the effects of R A when answering these questions.)
(a) What is the torque angle δ of the generator when supplying rated current at unity power factor?
(b) When this generator is running at full load with unity power factor, how close is it to the static stability
limit of the machine?
SOLUTION
(a) The torque δ angle can be found by calculating EA:
A= φ+R A A+ jX S A
1328 0 0.15 251 0 A 1.1 251 0 A
1393 11.4 EA= ∠ ° V
Thus the torque angle δ = 11.4°
(b) The static stability limit occurs at δ = 90° This generator is a very long way from that limit If we ignore the internal resistance of the generator, the output power will be given by
3 sin
A
S
V E P X
=
and the output power is proportional to sinδ Since sin 11.4° =0.198, and sin 90° =1.00, the static stability limit is about 5 times the current output power of the generator
5-6 A 480-V 400-kVA 0.85-PF-lagging 50-Hz four-pole ∆-connected generator is driven by a 500-hp diesel
engine and is used as a standby or emergency generator This machine can also be paralleled with the normal power supply (a very large power system) if desired
(a) What are the conditions required for paralleling the emergency generator with the existing power
system? What is the generator’s rate of shaft rotation after paralleling occurs?
Trang 5(b) If the generator is connected to the power system and is initially floating on the line, sketch the resulting
magnetic fields and phasor diagram
(c) The governor setting on the diesel is now increased Show both by means of house diagrams and by
means of phasor diagrams what happens to the generator How much reactive power does the generator supply now?
(d) With the diesel generator now supplying real power to the power system, what happens to the generator
as its field current is increased and decreased? Show this behavior both with phasor diagrams and with house diagrams
SOLUTION
(a) To parallel this generator to the large power system, the required conditions are:
1 The generator must have the same voltage as the power system
2 The phase sequence of the oncoming generator must be the same as the phase sequence of the
power system
3 The frequency of the oncoming generator should be slightly higher than the frequency of the
running system
4 The circuit breaker connecting the two systems together should be shut when the above conditions
are met and the generator is in phase with the power system
After paralleling, the generator’s shaft will be rotating at
120 50 Hz 120
1500 r/min 4
e m
f n
P
(b) The magnetic field and phasor diagrams immediately after paralleling are shown below:
I
E
A
jX
S I
A
B
R
B
S
B
net
(c) When the governor setpoints on the generator are increased, the emergency generator begins to supply
more power to the loads, as shown below:
I
E
A
jX
S I
A
f e
P
1
P
sys
P
G
Note that as the load increased with EA constant, the generator began to consume a small amount of reactive power
(d) With the generator now supplying power to the system, an increase in field current increases the
reactive power supplied to the loads, and a decrease in field current decreases the reactive power supplied
to the loads
Trang 6120
V φ
EA1
jX
S I
A
Q
sys
Q
1
Q
3
E
A3
IA3
IA2
I
A1
V φ
E
A1
jX
S I
A
Q
sys
Q
2
Q
1
E
A2
I
A2
IA1
V T
V T
5-7 A 13.8-kV 10-MVA 0.8-PF-lagging 60-Hz two-pole Y-connected steam-turbine generator has a
synchronous reactance of 12 Ω per phase and an armature resistance of 1.5 Ω per phase This generator is operating in parallel with a large power system (infinite bus)
(a) What is the magnitude of E A at rated conditions?
(b) What is the torque angle of the generator at rated conditions?
(c) If the field current is constant, what is the maximum power possible out of this generator? How much
reserve power or torque does this generator have at full load?
(d) At the absolute maximum power possible, how much reactive power will this generator be supplying or
consuming? Sketch the corresponding phasor diagram (Assume I F is still unchanged.)
