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Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66
www.ijera.com 58|P a g e
A Study on Protection of Cables by Solkor Differential Protection
Relay with Fibre Optic Pilot Wireor Metallic Pilot Wire
Ahmed Rashad .E. Bakr(1)
, KhaledI.M.Alduraie(2)
Electrical Networks Department, High Institute of Energy, Public Authority of Applied Education and Training,
KUWAIT
ABSTRACT
This paper intends to briefly compare the protection of buried three phase high voltage cable with
Solkordifferential protection relay using metallic pilot wires orfibre optic pilot wires.
Dielectric property of the fiber optic provides complete electrical isolation as well as interference free signaling.
This provides total immunity from GPR (ground potential rise), longitudinal induction, and differential mode
noise coupling andhigh-voltage hazards to personnel safety.
So Fibre optic provides great advantage for Solkor differential protection relaying.
KEYWORDS: Fiber optic pilot wires, Metallic pilot wires, Solkor Differential Protection Relay
I. INTRODUCTION
Solkor Differential protection was developed
and now progressed into a microprocessor
controlled, differential feeder protection system
providing complete protection for cable feeders.
Induced voltage is generated on metallic pilot wire
installed alongwith power cable. As the core of fibre
optic pilot wire is made of glass, which is an
insulator, no induced voltage is present.
II. Operation of the differential relay
with fibre optic pilot wire
The relay compares magnitude and phase angle
of measured currents at either end of protected
feeder, it operates for faults detected within the
protected Zone, indicated in Fig. 1.
Fig. 1 Differential Protection Operating
Characteristic
Thetheory of operation of the differential relay
with fiber optic pilot wire isexplained with reference
to the simplified schematic diagram inFig. 2.
RESEARCH ARTICLE OPEN ACCESS
Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66
www.ijera.com 59|P a g e
RYB
Fig. 2 Simplified schematic diagram
F/I Frequency to Current Converter
MR MeasuringRelay
R1Resistor 500 ohms
V/F Voltage to Frequency Converter
R2 Resistor 470 ohms
LED Light Source
R3 Resistor 30 ohms
PVT Light Sensing Detector
R4 Resistor 2.7 kohms
C Capacitor, 0.68 µF
TR Summation Transformer
Z Zener Diodes
A balanced 3-phase through current gives the
following secondary currents:
𝐼1𝐴 = 𝐼1𝐵 = 𝐼 𝑅 ·
𝑁𝐼 + 𝑁2
1920
+ 𝐼𝑆 .
𝑁2
1920
+ (𝐼 𝑅 + 𝐼𝑠
+ 𝐼 𝑇).
𝑁3
1920
𝑁1 + 𝑁2
1920
. 𝐼 𝑅 +
𝑁2
1920
. 𝐼𝑆
Since 𝐼 𝑅 + 𝐼𝑠 + 𝐼 𝑇 = 0
The summation transformer with rated current
𝐼𝑛 = 5 A has the following turn ratios:
𝑁1 = 4 𝑡 , 𝑁2 = 4 𝑡, 𝑁3 = 12 𝑡, 𝑁4 = 960 𝑡
Hence, for balanced 3-phase secondary current 5 A:
𝐼1𝐴 = 𝐼1𝐵 =
4 + 4 . 5
1920
+
4.5
1920
− 0.5 − 𝑗 0.866
= 0.018 𝐴
The voltage to frequency converter (V/F) for
relay in Station A receives a voltage which is
proportional to the current 𝐼1𝐴 via the optical fiber
link and the frequency to current converter (F/I) of
relay in Station B, the current 𝐼′1𝐴, equal to 𝐼1𝐴 in
magnitude and with only a small phase angle shift (
~5°) is injected in relay for Station B. Similarly,
a current 𝐼1𝐵 , equal to 𝐼′1𝐵 in magnitude and only
Station A
Station B
Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66
www.ijera.com 60|P a g e
with a small phase angle shift is injected in relay for
Station A.
Hence, in case of through currents which are
equal in Stations A and B, the secondary currents
𝐼1𝐴 and 𝐼1𝐵 are equal, and the currents 𝐼2𝐴 and 𝐼2𝐵
have the same magnitude and only a phase angle
difference of about 5° relative the Currents 𝐼1𝐴 and
𝐼1𝐵. The current through the measuring relay (MR)
will be negligible.
