hv manual for csvtu 8th sem

23
DEPARTMENT OF ELECTRICAL ENGINEERING vii TH sem B.E. electrical G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 1 G.H. RAISONI COLLEGE OF ENGINEERING DEPARTMENT OF ELECTRICAL ENGINEERING HIGH VOLATGE LABORATORY INDEX Sr. No. Name of Experiment Page No. 01 CALIBERATION OF VOLTMETER BY USING SPEHERE GAP METHOD 2 02 CALIBRATION OF VOLTMETER USING ROAD GAP AND POINT GAP 4 03 TO DETERMINE FLASH OVER VOLTAGE ACROSS PIN-TYPE INSULATOR 7 04 - TO DETERMINE STRING EFFICIENCY OF SUSPENSION TYPE INSULATOR.  9 05 - STUDY OF BREAK-DOWN VOLTAGE FOR DIFFERENT COMBINATION OF ELECTRODES. 12 06 DETERMINATION OF FAULT LOCATION BY DIGITALCABLE FAULT LOCATOR MODEL 2000A.  14 07 MEASUREMENT OF CAPACITANCE AND DISSIPATION FACTOR (TAN δ δ δ δ) OF SOLID INSULATING MATERIAL BY ELTEL CTS-500KIT. 16 08 STUDY THE FERRANTI EFFECT AND SURGE IMPEDANCE LOADING IN EHV LINE. 19 09 MEASUREMENT OF DIELECTRIC CONSTANT, DISSIPATION FACTOR (TAN δ δ δ δ) AND RESISTIVITY OF Oil. 22

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7/30/2019 Hv Manual for csvtu 8th sem

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 1

G.H. RAISONI COLLEGE OF ENGINEERINGDEPARTMENT OF ELECTRICAL ENGINEERING

HIGH VOLATGE LABORATORY

INDEX

Sr.

No.

Name of Experiment Page

No.

01 CALIBERATION OF VOLTMETER BY USING SPEHERE GAP

METHOD

2

02 CALIBRATION OF VOLTMETER USING ROAD GAP AND POINT

GAP

4

03 TO DETERMINE FLASH OVER VOLTAGE ACROSS PIN-TYPE

INSULATOR

7

04 - TO DETERMINE STRING EFFICIENCY OF SUSPENSION TYPE

INSULATOR.

9

05 - STUDY OF BREAK-DOWN VOLTAGE FOR DIFFERENT

COMBINATION OF ELECTRODES.

12

06 DETERMINATION OF FAULT LOCATION BY DIGITALCABLE

FAULT LOCATOR MODEL 2000A.

14

07 MEASUREMENT OF CAPACITANCE AND DISSIPATION

FACTOR (TAN δδδδ) OF SOLID INSULATING MATERIAL BY

ELTEL CTS-500KIT.

16

08 STUDY THE FERRANTI EFFECT AND SURGE IMPEDANCE

LOADING IN EHV LINE.

19

09 MEASUREMENT OF DIELECTRIC CONSTANT, DISSIPATION

FACTOR (TAN δδδδ) AND RESISTIVITY OF Oil.

22

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 2

EXPERIMENT NO: - 1

AIM: - CALIBERATION OF VOLTMETER BY USING SPEHERE GAP METHOD.

(1) 10 cm dia.(2) 5 cm dia.

APPARATUS: - Sphere gap, 10cm / 5cm dia, Control Panel, H.V. transformer (230V / 100KV,

10KVA), Capacitor Divider (100 pf), Connecting wires etc.

CIRCUIT DIAGRAM: -

THEORY: - A uniform field spark gap will always have a spark over voltage within a knowntolerance under constant atmospheric conditions. Hence sphere gap can be used for the

measurement of the peak value of the voltage, if the gap distance is known. The voltageto be measured is applied between the two spheres and the distance between them gives a

measure of spark over voltage.Irradiation of sphere gap is needed when measurements of voltage less than 50KV

are made with sphere gaps of 10cm dia. or less. There are various factors that affects the

spark over voltage of the sphere gap are,1) Nearby earthed objects.

