Laboratory Manual: Hirasugar Institute of Technology, Nidasoshi
Laboratory Manual: Hirasugar Institute of Technology, Nidasoshi
LABORATORY MANUAL
Prof P M Murari
Hirasugar Institute of Technology,Nidasohi
Sl. NO Experiments
1 Open Circuit and Short circuit tests on single phase step up or step
down transformer and predetermination of (i) Efficiency and
regulation (ii) Calculation of parameters of equivalent circuit.
2 Sumpner’s test on similar transformers and determination of
combined and individual transformer efficiency.
3 Parallel operation of two dissimilar single-phase transformers of
different kVA and determination of load sharing and analytical
verification given the Short circuit test data.
4 Polarity test and connection of 3 single-phase transformers in star –
delta and determination of efficiency and regulation under balanced
resistive load.
5 Comparison of performance of 3 single-phase transformers in delta –
delta and V – V (open delta) connection under load.
6 Scott connection with balanced and unbalanced loads.
7 Separation of hysteresis and eddy current losses in single phase
transformer.
8 Voltage regulation of an alternator by EMF and MMF methods.
9 Voltage regulation of an alternator by ZPF method.
10 Slip test – Measurement of direct and quadrature axis reactance and
predetermination of regulation of salient pole synchronous machines.
11 Performance of synchronous generator connected to infinite bus,
under constant power and variable excitation & vice - versa.
12 Power angle curve of synchronous generator
OBSERVATION:
TABULATION(SCC):
AIM: Predetermination of efficiency and regulation by open circuit and short circuit test on single
phase transformer, also calculate equivalent circuit parameters from short circuit and open
circuit test .
APPARATUS REQUIRED:
NATURE OF GRAPH:
CALCULATIONS:
I) PREDETERMINATION OF EFFICIENCY AND REGULATION
From Open Circuit Test:
𝐾�� ×1000
= �𝑎𝑡𝑒𝑑 𝑝𝑟𝑖�𝑎𝑟𝑦 �𝑜𝑙𝑡𝑎𝑔𝑒 = Amps
∴ 𝑐𝑜𝑠∅ 𝑠𝑐 �
=�𝑠𝑐𝑠𝑐�𝑠𝑐 =
Also, �𝑠𝑐 = �2 �
𝑠𝑐
= 1𝑒 Ω
∴ �1𝑒 = 2𝑠𝑐
�
�𝑠𝑐
Vsc
Z = = R2 + X2 = Ω
1e 1e 1e
Isc
∴ X1e = Z2 − R2 = Ω
1e 1e
Practically:
𝑥 × 𝐾�� × 103 𝑐𝑜𝑠� × 100
%𝜂=
𝑥 × 𝐾�� × 103 × 𝑐𝑜𝑠� +0 � +
𝑥2�𝑠𝑐
�1 �1𝑒 𝑐𝑜𝑠𝜑 ± �1 𝑥1𝑒 𝑠𝑖𝑛𝜑 × 100 +ve sign for lagging power factor
% Regulation = �1
EFFICIENCY TABULATION:
Power %R %R
factor (Leading) (Lagging)
0.1
0.2
0.3
0.4
CONCLUSION:
VIVA VOCE
CIRCUIT DIAGRAM:
OBSERVATION:
1. KVA rating of transformer T1= KVA
2. Primary voltage = _V
3. Secondary voltage = _V
4. KVA rating of transformer T2= KVA
5. Primary voltage = V
6. Secondary voltage = V
7. Full load current = Amps.
NATURE OF GRAPH:
EXPT.NO.2 DATE:
SUMPNER’S TEST ON SIMILAR TRANSFORMERS AND DETERMINATION
OF COMBINED AND INDIVIDUAL TRANSFORMER EFFICIENCY.
AIM: To conduct sumpner’-s test on similar transformers and determination of combined and
individual transformer efficiency.