The measuring relay (MR) operates when the relay
current is 10-11 mA.
2.1 Requirements on the fibre optic wires
The protection relay is designed for 50 𝜇𝑚 core,
125 𝜇𝑚 cladding, graded index multi mode
communication fiber with wavelength 850 nm or
1300 nm.
If the fiber is "double-window" (specified
at both 850 nm and 1300 nm), then a Wavelength
Division Multiplexing (WDM) application is
possible. With optical couplers and decouplers, the
protection relay can communicate via a direct, all-
optical medium at 1300 nm while over the same
fiber pair and at the very same time, non-
protective functions, including very-high-bit-rate
computer data, can be time division multiplexed at
850 nm wavelength.
For multi mode fibers, the following figures for
coupled optical power (min value) and receiver
sensitivity are valid:
850 nm: Optical power coupled:
receiver sensitivity:
total system gain:
19 dB (80 𝜇W)
-5 dB 320 (nW)
24 dB
1300 nm: Optical power coupled:
receiver sensitivity:
total system gain:
15.4 dB (35 𝜇W)
-12.6 dB (55 nW)
28 dB
A system margin of 5 dB is recommended.
Hence, the maximum permissible system loss is 19 dB for 850 nm multimode and 23 dB for 1300 nm
multimode systems.
Examples on typical calculations are given below.
Ex. 1: Fiber Optic System Loss Tabulation for 850 nm System
LED optical power coupled (minimum) 80 𝜇W= 19 dB𝜇
Connector loss = 2.0 dB
Fiber loss:
Attenuation 4.8 Km (3 Miles)
(3 dB/Km) = 14.5 dB
Splices 3 x 0.5 dB = 1.5 dB
Exit loss = 0.2 dB
System Margin = 5.0 dB
Total loss = 23.2 dB𝜇
Received power = -4.2 dB𝜇
Receiver sensitivity = -5 dB𝜇
Excess power
= 0.8 dB𝜇
Ex. 2: Fiber Optic System Loss Tabulation for 1300 nm System
LED optical power coupled (minimum) 15.4 dB𝜇
Connector loss = 2.0 dB
Fiber loss:
Attenuation 20 Km (12.4 miles)
(1.0 dB/Km = 20.0 dB
Splices 3 x 0.2 dB = 0.6 dB
Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66
www.ijera.com 61|P a g e
Exit loss = 0.2 dB
System Margin = 5.0 dB
Total loss = 25.8 dB𝜇
Received power = - 10.4 dB𝜇
Receiver sensitivity = -12.6 dB𝜇
Excess power = 2.2 dB𝜇
2.2Requirements on the current transformers
For stability in case of external faults with large through fault currents, the CT's at both line ends
should be of the same type and have approximately the same saturation factor (ALF) at the actual secondary
load.
The current transformer secondary limiting emf (E2max ) shall meet the requirement.
>𝐼 𝐾𝑚𝑎𝑥 ∙ 𝑎 ∙
𝐼𝑠𝑛
𝐼𝑝𝑛
∙
5
𝐼 𝑁2
+ 𝑅 𝐶𝑇+ 𝑅 𝐿
where
a = 1 for 50 Hz
a = 1.6 for 60 Hz
𝐼 𝐾𝑚𝑎𝑥 = max. Fundamental frequency current fed into the line end in case of internal fault.
𝐼𝑠𝑛
=
rated secondary current of the CT
𝐼𝑝𝑛
=
rated primarycurrent of the CT
𝑅 𝐶𝑇
=
CT secondary winding resistance
𝑅 𝐿
=
Secondary winding resistance (loop resistance for direct earthed systems)
and additional load on the same core as protection relay.
For the above requirement, a dc time-constant of max 120 ms for the net is assumed.
III. Operation of the differential relay with metallic pilot wire
The theory of operation of the differential relay with metallic pilot wire (SolkorRf) isexplained with
reference to the simplified schematic diagram in Fig. 3.
Figure 3.SolkorRf Schematic
D1,D2,D3,D4,D5,D6,D7,D8- DIODES
Pg- Non Leaners Resistor
Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66
www.ijera.com 62|P a g e
Ra - Fixed Standard Resistor.