2) Atmospheric conditions & Humidity.3) Irradiation, &

4) Polarity and rise time of Waveforms.

FUSE

RUGULATINGTRANSFORMER

230 V / 100KV10KVA

HT SWITCH

V

230 VAC

SUPPLY V

Scale

100 PF

100 KV

230

V

1OO

KV

Spheregap

VoltageDivider

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 3

PROCEDURE: -1) Make the connections as shown in the circuit diagram.

2) For this experiment both the spheres must of same diameter.3) Adjust the suitable distance between the electrical say 0.5 cm and 1 cm from

control panel.4) Increase the voltage gradually from control panel till breakdown occur.

5) Measure this breakdown / spark over voltage for that gap.

6) Change the distance & increase the voltage gradually.7) Repeat the same procedure for both the sphere set.

8) Find the percentage error and plot the graph.

OBSERVATION TABLE: -

Sr.no.

Distancebetween

thesphere

(D) cm

Peak VBDV at

20o

and 76cm of HG

(A)

ActualBDV

= KV

(B)

RMS BDV(V2)

=KV/ √2

Value of BDVas per

voltmeterKV (V1)

V1-V2 V1-V2 / V1 *100 =

% Error

01

02

03

04

Relation between air density factor δ and correction factor K

δ 0.70 0.75 0.80 0.85 0.90 0.95 1.0 1.05 1.10 1.15

K 0.72 0.77 0.82 0.86 0.91 0.95 1.0 1.05 1.09 1.12

δ = P/760 * (273+20 / 273+ t)

P & t: - are atmospheric pressure and temperature while performing the experiments

δ : - Air density factor

K: - correction factor

RESULTS: - From this experiments we are able to get the various breakdown voltages fordifferent gaps between the electrodes.

QUESTIONS: - 1) Write in brief the effect of near by earthed object on the spark over

voltage of sphere gap.

2) Write in brief the effect of irradiation on the spark over voltage of

sphere gap.3) Explain the measurement of high voltage by capacitance voltage

divider method.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 4

EXPERIMENT NO: - 2

AIM: -CALIBRATION OF VOLTMETER USING ROAD GAP AND POINT GAP

APPARATUS: - Transformer (230/100 KV, 10 KVA)

Voltage Divider (100pf)Control Panel, connecting rods, connecting wires, etc.

TYPE (A): - ROD GAP METHOD

CIRCUIT DIAGRAM: -

THEORY: - A rod gap is also sometimes used for approximate measurement of peak

values of power frequency voltages and impulse voltages. The rods will be either

square edged or circular in spacing varies from 2 to 200 cm. The spark over voltage,

as in other gaps is affected by humidity and air density. (The power frequency

breaks down voltage for 1.27 cm square rod in air at 25

0

C and a pressure of 760 torrwith the vapour pressure of water of 15.5 torr.

FUSE

RUGULATINGTRANSFORMER

230 V / 100KV

10KVA

HT SWITCH

V

230 VAC

SUPPLY V

Voltagedivider100KV100PF

Rod Gap

100KV

230 V

Scale

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 5

TYPE (B): - POINT GAP METHOD

CIRCUIT DIAGRAM: -

THEORY: - A point gap method is also used for measurement of a peak value of power frequency,voltage and impulse voltage. Standard point gap is constructed and arranged according to the rules

specified by standard. Performing to high voltage testing techniques and point gap should bethoroughly studied. Complete arrangement consisting of two rods of equal length and cross section

area with their operating gear. Insulating sphere supporting frames leads up to the point at whichthe volt is to be measured. One point is perfectly connected directly to earth, while the other sphere

is connected to high voltage conductor leads coming from H. T. transformers.

