60313626 power system analysis lab manual
TRANSCRIPT
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
POWER SYSTEM ANALYSIS
SUBMITTED TO:
ENGR.M.JUNAID
SUBMITTED BY:
ASAD NAEEM
2006-RCET-EE-22
DEPARTMENT OF ELECTRICAL ENGINEERING (A CONSTITUENT COLLEGE: RACHNA COLLEGE OF ENGINEERING &
TECHNOLOGY GUJRANWALA) UNIVERSITY OF ENGINEERING & TECHNOLOGY LAHORE, PAKISTAN
POWER SYSTEM ANALYSIS LAB MANUAL
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01 To plot the daily load curve for the given data using MATLAB
02 Introduction to basics of Electrical Transients Analyzer Program (ETAP)
03 Evaluate the value of voltages for a 4-BUS system using node equations in MATLAB
04 Modeling and Load flow analysis of RCET power distribution network using ETAP
05 Bus elimination of a 4-BUS system using MATLAB
06 To study the Concept of Modifications of an Existing Bus-
Impedance Matrix & Implementing in MATLAB
07 Application of Gauss-Siedal and Newton-Raphson method for load flow studies on a three bus system using MATLAB
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08 Harmonic Load Modeling using built-in and user defined
models of ETAP
09 Impact of personal computer load on power distribution network of RCET
10 Flow of triplen harmonics (zero-sequence harmonics) during 5 different schemes of connection for a 3-phase transformer with
presence of large non-linear load using ETAP
11 Three phase short circuit analysis (3-phase faults-device duty) for a given power system using ETAP
12 Three phase short circuit analysis (3-phase faults-30 cycle
network) for a given power system using ETAP
13 Three phase short circuit analysis (LG, LL, LLG, & 3-Phase Faults - ½ Cycle) for a given power system using ETAP
14 Three phase short circuit analysis (LG, LL, LLG, & 3-Phase
Faults - 1.5 to 4 Cycle) for a given power system using ETAP
15 Three phase short circuit analysis (LG, LL, LLG, & 3-Phase Faults - 30 Cycle) for a given power system using ETAP
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EXPERIMENT#01
To plot the daily load curve for the given data using MATLAB
Given data:
Interval from To Load MW12 A.M 2 A.M 62 6 56 9 109 12 1512 P.M 2 P.M 122 4 144 6 166 8 188 10 1610 11 1211 12 A.M 6
Requirements:
1. Find average value of load 2. Find peak value of load 3. Find the load factor 4. Plot the load curve
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Theory Loads:
Loads of power systems are divided into three main categories that are given below.
1. Industrial Loads 2. Commercial Loads 3. Residential Loads
Very large industrial loads are served through the transmission lines. Large industrial loads are served directly from the sub-transmission level. And small industrial loads are served directly from the primary distribution network. The industrial loads are composite loads and induction motors from a high proportion of these loads. These composite loads are functions of voltage and frequency and form a major part of the system load. Commercial and residential load consist largely of lighting, heating and cooling. These loads are independent of frequency and consume negligibly small reactive power.
The real power of loads is expressed in terms of kilowatts or megawatts. The magnitude of load varies throughout the day and power must be available to the consumer on demand.
The daily load curve of a utility is a composite of demands made by various classes of users. The greatest value of load during a twenty four hours is called the peak or maximum demand. Smaller peaking generators may be commissioned to meet the peak load that occurs for only a few hours. In order to asses the usefulness of the generating plant the load factor is defined.
The load factor is the ratio of average load over a designated period of time to the peak load occurring in that period. Load factor may be given for a day, a month or an year. Yearly or annual load factor is the most useful since a year represents a full cycle of time. The daily load factor is
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Daily load factor = average load / peak load
Multiplying the numerator and denominator by a time period of 24 hr we have
Daily load factor= average load*24 hr / (peak load*24 hrs)
= energy consumed during 24 hr/ (peak load*24 hr)
The annual load factor is
Annual load factor = total annual energy / (peak load*8760 hr)
Today’s typical system load factors are in range of 55-70%. In Pakistan WAPDA standard for urban areas load factor is 60% and that of rural areas is 65%.
Matlab code:
data=[0 2 6;
2 6 5;
6 9 10;
9 12 15;
12 14 12;
14 16 14;
16 18 16;
18 20 18;
20 22 16;
22 23 12;
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23 24 6];
p=data(:,3);
Dt=data(:,2)-data(:,1);
w=p'*Dt;
pavg=w/sum(Dt)
peak=max(p)
LF=pavg/peak*100
L=length(data);
tt = [data(:,1) data(:,2)];
t = sort(reshape(tt, 1, 2*L));
for n = 1:L
pp(2*n-1)=p(n);
pp(2*n)=p(n);
end
plot(t,pp)
xlabel('TIME,Hr'),ylabel('P,MW')
Matlab results:
pavg =11.5417
peak =18
LF =64.1204
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0 5 10 15 20 254
6
8
10
12
14
16
18
TIME,Hr
P,M
W
COMMENTS:
In this experiment we learn how to find the daily load curve for any power system using MATLAB. Load curve is very important as we can achieve very important information from it like:
• Peak load • Average load • Load factor
These quantities are very helpful for understanding any power system.
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EXPERIMENT#02
Introduction to basics of Electrical Transients Analyzer Program (ETAP)
What is ETAP?
ETAP is the most comprehensive analysis platform for the design, simulation, operation, control, optimization, and automation of generation, transmission, distribution, and industrial power systems.
Project Toolbar The Project Toolbar contains icons that allow you to perform shortcuts of many commonly used functions in PowerStation.
Create Create a new project file
Open Open an existing project file
Save Save the project file
Print Print the one‐line diagram or U/G raceway system
Cut Cut the selected elements from the one‐line diagram or U/G raceway system to the Dumpster
Copy Copy the selected elements from the one‐line diagram or U/G raceway system to the Dumpster
Paste Paste elements from a Dumpster Cell to the one‐line diagram or U/G raceway system
Zoom In Magnify the one‐line diagram or U/G raceway system
Zoom Out Reduce the one‐line diagram or U/G raceway system
Zoom to Fit Page Re‐size the one‐line diagram to fit the window
Check Continuity Check the system continuity for non‐energized elements
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Power Calculator Activate PowerStation Calculator that relates MW, MVAR, MVA, kV, Amp, and PF together with either kVA or MVA units
Help Point to a specific area to learn more about PowerStation
Mode Toolbar ETAP offers a suite of fully integrated software solutions including arc flash, load flow, short circuit, transient stability, relay coordination, cable ampacity, optimal power flow, and more. Its modular functionality can be customized to fit the needs of any company, from small to large power systems.
Edit Mode Edit mode enables you to build your one‐line diagram, change system connections, edit engineering properties, save your project, and generate schedule reports in Crystal Reports formats. The Edit Toolbars for both AC and DC elements will be displayed to the right of the screen when this mode is active. This mode provides a wide variety of tasks including:
∙ Drag & Drop Elements ∙ Connect Elements ∙ Change IDs ∙ Cut, Copy, & Paste Elements ∙ Move from Dumpster ∙ Insert OLE Objects ∙ Cut, Copy & OLE Objects ∙ Merge PowerStation Project ∙ Hide/Show Groups of Protective Devices ∙ Rotate Elements ∙ Size Elements ∙ Change Symbols ∙ Edit Properties ∙ Run Schedule Report Manager
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
Example implementation:
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EXPERIMENT#03
Evaluate the value of voltages for a 4BUS system using node equations in MATLAB
GIVEN ONE LINE DIAGRAM
REACTANCE DIAGRAM
In the first step, we draw the reactance diagram of the given one-line diagram as shown below:
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SOURCE TRANSFORM
• After making the reactance diagram, we apply source transformation on the given network by replacing the voltage sources with current sources
• Replace all the reactance by admittances using the relation:
• Y=1/X • The resultant diagram now can be shown as:
NODE EQUATIONS
Now, using the above figure write the node equations of the system:
• Applying KCL at node-1:
I1= (V1-0) y10 + (V1-V4) y14+ (V1-V3) y13
I1= (y10+y14+y13) V1 + 0V2 + (-y13) V3+ (-y14) V4
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• Applying KCL at node-2:
I2= (V2-0) y20 + (V2-V3) y23+ (V2-V4) y24
I2= 0V1+ (y20+y23+y24) V2 + (-y23) V3+ (-y24) V4
• Applying KCL at node-3:
I3= (V3-0) y30 + (V3-V1) y31+ (V3-V4) y34 + (V3-V2) y32
I3= (-y31) V1+ (-y32) V2+ (y30+y31+y34) V3 + (-y34) V4
• Applying KCL at node-4:
0= (V4-V1) y14+ (V4-V3) y43 + (V4-V2) y42
0= (-y14) V1+ (-y42) V2 + (-y34) V3+ (y14+y43+y42) V4
Matrix form of the node equations is:
Where:
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CALCULATIONS
MATLAB CODE
YBUS= [0-9.80i 0 0+4.00i 0+5.00i;
0 0-8.30i 0+2.50i 0+5.00i;
0+4.00i 0+2.50i 0-15.30i 0+8.00i;
0+5.00i 0+5.00i 0+8.00i 0-18.00i];
I= [0-1.20i; 0-0.7200-0.9600i; 0-1.2000i; 0];
ZBUS=inv (YBUS);
V=ZBUS*I
MATLAB RESULTS
V =
1.4111 - 0.2668i
1.3831 - 0.3508i
1.4059 - 0.2824i
1.4010 - 0.2971i
POWER SYSTEM ANALYSIS LAB MANUAL
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COMMENTS:
In this experiment we learn that using the bus impedance or admittance matrix we can find the voltages and currents for all buses of a given power system.
Moreover, we use MATLAB for the calculation of these quantities by just entering the bus impedance matrix and one given quantity (current or voltage) and MATLAB gives the results of very complex networks within no time.
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EXPERIMENT#04
Modeling and Load flow analysis of RCET power distribution network using ETAP INTRODUCTION:
LOAD FLOW STUDIES
In power engineering, the power flow study (also known as load-flow study) is an important tool involving numerical analysis applied to a power system. Unlike traditional circuit analysis, a power flow study usually uses simplified notation such as a one-line diagram and per-unit system, and focuses on various forms of AC power (i.e: reactive, real, and apparent) rather than voltage and current. It analyses the power systems in normal steady-state operation. There exist a number of software implementations of power flow studies.
The great importance of power flow or load-flow studies is in the planning the future expansion of power systems as well as in determining the best operation of existing systems. The principal information obtained from the power flow study is the magnitude and phase angle of the voltage at each bus and the real and reactive power flowing in each line.
LOAD FLOW STUDIES IN ETAP
ETAP load flow analysis software calculates bus voltages, branch power factors, currents, and power flows throughout the electrical system. ETAP allows for swing, voltage regulated, and unregulated power sources with multiple power grids and generator connections. It is capable of performing analysis on both radial and loop systems. ETAP
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allows you to select from several different methods in order to achieve the best calculation efficiency and accuracy.
Run Load Flow Studies
Update Cable Load Currents
Load Flow display Option
Alert View
Report Manager
Halt current calculations
Net on line data
STEPS
Modeling of the main network Modeling of composite networks Running of load flow analysis Complete report from ETAP load flow analyzer
POWER SYSTEM ANALYSIS LAB MANUAL
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MODELING OF BASIC RCET NETWORK
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MODELING OF COMPOSITE NETWORKS
STAFF COLONY:
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OLD BUILDING:
NEW BUILDING:
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HOSTEL-A,B:
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HOSTEL-E:
Complete ETAP load flow analysis report of the given network is attached with this experiment.
COMMENTS:
In this experiment we learn how to:
• Model a power system in ETAP • Model composite networks in a basic network • Assign properties of components added • Study the load flow analysis for that network
POWER SYSTEM ANALYSIS LAB MANUAL
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EXPERIMENT#05
Bus elimination of a 4BUS system using MATLAB
REACTANCE DIAGRAM
It is given that the transformer and generator at bus-3 are disconnected, so the reactance diagram now becomes:
SOURCE TRANSFORM
• After making the reactance diagram, we apply source transformation on the given network by replacing the voltage sources with current sources
• Replace all the reactance by admittances using the relation:
• Y=1/X • The resultant diagram now can be shown as:
POWER SYSTEM ANALYSIS LAB MANUAL
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Part‐1: Elimination of Bus‐3&4
MATRIX FORM
Where:
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MATLAB CODE
>>YBUS= [0-9.80i 0 0+4.00i 0+5.00i;
0 0-8.30i 0+2.50i 0+5.00i;
0+4.00i 0+2.50i 0-14.5i 0+8.00i;
0+5.00i 0+5.00i 0+8.00i 0-18.00i];
>>K= [0-9.80i 0; 0 0-8.30i];
>>L= [0+4.00i 0+5.00i; 0+2.50i 0+5.00i];
>>M= [0-14.5i 0+8.00i; 0+8.00i 0-18.00i];
>>LT= [0+4.00i 0+2.50i; 0+5.00i 0+5.00i];
>>N=inv (M);
>>P=L*N*LT;
>>Ybus=K-P
MATLAB RESULTS
Ybus =
0 - 4.8736i 0 + 4.0736i
0 + 4.0736i 0 - 4.8736i
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Part-2: Elimination Bus-4
MATLAB CODE:
>>Ybus=[-9.8i 0 4.0i 5i;
0 -8.3i 2.5i 5i;
4i 2.5i -14.5i 8i;
5i 5i 8i -18i];
>>K=[-9.8i 0 4i;0 -8.3i 2.5i;4i 2.5i -14.5i];
>>L=[5i;5i;8i];
>>M=[-18i];
>>P=L';
>>T=inv(M);
>>A=K-L*T*P
MATLAB RESULTS
A=
0 -11.1889i 0 - 1.3889i 0 + 1.7778i
0 - 1.3889i 0 - 9.6889i 0 + 0.2778i
0 + 1.7778i 0 + 0.2778i 0 -18.0556i
Part-3: Elimination Bus-3
MATLAB CODE:
>>P=[-11.1889i -1.3889i;-1.3889i -9.6889i];
>>Q=[1.7778i;0.2778i];
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>>R=[-18.0556i];
>>S=Q';
>>T=inv(R);
>>B=P-Q*T*S
MATLAB RESULTS
B =
0 -11.3639i 0 - 1.4163i
0 - 1.4163i 0 - 9.6932i
COMMENTS:
Bus impedance matrix is a very important tool for the calculation of voltages and currents at all the buses of a given network. Suppose that any fault occurs in the power system then we can get a task to modify the bus impedance matrix by eliminating the faulty node which will reduce the order of matrix by eliminating the faulty node.