SOLUTION
(a) The phase voltage of this generator at rated conditions is
13,800 V
7967 V 3
The armature current per phase at rated conditions is
10, 000, 000 VA
418 A
A
T
S I
V
Therefore, the internal generated voltage at rated conditions is
E =Vφ+ I + I
7967 0 1.5 418 36.87 A 12.0 418 36.87 A
12,040 17.6 V
A
Trang 7The magnitude of E A is 12,040 V
(b) The torque angle of the generator at rated conditions is δ = 17.6°
(c) Ignoring R A , the maximum output power of the generator is given by
MAX
3 3 7967 V 12,040 V
24.0 MW
12
A
S
V E P
X
φ
Ω The power at maximum load is 8 MW, so the maximum output power is three times the full load output power
(d) The phasor diagram at these conditions is shown below:
jX
S I
A
V φ
I
A
E
A
I
A
R
A
Under these conditions, the armature current is
12,040 90 V - 7967 0 V
1194 40.6 A 1.5 12.0
A A
E V
The reactive power produced by the generator at this point is
3 A sin 3 7967 V 1194 A sin 0 40.6 18.6 MVAR
The generator is actually consuming reactive power at this time
5-8 A 480-V, 100-kW, two-pole, three-phase, 60-Hz synchronous generator’s prime mover has a no-load speed
of 3630 r/min and a full-load speed of 3570 r/min It is operating in parallel with a 480-V, 75-kW, four-pole, 60-Hz synchronous generator whose prime mover has a no-load speed of 1800 r/min and a full-load speed of 1785 r/min The loads supplied by the two generators consist of 100 kW at 0.85 PF lagging
(a) Calculate the speed droops of generator 1 and generator 2
(b) Find the operating frequency of the power system
(c) Find the power being supplied by each of the generators in this system
(d) If V T is 460 V, what must the generator’s operators do to correct for the low terminal voltage?
SOLUTION The no-load frequency of generator 1 corresponds to a frequency of
nl1
3630 r/min 2
60.5 Hz
m
n P
The full-load frequency of generator 1 corresponds to a frequency of
Trang 8122
fl1
3570 r/min 2
59.5 Hz
m
n P
The no-load frequency of generator 2 corresponds to a frequency of
nl2
1800 r/min 4
60.00 Hz
m
n P
The full-load frequency of generator 2 corresponds to a frequency of
fl2
1785 r/min 4
59.50 Hz
m
n P
(a) The speed droop of generator 1 is given by
nl fl 1
fl
3630 r/min 3570 r/min
3570 r/min
n
The speed droop of generator 2 is given by
nl fl 2
fl
1800 r/min 1785 r/min
1785 r/min
n
(b) The power supplied by generator 1 is given by
1 P1 nl1 sys
P =s f − f
and the power supplied by generator 1 is given by
2 P2 nl2 sys
P =s f − f
The power curve’s slope for generator 1 is
1
nl fl
0.1 MW
0.1 MW/Hz 60.5 Hz 59.5 Hz
P
P s
The power curve’s slope for generator 1 is
2
nl fl
0.075 MW
0.150 MW/Hz 60.00 Hz 59.50 Hz
P
P s
The no-load frequency of generator 1 is 60.5 Hz and the no-load frequency of generator 2 is 60 Hz The total power that they must supply is 100 kW, so the system frequency can be found from the equations
LOAD 1 2
P = + P P
LOAD P1 nl1 sys P2 nl2 sys
100 kW= 0.1 MW/Hz 60.5 Hz− f + 0.15 MW/Hz 60.0 Hz− f
100 kW=6050 kW− 0.10 MW/Hz f +9000 kW− 0.15 MW/Hz f
(0.25 MW/Hz)fsys =6050 kW+9000 kW 100 kW− sys
14,950 kW
59.8 Hz 0.25 MW/Hz
(c) The power supplied by generator 1 is
Trang 9( ) ( )( )
1 P1 nl1 sys 0.1 MW/Hz 60.5 Hz 59.8 Hz 70 kW
The power supplied by generator 2 is
2 P2 nl2 sys 0.15 MW/Hz 60.0 Hz 59.8 Hz 30 kW
(d) If the terminal voltage is 460 V, the operators of the generators must increase the field currents on
both generators simultaneously That action will increase the terminal voltages of the system without changing the power sharing between the generators
5-9 Three physically identical synchronous generators are operating in parallel They are all rated for a full
load of 3 MW at 0.8 PF lagging The no-load frequency of generator A is 61 Hz, and its speed droop is 3.4 percent The no-load frequency of generator B is 61.5 Hz, and its speed droop is 3 percent The no-load frequency of generator C is 60.5 Hz, and its speed droop is 2.6 percent
(a) If a total load consisting of 7 MW is being supplied by this power system, what will the system
frequency be and how will the power be shared among the three generators?
(b) Create a plot showing the power supplied by each generator as a function of the total power supplied to
all loads (you may use MATLAB to create this plot) At what load does one of the generators exceed its ratings? Which generator exceeds its ratings first?
(c) Is this power sharing in (a) acceptable? Why or why not?
(d) What actions could an operator take to improve the real power sharing among these generators?