FUSE

RUGULATING

TRANSFORMER

230 V / 100KV

10KVA

HT SWITCH

V

230 V

ACSUPPLY V

VoltageDivider

100PF

100KV

PointGap

Scale

100KV

230 V

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 6

OBSERVATION TABLE: -

1) FOR ROD GAP

B. D. V.Sr.No.

Distancebetween

rods in cmStandard

value

(peak

value inKV) (A)

Peak value at

existing

temperature

B = KA .(KV)

RMS

value

= B / √2

RMS value of BDV V1 (from

voltmeter)

% error= V1-V2 /V1

*100

δ = P/760 * (273+20 / 273+ t)

P & t: - are the atmospheric pressure and temperature while doing the practicalδ: - Air density factor

K: - correction factor

2) FOR POINT GAP

Sr. No. Distance in cm or

mm

BDV in KV (voltmeter)

01

02

03

PROCEDURE: - Same as “Calibration of voltmeter by using sphere gap”

GRAPH: - FOR ROD GAP(i) Distance Vs RMS BDV (Std & Observed)

(ii) Distance Vs % Error.

FOR POINT GAP(i) Distance Vs RMS (Observed)

RESULT: - Find out the BDV for different spacing and plot the graph between spacing and

Standard / observed BDV rms reading & compare the values.

QUESTIONS: -(1) Explain the effect of atmospheric conditions on the spark over voltage of rod

gap.(2) Write the advantages of high voltage voltage measurement by electrostatic

voltmeter.(3) Explain the high voltage measurement by resistance voltage divider method.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 7

EXPERIMENT NO: - 3

AIM: -TO DETERMINE FLASH OVER VOLTAGE ACROSS PIN-TYPE INSULATOR1) UNDER DRY CONDITION

2) UNDER WET CONDITION

APPARATUS: - 1) H. V. transformer, 230V / 100KV, 10 KVA

2) 11KV pin type fixed on table and its bottom is earthed.3) Connecting wires & rod.

4) Control panel etc.

CIRCUIT DIAGRAM: -

THEORY: - It is one of the earliest designs used for supporting line conductor. The pin

insulator is supported on the forged steel pins and bolds, which are skewed to the crosssection of this supporting structure.

The conductor is lied to insulator on the grooves. In order to increase the leakagepath, one, two or three rain shades are so designed when these insulators are wet even then

sufficient dry space is provided by the inner shades.

For higher voltages the thickness of the material required for the purpose of the

insulation. But the practical way is to use more than one insulator unit instead of increasingthe thickness.

Flashover distances when the insulators are dry and wet are different. The flash over

voltage when the insulator is wet is less. The rain shades should not disturb the voltagedistribution. They are so designed that their surface is right angle to electrostatic lines of

forces or they must try to lie in the equipotential.The pin type insulator is reliable for voltage level upto 50KV max. and They are

never used for voltage beyond 80 KV. Since the suspension insulator is more reliable andcheaper. The modern practice is “not to used” the pin type insulator beyond 33KV.

FUSE

RUGULATING

TRANSFORMER

230 V / 100KV10KVA

HT SWITCH

V

230 VAC

SUPPLY V

VoltageDivider

100PF100KV

Pin

Insulator

100KV

230 V

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 8

PROCEDURE: -1) Make the connection as shown in circuit diagram.2) Increase the voltage across pin type insulator (Dry condition) gradually from control

panel till spark over gets.3) Note down this spark over voltage.

4) Repeat the process for Wet condition.5) Compare the observed value with standard value & find out the percentage error.

OBSERVATION TABLE: -

Pin Type Insulator = WD-10 typeFlash over voltage – Dry condition = 62.5 KV RMS

Wet condition = 38 KV RMS

1) For Dry Condition: -

Sr. No. Std. Flash overVoltage (V1)

RMS KV

Measured flash overvoltage (V2) KV

RMS voltmeter reading

% error= (V1-

V2/V1)*100

Avg. error

2) For Wet Condition: -

Sr. No. Std. Flash over

Voltage (V1)RMS KV

Measured flash over

voltage (V2) KVRMS voltmeter reading

% error

= (V1-V2/V1)*

100

Avg. error

RESULT: - The flashover voltage across pin type insulator is found to be ______KV

in dry condition. And _________ KV in wet condition.

QUESTIONS: -1. Write the comparison between pin insulator type Wc & Wd.