In this experiment we learn how to:
• Eliminate last two nodes together • Eliminate only one last node
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EXPERIMENT#06
To study the Concept of Modifications of an Existing BusImpedance Matrix & Implementing in MATLAB
IMPEDANCE MATRIX
Impedance matrix is a very important tool in power system analysis. Using this matrix we can find:
• Voltages at all buses when currents are given • Currents at all buses when voltages are given
So it is very important that how to modify the bus impedance matrix when any new impedance is add into the original system.
Suppose a power system with n-buses having the impedances matrix of order n*n:
There are four cases that can take place while adding a new impedance Zb in the system:
• Adding Zb from a new bus-P to reference bus • Adding Zb from a new bus-P to an existing bus-K • Adding Zb from an existing bus-K to reference bus • Adding Zb between two existing buses
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MODIFICATION CASES
CASE‐1: ADDING Zb FROM A NEW BUS TO REFERENCE BUS
This condition is explained in the following diagram:
Clearly,
Vp-0=Ib*Zb
Vp=Ib*Zb
Hence the modified matrix will take the form as:
MATLAB CODE
function [Z]=Case1(Zorg,Zb)
Zorg=[1 2 3 4;2 5 6 7;3 6 8 9;4 7 9 10]
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Zb=17;
l=length(Zorg);
for i=1:l+1
for j=1:l+1
if i<=l && j<=l
Znew(i,j)=Zorg(i,j);
elseif i==l+1 && j==l+1
Znew(i,j)=Zb;
else
Znew(i,j)=0;
end
end
end
Znew
MATLAB RESULTS
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CASE‐2: ADDING Zb FROM A NEW BUS‐P TO AN EXISTING BUS‐K
This condition is explained in the following diagram:
Clearly,
Vp-Vk,new=Ip*Zb
Vp=Vk,new+Ip*Zb
Where,
Vk,new=Vk,org+Ip*Zkk
Vp= Vk,org+Ip(Zkk+Zb)
Hence the modified matrix will take the form as:
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MATLAB CODE:
function [Z]=CASE2(Zorg,Zb) Zorg=[1 2 3 4;2 5 6 7;3 6 8 9;4 7 9 10] Zb=5; l=length(Zorg); row =Zorg(l,:); column =Zorg(:,l); for i=1:l+1 for j=1:l+1 if i<=l && j<=l Znew(i,j)=Zorg(i,j); elseif i==l+1 for p=1:l Znew(i,p)=row(p); end elseif j==l+1 for q=1:l Znew(q,j)=column(q); end end if i==l+1 && j==l+1 Znew(i,j)=Zb+Zorg(l,l); end end end Znew
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MATLAB RESULTS
CASE‐3: ADDING Zb FROM AN EXISTING BUS‐K TO REFERENCE
BUS
This condition is explained in the following diagram:
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Here we can apply the same case as in case-2 and then put Vp=0. This task can be achieved by eliminating the last row and column of the Znew matrix.
Now this matrix is of the order (n+1)*(n+1), we have to achieve a matrix of order n*n using formula:
Zkj(new)=Zkj(org)-(Zk(n+1)Z(n+1)j/Zkk+Zb)
In this case,
K=n
MATLAB CODE:
function [Z]=CASE3(Zorg,Zb)
Zorg=[1 2 3 4;2 5 6 7;3 6 8 9;4 7 9 10]
Zb=5;
l=length(Zorg);
row =Zorg(l,:);
column =Zorg(:,l);
for i=1:l+1
for j=1:l+1
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if i<=l && j<=l
Znew(i,j)=Zorg(i,j);
elseif i==l+1
for p=1:l
Znew(i,p)=row(p);
end
elseif j==l+1
for q=1:l
Znew(q,j)=column(q);
end
end
if i==l+1 && j==l+1
Znew(i,j)=Zb+Zorg(l,l);
end
end
end
Znew
for a=1:l
for b=1:l
K(a,b)=Znew(a,b);
end
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end
for a=1:l
L(a,1)=Znew(a,5);
end
M=Znew(l+1,l+1);
P=L';
T=inv(M);
Zwithnewbusrefferenced=K-L*T*P
MATLAB RESULTS
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CASE‐4: ADDING Zb BETWEEN TWO EXISTING BUSES
This condition is explained in the following diagram:
In this case,
Zbb=Zb+Zjj+Zkk-2Zjk
Hence the modified matrix will take the form as:
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Here again we have to eliminate the last row and column to achieve the final matrix.
MATLAB CODE:
function [Z]=CASE4(Zorg,Zb)
Zorg=[1 2 3 4;2 5 6 7;3 6 8 9;4 7 9 10]
Zb=5;
l=length(Zorg);
R1 =Zorg(l,:);
C1 =Zorg(:,l);
R2 =Zorg(l-1,:);
C2 =Zorg(:,l-1);
for i=1:l+1
for j=1:l+1
if i<=l && j<=l
Znew(i,j)=Zorg(i,j);
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elseif i==l+1
for p=1:l
Znew(i,p)=R1(p)-R2(p);
End
elseif j==l+1
for q=1:l
Znew(q,j)=C1(q)-C2(q);
End
End
if i==l+1 && j==l+1
Znew(i,j)=Zb+Zorg(l,l)+Zorg(l-1,l-1)-(2*Zorg(l,l-1));
end
end
end
Znew
for a=1:l
for b=1:l
K(a,b)=Znew(a,b);
end
end
for a=1:l
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L(a,1)=Znew(a,5);
end
M=Znew(l+1,l+1);
P=L';
T=inv(M);
Zfinal=K-L*T*P
MATLAB RESULTS
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COMMENTS:
Bus impedance matrix is a very important tool for the calculation of voltages and currents at all the buses of a given network. Suppose that any improvement occurs in the power system then we can get a task to modify the bus impedance matrix by adding the new impedance in the system. The new impedance can be added in four different conditions:
• Addition of new impedance from a new bus to reference bus
• Addition of new impedance from a new bus to existing bus
• Addition of new impedance from an existing bus to reference bus
• Addition of new impedance between two existing buses
In this experiment we learn how to modify the bus impedance matrix for all four cases using MATLAB.
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EXPERIMENT#07
Application of GaussSiedal and NewtonRaphson method for load flow studies on a three bus system using MATLAB(Implimentation of example#6.7,6.8 & 6.10 from POWER SYSTEM ANALYSIS by HadiSaadat)
EXAMPLE 6.7
Given figure shows the one line diagram of a simple three bus system with generation at bus-1. The magnitude of voltage at bus-1 is adjusted to 1.05 per unit. The scheduled loads at buses-2 and 3 are as marked on the diagram. Line impedances are marked in per unit on a 100-MVA base and the line charging susceptances are neglected.