Rp - Padding Resistor.
TR - Summation Transformer
MR - Measuring relay
In addition to the basic components there are at each end, three non-linear resistors, a tapped „pg‟ resistor
and three diodes. The non-linear resistors are used to limit the voltage appearing across the pilots and the
operating element. The purpose of the „padding‟ resistors at each end is to bring the total pilot loop resistance up
to a standard value. The protection is therefore always working under constant conditions and its performance is
to a large extent of the resistance of the pilot cable‟ The „padding‟ resistors comprise five series connected
sections, each section having a short circuiting link. The values of the resistance on the sections are 35 ohms, 65
ohms, 130 ohms, 260ohms and 500ohms.
For SolkorRf without isolating transformers the value chosen should be as near as possible to ½(2000-Rp)
ohms.
Referring to the basic circuit of SolkorRf as shown in Figure 3, the circulating current will flow from the
summation transformer through the diode or the resistor depending on the polarity of the summation transformer
output.
The main purpose of the summation transformer is to enable either balanced or unbalanced three phase
currents to be re-produced as a single phase quantityas shown in Figure 4.
As this device is essentially a transformer it can also be used to reduce the burden imposed by the pilot circuit
on the current transformers by changing the
impedance levels. it provides isolation between the current transformers and the pilot circuit.
Figure 4.Summation transformer
Pilot wires are exposed to a number of hazards that can interfere with the proper operation of the scheme or cause
damage to the pilot circuit and associated equipment. The most common hazards are:
1. Rise in station ground potential (GPR).
Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66
www.ijera.com 63|P a g e
2. Induced voltages.
3. Lightning.
A substantial voltage rise can occur at the substation ground mat relative to the remote ground potential. This voltage
rise can cause excessive insulation stresses on the pilot wire relay, the pilot wire monitoring relay, the pilot wires, and
between pilot wires and other conductors in the same cable.
Fig 5. - Station mat .ground potential rise
As illustrated in Figure 4, the typical condition resulting in ground potential rise is a single-phase-to-ground fault
on the power system. With ground current flowing through the Station A ground mat, there will be a voltage difference
between this mat and the remote ground potential. The magnitude of this voltage depends on the magnitude of the
current and on the impedance between the station ground and the remote ground. The value of the ground current is usually
available from system fault studies. The impedance between the mat and the remote ground is determined by calculation
or test.
Fig 6.Typical Ground Potential Profile During SLG Fault
The diagram in Figure 5 represents a typical voltage profile of the potential difference between the pilot cable and
ground during a single-phase-to-ground fault. As is apparent from the plot, the potential of earth near the pilot wire
cable tends to be at the remote ground potential for most of the length of the pilot run. Hence, if the cable is not
grounded, it will assume a potential near that of the remote ground because of the capacitive coupling. Thus, the potential
rise of the station ground mat results in a significant voltage difference between the station ground mat and the pilot cable
with its connected station equipment. If this voltage difference becomes too great, there is danger to personnel and the
possibility of damage to the pilot wire relays, the connected equipment, and the pilot wire itself. If this voltage
difference exceeds 600 volts, protection of the pilot wires is usually necessary since this is the continuous voltage
insulation level of the connected relays, terminal boards, panels and standard telephone cables.
The value of the induced voltage in metallic pilot wires is calculated using the following formula.
V = C.L.i.K
Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66
www.ijera.com 64|P a g e
Where: V induced longitudinal voltage [V]
C mutual impedance per unit length [ohm/km]
L length of exposure (between power and communication cable) [km]
i fault current [A]
K shielding factor {K-1 for no shielding}
The mutual impedance, C of two parallel circuits having earth returns is given by
C = 2𝜋𝑓│𝑙𝑜𝑔𝑒 (1 +
6 𝑥105
𝑝
𝑑2 𝑓
)│𝑥10−4
[𝑜𝑕𝑚/𝑘𝑚]
Where: d geometric separation between earth return circuits in metres
p earth resistivity in ohm-metres
f system frequency in Hz
If the shield is not grounded on both ends the shield current is zero and the shielding factor K is 1.