2. Write the dimensions of the different types of pin insulator and theirflash over voltage under dry and wet condition.

3. Compare the properties of procelain and glass insulator.

4. List the solid dielectrics used in practice.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 9

EXPERIMENT NO: - 4

AIM: - TO DETERMINE STRING EFFICIENCY OF SUSPENSION TYPE INSULATOR.

APPARATUS: - String of Suspension Type Insulator, Sphere Gap, HV transformers 230V/100KV10KVA,

Control Panel, Connecting rods etc.

CIRCUIT DIAGRAM: -

THEORY: - Suspension type insulator consists of number of porcelain discs connected inseries by metal links in the form of a string. The conductor is suspended at bottom end of

the string while the other end is secured to the cross arm of tower. Each disc is designed forlow voltage say 11KV. The number of discs in series would obviously depend on working

voltage e.g. for 66KV, 6discs are required. The ratio of voltage across the whole string to

the product of number of discs & voltage across discs nearest to the conductor is known as

string efficiency.

Voltage across stringString efficiency = _______________________________________________________

n * voltage across disc to nearest conductor

Where n = number of discs.

FUSE

RUGULATING

TRANSFORMER

230 V / 100KV

10KVA

HT SWITCH

V

230 V

AC

SUPPLY V

Scale

100 PF

100 KV

230

V

1OO

KV

Spheregap

VoltageDivider

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 10

String efficiency is an important consideration since it decides potential distribution

along string. The greater the string η, more uniform is the voltage distribution. Although

it is impossible to achieve 100% string η, yet efforts should be made to improve it as

close as possible to this value. The inequality of voltage distribution increases which inincrease in no. of discs in the string. Therefore shorter string has more efficiency than

longer one. String efficiency can be increased by1) Using longer cross-arm.2)Grading the insulator

3) Using a grid ring.

PROCEDURE: -1) Make the connections as shown in circuit diagram.

2) Set the distance between 10cm diameter sphere to maximum value.

3) Apply a constant voltage to the string say for 7 discs,11KV*7=77KV

4) Now reduce the distance between the spheres till flashover occurs.

5) Note the corresponding distance between the spheres at flashover.

6) Make supply off and make connections for second step, keep maximum distancebetween the spheres

7) Decrease the distance from control panel till flash over occurs. It gives the BDV for (n-

1) discs excepting the bottom discs.8) Repeat the procedure for all discs.

OBSERVATION TABLE: -

δ = P/760 * (273+20 / 273+ t)

P & t: - are atmospheric pressure and temperature while performing the

experimentsδ : - Air density factorK: - correction factor

FOR 10 CM DIAMETER SPHERE: -

Sr. No. Distance

between sphereat which spark

over takes place

in cm

Spark over KV

peak at 200C &

760mm HG std.

From

manufactures

table A

BDV peak at

room temp. &pressure in

KV

B= KA

RMS value

of BDV inKV

=B/ √2

String

efficiency

η

01

02

03

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 11

Voltage across the string V1

String efficiency ηηηη = __________________________________________________________ = ________________

n * voltage across the disc nearer to conductor n* (V1 - V2)

RESULT: - It is found that voltage across the each disc is not uniform. & string efficiency of

suspension type insulator is found to _________ % .

DISCUSSIONS:- 1) Why it is necessary to calculate string efficiency.2) How string efficiency can be increase.

3) What is efficiency for pin type insulator.

4) Is it necessary to calculate string efficiency in case of dc supply.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 12

EXPERIMENT NO: -5

AIM: - STUDY OF BREAK-DOWN VOLTAGE FOR DIFFERENT COMBINATION OF

ELECTRODES.1) SPHERE 10 CM DIA & SPHERE 5 CM DIA.

2) SPHERE 10 CM DIA & ROD.

3) SPHERE 10 CM DIA & POINT.

APPARATUS: - Sphere, Rod, & Point electrode, control unit, HV transformer 10KVA,230V/100KV,

Capacitor Voltage Divider, Connecting wires etc.