APPARATUS REQUIRED:
S.no Particulars Range Quantity
1 Voltmeter MI 0-300V 1 Nos
2 Voltmeter MI 0-75V 2 Nos
3 Ammeter MI 0-2A 1 No
4 Ammeter MI 0-5A 1 No
5 Wattmeter MI 300V / 5A LPF 1 No
6 Wattmeter MI 75V/5A UPF 1 No
7 1-phase auto-transformer 230V/0-260V 2 Nos
1KVA, 230V/115V
8 Transformers 2 Nos
Single phase, 50Hz
9 Connecting wires -- Few
THEORY:
The Sumpner’s test is conducted simultaneously on two identical transformers and
provides data for finding the efficiency, regulation and the effect of temperature rise.
Operation: The secondary’s of the transformer are in phase opposition with switch S 1 closed and
switch S2 open, there will be no circulating current in the loop circuit. It is because the induced
emf’s in the secondaries are equal and in opposition. The reading of the wattmeter W 1 will be
equal to the core losses of two transformers.
Individual
transformer%
η
Combined
transformer %
η
CALCULATIONS:
W2 WSC
= 2
= Watts.
CALCULATIONS:
CONCLUSION:
OBSERVATION:
AIM: Conduct an experiment to understand load sharing by two single phase transformer
connected in parallel.
APPARATUS REQUIRED:
THEORY:
The secondary emf of the two transformers are equal because they have the same turns ratio and
have their primary connected to the same supply.
The transformers are connected in parallel when the load on them is more than the rating
of individual transformer, generally smaller units are operated in parallel which share a common
load. The parallel operation is advantageous as they can be interchangeable in some conditions for
satisfactory. Hence polarity should be carried out for proper operation. The voltage ratio of
primary and secondary must be same. The % impedance should be same in magnitude and hence
same transformer ratio in order to avoid the circulating current and operating at different power
factor.
PROCEDURE:
CONCLUSION:
VIVA VOCE
CIRCUIT DIAGRAM:
I. POLARITY TEST:
a) SUBTRACTIVE:
- -
+ +
b) ADDITIVE:
EXPT.NO.4 DATE:
POLARITY TEST AND CONNECTION OF 3 SINGLE-PHASE TRANSFORMERS IN
STAR – DELTA AND DETERMINATION OF EFFICIENCY AND REGULATION
UNDER BALANCED RESISTIVE LOAD.
AIM: Conduct polarity test on single phase transformer and connection of 3- single phase
transformers in star-Delta and determination of efficiency and regulation under balanced
resistive loads.
APPARATUS REQUIRED:
THEORY:
A Star-delta connection of transformer is mainly used in the substation and in
transmission line. The main use connection is to step down the voltage. The neutral available on
primary side is grounded. It can be seen that there is a phase difference of 30º between primary
and secondary line voltages. In this type of connection, primary is connected in star fashion and
the secondary is connected in delta fashion.
PROCEDURE:
I. Polarity Test:
OBSERVATIONS:
1. KVA= KVA
2. Primary Voltage = V
3. Secondary Voltage = V
4. Current = Amps.
5. Phases = Phase.
TABULATION:
Primary side Secondary side
S.no %η %R
V1 in volts I1 in Amps V2 in Volts I2 in Amps
1
CONCLUSION:
VIVA VOCE
EXPT 5 DATE
COMPARISON OF PERFORMANCE OF 3 SINGLE-PHASE TRANSFORMERS IN
DELTA – DELTA AND V – V (OPEN DELTA) CONNECTION UNDER LOAD.
APPARATUS REQUIRED:
THEORY:
As seen previously in connection of three single phase transformers that if one of
the transformers is unable to operate then the supply to the load can be continued with the
remaining tow transformers at the cost of reduced efficiency. The connection that
obtained is called V-V connection or open delta connection.
If one of the transformers fails in ∆ - ∆ bank and if it is required to continue the supply
eventhough at reduced capacity until the transformer which is removed from the bank is
repaired or a new one is installed then this type of connection is most suitable.
When it is anticipated that in future the load increase, then it requires closing of open
delta. In such cases open delta connection is preferred.
Key point : It can be noted here that the removal of one of the transformers will not give
the total load carried by V - V bank as tow third of the capacity of ∆ - ∆ bank.
The load that can be carried by V - V bank is only 57.7% of it. it can be proved as
follows.