IV. Comparison between SolkorR/RF relay uses metallic pilot wires&SolkorNrelay uses
Fibre optic pilot wires
Table.1
S.NO. DESCRIPTION
SOLKOR-R/RF
WITH METALLIC PILOT
WIRES
SOLKOR-N
WITH FIBRE OPTIC
PILOT WIRES
1) Circuit type Static / Electro-Mechanical Numerical
2) Barrier Transformer Required for higher Voltage
level
Not required
3) CT Ratio both side To be same With Different CT ratio, it can
be programmable to match
with other END.
4) Pilot Supervision Separate relay required Inbuilt
5) Padding Resistance To set value according to pilot
resistance
Not required
6) Pickup Different Values for Each
Phases
Same for all Phases
7) Metering Not possible Measurement display
available
8) Trip circuit supervision Not possible Available
9) Breaker failure Not possible Available
10) Fault recorder Not possible Available
11) Protection Signal Delay Not possible Available
12) Programmable Out put Not possible Available
13) Distance Shorter Longer
14) Immunity, Reliability, Safety Less High
V. Comparison of Site Test Results between Solkor R/RF relay uses metallic pilot wires
&Solkor Nrelay uses Fibre optic pilot wires
Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66
www.ijera.com 65|P a g e
Site Test results are tabulated as below for Solkor R/RF relay uses metallic pilot wires &Solkor N relay
uses Fibre optic pilot wires
5.1SolkorRf mode in 7PG21 relay of Siemens makeuses metallic pilot wires
Table.2
Phase
Injected Current
(A)
Operating DC Current
(mA)
Pilot AC
Voltage(V)
Relay
Operation
Pilot
Circuit
R-N 0.125 11.35 45.22 TRIP OPEN
Y-N 0.154 11.35 45.20 TRIP OPEN
B-N 0.206 11.27 45.20 TRIP OPEN
R-Y 0.616 11.27 45.12 TRIP OPEN
Y-B 0.616 11.28 45.13 TRIP OPEN
R-B 0.308 11.27 45.13 TRIP OPEN
R-N 1.0 0 0 NO TRIP SHORT
R-N 1.0 41.03 135.8 TRIP OPEN
Operating Time at 1A: R-N : 28.9 mSec
5.2 Solkor N 7SG18 relay of Siemens make uses Fibre optic pilot wires
Idiff> Pick up Test:Diff. Setting=1.0
Table.3
Station Phase Pick-Up (A) Drop-Off (A)
Station A
R 0.998 0.936
Y 0.998 0.939
B 1.003 0.939
Differential Biasing Characteristic Test:
Table.4
Ib/In
Calculated Id/In Operated Id/In
Ph-E 3Ph R Y B RYB
1.0 1.250 1.250 1.247 1.247 1.247 1.235
2.0 1.750 1.750 1.618 1.618 1.627 1.618
3.0 2.750 2.750 3.00 2.994 3.00 3.00
4.0 4.250 4.250 4.433 4.637 4.645 4.552
Idiff> Timing Test:
Table.5
Station
Injected Current
Idiff> Operating Time ( mSec)
R Y B RYB
Station A
2*Idiff 47 45 48 47
5*Idiff 36 38 36 39
VI. CONCLUSION
Protection of buried three phase High Voltage
cable is studied with differential relay using metallic
pilot wires and fibre optic pilot wires.
Fibre optic pilot wire provides total safety for
operating personnel from High Voltage hazards due
to induced voltages. In addition to this, the numerical
relay which uses fibre optic has advanced features
such as measurements with display, event records,
fault records and compatibility for smart grid
substations.Fibre optic pilot wire can be incorporated
into network in planned upgrades.
Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com
ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66
www.ijera.com 66|P a g e
REFERENCES
[1] RADHO protection relay Buyer's Guide,
ABB
[2] Solkor N manual, Siemens
[3] Solkor R/Rf manual, Siemens
[4] Klewe, H.R.J. Interference between Power
systems and Telecommunications Lines,
Edward Arnold Ltd., London, 1958
[5] Electrical Transmission and Distribution
reference book, Westinghouse Electric
Corporation, 1964.
[6] “Application Guide AC Pilot Wire Relaying
System SPD and SPA Relays”, GE
publication GET-6462A.