THEORY: - The sphere gap between two spheres is a classical example of weakly non uniformfield, the degree of non-uniformity increases with increase in the ratio in the distance ‘S’ between

the electrodes to their diameter D. the sphere gap happen to be commonly acknowledged means in

the inter-national practice for the measurement of amplitudes of direct ac & impulse voltages. Volt-Second chara. of a sphere gap over a large internal of time is a horizontal straight line &

consequently the breakdown voltage of the gap does not depend upon the duration of application of

voltage & on the low of its variation with time. Out of all the gaps having a weak non uniform field

the sphere gap can be prepared mast easily & is has least dimensions. In case of a gap between twoplanes each plane will require to have rounded off edges & for the value discharge distance,

diameter of the plane electrode will have to be a few times larger than the diameter of sphere.

PROCEDURE: -1) Place the two spheres of diameter 10cm & 5cm. respectively are shown in

circuit diagram.

2) Set the distance between them at 0.5cm.3) Increase the voltage with the help of tap changing transformer.

4) Observe the voltage at which breakdown takes place.

5) Now increase the gap between the two spheres in steps of 0.5cm & observe thebreakdown voltage.

6) Take 5 set of readings.

7) Now replace the 5cm sphere with

i) A rod electrodeii) A point electrode & Repeat from step1.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 13

OBSERVATION TABLE: -

1) FOR SPHERE 10CM & 5CM ELECTRODE

Sr. No. Gap between the electrode (cm) BDV RMS01

02

03

2) FOR SPHERE 10CM & RAD ELECTRODE

Sr. No. Gap between the electrode (cm) BDV RMS

01

02

03

3) FOR SPHERE 10CM & POINT ELECTRODE

Sr. No. Gap between the electrode (cm) BDV RMS

01

02

03

RESULT: - The flashover voltage for the various combination of electrodes have been observedby varying the distance between them & graph of breakdown voltage Vs distance betwen

electrodes for these combination have been plotted.

CONCLUSION: - It is known that as the surface area between the two electrodes is reduced the

electric

field between than becomes non- linear in nature. Thus for the sphere gap the surface area is

maximum and hence the graph revels maximum linearity. As the surface area decreasesfrom rod

gap to point gap graph becomes more non-linear.

QUESTIONS: -

1. What are the effects of humidity on the spark over voltage.

2. What are various methods other than sphere gap used for HV

measurement.3. Hoe the field between two electrodes changes as the electrodes are changed.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 14

EXPERIMENT NO: 6

AIM: - DETERMINATION OF FAULT LOCATION BY DIGITALCABLE FAULT

LOCATORMODEL 2000A.

APPARATUS: - Digital cable fault locator, Kit with circuit, connecting wires etc.

-

THEORY: - Fault locator is an essential complement to distance protective relay for transmission

lines and fault recorder. Fault location are installed along with distance protection scheme and faultrecorders, fault locator measures and indicates accurately the distance between the substation and

the point of fault. Fault locator is connected to the line secondary CTs & VTs of the line undernormal conditions, the fault locator monitors three phase currents & the ground current, voltage

input signals continuously. The operation of the fault locator is with following steps (1) Datacollection, (2) Starting of fault locator, (3) Sorting of measured instantaneous values, (4) Filtering

of measured signals, (5) Determination of type of fault, (6) Solution of fault equation, (7) Pre-

location of results.The input analog signals are converted into digital signals in A/D converter and stored

in memory for every six cycles continuously. When a fault occurs, trip circuit from the protectiverelay initiates the fault locator’s calculation program. The pre-fault sample values & during fault

sample values are used for calculating the distance of the fault. The calculation of distance is based

on the principle relays. The fault distance is shown as % of total line length on two digital front

mounted LED display.

Various types of fault that occur in a power systems are1) Shunt type fault

a) Single line to ground fault (LG)b) Line to line ground fault (LL)

c) Double line to ground fault (LLG)

2) Series type faulta) Open conductor fault (one or two conductors are open)

PROCEDURE: -

1) Connect all batteries i.e. 6V 10A & 12V, 3.8A.

2) Switch ON the instrument. 3) Create a fault at (20% to 100%) in between appropriate phases. 4) Connect stimulating Board according to diagram.