It can be seen from the Fig. 2(a)
∆ - ∆ capacity = √3 VL IL = √3 VL (√3 Iph )
∆ - ∆ capacity = 3 VL Iph.................................................(i)
It can also be noted from the Fig. 2(b) that the secondary line current I L is equal to the
phase current Iph.
V- V capacity = √3 VL IL = √3 VL Iph....................................(ii)
Dividing equation (ii) by equation (i)
CIRCUIT DIAGRAM:
PROCEDURE:
I. Delta-Delta Connection:
CALCULATION:
Output power
V2 I2 × 100 =
%η= Input power =
V1 I1
V02 - V2 × 100 =
% Regulation =
V02
PROCEDURE:
CALCULATION:
Output power
V2 I2 × 100 =
%η= Input power =
V1 I1
V02
CONCLUSION:
VIVA VOCE
CIRCUIT DIAGRAM:
EXPT.NO.6 DATE:
SCOTT CONNECTION WITH BALANCED AND UNBALANCED LOADS
AIM: To determine the load shared by two transformers when they are connected in scott .
APPARATUS REQUIRED:
THEORY:
The Scott connection is the most common method of connecting two single phase transformers to
perform the 3- to 2- conversion and vice-versa. The two transformers are connected electrically
but not magnetically, one transformer is called main transformer and other is auxiliary or teaser
transformer. The main transformer is having 50% tapping and auxiliary transformer is having
86.6% tapping.
One end of primary winding of the auxiliary transformer is connected to the centre
tapping provided on the primary winding of the main transformer with equal number of turns on.
The voltage per turn is same in primary of both main & teaser transformer with equal
number of turn on secondary on both the transformer. The secondary voltage will be equal in
magnitude which results in symmetrical & phase system.
PROCEDURE:
TABULATION:
FOR BALANCED LOAD:
S.no Current Current Current Voltage Voltage Lamp load
I1 Amps IL1 Amps IL2 Amps V1 Volts V2 Volts In Watts
1.
2.
3.
4.
FOR UNBALANCED LOAD:
2.
3.
4.
CALCULATION:
CONCLUSION:
VIVA VOCE
NATURE OF GRAPH:
EXPT.NO.7 DATE:
SEPARATION OF HYSTERESIS AND EDDY CURRENT LOSSES IN SINGLE
PHASE TRANSFORMER.
AIM: To separate the eddy current loss and hysteresis loss from the iron loss of single phase
transformer.
APPARATUS REQUIRED:
S.no Particulars Range Quantity
1 Rheostat 1250Ω , 0.8A
2 Wattmeter 300 V, 5A
3 Ammeter (0-2) A
5 Voltmeter (0-300) V
7 Connecting Wires -- --
1KVA, 230V/115V
8 Transformers 1 Nos
Single phase, 50Hz
DC Motor coupled with
9 --
alternator
10 Connecting wires -- Few
THEORY: *Refer: 1) Theory and performance of Electrical Machines, by J.B. Gupta.
2) A Text book of Electrical Technology, by B.L. Theraja & A.K. Theraja.
PROCEDURE:
Wattmeter
Speed in Frequency Voltage Iron loss Wi/f
S.no reading
RPM in HZ V (volts) Wi(watts) Joules
(Watts)
1
2
3
4
5
6
7
8
FORMULAE USED:
1. Frequency, f =(P*Ns) / 120 in Hz P = No.of Poles & Ns = Synchronous speed in rpm.
2. Hysteresis Loss Wh = A * f in Watts A = Constant (obtained from graph)
3. Eddy Current Loss We = B * f2 in Watts B = Constant (slope of the tangent drawn to
the curve)
4. Iron Loss Wi = Wh + We in Watts Wi / f = A + (B * f)
Here the Constant A is distance from the origin to the point where the line cuts the Y-
axis in the graph between Wi / f and frequency f. The Constant B is Δ(Wi / f ) / Δf
CALCULATIONS:
CONCLUSION:
VIVA VOCE
CIRCUIT DIAGRAM:
a) For OC Test:
OBSERVATION:
a) For OC Test :
b) For SC Test:
TABULATION:
b) For SC Test :
APPARATUS REQUIRED:
THEORY:
The KVA ratings of commercial alternators are very high (ex: 500MVA). So, it’s not
convenient to determine voltage regulation by direct loading. Therefore we have to determine
voltage regulation by indirect methods. These methods require very small power as compared to
direct loading method. The EMF and MMF methods are indirect methods.