[7] GE Publication GEK-112994A, 2005, L90
Line Differential Relay, Instruction Manual.

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A Study on Protection of Cables by Solkor Differential Protection Relay with Fibre Optic Pilot Wireor Metallic Pilot Wire

  • 1. Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66 www.ijera.com 58|P a g e A Study on Protection of Cables by Solkor Differential Protection Relay with Fibre Optic Pilot Wireor Metallic Pilot Wire Ahmed Rashad .E. Bakr(1) , KhaledI.M.Alduraie(2) Electrical Networks Department, High Institute of Energy, Public Authority of Applied Education and Training, KUWAIT ABSTRACT This paper intends to briefly compare the protection of buried three phase high voltage cable with Solkordifferential protection relay using metallic pilot wires orfibre optic pilot wires. Dielectric property of the fiber optic provides complete electrical isolation as well as interference free signaling. This provides total immunity from GPR (ground potential rise), longitudinal induction, and differential mode noise coupling andhigh-voltage hazards to personnel safety. So Fibre optic provides great advantage for Solkor differential protection relaying. KEYWORDS: Fiber optic pilot wires, Metallic pilot wires, Solkor Differential Protection Relay I. INTRODUCTION Solkor Differential protection was developed and now progressed into a microprocessor controlled, differential feeder protection system providing complete protection for cable feeders. Induced voltage is generated on metallic pilot wire installed alongwith power cable. As the core of fibre optic pilot wire is made of glass, which is an insulator, no induced voltage is present. II. Operation of the differential relay with fibre optic pilot wire The relay compares magnitude and phase angle of measured currents at either end of protected feeder, it operates for faults detected within the protected Zone, indicated in Fig. 1. Fig. 1 Differential Protection Operating Characteristic Thetheory of operation of the differential relay with fiber optic pilot wire isexplained with reference to the simplified schematic diagram inFig. 2. RESEARCH ARTICLE OPEN ACCESS
  • 2. Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66 www.ijera.com 59|P a g e RYB Fig. 2 Simplified schematic diagram F/I Frequency to Current Converter MR MeasuringRelay R1Resistor 500 ohms V/F Voltage to Frequency Converter R2 Resistor 470 ohms LED Light Source R3 Resistor 30 ohms PVT Light Sensing Detector R4 Resistor 2.7 kohms C Capacitor, 0.68 µF TR Summation Transformer Z Zener Diodes A balanced 3-phase through current gives the following secondary currents: 𝐼1𝐴 = 𝐼1𝐵 = 𝐼 𝑅 · 𝑁𝐼 + 𝑁2 1920 + 𝐼𝑆 . 𝑁2 1920 + (𝐼 𝑅 + 𝐼𝑠 + 𝐼 𝑇). 𝑁3 1920 𝑁1 + 𝑁2 1920 . 𝐼 𝑅 + 𝑁2 1920 . 𝐼𝑆 Since 𝐼 𝑅 + 𝐼𝑠 + 𝐼 𝑇 = 0 The summation transformer with rated current 𝐼𝑛 = 5 A has the following turn ratios: 𝑁1 = 4 𝑡 , 𝑁2 = 4 𝑡, 𝑁3 = 12 𝑡, 𝑁4 = 960 𝑡 Hence, for balanced 3-phase secondary current 5 A: 𝐼1𝐴 = 𝐼1𝐵 = 4 + 4 . 5 1920 + 4.5 1920 − 0.5 − 𝑗 0.866 = 0.018 𝐴 The voltage to frequency converter (V/F) for relay in Station A receives a voltage which is proportional to the current 𝐼1𝐴 via the optical fiber link and the frequency to current converter (F/I) of relay in Station B, the current 𝐼′1𝐴, equal to 𝐼1𝐴 in magnitude and with only a small phase angle shift ( ~5°) is injected in relay for Station B. Similarly, a current 𝐼1𝐵 , equal to 𝐼′1𝐵 in magnitude and only Station A Station B