(A) Using the Gauss-Siedal method, determine the phasor values of the voltage at the load buses 2 and 3 (P&Q buses) accurate to four decimal places
(B) Find the slack bus real and reactive power (C) Determine the line flows and line losses. Construct a
power flow diagram showing the direction of line flow
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SOLUTION
Line impedances are converted to admittances:
At the P-Q buses, the complex loads expressed in per unit are:
S2sch=-(256.6+j110.2)/100= -2.566-j1.102 pu
S3sch=-(138.6+j45.2)/100= -1.386-j0.452 pu
Starting from an initial estimate of V2(0)=1.0+j0.0 and
V3(0)=1.0+j0.0
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GAUSS-SIEDEL FARMULA
SLACK1=conj(V1)*[V1*(y12+y13)-( y12*V2+y13*V3)] Sij=Vi*conj(Iij) Iij=yij*(Vi-Vj)
MATLAB CODE
y12=10-j*20; y13=10-j*30; y23=16-j*32; V1=1.05+j*0;
%CODE FOR PART-A
iter=0; s2=-2.566-j*1.102; s3=-1.386-j*0.452; V2=1+j*0.0; V3=1+j*0.0; for I=1:10; iter=iter+1; V2=(conj(s2)/conj(V2)+y12*V1+y23*V3)/(y12+y23); V3=(conj(s3)/conj(V3)+y13*V1+y23*V2)/(y13+y23); end V2 V3
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%CODE FOR PART-B
Pslack=conj(V1)*[V1*(y12+y13)-(y12*V2+y13*V3)]
%CODE FOR PART-C I12=y12*(V1-V2) I21=-I12 I13=y13*(V1-V3) I31=-I13 I23=y23*(V2-V3) I32=-I23 s12=V1*conj(I12) s21=V2*conj(I21) s13=V1*conj(I13) s31=V3*conj(I31) s23=V2*conj(I23) s32=V3*conj(I32) SL12=s12+s21 SL13=s13+s31 SL23=s23+s32
MATLAB RESULTS
PART-A RESULTS
V2 =
0.9800 - 0.0600i
V3 =
1.0000 - 0.0500i
PART-B RESULTS
SLACK-BUS POWER
Pslack = 4.0949 - 1.8900i
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PART-C RESULTS
I12 = 1.9000 - 0.8000i
I21 = -1.9000 + 0.8000i
I13 = 2.0000 - 1.0000i
I31 = -2.0000 + 1.0000i
I23 = -0.6400 + 0.4800i
I32 = 0.6400 - 0.4800i
LINE FLOWS
s12 = 1.9950 + 0.8400i
s21 = -1.9100 - 0.6700i
s13 = 2.1000 + 1.0500i
s31 = -2.0500 - 0.9000i
s23 = -0.6560 - 0.4320i
s32 = 0.6640 + 0.4480i
LINE LOSSES
SL12 = 0.0850 + 0.1700i
SL13 = 0.0500 + 0.1500i
SL23 = 0.0080 + 0.0160i
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EXAMPLE 6.8
Given figure shows the one line diagram of a simple three bus system with generators at buses-1 and 3. The magnitude of voltage at bus-1 is adjusted to 1.05pu. voltage magnitude at bus-3 is fixed at 1.04 pu with a real power generation of 200MW. A load consisting of 400MW and 250MVAR is taken from bus-2. Line impedances are marked in per unit on a 100MVA base, and the line charging susceptances are neglected. Obtain the power flow solution by the Gauss-Siedal method including line flows and line losses.
Where,impedances are replaced by admittances as:
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FARMULA’S
S3=conj(V3)*(y33*V3-y13*V1-y23*V2) Q3=-imag(conj(V3)*(y33*V3-y13*V1-y23*V2))
MATLAB CODE
y12=10-j*20; y13=10-j*30; y23=16-j*32; y33=y13+y23; V1=1.05+j*0; format long iter=0; s2=-4.0-j*2.5; p3=2; V2=1+j*0.0; Vm3=1.04; V3=1.04+j*0; for I=1:10; iter=iter+1; E2=V2; E3=V3; V2=(conj(s2)/conj(V2)+y12*V1+y23*V3)/(y12+y23) DV2=V2-E2; Q3=-imag(conj(V3)*(y33*V3-y13*V1-y23*V2)) s3=p3+j*Q3; Vc3=(conj(s3)/conj(V3)+y13*V1+y23*V2)/(y13+y23); Vi3=imag(Vc3); Vr3=sqrt(Vm3^2-Vi3^2);
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V3=Vr3+j*Vi3 DV3=V3-E3; end V2 V3 Q3 format short I12=y12*(V1-V2); I21=-I12; I13=y13*(V1-V3); I31=-I13; I23=y23*(V2-V3); I32=-I23; s12=V1*conj(I12); s21=V2*conj(I21); s13=V1*conj(I13); s31=V3*conj(I31); s23=V2*conj(I23); s32=V3*conj(I32); I1221=[I12,I21]; I1331=[I13,I31]; I2332=[I23,I32]; SL12=s12+s21 SL13=s13+s31 SL23=s23+s32 S1=(s12+s13) S2=(s23+s21) S3=(s31+s32) S12=s12 S21=s21 S13=s13 S31=s31 S23=s23 S32=s32
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MATLAB RESULTS
ITERATION RESULTS:
1ST ITERATION
V2 = 0.974615384615385 - 0.042307692307692i
Q3 = 1.160000000000002
V3 = 1.039987148574197 - 0.005170183798502i
2ND ITERATION
V2 = 0.971057059512953 - 0.043431876337850i
Q3 = 1.387957731052817
V3 = 1.039974378708180 - 0.007300111679686i
3RD ITERATION
V2 = 0.970733708554698 - 0.044791724463619i
Q3 = 1.429040300785471
V3 = 1.039966679445820 - 0.008325001047174i
4TH ITERATION
V2 = 0.970652437281433 - 0.045329920732880i
Q3 = 1.448333275594840
V3 = 1.039963173621928 - 0.008752000354604i
5TH ITERATION
V2 = 0.970623655331095 - 0.045554240372625i
Q3 = 1.456209166612119
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V3 = 1.039961668920058 - 0.008929007616053i
6TH ITERATION
V2 = 0.970612037114234 - 0.045646940090561i
Q3 = 1.459469889628077
V3 = 1.039961037734205 - 0.009002221658867i
7TH ITERATION
V2 = 0.970607253520093 - 0.045685276728252i
Q3 = 1.460818201396914
V3 = 1.039960775170297 - 0.009032502820155i
8TH ITERATION
V2 = 0.970605276281561 - 0.045701131870879i
Q3 = 1.461375872168914
V3 = 1.039960666313617 - 0.009045027392915i
9TH ITERATION
V2 = 0.970604458527297 - 0.045707689707255i
Q3 = 1.461606535170454
V3 = 1.039960621244008 - 0.009050207830587i
10TH ITERATION
V2 = 0.970604120282796 - 0.045710402176455i
Q3 = 1.461701943643423
V3 = 1.039960602594413 - 0.009052350604469i
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FINAL RESULTS:
V2 = 0.970604120282796 - 0.045710402176455i
V3 = 1.039960602594413 - 0.009052350604469i
Q3 = 1.461701943643423
SL12 = 0.0839 + 0.1679i
SL13 = 0.0018 + 0.0055i
SL23 = 0.0985 + 0.1969i
S1 = 2.1841 + 1.4085i
S2 = -3.9999 - 2.5000i
S3 = 2.0000 + 1.4618i
S12 = 1.7936 + 1.1874i
S21 = -1.7096 - 1.0195i
S13 = 0.3906 + 0.2212i
S31 = -0.3887 - 0.2157i
S23 = -2.2903 - 1.4805i
S32 = 2.3888 + 1.6775i
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EXAMPLE 6.10
Given figure shows the one line diagram of a simple three bus system with generators at buses-1 and 3. The magnitude of voltage at bus-1 is adjusted to 1.05pu. voltage magnitude at bus-3 is fixed at 1.04 pu with a real power generation of 200MW. A load consisting of 400MW and 250MVAR is taken from bus-2. Line impedances are marked in per unit on a 100MVA base, and the line charging susceptances are neglected. Obtain the power flow solution by the Newton-Raphson method including line flows and line losses.
Where,impedances are replaced by admittances as:
The bus impedance matrix can be constructed as:
YBUS=[20-j50 -10+j20 -10+j30
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-10+j20 26-j52 -16+j32
-10+j30 -16+j32 26-j62];
FARMULA’S
P1=V1^2*Y11*cos(Ѳ11)+V1*V2*Y12*cos(Ѳ12-d1+d2)+... V1*V3*Y13*cos(Ѳ13-d1+d3) Q1=-V1^2*Y11*sin(Ѳ11)-V1*V2*Y12*sin(Ѳ12-d1+d2)-... V1*V3*Y13*sin(Ѳ13-d1+d3) Q3=-V3*V1*Y31*sin(Ѳ31)-d3+d1)-V3*V2*Y32*... sin(Ѳ32-d3+d2)-V3^2*Y33*sinѲ33
MATLAB CODE V=[1.05;1.0;1.04]; d=[0;0;0]; Ps=[-4;2.0]; Qs=-2.5; YB=[20-j*50 -10+j*20 -10+j*30 -10+j*20 26-j*52 -16+j*32 -10+j*30 -16+j*32 26-j*62]; Y=abs(YB); t=angle(YB); iter=0; pwracur=0.00025; %power accuracy DC=10; %set the maximun power residue to a high value while max(abs(DC))>pwracur iter=iter+1 P=[V(2)*V(1)*Y(2,1)*cos(t(2,1)-d(2)+d(1))+V(2)^2*Y(2,2)*cos(t(2,2))+... V(2)*V(3)*Y(2,3)*cos(t(2,3)-d(2)+d(3)); V(3)*V(1)*Y(3,1)*cos(t(3,1)-d(3)+d(1))+V(3)^2*Y(3,3)*cos(t(3,3))+... V(3)*V(2)*Y(3,2)*cos(t(3,2)-d(3)+d(2))];
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Q=-V(2)*V(1)*Y(2,1)*sin(t(2,1)-d(2)+d(1))-V(2)^2*Y(2,2)*sin(t(2,2))-... V(2)*V(3)*Y(2,3)*sin(t(2,3)-d(2)+d(3)); J(1,1)=V(2)*V(1)*Y(2,1)*sin(t(2,1)-d(2)+d(1))+... V(2)*V(3)*Y(2,3)*sin(t(2,3)-d(2)+d(3)); J(1,2)=-V(2)*V(3)*Y(2,3)*sin(t(2,3)-d(2)+d(3)); J(1,3)=V(1)*Y(2,1)*cos(t(2,1)-d(2)+d(1))+2*V(2)*Y(2,2)*cos(t(2,2))+... V(3)*Y(2,3)*cos(t(2,3)-d(2)+d(3)); J(2,1)=-V(3)*V(2)*Y(3,2)*sin(t(3,2)-d(3)+d(2)); J(2,2)=V(3)*V(1)*Y(3,1)*sin(t(3,1)-d(3)+d(1))+... V(3)*V(2)*Y(3,2)*sin(t(3,2)-d(3)+d(2)); J(2,3)=V(3)*Y(2,3)*cos(t(3,2)-d(3)+d(2)); J(3,1)=V(2)*V(1)*Y(2,1)*cos(t(2,1)-d(2)+d(1))+... V(2)*V(3)*Y(2,3)*cos(t(2,3)-d(2)+d(3)); J(3,2)=-V(2)*V(3)*Y(2,3)*cos(t(2,3)-d(2)+d(3)); J(3,3)=-V(1)*Y(2,1)*sin(t(2,1)-d(2)+d(1))-2*V(2)*Y(2,2) *sin(t(2,2)) ... V(3)*Y(2,3)*sin(t(2,3)-d(2)+d(3)); DP=Ps-P; DQ=Qs-Q; DC=[DP;DQ] J DX=J\DC d(2)=d(2)+DX(1); d(3)=d(3)+DX(2); V(2)=V(2)+DX(3); V, d, delta=180/pi*d; end P1=V(1)^2*Y(1,1)*cos(t(1,1))+V(1)*V(2)*Y(1,2)*cos(t(1,2)- d(1)+d(2))+... V(1)*V(3)*Y(1,3)*cos(t(1,3)-d(1)+d(3)) Q1=-V(1)^2*Y(1,1)*sin(t(1,1))-V(1)*V(2)*Y(1,2)*sin(t(1,2)-d(1)+d(2))-... V(1)*V(3)*Y(1,3)*sin(t(1,3)-d(1)+d(3)) Q3=-V(3)*V(1)*Y(3,1)*sin(t(3,1)-d(3)+d(1))-V(3)*V(2)*Y(3,2)*... sin(t(3,2)-d(3)+d(2))-V(3)^2*Y(3,3)*sin(t(3,3))
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MATLAB RESULTS
1ST ITERATION DC =
-2.8600
1.4384
-0.2200
J =
54.2800 -33.2800 24.8600
-33.2800 66.0400 -16.6400
-27.1400 16.6400 49.7200
DX =
-0.0453
-0.0077
-0.0265
V =
1.0500
0.9735
1.0400
d = 0
-0.0453
-0.0077
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2ND ITERATION
DC = -0.0992
0.0217
-0.0509
J =
51.7247 -31.7656 21.3026
-32.9816 65.6564 -15.3791
-28.5386 17.4028 48.1036
DX =
-0.0018
-0.0010
-0.0018
V =
1.0500
0.9717
1.0400
d =
0
-0.0471
-0.0087
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3RD ITERATION
DC =
1.0e-003 *
-0.2166
0.0382
-0.1430
J =
51.5967 -31.6939 21.1474
-32.9339 65.5976 -15.3516
-28.5482 17.3969 47.9549
DX =
1.0e-005 *
-0.3856
-0.2386
-0.4412
V =
1.0500
0.9717
1.0400
d = 0
-0.0471
-0.0087
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FINAL RESULTS:
P1 =
2.1842
Q1 =
1.4085
Q3 =
1.4618
COMMENTS:
Power system calculations are mostly very complex for large power systems. To analyze such power systems, there are two very important iterative methods:
• Gauss Siedel Method • Newton Raphson method
In this experiment we learn how to apply these two methods using MATLAB.
Gauss-Seidel iteration has two advantages:
• Errors do not accumulate during the calculation. If the procedure converges, it approaches the correct answer without rounding errors such as can occur during inversion of large matrices.
• The method can be used for nonlinear sets of equations.
While Newton Raphson method is readily applied to non-linear equations, and can use finite-difference estimates of the derivatives to evaluate the gradients.
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EXPERIMENT#08
Harmonic Load Modeling using builtin and user defined models of ETAP
HARMONIC ANALYSIS
Because of the wide and ever increasing applications of power electronic devices, such as variable speed drives, uninterruptible power supplies (UPS), static power converters, etc., power system voltage and current quality has been severely affected in some areas. In these areas components other than that of fundamental frequency can be found to exist in the distorted voltage and current waveforms. These components usually are the integer multipliers of the fundamental frequency, called harmonics. In addition to electronic devices, some other non‐linear loads, or devices including saturated transformers, arc furnaces, fluorescent lights, and cycloconverters are also responsible for the deterioration in power system quality.
HARMONIC SOURCES
The following components can be modeled as a harmonic voltage source in PowerStation:
• Power Grid • Synchronous Generator • Inverter • Charger/Converter
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• Static Load
IMPORTANT DEFINITIONS
Transients
The term transient has long been used in the analysis of power system variations to denote an event that is undesirable and momentary in nature. Transient is “that part of the change in a variable that disappears during transition from one steady state operating condition to another.”
Impulsive transient
An impulsive transient is a sudden; non–power frequency change in the steady‐state condition of voltage, current, or both that is unidirectional in polarity (primarily either positive or negative).
Oscillatory transient
An oscillatory transient is a sudden, non–power frequency change in the steady‐state condition of voltage, current, or both, that includes both positive and negative polarity values.
Long-Duration Voltage Variations
Long‐duration variations encompass root‐mean‐square (rms) deviations at power frequencies for longer than 1 minute.
Overvoltage
An overvoltage is an increase in the rms ac voltage greater than 110 percent at the power frequency for duration longer than 1
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min. Over voltages are usually the results of load switching (e.g., switching off a large load or energizing a capacitor bank).
Under voltage
An under voltage is a decrease in the rms ac voltage to less than 90 percent at the power frequency for a duration longer than 1 min. Under voltages are the results of switching events that are the opposite of the events that cause over voltages.
Short-Duration Voltage Variations
This category encompasses the IEC category of voltage dips and short interruptions. Each type of variation can be designated as instantaneous, momentary, or temporary, depending on its duration.
Short‐duration voltage variations are caused by fault conditions, the energization of large loads which require high starting currents, or intermittent loose connections in power wiring.
Interruption
An interruption occurs when the supply voltage or load current decreases to less than 0.1 pu for a period of time not exceeding 1 min.
Sags (dips)
Sag is a decrease to between 0.1 and 0.9 pu in rms voltage or current at the power frequency for durations from 0.5 cycle to 1 min.
Swells
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A swell is defined as an increase to between 1.1 and 1.8 pu in rms voltage or current at the power frequency for durations from 0.5 cycle to 1 min.
Voltage Imbalance
Voltage imbalance (also called voltage unbalance) is sometimes defined as the maximum deviation from the average of the three‐phase voltages or currents, divided by the average of the three‐phase voltages or currents, expressed in percent.
Waveform Distortion
Waveform distortion is defined as a steady‐state deviation from an ideal sine wave of power frequency principally characterized by the spectral content of the deviation.
Harmonics
Harmonics are sinusoidal voltages or currents having frequencies that are integer multiples of the frequency at which the supply system is designed to operate (termed the fundamental frequency usually 50 or 60 Hz).
Interharmonics
Voltages or currents having frequency components that are not integer multiples of the frequency at which the supply system is designed to operate (e.g., 50 or 60 Hz) are called Interharmonics.
Odd harmonics
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Voltages or currents having frequency components that are odd integer multiples of the frequency at which the supply system is designed to operate (e.g., 50 or 60 Hz) are called odd harmonics.
Even harmonics
Voltages or currents having frequency components that are even integer multiples of the frequency at which the supply system is designed to operate (e.g., 50 or 60 Hz) are called even harmonics.
Voltage Fluctuation
Voltage fluctuations are systematic variations of the voltage envelope or a series of random voltage changes, the magnitude of which does not normally exceed the voltage ranges specified by ANSI C84.1 of 0.9 to 1.1 pu.
Power Frequency Variations
Power frequency variations are defined as the deviation of the power system fundamental frequency from it specified nominal value (e.g., 50 or 60 Hz).
Power factor, displacement
The power factor of the fundamental frequency components of the voltage and current waveforms
Power factor (true)
The ratio of active power (watts) to apparent power (volt amperes)
Total harmonic distortion (THD)
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The ratio of the root mean square of the harmonic content to the rms value of the fundamental quantity, expressed as a percent of the fundamental.
Triplen harmonics
A term frequently used to refer to the odd multiples of the third harmonic, which deserve special attention because of their natural tendency to be zero sequence.
ONE LINE DIAGRAM
MODELING OF HARMONIC LOAD
• Double click on the charger • Select the harmonics section • Select the type of harmonics from the given library of
harmonics
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BUILT-IN MODELS OF ETAP
ROCKWELL (12-Pulse-VFD)
ROCKWELL (18-Pulse-VFD)
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ROCKWELL (6-Pulse-VFD)
TOSHIBA (PWM-ASD)
TYPICAL (LCI)
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TYPICAL-IEEE (12-Pulse1)
TYPICAL-IEEE (12-Pulse2)
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TYPICAL-IEEE (18-Pulse-CT)
TYPICAL-IEEE (18-Pulse-VT)
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TYPICAL-IEEE (6-Pulse1)
TYPICAL-IEEE (6-Pulse2)
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TYPICAL-IEEE (Fluorescent)
TYPICAL-IEEE (Large-ASD)
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TYPICAL-IEEE (SPC)
TYPICAL-IEEE (XFMR-Magnet)
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USER DEFINED MODELING
• Go to the library tab given on the main window of ETAP • Select the harmonic section • Click on add tab • Enter the name of new harmonic model • Click on edit tab • Enter the spectrum components in the table
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COMMENTS
In this experiment, we learnt:
• How to model a harmonic load using built-in models • How to built a user-defined harmonic model • How to model a harmonic load using user-defined
models
So, ETAP is a very powerful tool for harmonic analysis of any power distribution network.
EXPERIMENT#09
Impact of personal computer load on power distribution network of RCET
Harmonics
Harmonics are sinusoidal voltages or currents having frequencies that are integer multiples of the frequency at which the supply system is designed to operate (termed the fundamental frequency usually 50 or 60 Hz).
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PC LOAD THD’S
Harmonic No. %THD 3rd 91.63 5th 86.61 7th 69.87 9th 44.76 11th 54.81 13th 46.44 15th 46.44 17th 33.05 19th 24.70 23rd 11.74 25th 7.900 29th 5.120
%THD 178.97
ONE LINE DIAGRAM
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LOAD FLOW DIAGRAM
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LOAD FLOW ANALYSIS REPORT
HARMONIC ANALYSIS RESULTS
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VOLTAGE WAVEFORMS & SPECTRAS
BUS-5:
BUS-11:
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BUS-27:
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BUS-33:
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CURRENT WAVEFORMS & SPECTRAS
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CABLE-2:
CABLE-7:
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CABLE-11:
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CABLE-18:
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HARMONIC ANALYSIS REPORT
COMMENTS
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In this experiment, we learnt:
• How to apply harmonic analysis to a power distribution network
• How to perform load flow analysis on a power distribution network
• How to perform harmonic analysis on a power distribution network
• How to get harmonic spectra at required locations
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EXPERIMENT#10
Flow of triplen harmonics (zerosequence harmonics) during 5 different schemes of connection for a 3phase transformer with presence of large nonlinear load using ETAP
ONE LINE DIAGRAM
HARMONIC MODEL USED
PC load is used as a source of harmonics in this experiment that has the following range of THD’S.
Harmonic No. %THD 3rd 91.63
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5th 86.61 7th 69.87 9th 44.76 11th 54.81 13th 46.44 15th 46.44 17th 33.05 19th 24.70 23rd 11.74 25th 7.900 29th 5.120
%THD 178.97
5 DIFFERENT SCHEMES OF TRANSFORMER WINDING
PRIMARY SIDE SECONDARY SIDE 1 Y-Grounded Y-Ungrounded 2 Y-Grounded Y-Grounded 3 Y-Grounded Delta 4 Y-Ungrounded Delta 5 Delta Delta
HARMONIC ANALYSIS RESULTS
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
CASE-1:
Transformer primary side Y-Grounded and secondary Y-Ungrounded
VOLTAGE SPECTRA ON LT-SIDE
VOLTAGE SPECTRA ON HT-SIDE
VOLTAGE WAVEFORM ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
VOLTAGE WAVEFORM ON HT-SIDE
CURRENT SPECTRA ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
CURRENT SPECTRA ON HT-SIDE
CURRENT WAVEFORM ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
CURRENT WAVEFORM ON HT-SIDE
OBSERVATIONS:
Harmonic source is connected on the LT side of transformer, so the triplen harmonics are blocked due to ungrounded Y-connection. The magnitude of remaining harmonic components is reduced on the HT side of transformer.
CASE-2:
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
Transformer primary side Y-Grounded and secondary Y-Grounded
VOLTAGE SPECTRA ON LT-SIDE
VOLTAGE SPECTRA ON HT-SIDE
VOLTAGE WAVEFORM ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
VOLTAGE WAVEFORM ON HT-SIDE
CURRENT SPECTRA ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
CURRENT SPECTRA ON HT-SIDE
CURRENT WAVEFORM ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
CURRENT WAVEFORM ON HT-SIDE
OBSERVATIONS:
Harmonic source is connected on the LT side of transformer, so the triplen harmonics are not blocked due to grounded Y-connection. The triplen harmonics are also present on the HT side of transformer as that is also Y-grounded.
CASE-3:
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
Transformer primary side Y-Grounded and secondary Delta
VOLTAGE SPECTRA ON LT-SIDE
VOLTAGE SPECTRA ON HT-SIDE
VOLTAGE WAVEFORMS ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
VOLTAGE WAVEFORM ON HT-SIDE
CURRENT SPECTRA ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
CURRENT SPECTRA ON HT-SIDE
CURRENT WAVEFORM ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
CURRENT WAVEFORM ON HT-SIDE
OBSERVATIONS:
Harmonic source is connected on the LT side of transformer, so the triplen harmonics are blocked due to delta-connection. The triplen harmonics are also blocked on the HT side of transformer as there are no triplen harmonics on secondary side of transformer.
CASE-4:
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
Transformer primary side Y-Ungrounded and secondary Delta
VOLTAGE SPECTRA ON LT-SIDE
VOLTAGE SPECTRA ON HT-SIDE
VOLTAGE WAVEFORM ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
VOLTAGE WAVEFORM ON HT-SIDE
CURRENT SPECTRA ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
CURRENT SPECTRA ON HT-SIDE
CURRENT WAVEFORM ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
CURRENT WAVEFORM ON HT-SIDE
OBSERVATIONS:
Harmonic source is connected on the LT side of transformer, so the triplen harmonics are blocked due to delta-connection. The triplen harmonics are also blocked on the HT side of transformer as there are no triplen harmonics on secondary side of transformer.
CASE-5:
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
Transformer primary side Delta and secondary Delta
VOLTAGE SPECTRA ON LT-SIDE
VOLTAGE SPECTRA ON HT-SIDE
VOLTAGE WAVEFORM ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
VOLTAGE WAVEFORM ON HT-SIDE
CURRENT SPECTRA ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
CURRENT SPECTRA ON HT-SIDE
CURRENT WAVEFORM ON LT-SIDE
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
CURRENT WAVEFORM ON HT-SIDE
OBSERVATIONS:
Harmonic source is connected on the LT side of transformer, so the triplen harmonics are blocked due to delta-connection. The triplen harmonics are also blocked on the HT side of transformer as there are no triplen harmonics on secondary side of transformer. Moreover, primary side is also delta-connected.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
EXPERIMENT#11
Three phase short circuit analysis (3phase faultsdevice duty) for a given power system using ETAP
SHORT CIRCUIT ANALYSIS
The power station short circuit analysis program analyze the effect of three phase, line to ground, line to line, and line to line to ground faults on the electrical distribution networks. The program calculates the total short circuit currents as well as the contributions of individual motors, generators, and utility ties in the system. Fault duties are in compliance with the latest editions of the ANSI/IEEE standards and IEC standards.
The ANSI/IEEE Short-Circuit Toolbar and IEC Short-Circuit Toolbar sections explain how you can launch a short-circuit calculation, open and view an output report, or select display options. The Short-Circuit Study Case Editor section explains how you can create a new study case, what parameters are required to specify a study case, and how to set them. The Display Options section explains what options are available for displaying some key system parameters and the output results on the one-line diagram, and how to set them.
Short-Circuit Toolbar This toolbar is active when you are in Short-Circuit mode and the standard is set to ANSI in the Short-Circuit Study Case Editor.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
3-Phase Faults - Device Duty
Click on this button to perform a three-phase fault study per ANSI C37 Standard. This study calculates momentary symmetrical and asymmetrical rms, momentary asymmetrical crest, interrupting symmetrical rms, and interrupting adjusted symmetrical rms short-circuit currents at faulted buses. The program checks the protective device rated close and latching, and adjusted interrupting capacities against the fault currents, and flags inadequate devices.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
Generators and motors are modeled by their positive sequence sub-transient reactance.
ONE LINE DIAGRAM
FAULTY POINT
• BUS-15
There is a short circuit fault on bus-15.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
LOAD FLOW DIAGRAM
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
SHORT CIRCUIT ANALYSIS DIAGRAM
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
COMMENTS:
In this experiment, we use three phase fault-device duty analysis to analyze the effect of fault on the system.
Following results are obtained in this experiment:
At bus-15:
Before fault After fault Current 568A 4.8KA
Power flow 345KW 3.6KW
We observe that the current flowing through bus-15 is increased up to many times as compared to the current before fault.
We observe that the power flowing through bus-15 is decreased up to many times as compared to the power before fault due to the short circuit at bus-15 as the load connected to that bus is now shorted and no power is flowing into that load.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
EXPERIMENT#12
Three phase short circuit analysis (3phase faults30 cycle network) for a given power system using ETAP
3-Phase Faults – 30-Cycle Network
Click on this button to perform a three-phase fault study per ANSI standards. This study calculates short-circuit currents in their rms values after 30 cycles at faulted buses.
Generators are modeled by their positive sequence transient reactance’s, and short-circuit current contributions from motors are ignored.
ONE LINE DIAGRAM
FAULTY POINT
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
• BUS-15
There is a short circuit fault on bus-15.
LOAD FLOW DIAGRAM
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
SHORT CIRCUIT ANALYSIS DIAGRAM
COMMENTS:
In this experiment, we use three phase fault-device duty analysis to analyze the effect of fault on the system.
Following results are obtained in this experiment:
At bus-15:
Before fault After fault Current 568A 3.6KA
Power flow 345KW 3.6KW
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
We observe that the current flowing through bus-15 is increased up to many times as compared to the current before fault.
We observe that the power flowing through bus-15 is decreased up to many times as compared to the power before fault due to the short circuit at bus-15 as the load connected to that bus is now shorted and no power is flowing into that load.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
EXPERIMENT#13
Three phase short circuit analysis (LG, LL, LLG, & 3Phase Faults ½ Cycle) for a given power system using ETAP
LG, LL, LLG, & 3-Phase Faults - ½ Cycle
Click on this button to perform line-to-ground, line-to-line, line-to-line-to-ground, and three-phase fault studies per ANSI standards. This study calculates short-circuit currents in their rms values at ½ cycles at faulted buses.
Generators and motors are modeled by their positive, negative, and zero sequence sub-transient reactance.
In all the unbalanced fault calculations (½ cycle, 1.5-4 cycle and 30 cycles), it is assumed that the negative sequence impedance of a machine is equal to its positive sequence impedance. Generator, motor, and transformer grounding types and winding connections are taken into consideration when constructing system positive, negative, and zero sequence networks.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
ONE LINE DIAGRAM
FAULTY POINT
• BUS-15
There is a short circuit fault on bus-15.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
LOAD FLOW DIAGRAM
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
SHORT CIRCUIT ANALYSIS DIAGRAM
COMMENTS:
In this experiment, we use three phase fault-device duty analysis to analyze the effect of fault on the system.
Following results are obtained in this experiment:
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
At bus-15:
Before fault After fault Current 568A 6.2KA
Power flow 345KW 5.1KW
We observe that the current flowing through bus-15 is increased up to many times as compared to the current before fault.
We observe that the power flowing through bus-15 is decreased up to many times as compared to the power before fault due to the short circuit at bus-15 as the load connected to that bus is now shorted and no power is flowing into that load.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
EXPERIMENT#14
Three phase short circuit analysis (LG, LL, LLG, & 3Phase Faults 1.5 to 4 Cycle) for a given power system using ETAP
LG, LL, LLG, & 3-Phase Faults - 1.5 to 4 Cycle
Click on this button to perform three-phase, line-to-ground, line-to-line, line-to-line-to-ground, and three-phase fault studies per ANSI standards. This study calculates short-circuit currents in their rms values between 1.5 to 4 cycles at faulted buses.
Generators are modeled by their positive, negative, and zero sequence sub-transient reactance, and motors are modeled by their positive, negative and zero sequence transient reactance. Generator, motor and transformer grounding types and winding connections are taken into considerations when constructing system positive, negative, and zero sequential networks.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
ONE LINE DIAGRAM
FAULTY POINT
• BUS-15
There is a short circuit fault on bus-15.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
LOAD FLOW DIAGRAM
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
SHORT CIRCUIT ANALYSIS DIAGRAM
COMMENTS:
In this experiment, we use three phase fault-device duty analysis to analyze the effect of fault on the system.
Following results are obtained in this experiment:
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
At bus-15:
Before fault After fault Current 568A 5.7KA
Power flow 345KW 5KW
We observe that the current flowing through bus-15 is increased up to many times as compared to the current before fault.
We observe that the power flowing through bus-15 is decreased up to many times as compared to the power before fault due to the short circuit at bus-15 as the load connected to that bus is now shorted and no power is flowing into that load.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
EXPERIMENT#15
Three phase short circuit analysis (LG, LL, LLG, & 3Phase Faults 30 Cycle) for a given power system using ETAP
LG, LL, LLG, & 3-Phase Faults - 30 Cycle
Click on this button to perform three-phase, line-to-ground, line-to-line, line-to-line-to-ground, and three-phase fault studies per ANSI standards. This study calculates short-circuit currents in their rms values at 30-cycles at faulted buses.
Generators are modeled by their positive, negative, and zero sequence reactance, and short-circuit current contributions from motors are ignored. Generator, motor, and transformer grounding types and winding connections are taken into consideration when constructing system positive, negative, and zero sequence networks.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
ONE LINE DIAGRAM
FAULTY POINT
• BUS-15
There is a short circuit fault on bus-15.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
LOAD FLOW DIAGRAM
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
SHORT CIRCUIT ANALYSIS DIAGRAM
COMMENTS:
In this experiment, we use three phase fault-device duty analysis to analyze the effect of fault on the system.
Following results are obtained in this experiment:
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
At bus-15:
Before fault After fault Current 568A 4.8KA
Power flow 345KW 4.8KW
We observe that the current flowing through bus-15 is increased up to many times as compared to the current before fault.
We observe that the power flowing through bus-15 is decreased up to many times as compared to the power before fault due to the short circuit at bus-15 as the load connected to that bus is now shorted and no power is flowing into that load.
POWER SYSTEM ANALYSIS LAB MANUAL
ASAD NAEEM 2006‐RCET‐EE‐22
COMPARISON OF SHORT CIRCUIT ANALYSIS
CURRENT POWER 3‐phase faults‐device duty
4.8
3.6
3‐phase faults‐30 cycle network
3.6
3.6
LG, LL, LLG, & 3‐Phase Faults ‐ ½
Cycle
6.2
5.1
LG, LL, LLG, & 3‐Phase Faults ‐ 1.5 to
4 Cycle
5.7
5
LG, LL, LLG, & 3‐Phase Faults ‐ 30
Cycle
4.8
4.8