In EMF method, we are determining the armature resistance Ra and synchronous
impedance
For some selected value of field current If. Then we are finding synchronous reactance
Xs= X 𝑠− R2 .aOnce know about Ra and Xs draw the phasor diagram for any load and any power
2
factor.
Taking Ia as reference phasor, then IaRa drop is in phase with Ia while Ia Xs leads Ia by 90º.
The phaser sum of V, IaRa and IaXs gives the no load emf E0.
E0= 𝑂� 2 + �� 2
�0 − �
∴ % �𝑜𝑙𝑡𝑎𝑔𝑒 𝑟𝑒𝑔𝑢𝑙𝑎𝑡𝑖𝑜𝑛 = × 100
�
The main drawback of this method is its approximate method. The reason is the combined
effect of XL (armature reactance) and XAR (reactance of armature reaction) is measured on short
circuit. Since current in this condition is almost lagging 90º, the armature reaction will produce its
worst demagnetizing effect. This method gives value higher than the value obtained from the
actual load test for this reason it is called pessimistic method.
In MMF method it is assumed that the armature leakage reactance to be additional armature
reaction neglecting armature resistance, this method assumes that change in terminal pd on load is
due to entirely armature reaction. Same tests (OCC and SC) required for this test also, but
interpretation of result only is different.
i) Suppose the alternator is supplying full load current at normal voltage V and ZPF lagging. Then
dc field amp-turn required will be those needed to produce normal voltage ‘V’ Let OA= field
AT required to produce the normal voltage ‘V’ at no load OB 1= field AT required to neutralize
the armature reaction, then total field AT required are phasor sum of OA and OB, The OA can
be found from OCC and OB1 can be determined from SCC.
ii) At full load current of ZPF lead the armature AT are unchanged, since they aid the main
field, less field AT is required to produce the given emf
Total field AT, AB2=A0-B2O
B2O=field AT required to neutralize armature reaction. Here A 0 is determined from
OCC and B2O from SCC.
iii)Between zero lagging and zero leading power factors, the armature mmf rotates through 180º
At UPF armature reaction is cross magnetizing only. Therefore OB 3 is drawn perpendicular to
AO No AB3 shows the required AT in magnitude and direction.
This method gives a regulation lower than actual performance of machine. For this reason it is
known as optimistic method.
Ia(Rated) Isc
If If2 If1 If
PROCEDURE:
CALCULATATION:
= Ω
Xs = _ 2 − 2
Xs = Ω
2 2
E0 = �𝑝� 𝑐𝑜𝑠𝜑 + �𝑎 �𝑎 + �𝑝� 𝑠𝑖𝑛𝜑 ± �𝑎 �𝑠
Where Vph �𝐿
= = = V
3
2 2
Ea = �𝑝� 𝑐𝑜𝑠𝜑 + �𝑎 �𝑎 + � 𝑠𝑖𝑛𝜑 + �𝑎 �𝑠
=
=
0 −�𝑝 �
Voltage Regulation= � × 100
�𝑝 �
= X 100
=
=
0 −�𝑝 �
Voltage Regulation= � × 100
�𝑝 �
= X 100
=
=
0 −�𝑝 �
Voltage Regulation= � × 100
�𝑝 �
= X 100
=
For MMF Method:
Armature resistance = Ra = Ω
Voc
/phase = � =
3
=
�𝑓2=
From graph �𝑓1 =
If 2=( If1+ If2sinφ)2+( I f2cosφ)2------- lagging p.f for I ffind E ph(lag)from graph I
2
=( sinφ) 2+( I f2
f I -f1 I f2 cosφ)2------- leading p.f for I ffind E ph(lead) from graph I
2 2 2
=(
f I )f1+( I ) -------
f2 Unity p.f for I findf E fromph(upf)
graph
CALCULATIONS:
CONCLUSION
VIVA VOCE:
CIRCUIT DIAGRAM:
b) For OC Test:
OBSERVATION:
THEORY:
The regulation obtained by MMF and EMF methods is based on the total synchronous
reactance (The sum of reactance due to armature leakage flux and due to armature reaction effect)
This method is based on the separation of reactance due to leakage flux and that due to armature
reaction flux. Therefore, it is more accurate method.