  • 3. Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66 www.ijera.com 60|P a g e with a small phase angle shift is injected in relay for Station A. Hence, in case of through currents which are equal in Stations A and B, the secondary currents 𝐼1𝐴 and 𝐼1𝐵 are equal, and the currents 𝐼2𝐴 and 𝐼2𝐵 have the same magnitude and only a phase angle difference of about 5° relative the Currents 𝐼1𝐴 and 𝐼1𝐵. The current through the measuring relay (MR) will be negligible. The measuring relay (MR) operates when the relay current is 10-11 mA. 2.1 Requirements on the fibre optic wires The protection relay is designed for 50 𝜇𝑚 core, 125 𝜇𝑚 cladding, graded index multi mode communication fiber with wavelength 850 nm or 1300 nm. If the fiber is "double-window" (specified at both 850 nm and 1300 nm), then a Wavelength Division Multiplexing (WDM) application is possible. With optical couplers and decouplers, the protection relay can communicate via a direct, all- optical medium at 1300 nm while over the same fiber pair and at the very same time, non- protective functions, including very-high-bit-rate computer data, can be time division multiplexed at 850 nm wavelength. For multi mode fibers, the following figures for coupled optical power (min value) and receiver sensitivity are valid: 850 nm: Optical power coupled: receiver sensitivity: total system gain: 19 dB (80 𝜇W) -5 dB 320 (nW) 24 dB 1300 nm: Optical power coupled: receiver sensitivity: total system gain: 15.4 dB (35 𝜇W) -12.6 dB (55 nW) 28 dB A system margin of 5 dB is recommended. Hence, the maximum permissible system loss is 19 dB for 850 nm multimode and 23 dB for 1300 nm multimode systems. Examples on typical calculations are given below. Ex. 1: Fiber Optic System Loss Tabulation for 850 nm System LED optical power coupled (minimum) 80 𝜇W= 19 dB𝜇 Connector loss = 2.0 dB Fiber loss: Attenuation 4.8 Km (3 Miles) (3 dB/Km) = 14.5 dB Splices 3 x 0.5 dB = 1.5 dB Exit loss = 0.2 dB System Margin = 5.0 dB Total loss = 23.2 dB𝜇 Received power = -4.2 dB𝜇 Receiver sensitivity = -5 dB𝜇 Excess power = 0.8 dB𝜇 Ex. 2: Fiber Optic System Loss Tabulation for 1300 nm System LED optical power coupled (minimum) 15.4 dB𝜇 Connector loss = 2.0 dB Fiber loss: Attenuation 20 Km (12.4 miles) (1.0 dB/Km = 20.0 dB Splices 3 x 0.2 dB = 0.6 dB
  • 4. Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66 www.ijera.com 61|P a g e Exit loss = 0.2 dB System Margin = 5.0 dB Total loss = 25.8 dB𝜇 Received power = - 10.4 dB𝜇 Receiver sensitivity = -12.6 dB𝜇 Excess power = 2.2 dB𝜇 2.2Requirements on the current transformers For stability in case of external faults with large through fault currents, the CT's at both line ends should be of the same type and have approximately the same saturation factor (ALF) at the actual secondary load. The current transformer secondary limiting emf (E2max ) shall meet the requirement. >𝐼 𝐾𝑚𝑎𝑥 ∙ 𝑎 ∙ 𝐼𝑠𝑛 𝐼𝑝𝑛 ∙ 5 𝐼 𝑁2 + 𝑅 𝐶𝑇+ 𝑅 𝐿 where a = 1 for 50 Hz a = 1.6 for 60 Hz 𝐼 𝐾𝑚𝑎𝑥 = max. Fundamental frequency current fed into the line end in case of internal fault. 𝐼𝑠𝑛 = rated secondary current of the CT 𝐼𝑝𝑛 = rated primarycurrent of the CT 𝑅 𝐶𝑇 = CT secondary winding resistance 𝑅 𝐿 = Secondary winding resistance (loop resistance for direct earthed systems) and additional load on the same core as protection relay. For the above requirement, a dc time-constant of max 120 ms for the net is assumed. III. Operation of the differential relay with metallic pilot wire The theory of operation of the differential relay with metallic pilot wire (SolkorRf) isexplained with reference to the simplified schematic diagram in Fig. 3. Figure 3.SolkorRf Schematic D1,D2,D3,D4,D5,D6,D7,D8- DIODES Pg- Non Leaners Resistor
  • 5. Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66 www.ijera.com 62|P a g e Ra - Fixed Standard Resistor. Rp - Padding Resistor. TR - Summation Transformer MR - Measuring relay In addition to the basic components there are at each end, three non-linear resistors, a tapped „pg‟ resistor and three diodes. The non-linear resistors are used to limit the voltage appearing across the pilots and the operating element. The purpose of the „padding‟ resistors at each end is to bring the total pilot loop resistance up to a standard value. The protection is therefore always working under constant conditions and its performance is to a large extent of the resistance of the pilot cable‟ The „padding‟ resistors comprise five series connected sections, each section having a short circuiting link. The values of the resistance on the sections are 35 ohms, 65 ohms, 130 ohms, 260ohms and 500ohms. For SolkorRf without isolating transformers the value chosen should be as near as possible to ½(2000-Rp) ohms. Referring to the basic circuit of SolkorRf as shown in Figure 3, the circulating current will flow from the summation transformer through the diode or the resistor depending on the polarity of the summation transformer output. The main purpose of the summation transformer is to enable either balanced or unbalanced three phase currents to be re-produced as a single phase quantityas shown in Figure 4. As this device is essentially a transformer it can also be used to reduce the burden imposed by the pilot circuit on the current transformers by changing the impedance levels. it provides isolation between the current transformers and the pilot circuit. Figure 4.Summation transformer Pilot wires are exposed to a number of hazards that can interfere with the proper operation of the scheme or cause damage to the pilot circuit and associated equipment. The most common hazards are: 1. Rise in station ground potential (GPR).
  • 6. Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66 www.ijera.com 63|P a g e 2. Induced voltages. 3. Lightning. A substantial voltage rise can occur at the substation ground mat relative to the remote ground potential. This voltage rise can cause excessive insulation stresses on the pilot wire relay, the pilot wire monitoring relay, the pilot wires, and between pilot wires and other conductors in the same cable. Fig 5. - Station mat .ground potential rise As illustrated in Figure 4, the typical condition resulting in ground potential rise is a single-phase-to-ground fault on the power system. With ground current flowing through the Station A ground mat, there will be a voltage difference between this mat and the remote ground potential. The magnitude of this voltage depends on the magnitude of the current and on the impedance between the station ground and the remote ground. The value of the ground current is usually available from system fault studies. The impedance between the mat and the remote ground is determined by calculation or test. Fig 6.Typical Ground Potential Profile During SLG Fault The diagram in Figure 5 represents a typical voltage profile of the potential difference between the pilot cable and ground during a single-phase-to-ground fault. As is apparent from the plot, the potential of earth near the pilot wire cable tends to be at the remote ground potential for most of the length of the pilot run. Hence, if the cable is not grounded, it will assume a potential near that of the remote ground because of the capacitive coupling. Thus, the potential rise of the station ground mat results in a significant voltage difference between the station ground mat and the pilot cable with its connected station equipment. If this voltage difference becomes too great, there is danger to personnel and the possibility of damage to the pilot wire relays, the connected equipment, and the pilot wire itself. If this voltage difference exceeds 600 volts, protection of the pilot wires is usually necessary since this is the continuous voltage insulation level of the connected relays, terminal boards, panels and standard telephone cables. The value of the induced voltage in metallic pilot wires is calculated using the following formula. V = C.L.i.K