SOLUTION
(a) Speed droop is defined as
fl SD
1 100
f
f =
+ Thus, the full-load frequencies of generators A, B, and C are
nl,A fl,A
A
61 Hz
59.0 Hz
f
nl,B fl,B
B
61.5 Hz
59.71 Hz
f
nl,C fl,C
C
60.5 Hz
58.97 Hz
f
and the slopes of the power-frequency curves are:
3 MW
1.5 MW/Hz
2 Hz
PA
3 MW
1.676 MW/Hz 1.79 Hz
PB
3 MW
1.961 MW/Hz 1.53 Hz
PC
Trang 10124
(a) The total load is 7 MW, so the system frequency is
LOAD PA nlA sys PB nlB sys PC nlC sys
7 MW= 1.5 61.0−f + 1.676 61.5− f + 1.961 60.5−f
7 MW=91.5 1.5− f +103.07 1.676− f +118.64 1.961− f
sys
5.137f =306.2
sys 59.61 Hz
f = The power supplied by each generator will be
( nlA sys) (1.5 MW/Hz 61.0 Hz)( 59.61 Hz) 2.09 MW
( nlB sys) (1.676 MW/Hz 61.5 Hz)( 59.61 Hz) 3.17 MW
B PB
( nlC sys) (1.961 MW/Hz 60.5 Hz)( 59.61 Hz) 1.74 MW
C PC
(b) The equation in part (a) can be re-written slightly to express system frequency as a function of load
LOAD 1.5 61.0 sys 1.676 61.5 sys 1.961 60.5 sys
LOAD 91.5 1.5sys 103.07 1.676 sys 118.64 1.961 sys
5.137f =313.2−P
LOAD sys
313.2 5.137
P
=
A MATLAB program that uses this equation to determine the power sharing among the generators as a function of load is shown below:
% M-file: prob5_9b.m
% M-file to calculate and plot the power sharing among
% three generators as a function of load
% Define values for this generator
fnlA = 61.0; % No-load freq of Gen A
fnlB = 61.5; % No-load freq of Gen B
fnlC = 60.5; % No-load freq of Gen C
spA = 1.5; % Slope of Gen A (MW/Hz)
spB = 1.676; % Slope of Gen B (MW/Hz)
spC = 1.961; % Slope of Gen C (MW/Hz)
Pload = 0:0.05:10; % Load in MW
% Calculate the system frequency
fsys = (313.2 - Pload) / 5.137;
% Calculate the power of each generator
PA = spA * ( fnlA - fsys);
PB = spB * ( fnlB - fsys);
PC = spC * ( fnlC - fsys);
% Plot the power sharing versus load
plot(Pload,PA,'b-','LineWidth',2.0);
Trang 11hold on;
plot(Pload,PB,'k ','LineWidth',2.0);
plot(Pload,PC,'r-.','LineWidth',2.0);
plot([0 10],[3 3],'k','LineWidth',1.0);
plot([0 10],[0 0],'k:');
title ('\bfPower Sharing Versus Total Load');
xlabel ('\bfTotal Load (MW)');
ylabel ('\bfGenerator Power (MW)');
legend('Generator A','Generator B','Generator C','Power Limit');
grid on;
hold off;
The resulting plot is shown below:
This plot reveals that there are power sharing problems both for high loads and for low loads Generator B
is the first to exceed its ratings as load increases Its rated power is reached at a total load of 6.45 MW
On the other hand, Generator C gets into trouble as the total load is reduced When the total load drops to 2.4 MW, the direction of power flow reverses in Generator C
(c) The power sharing in (a) is not acceptable, because Generator 2 has exceeded its power limits
(d) To improve the power sharing among the three generators in (a) without affecting the operating
frequency of the system, the operator should decrease the governor setpoints on Generator B while simultaneously increasing them in Generators A and C
5-10 A paper mill has installed three steam generators (boilers) to provide process steam and also to use some its
waste products as an energy source Since there is extra capacity, the mill has installed three 5-MW turbine generators to take advantage of the situation Each generator is a 4160-V 6250-kVA 0.85-PF-lagging two-pole Y-connected synchronous generator with a synchronous reactance of 0.75 Ω and an armature resistance of 0.04 Ω Generators 1 and 2 have a characteristic power-frequency slope s P of 2.5 MW/Hz, and generators 2 and 3 have a slope of 3 MW/Hz
(a) If the no-load frequency of each of the three generators is adjusted to 61 Hz, how much power will the
three machines be supplying when actual system frequency is 60 Hz?