Regulation by this method, the data required are i) Effective resistance of armature
winding ii) Open circuit characteristic iii) Field current to circulate full load current in the stator
iv) Zero power factor full load voltage characteristics- a curve between terminal voltage and
excitation while machine is being run on synchronous speed and delivering full load current at
zero power factor.A machine is run at synchronous speed by prime mover. A purely inductive load
is connected across the armature terminals and the excitation is raised so as to cause flow of full
load armature current. The value of reactance is increased in such a way that the excitation current
is adjusted to a value that causes full load rated armature current. The armature terminal voltages
are varied from 125% to 25% of rated voltage in steps, maintaining speed and rated armature
current constant throughout the test. The curve is drawn between terminal voltage and excitation
current, gives the zero power factor lagging characteristics. There is a definite relationship
between zero power factor lagging characteristics and an open circuit characteristics of an
alternator. The ZPF characteristic curve is of exactly of same shape as the OCC but it is shifted
vertically downward by leakage reactance drop IX L and horizontally by the armature reaction
MMF.
NATURE OF GRAPH
Eph P
E1ph
R
Q S
Voltage in volts
If1 If If
CIRCUIT DIAGRAM:
b) For SC Test:
TABULATION:
b) For SC Test :
PROCEDURE:
Terminal
Sl.no If in Amps
Voltage V
1
CALCULATIONS:
From potier triangle PQR, the armature leakage reactance drop is L(RS)
Iph*XLph= L(RS)*scale
Case 1)
Find (E1ph)2=(VphcosФ)2+( VphsinФ+ Iph*XLph)2 From
OCC corresponding If1 is calculated
From potier triangle ,field current balancing armature reaction is L(PS)
If2=L(PS)*Scale
Add If1 & If2 to get If
Find -------
I 2=( I + I sinφ)2+( I cosφ)2 lagging p.f
f2 f1 f2 2 f2 2--------
I =( I - I sinφ) +( I cosφ) leading p.f
f f1 f2 f2
I 2=( I )2+( I )2------- Unity p.f
f f1 f2
For If from graph calculate Eph
Voltage Regulation=(Eph-Vph)/ Vph *100
CALCULATIONS:
CONCLUSION:
VIVA VOCE:
CIRCUIT DIAGRAM:
OBSERVATION:
APPARATUS REQUIRED:
A salient pole synchronous machine has non uniform air gap, due to which its reactance
varies with rotor position. Thus salient pole machine possesses two axis of geometric symmetry i)
field pole axis, or d-axis or direct axis ii) Axis passing through the centers of interpolar space
called the quadrature axis or q-axis. Where as in cylindrical rotor machine only one axis of
symmetry (Pole axis or d-axis) in salient pole machines X q= 0.6 to 0.7 times Xd. Where as in
cylindrical rotor machine Xd= Xq.
The value of Xd and Xq are determined by applying balanced reduced voltage say V volts
to an excited machine at a speed little less than synchronous speed (The slip is less than 1%).
TABULATION:
%Regulation
Vmax in Vmin in Imax in Imin in Xd Xq
Sl.No Volts Volts Amps Amps 0.8(lag) 0.8(Lead)
CALCULATIONS:
Maximum voltage
Xd=
Minimum current
Minimum voltage
Xq=
Maximum current
PROCEDURE:
CONCLUSION:
Viva Voce:
Hirasugar Institute of Technology,Nidasohi
CIRCUIT DIAGRAM:
OBSERVATION:
APPARATUS REQUIRED:
PROCEDURE
a. Operation on Infinite Bus Bar
1. Connections are made as shown in the circuit diagram (4.a)
2. Keeping the rheostat R1 in the field circuit of motor in cut-out position, the rheostat
R2 in the armature circuit of motor and the rheostat R3 in the field circuit of
alternator in cut-in positions, the bus bar switch (S2) and synchronizing switch (S3) in
open positions, the supply switch (S1) is closed.