  • 7. Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66 www.ijera.com 64|P a g e Where: V induced longitudinal voltage [V] C mutual impedance per unit length [ohm/km] L length of exposure (between power and communication cable) [km] i fault current [A] K shielding factor {K-1 for no shielding} The mutual impedance, C of two parallel circuits having earth returns is given by C = 2𝜋𝑓│𝑙𝑜𝑔𝑒 (1 + 6 𝑥105 𝑝 𝑑2 𝑓 )│𝑥10−4 [𝑜𝑕𝑚/𝑘𝑚] Where: d geometric separation between earth return circuits in metres p earth resistivity in ohm-metres f system frequency in Hz If the shield is not grounded on both ends the shield current is zero and the shielding factor K is 1. IV. Comparison between SolkorR/RF relay uses metallic pilot wires&SolkorNrelay uses Fibre optic pilot wires Table.1 S.NO. DESCRIPTION SOLKOR-R/RF WITH METALLIC PILOT WIRES SOLKOR-N WITH FIBRE OPTIC PILOT WIRES 1) Circuit type Static / Electro-Mechanical Numerical 2) Barrier Transformer Required for higher Voltage level Not required 3) CT Ratio both side To be same With Different CT ratio, it can be programmable to match with other END. 4) Pilot Supervision Separate relay required Inbuilt 5) Padding Resistance To set value according to pilot resistance Not required 6) Pickup Different Values for Each Phases Same for all Phases 7) Metering Not possible Measurement display available 8) Trip circuit supervision Not possible Available 9) Breaker failure Not possible Available 10) Fault recorder Not possible Available 11) Protection Signal Delay Not possible Available 12) Programmable Out put Not possible Available 13) Distance Shorter Longer 14) Immunity, Reliability, Safety Less High V. Comparison of Site Test Results between Solkor R/RF relay uses metallic pilot wires &Solkor Nrelay uses Fibre optic pilot wires
  • 8. Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66 www.ijera.com 65|P a g e Site Test results are tabulated as below for Solkor R/RF relay uses metallic pilot wires &Solkor N relay uses Fibre optic pilot wires 5.1SolkorRf mode in 7PG21 relay of Siemens makeuses metallic pilot wires Table.2 Phase Injected Current (A) Operating DC Current (mA) Pilot AC Voltage(V) Relay Operation Pilot Circuit R-N 0.125 11.35 45.22 TRIP OPEN Y-N 0.154 11.35 45.20 TRIP OPEN B-N 0.206 11.27 45.20 TRIP OPEN R-Y 0.616 11.27 45.12 TRIP OPEN Y-B 0.616 11.28 45.13 TRIP OPEN R-B 0.308 11.27 45.13 TRIP OPEN R-N 1.0 0 0 NO TRIP SHORT R-N 1.0 41.03 135.8 TRIP OPEN Operating Time at 1A: R-N : 28.9 mSec 5.2 Solkor N 7SG18 relay of Siemens make uses Fibre optic pilot wires Idiff> Pick up Test:Diff. Setting=1.0 Table.3 Station Phase Pick-Up (A) Drop-Off (A) Station A R 0.998 0.936 Y 0.998 0.939 B 1.003 0.939 Differential Biasing Characteristic Test: Table.4 Ib/In Calculated Id/In Operated Id/In Ph-E 3Ph R Y B RYB 1.0 1.250 1.250 1.247 1.247 1.247 1.235 2.0 1.750 1.750 1.618 1.618 1.627 1.618 3.0 2.750 2.750 3.00 2.994 3.00 3.00 4.0 4.250 4.250 4.433 4.637 4.645 4.552 Idiff> Timing Test: Table.5 Station Injected Current Idiff> Operating Time ( mSec) R Y B RYB Station A 2*Idiff 47 45 48 47 5*Idiff 36 38 36 39 VI. CONCLUSION Protection of buried three phase High Voltage cable is studied with differential relay using metallic pilot wires and fibre optic pilot wires. Fibre optic pilot wire provides total safety for operating personnel from High Voltage hazards due to induced voltages. In addition to this, the numerical relay which uses fibre optic has advanced features such as measurements with display, event records, fault records and compatibility for smart grid substations.Fibre optic pilot wire can be incorporated into network in planned upgrades.
  • 9. Ahmed Rashad .E. Bakr Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 5, Issue 2, ( Part -3) February 2015, pp.58-66 www.ijera.com 66|P a g e REFERENCES [1] RADHO protection relay Buyer's Guide, ABB [2] Solkor N manual, Siemens [3] Solkor R/Rf manual, Siemens [4] Klewe, H.R.J. Interference between Power systems and Telecommunications Lines, Edward Arnold Ltd., London, 1958 [5] Electrical Transmission and Distribution reference book, Westinghouse Electric Corporation, 1964. [6] “Application Guide AC Pilot Wire Relaying System SPD and SPA Relays”, GE publication GET-6462A. [7] GE Publication GEK-112994A, 2005, L90 Line Differential Relay, Instruction Manual.