5) Keep Earth / open switch in earth position. 6) Keep V1/V2 voltage switch in V1 position.

7) Keep fault resistance selector in 1MΩ position.

8) Keep V1/V2 voltage range selector switch at 20V position. 9) Null display reading to zero.

10) Press push to read V1 display. 11) Change V1/V2 switch to V2 position.

12) Press push to read V2 display.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 15

RESULT: - All types of faults are located by digital cable fault locator.

CONCLUSION: - It is found that the calculation of distance is based on the principle of distance

relay. Alsofault location chosen in a % of total length is nearly equal to the distance of fault from end

(calculated)i.e. selected value of fault locations & calculated value of fault locations are found to be

same .

QUESTIONS: -1. What are the principles used to locate open circuit fault?

2. What are the principles used to locate short circuit fault.3. What are the methods to know the types of fault?

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 17

PROCEDURE: -

1) Clean the transformer after isolating from the system and other accessories.

2) Remove oil and dry it.3) Short the HV & LV terminals.

4) Short the Neutral to corresponding terminal.5) For UST Place the selector switch at UST (Ungrounded Sample Test CHL) For UST - means

measurement of H – L.6) Repeat the operating instruction (1 to 14).

7) For second set of observation – ie. For measurement of H – GND – keep selector switch at L –

Guard. And repeat the operating instruction.

OBSERVATIONS: - UST = Ungrounded Specimen Test.

GST = Grounded Specimen Test

1) FOR CAPACITANCE: -

Sr. No. Mode Multiplier

A

Switch

B

Dial

C

Capacitance calculation =

A X (B + 0.C )01 UST 0.001uf 7 561 .007561

02

CALCULATIONS: -

Capacitance = A X ( B+0.C)= .001*7 + .001* .561

= 0.007561 uF= 7561 PF= 75.61%

2) FOR DISSIPATION FACTOR (tan δδδδ): -

Sr. No. Mode DissipationFactor (DF)

Range

DialD

% tan δ = Lower Scale +0.D * (Difference of Scale)

01 UST 10-20 258

02

RESULT: - Capacitance and % tan δ between two winding are found to be as follows,

1) between H & L UST ----------, ----------%2) between H & L Guard ---------, ---------%

3) between L & H Guard ----------, ----------%

PRECAUTIONS: -

1) Transformer must be isolated from the supply and load.

2) Clean the transformer and transformer bushings.3) Results will be better in the dry atmosphere.

4) While shorting the HV & LV terminals sag is not allowed.5) Person should kept away several feet the test object, otherwise it may affects on the

results.6) It should be noted that in the GST mode of testing, the full test voltage is present

between the shells of the UHF connector and the body of the unit. Take care as to not tocome in contact with these two simultaneously.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 18

7) This instrument must always be connected to ground with the supplied leads and front

panel ground binding post prior to and during all measurements.

8) The apparatus being tested must be cleaned and correctly grounded to avoid anypossibility of lethal floating potential.

QUESTIONS: -

1. Which are the different circuits used for the measurement of capacitanceand dissipation factor.

2. What information we get from the dissipation factor and capacitance

related to insulation.3. List the methods to detect partial discharge.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 19

EXPERIMENT NO:8

AIM: - STUDY THE FERRANTI EFFECT AND SURGE IMPEDANCE LOADING IN

EHV LINE.

THEORY: -

1) FERRANTI EFFECT:

The phenomenon of rise in voltage at the receiving end of the open circuited or lightlyloaded line is called the Ferranti effect, owing to its first being observed on the Deptford

mains laid down by S. Z. De Ferranti in1890. This rise in voltage is due to the end of self-

inductance of the charging current being is phase with the applied voltage at the sending end

of the line & thus both capacitance & inductance are necessary to call this phenomenon.The effect becomes more pronounced as the line length increases.

To prove this analytically, consider the equation Vs for nominal π model of line,

Z=R+JX

Vs = A VR + B IR = (1+ YZ/2) VR + Z IR

At no load IR = 0

Vs = (1 + YZ/2) VR

Vs – VR = (YZ/2) VR

Where Z = (r + jwL)l & Y = jwCl l = length of line

If resistance of line neglected ; Z = jwLl

Vs – VR = ½ (jwLl) * ( jwCl) VR

Vs - VR = -1/2 (w2l2) LC VR

For overhead lines,

1/ √LC = Velocity of propagation of electromagnetic waves on the line

= Velocity of light = 3 * 108 m/s.

Vs – VR = - ½ [( 2πf)2

l2] / (3*10

8)2

VR

Thus (Vs – VR ) is negative. It means that VR>Vs. also it is clear that Ferranti effect

depends on frequency and length of line. It does not depend on conductor diameter and

spacing between conductor.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 20

2) SURGE IMPEDANCE LOADING:

Surge Impedance: - The square root of the ratio of the line impedance (Z) & shunt

admittance (Y) is called the surge impedance (Zo) of the line i.e. Zo = √(Z/Y) where Z =R +

jX & Y =G + jB. Surge impedance is the characteristic impedance of a loss free line. For a

heavy copper conductor & well insulated line the resistance (R) & leakage conductance (G)

can be taken as zero & therefore, surge impedance Zo = √(L/C) which is a pure resistance.

Its value varies between 400Ω & 600Ω in case of overhead transmission line and 40Ω &

60Ω in case of underground cable.

SIL: - This is defined as the load (of unity power factor) that can be delivered by the lineof negligible resistance. Power transmitted, PR =VRL2

/ Zo MW, where VRL is the receiving

end line voltage in KV & Zo is the surge impedance in Ω. PR is called the surge impedanceloading or natural power of the line.

The above expression gives the limit of the maximum power that can be deliveredby a line & is useful in the design of transmission line. This can be used for the comparison

of loads that can be carried on the transmission line at different voltages.

The power transmitted through a long transmission line can be increased either by

increasing is the value of receiving end voltage ( VRL) or by reducing surge impedance

(Zo).

Nowadays the trend is of employing higher & higher voltages for transmission,

therefore this is the most commonly adopted method for increasing the power limit beyondwhich it is neither economical nor practicable to increase the value of receiving end line

voltages.

Since the spacing between the conductors, which depends upon the line voltage

employed, cannot be reduced much, so the value of surge impedance (Zo) cannot be variedas such. However, some artificial means, such as series capacitors (capacitors in series with

the transmission lines) or shunt capacitors (capacitors in parallel with the transmission lines)can be used to reduced the value of surge impedance (Zo).

For a loss free transmission line, surge impedance, Zo = √ (L/C) & propagation

constant, γ = jw√LC = jB where B is the phase shift, which determines the torque angle δ between Vs & VR & hence the system stability.

By the use of series capacitors, surge impedance (Zo) & phase shift (B) getreduced due to decrease of line inductance (L). This improves the system stability limit also.

But it causes difficulties under short circuit conditions of the system as no satisfactoryprotection of capacitors has yet been devised. These capacitors are also helpful in reducing

line drops & so voltage variations.

By use of shunt capacitors, through the surge impedance (Zo) is reduced but the

phase shift (B) is increased due to increase in the value of C. Hence stability conditionsbecome worse, specially when synchronous machines are used as loads. So this method is

not used in case of long transmission lines, specially when stability limits are present.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 21

OBSERVATION TABLE: -

1) SURGE IMPEDANCE LOADING

Sr. No. Psend Vsend Isend Prec Vrec Irec

01

02

2) FERRANTI EFFECT

Sr. No. Vsend Vrec

01

02

CALCULATION: -For SIL, Power transmitted,

PR = V2

RL / Zo MW.

QUESTIONS: -

1. Clearly explain the Ferranti effect in the field of electrical power system.

2. What is surge impedance and surge impedance loading.

3. What is difference between characteristic impedance and surgeimpedance.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

G.H.RAISONI COLLEGE OF ENGINEERING, NAGPUR 22

EXPERIMENT NO:9

AIM: - MEASUREMENT OF DIELECTRIC CONSTANT, DISSIPATION FACTOR (TAN

δδδδ) AND

RESISTIVITY OF OIL.

APPARATUS: - Oil Loss Angle Meter (Model MLO – 1D), Million Megaohm Meter (Model LS

– 3D),Three Terminal Oil Test Cell, Heating Chamber etc.

THEORY: - Explain the schering bridge

PROCEDURE: -

A) Measurement of Dielectric Constant

Equipment: - Oil Loss Angle Meter, Three Terminal Oil Test Cell.

Before proceeding to make this test, clean the oil cell throughly. This may be ensured bytesting empty clean cell on Million Megohm Meter.

1) connect the oil loss angle meter to 230V AC, 50 Hz power supply.2) Switch on the equipment.

3) Keep ‘OPERATE’ switch in ‘SET ZERO’ position.

4) Keep the voltage at zero.

5) Mount the oil cell on insulated base plate and connect the empty cell to the oil loss anglemeter by the cable provided. The connection should be (a) Terminal HV connect to

outer case. (b) Terminal LV to inner case & (c) Guard terminal should be connect tomiddle terminal of oil test cell.

6) Now put ‘OPERATE’ switch in ‘HV ON’ position.

7) Gradually raise the voltage to about 300V.

8) With the help of ‘NULL’ control adjust the null meter to read 1.00.

9) Put ‘OPERATE’ switch in ‘SET ZERO’ position.10) Do not alter or disturb the voltage or control knob.11) Pour required quantity of oil in the cell

12) Now put ‘OPERATE’ switch in ‘HV ON’ position.13) Null meter will show a different reading. This new reading directly shows the Dielectric

Constant of the sample under test.

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DEPARTMENT OF ELECTRICAL ENGINEERING viiTH

sem B.E. electrical

B) MEASUREMENT OF DISSIPATION FACTOR (TAN δδδδ)

Equipment: - Oil Loss Angle Meter, Three Terminal Oil Test Cell, Heating Chamber etc.

Tan δ for oils is normally measured at 900

C as recommended by I. S. I., but for R& D purpose itcan be at any temperature upto 150

0C.

1) Clean the Oil Cell throughly, this can be ensured by measuring resistance on

Million Megohm Meter which should by practically infinite.

2) Pour oil to be tested in the cell gradually, the oil enters the space cavity inbetween the electrodes of cell through holes provided.

3) Keep Oil Cell in Heating Chamber.

4) Connect Heating Chamber to 230V AC, 50 Hz supply.

5) Switch on the Heating Chamber. Pilot lamp will come on.

6) Switch on the Heater by a switch marked Heater ON/OFF. LED will glow indicating

that Heater is ON.7) Connect the sensing probe to the Heating Chamber by means of connecting its 3 pin

lunar socket probe in the oil cell carefully.

8) The meter on Heating Chamber will indicate the temperature of the oil in cell.9) Connect Oil Loss Angle Meter to 230V AC, 50Hz power supply.

10) Keep the voltage Zero and ‘OPERATE’ switch in ‘SET ZERO’ position.11) Connect the Three Terminal Oil Cell to the instrument.

12) Slowly raised the voltage to create the desired stress level.13) When the temperature of oil cell in heating chamber reach to 900C, then heater supply

will be cut off automatically and heater ‘ON’ indication lamp will go off. The trip

setting may be changed if required by adjusting the ‘TRIP SET control.

14) Put ‘OPERATE’ switch in ‘HV ON’ position.15) When the temperature is 900C, with the help of ‘NULL’ control adjust the null indicator

to read 5.00.

16) Again put ‘OPERATE’ switch in SET ZERO. Set the zero on tan δ meter carefully with

the help of set zero control.

17) Put ‘OPERATE’ switch in ‘HV ON’ position and read the value of tan δ on the DP %directly in percentage.

QUESTIONS: -1. What are the various methods to calculate dielectric constant, dissipation

factor and resistivity of oil.

2. Write all the parameters for good quality transformer oil.3. What is meant by pure and commercial liquid.