3. The motor is brought to the synchronous speed of the alternator by gradually
cutting out the rheostat R2 and cutting in the rheostat R1, if necessary. By gradually
cutting out the rheostat R3, the alternator voltage is built-up to the bus
bar voltage.
4. Now, bus bar switch (S2) is closed, and the phase sequence is verified. For correct
phase sequence, all the lamps will flicker simultaneously. Otherwise, they flicker
alternately. If they flicker alternatively, the bus bar voltage switch is opened and any
two terminals of the bus bar supply are interchanged.
5. Repeat step number 2, 3 and 4.
6. By varying the rheostats R1, R2 and R3 the dark period of the lamps are obtained.
7. When all the lamps are in dark condition, the synchronization switch S3 is closed
and now the alternator is connected in parallel with the bus bar.
8. Switches (S3) and (S2) are opened; all the rheostats are brought back to their
respective initial positions, and supply switch (S1) is opened.
b. Constant Power - Variable Excitation Operation
1. Connections are made as shown in the circuit diagram (4.b)
2. Follow the procedure steps 2, 3.
3. By gradually cutting out the rheostat R3, the alternator voltage is built-up to its rated
voltage.
4. Apply load gradually.
5. Vary generator excitation (R3) to keep wattmeter readings constant (Total Power).
6. Tabulate the readings.
7. Bring back the load to zero, reduce the excitation to a normal value and all rheostats
are brought back to respective initial positions & supply switch (S1) is opened.
CALCULATIONS:
CONCLUSION:
P.A. COLLEGE OF ENGINEERING
VIVA VOCE:
EXPT NO 12 DATE:
POWER ANGLE CURVE OF SYNCHRONOUS GENERATOR
APPARATUS REQUIRED:
1 Voltmeters 0-30V MC 01
0-500V MI 01
2 Ammeters 0-10/20A MI 01
0-1/2A MC 01
4 Tachometer - - 01
PROCEDURE
2. Keeping the rheostat R1 in the field circuit of motor in cut-out position, the rheostat
R2 in the armature circuit of the motor and the rheostat R3 in the field of the
alternator in cut-in positions and TPST (S2) in open position, the supply switch (S1)
is closed
3. The motor is brought to synchronous speed by cutting out the rheostat R2 and then
by cutting in the rheostat R1, if necessary.
4. By gradually cutting out the rheostat R3, the readings of ammeter (A1, 0-2A) and
voltmeter (V) are noted down.
5. The above step is continued until voltmeter reads about 1.25 times the rated
voltage of the alternator.
1. The rheostat R3 is brought to its initial position (cut-in) and TPST (S2) is closed.
2. By gradually cutting out the rheostat R3, reading of the ammeter (A2, 0-10/20A) is
adjusted to the rated current of the alternator and the corresponding field current (A1)
is noted down.
3. All the rheostats are brought back to their respective initial positions, TPST switch(S2)
and supply switch (S1) are opened.
V I Resistance Resistance
Sl.No
(Volts) (Ampere) RDC = V/I Ω RAC =1.5*RDC
Determination of Armature Resistance (Ra) by V-I Method
1. Connections are made as shown in the circuit diagram(13.b)
2. Keeping the rheostat in cut-in position, the supply switch (S1) is
closed, Rheostat is adjusted to any value of current (say 1A) and the
readings of ammeter and voltmeter are noted down.
3. The supply switch (S1) is opened.
CALCULATION
EMF Method
1. Draw OCC and SCC for suitable scales as shown in model graph no (1).
2. Mark a point A on the OCC corresponding to the rated voltage and draw a Perpendicular
so that it cuts SCC line at a point B and X-axis at point C.
3. Corresponding to point A, E1 is the open circuit voltage per phase, and BC is the Short
circuit current.
4. Therefore Synchronous impedance per phase Zs = E1/I1Ω (If Constant) Synchronous
reactance per phase Xs = √ Zs2- Ra2 Ω s a
Model Graph
Sl. If Ia W1 x K1 W2 x K2 |V| |E| P = W1 + W2 δ
N (rpm)
No. (Amps) (Amps) (Watt) (Watt) (Volts) (Volts) (Watt) Degree
Model Graph
CONCLUSION:
VIVA VOCE: