SlideShare a Scribd company logo
1 of 5
Download to read offline
USE OF SPIRAL PROTECTORS FOR PREVENTING FATIGUE DAMAGE
OF TRANSMISSION LINE CABLES
E. L. Nikiforov1
Translated from Élektricheskie Stantsii, No. 6, 2002, pp. 70 – 74.
Results of a measurement of the distribution of component forces in an “ACSR with wound spiral protector
from steel wires” system fastened in a suspension clamp of an overhead transmission line are presented. Cor-
relation dependences for the tensile force acting in the cable under the protector are obtained. It is shown that
the tensile force in the cable under the protector decreases from the value T in the span to a minimum value in
the middle of the suspension clamp. At a tensile force T equal to 30% of the standard strength of the wire the
tensile force in the suspension clamp is 8.1%, and the wires in the OL cable do not suffer from fatigue damage.
Spiral protectors from steel wires are recommended for protecting OL cables from fatigue damage under the
action of standing vibration waves.
Key words: overhead transmission lines, cables, ground wire, strain, vibration, metal fatigue, fatigue protec-
tion, spiral protector, distribution of forces in the protector-cable combination, vibration protection of
connectors.
Spiral protectors from steel wires fastened over the inter-
nal surface by an abrasive adhesive are widely used for pro-
tecting suspension clamps of the optical fibers of cables of
grade ADSS and cables built into the ground wire (OPGW).
Spiral wires 2 – 5 pieces in a strand with a pitch of
100 – 150 mm are wound on the ground wire fully covering
its surface on a length of 2 – 2.5 m. The suspension clamp is
mounted in the middle of the protector. The inner diameter of
the protector is about 1 mm less than the diameter of the
ADSS (or OPGW) cable, which is responsible for the ap-
pearance of a friction force on the OPGW/protector bound-
ary. The presence of a friction force on the surfaces of the
“OPWG – spiral protector wires” system should create a ten-
sile strain in the protector wires upon the stretching of the
OPGW, i.e., the protector should receive a part of the force
stretching the OPGW. Since the OPGW as a mechanical
structure is an analog of grade AS cable (aluminum-steel),
stretching of the “AS cable – spiral protector” system should
decrease the tensile force in the cable in the place of fasten-
ing of the protector and of the suspension clamp and raise the
reliability of operation of the AS (or A) cable.
In order to evaluate the distribution of tensile forces in
the “spiral protector — AS cable – suspension clamp,” the
system specialists of VNIIÉ tested such a system for the ten-
sile strength in a static mode. The spiral protector was wound
under a tensile force of 2 kN in the cable.
The 2.3-m-long protector consisted of 18 steel wires
about 2.8 mm in diameter (their total section was 110.8 mm2)
at a pitch of 136 mm; the winding was directed from the
left – upward – to the right like the winding of the external
layer of the aluminum wires in the AS 120/19 cable. The
protector was used for the second time after a tensile test
(stretching to 27 kN) of an ADSS optical coupling cable.
Devices for measuring the elongation Äl of the cable
were mounted on the AS 120/19 cable, on the protector, and
in two places of the protector combined with the cable on a
length l0. For the cable l0 = 1000 mm; for the protector-cable
combination l0 = 400 mm. The elongation Äl was measured
by an indicator accurate to 0.01 mm. The result of the mea-
surement was expressed in relative units å = l/l0. The accu-
racy of the measurement of the elongation of the cable was
0.01/1000 = 10–5 mm/mm; the accuracy of the measurement
of the elongation of the protector-cable combination was
0.01/400 = 0.25 ´ 10–4 mm/mm.
The tensile force T applied to the AS 120/19 cable was
measured by a dynamometer accurate to 2%.
Figure 1 presents the curves T = f (å) for the AS120/19
cable and the curves T = f1(åm) and T = f2(åm) for the ca-
ble-protector combination. The value of Äl was measured in
two places of the protector, i.e., at a distance of 15 – 415 mm
from the middle of the body of the suspension clamp for
f1(åm) and at a distance of 15.0 – 415 mm from the protector
edge for f2(åm).
It follows from the obtained results (Fig. 1) that at the
same force T, which acts both on the cable in the span and on
the protector-cable combination, the relative strain åm on the
length l0 = 400 mm for the protector-cable combination is
substantially lower than that for the cable outside the protec-
tor. The dependences T = f1(åm) and T = f2(åm) obtained on
157
1570-145X/02/3603-0157$27.00 © 2002 Plenum Publishing Corporation
Power Technology and Engineering Vol. 36, No. 3, 2002
1
All-Russia Electric Power Research Institute (VNIIÉ), Moscow, Russia.
the two segments l0 of the protector-cable combination differ
substantially from each other. With the closeness of l0 to the
suspension clamp at equal T the relative strain åm decreases,
i.e., åm varies over the length of the protector. Therefore, we
should presume that within Äl0 the relative strain in each sec-
tion of the protector-cable combination decreases with close-
ness of the section to the suspension clamp. Consequently,
for the protector-cable combination the measured values of
åm on the length l0 of the protector should be referred to the
middle of l0. In what follows the relative strains measured for
the protector-cable combination will be denoted å1m (at a dis-
tance l = 400 mm from the middle of the suspension clamp)
and å2m (at a distance l = 900 mm from the middle of the sus-
pension clamp).
According to the data of Fig. 1 the dependence of the
tensile strength T acting on the tested cable AS 120/19 on
the relative strain å is approximated by an exponential func-
tion
T1 = a1 exp b1å, (1)
where a1 = 1.89221, b1 = 860.741, and the correlation coeffi-
cient r1 = 0.98644 (for the given cable).
Equation (1) is applicable to both the cable in the span
and to the part of the cable under the protector.
Measurements show that for the “protector-cable AS120/19”
combination the dependence of the mean value of the rela-
tive strain åm (Fig. 1) in the middle of l0 on the tensile force T
can be approximated by the expression
åm = a2T + b2. (2)
The values of parameters in Eq. (2) for the distances
l1 = 400 mm and l2 = 900 mm from the middle of the suspen-
sion clamp are presented below (r2 is the correlation coeffi-
cient).
l1 = 400 mm l2 = 900 mm
a2 9.042 ´ 10–5
1.152 ´ 10–4
b2 1.531 ´ 10–5
3.172 ´ 10–4
r2 0.99842 0.99705
We use Eq. (2) to calculate å1m in the middle of the seg-
ment l0 for a given force T acting on the protector-cable com-
bination and on the wire outside the protector-cable combi-
nation at a distance l = 400 mm from the middle of the sus-
pension clamp. The obtained value of å1m is substituted into
Eq. (1) to calculate the force ¢T1 acting on the cable in the sec-
tion of the protector-cable combination at a distance
l = 400 mm from the middle of the suspension clamp. Simi-
lar calculations are performed for T equal to 10, 15, and
19 kN in order to find å2m and ¢¢T1 in the section lying at
l = 900 mm from the middle of the suspension clamp
(Fig. 1).
The equation
T2 = T – T1 (3)
is used to calculate the component T2 of the force T acting in
the protector in the considered section of the protector-cable
combination ( ¢T2 at a distance l = 400 mm and ¢¢T2 at a dis-
tance l = 900 mm from the middle of the suspension clamp).
Table 1 presents the computational results obtained with
the help of Eqs. (1) – (3).
It can be see from the data of Table 1 that the value of the
force ¢T1 in the cable under the protector is more than two
times lower than the force T outside the protector.
We used the data of Table 1 to obtain the dependences
T1 = f (l ) and T2 = f (l ) at a given value of the tensile force T.
The dependences T1 = f (l ) for the cable under the protector
at T = 10, 15, and 19 kN were approximated by the equation
T1 = a4 exp b4l, (4)
The values of a4 and b4 for Eq. (4) are presented in
Table 2.
Figure 2 presents the dependences T1 = f (l ) calculated
from Eq. (4) at T = 10, 15, and 19 kN.
The dependence T2 = f (l ) for the spiral protector is ap-
proximated by the equation
T2 = a5l2 + b5l + C5. (5)
The parameters a5, b5, and C5 of Eq. (5) are presented in
Table 3.
158 E. L. Nikiforov
20
15
10
5
1·10–3
2·10–3
3·10–3
T, kN
T T2 1¢ ¢= –T
T1¢¢
T1¢T1¢
T1¢¢¢
T
f1 m( )å f2( )åm
f ( )å
f3( )åm
å1m¢ å2m¢¢ å
0
Fig. 1. Tensile force T as a function of the relative strain: f1(åm), for
the protector at a distance l = 400 mm from the middle of the sus-
pension clamp according to Eq. (2); f2(åm), the same at a distance
l = 900 mm from the middle of the suspension clamp according to
Eq. (2); f3(åm), in the middle of the protector without suspension
clamp; f (å) for the cable outside the protector according to Eq. (1).
Figure 2 presents the dependences T2 = f (l ) at T = 10,
15, and 19 kN.
The coefficient a4 in Eq. (4) is equal to T1 at l = 0, i.e., a4
gives the value of the tensile force in the cable in the middle
of the suspension clamp. Accordingly, in Eq. (5) the coeffi-
cient C5 = T2 at l = 0, i.e., gives the value of the tensile force
T2 in the spiral protector in the middle of the suspension
clamp.
We can infer from the data of Table 2 at l = 0 that a4 = T1
= f (T ) for the middle of the suspension clamp and from the
data of Table 3 that C5 = T2 = f (T ). The dependences
T1 = f (T ) and T2 = f (T ) can be approximated by a linear
equation
T1,2 = a6T + b6. (6)
Table 4 presents the values of the parameters a6 and b6 in
Eq. (6) used for calculating T1 and T2 (in kN) at l = 0 in the
middle of the suspension clamp.
Analyzing Eq. (6) and the data of Table 4 we will see
that the tensile force T1 in the middle of the suspension
clamp for the tested specimen of cable AS 120/19 is equal to
0.17T; in the wires of the spiral protector in the middle of the
suspension clamp T2 » 0.73T.
At T = 0.45TR (TR is the standard strength of the cable)
permitted by the operating rules at the minimum tempera-
ture, the tensile force T1 in the cable in the middle of the sus-
pension clamp in relative units will be T1/TR » (0.27 ´
´ 0.45TR)/TR » 0.127 of the standard strength of the cable.
For the mean annual temperature used in the operating rules
the tensile force T in the cable should not exceed 0.3TR. Un-
der these conditions in the middle of the suspension clamp
under the spiral protector T1/TR = (0.27 ´ 0.3TR)/TR = 0.081
of the standard strength of the cable. It should be noted that
at the mean annual temperature and T < 0.133TR (according
to the operating rules) cables of grades AS and AZh do not
require protection from vibration.
The presented results of an analysis of the distribution of
forces in the protector-cable combination in the “cable
AS 120/19 – spiral protector – suspension clamp PGN-5-3”
system show that the use of a spiral protector mounted on the
cable at T » 2 kN creates conditions under which the wires of
the protector receive a part of the force T upon the growth of
the latter so that the tensile force T1 in the cable under the
protector in the middle of the suspension clamp amounts to
0.27T. Due to the decrease in the tensile force T1 in the cable,
its part under the suspension clamp is fully protected from
fatigue damage.
The component of the tensile force acting over the axis
of the cable in the spiral protector in the middle of the sus-
Use of Spiral Protectors for Preventing Fatigue Damage of Transmission Line Cables 159
TABLE 1. Components of Forces Acting in the Cable and the Protector
Parameter
Tensile force T, kN Distance l of the section
from the middle of the
suspension clamp, mm10 15 19
¢T1 — in the cable under the protector, kN 4.17 6.16 8.41 400
¢T2 — longitudinal component over the axis of the cable in the wires of the protector, kN 5.83 8.84 10.59 400
¢T2 — in the cable under the protector on the side of the protector edge, kN 6.6 11.08 16.77 900
¢¢T2 — longitudinal component over the axis of the cable in the wires of the protector, kN 3.4 3.92 2.23 900
T2 — at the end of the protector, kN 0 0 0 1100
TABLE 2. Parameters of Eq. (4)
Parameter
Tensile force T, kN
10 15 19
a4 2.51899 3.69909 5.28055
b4 1.185 ´ 10–3
1.249 ´ 10–3
1.168 ´ 10–3
r4 0.97723 0.99759 0.99985
TABLE 3. Parameters of Eq. (5)
Parameter
Tensile force T, kN
10 15 19
a5 –5.38 ´ 10–6
–6.805 ´ 10–6
–4.98 ´ 10–6
b5 –4.14 ´ 10–4
–2.458 ´ 10 – 3
–7.59 ´ 10 – 3
C5 7.3293 11.1986 13.9036
20
15
10
5
0 500 1000 l, mm
T T1 2, , kN
T1
T1
T1
T2
T2
T2
Fig. 2. Variation of the components T1 [Eq. (4)] and T2 [Eq. (5)]
with distance from the middle of the PGN-5-3 suspension clamp:
™, at T = 19 kN; Ï, at T = 15 kN; ˜, at T = 10 kN.
pension clamp changes from zero to 13.9 kN when the ten-
sile force in the cable of the OL span changes from 2 to
19 kN. The maximum force in one wire can attain 13.9/18
= 0.772 kN and the voltage can attain 0.772/6.057 = 0.125
kN/mm2. Consequently, the protector is a reliable element of
the “protector – cable – suspension clamp” system under the
action of standing vibration waves on the OL.
We tested the strength of the “protector – cable – suspen-
sion clamp” system under the action of standing vibration
waves. The tests were performed for AS 120/19, OKGT-01-
6-30, and OKGT-MT-12 (OPGW) cables. Table 5 presents
the conditions of the tests.
After the tests, the wires of the cable and the OPGW ex-
hibited no obvious damage.
The AS 120/19 cable was later tested for tensile strength
at 0.45TR = 18.6 kN. The wires were not damaged. Segments
of the OKGT-01-6-30 and OKGT-MT-12 cables were tested
for breakage of the wires at a distance ±20 cm from the mid-
dle of the PGN-2 suspension clamp.
The results of the tests of OKGT-01-6-30 were as fol-
lows:
— the steel wires had óm = 169.8 kgf/mm2 with coeffi-
cient of variation of 1.08%;
— the four aluminum alloy wires had óm = 37.5
kgf/mm2;
The tests of OKGT-MT-12 showed the following:
— the steel wires had óm = 167.3 kgf/mm2 with coeffi-
cient of variation of 0.06%;
— the four aluminum alloy wires had óm = 37.23
kgf/mm2.
The results of our study performed under the condition
that the protector was mounted at a tensile force of 2 – 3 kN
allow us to recommend that the use of vibration dampers on
OL should be stopped. This will raise the reliability of over-
head transmission cables due to the reduction of the number
of not always reliable units.
Intense vibration of a cable for over 108 vibration cycles
had never led to damage of OL cables outside clamps. There-
fore, the cable itself outside suspension clamps is absolutely
reliable under the action of standing vibration waves.
Problems arise in spans bearing cable connectors.
Experience shows that OL may fail due to fatigue dam-
age of cables and suspension strands caused by vibration at
the sites of cable inlets to the connectors (both oval and
pressed). Such damage of OL cables occurs in the presence
of Stockbridge-type vibration dampers. According to the
data of the Northern Electric Network of the Tyumen’énergo
Company, 63 cases of cable breakage and 18 breakages of
suspension strands at the inlet to connectors occurred in
1986 – 2000. Fatigue damage of OL cables at connector in-
lets can be caused either by insufficiently effective absorp-
tion of energy by the Stockbridge dampers or by the fact that
the mass of the connector frequently plays the role of a re-
flector of energy pulses. With time, standing vibration waves
arise in the cable segment between the suspension clamp and
the connector. Tests of OL have shown that the installation of
two Stockbridge dampers at the suspension clamp does not
provide effective protection of the cable at the inlet to the
connector from fatigue damage.
There are three ways for preventing fatigue damage of
OL cables and strands. The first one is used very widely and
consists in mounting special devices (vibration dampers)
near the connector for absorbing the energy pulses carried by
the wind. The second way consists in the use of devices that
decrease the bending strains of the cable to a safe level. The
third method involves a decrease in the tensile force at the
mean annual temperature to T < 0.133TR.
The method of reduction of bending strains of the cable
at connector inlets by raising the rigidity of the cable-con-
nector system is the most efficient.
The simplest method for increasing the rigidity of the ca-
ble-connector system for an oval connection consists in
dense winding of two steel cores 3 – 4 m long, which are
made from the AS cable suspended in the given OL, onto the
cable and the connector. This variant was realized and tested
by the VTI under the action of standing vibration waves on a
“cable AS 120/19 – connector SOAS 120-3” system.
The test was performed under the following conditions:
tensile force of 10 kN (0.24 of the standard strength of the
cable), vibration amplitude of 5 mm in the half-wave anti-
node, 2.2- and 2.96-cm-long connectors in the node of adja-
cent half-waves, vibration frequency of 19.68 sec–1.
After the action of over 108 vibration cycles on the cable
we did not detect obvious fatigue damage in the wires. In
the subsequent static mode the tensile force was increased
to 18.6 kN (0.45 of the standard strength of the AS 120/19
cable) and maintained for seven days. No hidden defects in
the wires were detected.
From the standpoint of mechanics, the distribution of
forces in the protector-cable combination is determined by
160 E. L. Nikiforov
TABLE 4. Parameters of Eq. (6) for Calculating T1 and T2
Parameter
Calculated force
T1 T2
a6 0.26989 0.73599
b6 –9,455 ´ 10–2
1.16 ´ 10–2
r 0.9952 0.99984
Note. r, Correlation coefficient.
TABLE 5. Conditions of the Test
Parameter AS 120/19 OKGT-01-6-30 OKGT-MT-12
Tensile force
in fractions of TR 0.24 0.25 0.25
Vibration amplitude
in half-wave
antinode, mm 5 6.2 7.3
Half-wave length, m 2.67 5.4 3.96
Vibration frequency,
sec–1
19.68 16.45 23.0
Vibration cycles 108
108
108
the compression and bending of the cable in the suspension
clamp. Upon the appearance of a tensile force T, the wires of
the cable in the protector-cable combination deform on the
segment Äl near the suspension clamp, i.e., a tensile force T0
starts to act over the axis of the protector at an angle å to the
axis of the cable.
For the tested protector
a =
+
= °arctan . ,
d d
L
c w
7539
where dc = 15.2 mm is the diameter of the cable, dw = 2.8
mm is the diameter of the wires in the spiral, and L is the spi-
ral pitch.
Along the axis of the cable the component T02 of the
force T0 is determined as
T02 = T0 cos á.
The component ¢T02 of the force T0 is perpendicular to the
axis of the cable
T02 ¢ = T0 sin á.
The force ¢T02 creates a torque that spins the spiral of the
protector clockwise, which increases the force of compres-
sion of the surfaces of the cable and the spiral wires. As a re-
sult, the friction force of the wire surfaces increases. This in-
creases T0 by a value ÄT0 upon further growth in the force T
by ÄT. Then the spinning of the spiral wires of the protector
propagates to the end of the protector.
We performed tensile tests of the protector-cable system
without suspension clamps in order to evaluate the effect of
the compression of the cable and of bending of the cable in
the clamp. After removing the clamp and straightening the
cable of the segment of the protector-cable combination that
had been under the clamp, we measured the tensile strains of
the system at l = 400 mm. The results are presented in Fig. 1
[the curve f3(åm)]. Measurements showed that the mean value
of the tensile force in the wires of the protector T2 »1 kN
for T ranging within 10 – 19 kN, and the tensile force in the
cable ¢¢T1 = T – 1 kN.
It is more expedient to realize the “spiral protector – cable
– suspension clamp” system for OL on the basis of protectors
fabricated from nonmagnetic steel as required by the
TU-3-1303-27–91 Specifications. In this case the energy
losses to back magnetization of the steel of the protector’s
wires will be absent.
CONCLUSIONS
1. Tensile tests of the “spiral protector – cable
AS 120/19 – suspension clamp PGN-5-3” system have
shown that the installation of a spiral protector on an OL ca-
ble under a tensile force of 2 – 3 kN with subsequent clamp-
ing in the suspension clamp, bending in the clamp, and
growth in the tensile force T in the cable suspended on the
cross-arm of the OL pole creates conditions for an increase in
the tensile force T2 in the wires of the spiral protector. As a
result, a tensile force T1 = T – T2 arises in the cable under the
protector, which is lower than the force acting the cable out-
side the protector. The lowest value of the tensile force T1 oc-
curs in the middle of the suspension clamp. At the mean an-
nual temperature and a tensile force T equal to 0.3 of the
standard strength of the cable, the tensile force T1 in the cable
under the protector in the middle of the suspension clamp
amounts to 0.081 of the strength of the cable; under these
conditions fatigue damage does not arise in the wires of the
cable in the case of vibration.
2. We tested the vibration resistance of the “spiral pro-
tector – cable – suspension clamp” system. Under the condi-
tions presented in Table 5 the wires had no fatigue damage
after 108 vibration cycles.
3. The use of the “spiral protector – cable – suspension
clamp” system in overhead transmission lines for reducing
the tensile force in the cable under the suspension clamp to
safe values makes it possible to eliminate vibration dampers
in spans bearing no cable connectors.
4. In OL spans bearing cable connectors the bending
strain in the wires of the cable at the inlet to the connector
can be reduced to safe values by using a device from steel
cores of AS cables wound on the cable and on the connector.
5. In order to avoid energy losses to back magnetization
of the steel of the protector wires, it is recommended to pro-
duce protector spirals from nonmagnetic steel wire.
Use of Spiral Protectors for Preventing Fatigue Damage of Transmission Line Cables 161

More Related Content

What's hot (20)

Belt drives extra
Belt drives extraBelt drives extra
Belt drives extra
 
Belt friction lecture_new
Belt friction  lecture_newBelt friction  lecture_new
Belt friction lecture_new
 
Emtp rv ic-part1
Emtp rv ic-part1Emtp rv ic-part1
Emtp rv ic-part1
 
Malus law salman
Malus law salmanMalus law salman
Malus law salman
 
Sadovic Lighting Performance Computation
Sadovic Lighting Performance ComputationSadovic Lighting Performance Computation
Sadovic Lighting Performance Computation
 
Waveguide
WaveguideWaveguide
Waveguide
 
Waveguides12
Waveguides12Waveguides12
Waveguides12
 
Microwave Engineering Lecture Notes
Microwave Engineering Lecture NotesMicrowave Engineering Lecture Notes
Microwave Engineering Lecture Notes
 
V belt drives
V belt drivesV belt drives
V belt drives
 
Magnetic circuits
Magnetic circuitsMagnetic circuits
Magnetic circuits
 
Wavegauide
WavegauideWavegauide
Wavegauide
 
phnsrl
phnsrlphnsrl
phnsrl
 
Working, Construction And Types of Band Brakes
Working, Construction And Types of Band BrakesWorking, Construction And Types of Band Brakes
Working, Construction And Types of Band Brakes
 
Magnetic circuit
Magnetic circuitMagnetic circuit
Magnetic circuit
 
ACCURATE NUMERICAL SIMULATION OF HIGHER ORDER SOLITON DECOMPOSITION IN PRESEN...
ACCURATE NUMERICAL SIMULATION OF HIGHER ORDER SOLITON DECOMPOSITION IN PRESEN...ACCURATE NUMERICAL SIMULATION OF HIGHER ORDER SOLITON DECOMPOSITION IN PRESEN...
ACCURATE NUMERICAL SIMULATION OF HIGHER ORDER SOLITON DECOMPOSITION IN PRESEN...
 
Strip lines
Strip linesStrip lines
Strip lines
 
Rectangular waveguides
Rectangular waveguidesRectangular waveguides
Rectangular waveguides
 
IRJET- Simulation Results of Circular Horn Antenna
IRJET- 	  Simulation Results of Circular Horn AntennaIRJET- 	  Simulation Results of Circular Horn Antenna
IRJET- Simulation Results of Circular Horn Antenna
 
Magnetic Circuits
Magnetic CircuitsMagnetic Circuits
Magnetic Circuits
 
3.magnetically coupled circuit
3.magnetically coupled circuit3.magnetically coupled circuit
3.magnetically coupled circuit
 

Similar to Fatigue damage

ESA Module 1 Part-B ME832. by Dr. Mohammed Imran
ESA Module 1 Part-B ME832. by Dr. Mohammed ImranESA Module 1 Part-B ME832. by Dr. Mohammed Imran
ESA Module 1 Part-B ME832. by Dr. Mohammed ImranMohammed Imran
 
Sag-Tension Analysis of AAAC Overhead Transmission Lines for Hilly Areas
Sag-Tension Analysis of AAAC Overhead Transmission Lines for Hilly AreasSag-Tension Analysis of AAAC Overhead Transmission Lines for Hilly Areas
Sag-Tension Analysis of AAAC Overhead Transmission Lines for Hilly AreasIJCSIS Research Publications
 
Analysis of Modeling of Current Differential Protection
Analysis of Modeling of Current Differential ProtectionAnalysis of Modeling of Current Differential Protection
Analysis of Modeling of Current Differential ProtectionIJPEDS-IAES
 
Prestress loss due to friction & anchorage take up
Prestress loss due to friction & anchorage take upPrestress loss due to friction & anchorage take up
Prestress loss due to friction & anchorage take upAyaz Malik
 
Experimental stress analysis BE notes by mohammed imran
Experimental stress analysis BE notes by mohammed imranExperimental stress analysis BE notes by mohammed imran
Experimental stress analysis BE notes by mohammed imranMohammed Imran
 
Stressanalysis linearityerror
Stressanalysis linearityerrorStressanalysis linearityerror
Stressanalysis linearityerrorNobantuNxumalo
 
Grounding of Multi Cable Transits for on-shore use
Grounding of Multi Cable Transits for on-shore useGrounding of Multi Cable Transits for on-shore use
Grounding of Multi Cable Transits for on-shore useMathieu Melenhorst
 
Ferroresonance Conditions in Wind Parks
Ferroresonance Conditions in Wind Parks Ferroresonance Conditions in Wind Parks
Ferroresonance Conditions in Wind Parks Bérengère VIGNAUX
 
Transient voltage distribution in transformer winding (experimental investiga...
Transient voltage distribution in transformer winding (experimental investiga...Transient voltage distribution in transformer winding (experimental investiga...
Transient voltage distribution in transformer winding (experimental investiga...eSAT Publishing House
 
Transient voltage distribution in transformer winding (experimental investiga...
Transient voltage distribution in transformer winding (experimental investiga...Transient voltage distribution in transformer winding (experimental investiga...
Transient voltage distribution in transformer winding (experimental investiga...eSAT Journals
 
Carbon nanotubes for Aerospace applications
Carbon nanotubes for Aerospace applicationsCarbon nanotubes for Aerospace applications
Carbon nanotubes for Aerospace applicationsnasreenhabeeb
 
Analysis of grading techniques in xlpe cable insulation by fem
Analysis of grading techniques in xlpe cable insulation by femAnalysis of grading techniques in xlpe cable insulation by fem
Analysis of grading techniques in xlpe cable insulation by femeSAT Publishing House
 
ANALYSIS OF LIGHTNING STRIKE WITH CORONA ON OHTL NEAR THE SUBSTATION BY EMTP
ANALYSIS OF LIGHTNING STRIKE WITH CORONA ON OHTL NEAR THE SUBSTATION BY EMTP ANALYSIS OF LIGHTNING STRIKE WITH CORONA ON OHTL NEAR THE SUBSTATION BY EMTP
ANALYSIS OF LIGHTNING STRIKE WITH CORONA ON OHTL NEAR THE SUBSTATION BY EMTP ADEIJ Journal
 

Similar to Fatigue damage (20)

S ag calc
S ag calcS ag calc
S ag calc
 
ESA Module 1 Part-B ME832. by Dr. Mohammed Imran
ESA Module 1 Part-B ME832. by Dr. Mohammed ImranESA Module 1 Part-B ME832. by Dr. Mohammed Imran
ESA Module 1 Part-B ME832. by Dr. Mohammed Imran
 
Sag-Tension Analysis of AAAC Overhead Transmission Lines for Hilly Areas
Sag-Tension Analysis of AAAC Overhead Transmission Lines for Hilly AreasSag-Tension Analysis of AAAC Overhead Transmission Lines for Hilly Areas
Sag-Tension Analysis of AAAC Overhead Transmission Lines for Hilly Areas
 
H010526975
H010526975H010526975
H010526975
 
Analysis of Modeling of Current Differential Protection
Analysis of Modeling of Current Differential ProtectionAnalysis of Modeling of Current Differential Protection
Analysis of Modeling of Current Differential Protection
 
Prestress loss due to friction & anchorage take up
Prestress loss due to friction & anchorage take upPrestress loss due to friction & anchorage take up
Prestress loss due to friction & anchorage take up
 
Fisika
FisikaFisika
Fisika
 
Experimental stress analysis BE notes by mohammed imran
Experimental stress analysis BE notes by mohammed imranExperimental stress analysis BE notes by mohammed imran
Experimental stress analysis BE notes by mohammed imran
 
Stressanalysis linearityerror
Stressanalysis linearityerrorStressanalysis linearityerror
Stressanalysis linearityerror
 
Grounding of Multi Cable Transits for on-shore use
Grounding of Multi Cable Transits for on-shore useGrounding of Multi Cable Transits for on-shore use
Grounding of Multi Cable Transits for on-shore use
 
Ferroresonance Conditions in Wind Parks
Ferroresonance Conditions in Wind Parks Ferroresonance Conditions in Wind Parks
Ferroresonance Conditions in Wind Parks
 
Transient voltage distribution in transformer winding (experimental investiga...
Transient voltage distribution in transformer winding (experimental investiga...Transient voltage distribution in transformer winding (experimental investiga...
Transient voltage distribution in transformer winding (experimental investiga...
 
Transient voltage distribution in transformer winding (experimental investiga...
Transient voltage distribution in transformer winding (experimental investiga...Transient voltage distribution in transformer winding (experimental investiga...
Transient voltage distribution in transformer winding (experimental investiga...
 
A5230104
A5230104A5230104
A5230104
 
Carbon nanotubes for Aerospace applications
Carbon nanotubes for Aerospace applicationsCarbon nanotubes for Aerospace applications
Carbon nanotubes for Aerospace applications
 
Sheath bonding method for underground cables
Sheath bonding method for underground cablesSheath bonding method for underground cables
Sheath bonding method for underground cables
 
Analysis of grading techniques in xlpe cable insulation by fem
Analysis of grading techniques in xlpe cable insulation by femAnalysis of grading techniques in xlpe cable insulation by fem
Analysis of grading techniques in xlpe cable insulation by fem
 
Ch25 ssm
Ch25 ssmCh25 ssm
Ch25 ssm
 
ANALYSIS OF LIGHTNING STRIKE WITH CORONA ON OHTL NEAR THE SUBSTATION BY EMTP
ANALYSIS OF LIGHTNING STRIKE WITH CORONA ON OHTL NEAR THE SUBSTATION BY EMTP ANALYSIS OF LIGHTNING STRIKE WITH CORONA ON OHTL NEAR THE SUBSTATION BY EMTP
ANALYSIS OF LIGHTNING STRIKE WITH CORONA ON OHTL NEAR THE SUBSTATION BY EMTP
 
Aq36257262
Aq36257262Aq36257262
Aq36257262
 

Recently uploaded

Standard vs Custom Battery Packs - Decoding the Power Play
Standard vs Custom Battery Packs - Decoding the Power PlayStandard vs Custom Battery Packs - Decoding the Power Play
Standard vs Custom Battery Packs - Decoding the Power PlayEpec Engineered Technologies
 
DeepFakes presentation : brief idea of DeepFakes
DeepFakes presentation : brief idea of DeepFakesDeepFakes presentation : brief idea of DeepFakes
DeepFakes presentation : brief idea of DeepFakesMayuraD1
 
AIRCANVAS[1].pdf mini project for btech students
AIRCANVAS[1].pdf mini project for btech studentsAIRCANVAS[1].pdf mini project for btech students
AIRCANVAS[1].pdf mini project for btech studentsvanyagupta248
 
Kuwait City MTP kit ((+919101817206)) Buy Abortion Pills Kuwait
Kuwait City MTP kit ((+919101817206)) Buy Abortion Pills KuwaitKuwait City MTP kit ((+919101817206)) Buy Abortion Pills Kuwait
Kuwait City MTP kit ((+919101817206)) Buy Abortion Pills Kuwaitjaanualu31
 
Thermal Engineering Unit - I & II . ppt
Thermal Engineering  Unit - I & II . pptThermal Engineering  Unit - I & II . ppt
Thermal Engineering Unit - I & II . pptDineshKumar4165
 
kiln thermal load.pptx kiln tgermal load
kiln thermal load.pptx kiln tgermal loadkiln thermal load.pptx kiln tgermal load
kiln thermal load.pptx kiln tgermal loadhamedmustafa094
 
Hazard Identification (HAZID) vs. Hazard and Operability (HAZOP): A Comparati...
Hazard Identification (HAZID) vs. Hazard and Operability (HAZOP): A Comparati...Hazard Identification (HAZID) vs. Hazard and Operability (HAZOP): A Comparati...
Hazard Identification (HAZID) vs. Hazard and Operability (HAZOP): A Comparati...soginsider
 
COST-EFFETIVE and Energy Efficient BUILDINGS ptx
COST-EFFETIVE  and Energy Efficient BUILDINGS ptxCOST-EFFETIVE  and Energy Efficient BUILDINGS ptx
COST-EFFETIVE and Energy Efficient BUILDINGS ptxJIT KUMAR GUPTA
 
Online food ordering system project report.pdf
Online food ordering system project report.pdfOnline food ordering system project report.pdf
Online food ordering system project report.pdfKamal Acharya
 
Computer Networks Basics of Network Devices
Computer Networks  Basics of Network DevicesComputer Networks  Basics of Network Devices
Computer Networks Basics of Network DevicesChandrakantDivate1
 
data_management_and _data_science_cheat_sheet.pdf
data_management_and _data_science_cheat_sheet.pdfdata_management_and _data_science_cheat_sheet.pdf
data_management_and _data_science_cheat_sheet.pdfJiananWang21
 
Air Compressor reciprocating single stage
Air Compressor reciprocating single stageAir Compressor reciprocating single stage
Air Compressor reciprocating single stageAbc194748
 
Employee leave management system project.
Employee leave management system project.Employee leave management system project.
Employee leave management system project.Kamal Acharya
 
Navigating Complexity: The Role of Trusted Partners and VIAS3D in Dassault Sy...
Navigating Complexity: The Role of Trusted Partners and VIAS3D in Dassault Sy...Navigating Complexity: The Role of Trusted Partners and VIAS3D in Dassault Sy...
Navigating Complexity: The Role of Trusted Partners and VIAS3D in Dassault Sy...Arindam Chakraborty, Ph.D., P.E. (CA, TX)
 
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXssuser89054b
 
Thermal Engineering -unit - III & IV.ppt
Thermal Engineering -unit - III & IV.pptThermal Engineering -unit - III & IV.ppt
Thermal Engineering -unit - III & IV.pptDineshKumar4165
 
Bridge Jacking Design Sample Calculation.pptx
Bridge Jacking Design Sample Calculation.pptxBridge Jacking Design Sample Calculation.pptx
Bridge Jacking Design Sample Calculation.pptxnuruddin69
 
Rums floating Omkareshwar FSPV IM_16112021.pdf
Rums floating Omkareshwar FSPV IM_16112021.pdfRums floating Omkareshwar FSPV IM_16112021.pdf
Rums floating Omkareshwar FSPV IM_16112021.pdfsmsksolar
 

Recently uploaded (20)

Standard vs Custom Battery Packs - Decoding the Power Play
Standard vs Custom Battery Packs - Decoding the Power PlayStandard vs Custom Battery Packs - Decoding the Power Play
Standard vs Custom Battery Packs - Decoding the Power Play
 
DeepFakes presentation : brief idea of DeepFakes
DeepFakes presentation : brief idea of DeepFakesDeepFakes presentation : brief idea of DeepFakes
DeepFakes presentation : brief idea of DeepFakes
 
AIRCANVAS[1].pdf mini project for btech students
AIRCANVAS[1].pdf mini project for btech studentsAIRCANVAS[1].pdf mini project for btech students
AIRCANVAS[1].pdf mini project for btech students
 
Kuwait City MTP kit ((+919101817206)) Buy Abortion Pills Kuwait
Kuwait City MTP kit ((+919101817206)) Buy Abortion Pills KuwaitKuwait City MTP kit ((+919101817206)) Buy Abortion Pills Kuwait
Kuwait City MTP kit ((+919101817206)) Buy Abortion Pills Kuwait
 
Thermal Engineering Unit - I & II . ppt
Thermal Engineering  Unit - I & II . pptThermal Engineering  Unit - I & II . ppt
Thermal Engineering Unit - I & II . ppt
 
kiln thermal load.pptx kiln tgermal load
kiln thermal load.pptx kiln tgermal loadkiln thermal load.pptx kiln tgermal load
kiln thermal load.pptx kiln tgermal load
 
Hazard Identification (HAZID) vs. Hazard and Operability (HAZOP): A Comparati...
Hazard Identification (HAZID) vs. Hazard and Operability (HAZOP): A Comparati...Hazard Identification (HAZID) vs. Hazard and Operability (HAZOP): A Comparati...
Hazard Identification (HAZID) vs. Hazard and Operability (HAZOP): A Comparati...
 
COST-EFFETIVE and Energy Efficient BUILDINGS ptx
COST-EFFETIVE  and Energy Efficient BUILDINGS ptxCOST-EFFETIVE  and Energy Efficient BUILDINGS ptx
COST-EFFETIVE and Energy Efficient BUILDINGS ptx
 
Online food ordering system project report.pdf
Online food ordering system project report.pdfOnline food ordering system project report.pdf
Online food ordering system project report.pdf
 
Computer Networks Basics of Network Devices
Computer Networks  Basics of Network DevicesComputer Networks  Basics of Network Devices
Computer Networks Basics of Network Devices
 
data_management_and _data_science_cheat_sheet.pdf
data_management_and _data_science_cheat_sheet.pdfdata_management_and _data_science_cheat_sheet.pdf
data_management_and _data_science_cheat_sheet.pdf
 
Air Compressor reciprocating single stage
Air Compressor reciprocating single stageAir Compressor reciprocating single stage
Air Compressor reciprocating single stage
 
Call Girls in South Ex (delhi) call me [🔝9953056974🔝] escort service 24X7
Call Girls in South Ex (delhi) call me [🔝9953056974🔝] escort service 24X7Call Girls in South Ex (delhi) call me [🔝9953056974🔝] escort service 24X7
Call Girls in South Ex (delhi) call me [🔝9953056974🔝] escort service 24X7
 
Employee leave management system project.
Employee leave management system project.Employee leave management system project.
Employee leave management system project.
 
Navigating Complexity: The Role of Trusted Partners and VIAS3D in Dassault Sy...
Navigating Complexity: The Role of Trusted Partners and VIAS3D in Dassault Sy...Navigating Complexity: The Role of Trusted Partners and VIAS3D in Dassault Sy...
Navigating Complexity: The Role of Trusted Partners and VIAS3D in Dassault Sy...
 
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
 
Thermal Engineering -unit - III & IV.ppt
Thermal Engineering -unit - III & IV.pptThermal Engineering -unit - III & IV.ppt
Thermal Engineering -unit - III & IV.ppt
 
Bridge Jacking Design Sample Calculation.pptx
Bridge Jacking Design Sample Calculation.pptxBridge Jacking Design Sample Calculation.pptx
Bridge Jacking Design Sample Calculation.pptx
 
FEA Based Level 3 Assessment of Deformed Tanks with Fluid Induced Loads
FEA Based Level 3 Assessment of Deformed Tanks with Fluid Induced LoadsFEA Based Level 3 Assessment of Deformed Tanks with Fluid Induced Loads
FEA Based Level 3 Assessment of Deformed Tanks with Fluid Induced Loads
 
Rums floating Omkareshwar FSPV IM_16112021.pdf
Rums floating Omkareshwar FSPV IM_16112021.pdfRums floating Omkareshwar FSPV IM_16112021.pdf
Rums floating Omkareshwar FSPV IM_16112021.pdf
 

Fatigue damage

  • 1. USE OF SPIRAL PROTECTORS FOR PREVENTING FATIGUE DAMAGE OF TRANSMISSION LINE CABLES E. L. Nikiforov1 Translated from Élektricheskie Stantsii, No. 6, 2002, pp. 70 – 74. Results of a measurement of the distribution of component forces in an “ACSR with wound spiral protector from steel wires” system fastened in a suspension clamp of an overhead transmission line are presented. Cor- relation dependences for the tensile force acting in the cable under the protector are obtained. It is shown that the tensile force in the cable under the protector decreases from the value T in the span to a minimum value in the middle of the suspension clamp. At a tensile force T equal to 30% of the standard strength of the wire the tensile force in the suspension clamp is 8.1%, and the wires in the OL cable do not suffer from fatigue damage. Spiral protectors from steel wires are recommended for protecting OL cables from fatigue damage under the action of standing vibration waves. Key words: overhead transmission lines, cables, ground wire, strain, vibration, metal fatigue, fatigue protec- tion, spiral protector, distribution of forces in the protector-cable combination, vibration protection of connectors. Spiral protectors from steel wires fastened over the inter- nal surface by an abrasive adhesive are widely used for pro- tecting suspension clamps of the optical fibers of cables of grade ADSS and cables built into the ground wire (OPGW). Spiral wires 2 – 5 pieces in a strand with a pitch of 100 – 150 mm are wound on the ground wire fully covering its surface on a length of 2 – 2.5 m. The suspension clamp is mounted in the middle of the protector. The inner diameter of the protector is about 1 mm less than the diameter of the ADSS (or OPGW) cable, which is responsible for the ap- pearance of a friction force on the OPGW/protector bound- ary. The presence of a friction force on the surfaces of the “OPWG – spiral protector wires” system should create a ten- sile strain in the protector wires upon the stretching of the OPGW, i.e., the protector should receive a part of the force stretching the OPGW. Since the OPGW as a mechanical structure is an analog of grade AS cable (aluminum-steel), stretching of the “AS cable – spiral protector” system should decrease the tensile force in the cable in the place of fasten- ing of the protector and of the suspension clamp and raise the reliability of operation of the AS (or A) cable. In order to evaluate the distribution of tensile forces in the “spiral protector — AS cable – suspension clamp,” the system specialists of VNIIÉ tested such a system for the ten- sile strength in a static mode. The spiral protector was wound under a tensile force of 2 kN in the cable. The 2.3-m-long protector consisted of 18 steel wires about 2.8 mm in diameter (their total section was 110.8 mm2) at a pitch of 136 mm; the winding was directed from the left – upward – to the right like the winding of the external layer of the aluminum wires in the AS 120/19 cable. The protector was used for the second time after a tensile test (stretching to 27 kN) of an ADSS optical coupling cable. Devices for measuring the elongation Äl of the cable were mounted on the AS 120/19 cable, on the protector, and in two places of the protector combined with the cable on a length l0. For the cable l0 = 1000 mm; for the protector-cable combination l0 = 400 mm. The elongation Äl was measured by an indicator accurate to 0.01 mm. The result of the mea- surement was expressed in relative units å = l/l0. The accu- racy of the measurement of the elongation of the cable was 0.01/1000 = 10–5 mm/mm; the accuracy of the measurement of the elongation of the protector-cable combination was 0.01/400 = 0.25 ´ 10–4 mm/mm. The tensile force T applied to the AS 120/19 cable was measured by a dynamometer accurate to 2%. Figure 1 presents the curves T = f (å) for the AS120/19 cable and the curves T = f1(åm) and T = f2(åm) for the ca- ble-protector combination. The value of Äl was measured in two places of the protector, i.e., at a distance of 15 – 415 mm from the middle of the body of the suspension clamp for f1(åm) and at a distance of 15.0 – 415 mm from the protector edge for f2(åm). It follows from the obtained results (Fig. 1) that at the same force T, which acts both on the cable in the span and on the protector-cable combination, the relative strain åm on the length l0 = 400 mm for the protector-cable combination is substantially lower than that for the cable outside the protec- tor. The dependences T = f1(åm) and T = f2(åm) obtained on 157 1570-145X/02/3603-0157$27.00 © 2002 Plenum Publishing Corporation Power Technology and Engineering Vol. 36, No. 3, 2002 1 All-Russia Electric Power Research Institute (VNIIÉ), Moscow, Russia.
  • 2. the two segments l0 of the protector-cable combination differ substantially from each other. With the closeness of l0 to the suspension clamp at equal T the relative strain åm decreases, i.e., åm varies over the length of the protector. Therefore, we should presume that within Äl0 the relative strain in each sec- tion of the protector-cable combination decreases with close- ness of the section to the suspension clamp. Consequently, for the protector-cable combination the measured values of åm on the length l0 of the protector should be referred to the middle of l0. In what follows the relative strains measured for the protector-cable combination will be denoted å1m (at a dis- tance l = 400 mm from the middle of the suspension clamp) and å2m (at a distance l = 900 mm from the middle of the sus- pension clamp). According to the data of Fig. 1 the dependence of the tensile strength T acting on the tested cable AS 120/19 on the relative strain å is approximated by an exponential func- tion T1 = a1 exp b1å, (1) where a1 = 1.89221, b1 = 860.741, and the correlation coeffi- cient r1 = 0.98644 (for the given cable). Equation (1) is applicable to both the cable in the span and to the part of the cable under the protector. Measurements show that for the “protector-cable AS120/19” combination the dependence of the mean value of the rela- tive strain åm (Fig. 1) in the middle of l0 on the tensile force T can be approximated by the expression åm = a2T + b2. (2) The values of parameters in Eq. (2) for the distances l1 = 400 mm and l2 = 900 mm from the middle of the suspen- sion clamp are presented below (r2 is the correlation coeffi- cient). l1 = 400 mm l2 = 900 mm a2 9.042 ´ 10–5 1.152 ´ 10–4 b2 1.531 ´ 10–5 3.172 ´ 10–4 r2 0.99842 0.99705 We use Eq. (2) to calculate å1m in the middle of the seg- ment l0 for a given force T acting on the protector-cable com- bination and on the wire outside the protector-cable combi- nation at a distance l = 400 mm from the middle of the sus- pension clamp. The obtained value of å1m is substituted into Eq. (1) to calculate the force ¢T1 acting on the cable in the sec- tion of the protector-cable combination at a distance l = 400 mm from the middle of the suspension clamp. Simi- lar calculations are performed for T equal to 10, 15, and 19 kN in order to find å2m and ¢¢T1 in the section lying at l = 900 mm from the middle of the suspension clamp (Fig. 1). The equation T2 = T – T1 (3) is used to calculate the component T2 of the force T acting in the protector in the considered section of the protector-cable combination ( ¢T2 at a distance l = 400 mm and ¢¢T2 at a dis- tance l = 900 mm from the middle of the suspension clamp). Table 1 presents the computational results obtained with the help of Eqs. (1) – (3). It can be see from the data of Table 1 that the value of the force ¢T1 in the cable under the protector is more than two times lower than the force T outside the protector. We used the data of Table 1 to obtain the dependences T1 = f (l ) and T2 = f (l ) at a given value of the tensile force T. The dependences T1 = f (l ) for the cable under the protector at T = 10, 15, and 19 kN were approximated by the equation T1 = a4 exp b4l, (4) The values of a4 and b4 for Eq. (4) are presented in Table 2. Figure 2 presents the dependences T1 = f (l ) calculated from Eq. (4) at T = 10, 15, and 19 kN. The dependence T2 = f (l ) for the spiral protector is ap- proximated by the equation T2 = a5l2 + b5l + C5. (5) The parameters a5, b5, and C5 of Eq. (5) are presented in Table 3. 158 E. L. Nikiforov 20 15 10 5 1·10–3 2·10–3 3·10–3 T, kN T T2 1¢ ¢= –T T1¢¢ T1¢T1¢ T1¢¢¢ T f1 m( )å f2( )åm f ( )å f3( )åm å1m¢ å2m¢¢ å 0 Fig. 1. Tensile force T as a function of the relative strain: f1(åm), for the protector at a distance l = 400 mm from the middle of the sus- pension clamp according to Eq. (2); f2(åm), the same at a distance l = 900 mm from the middle of the suspension clamp according to Eq. (2); f3(åm), in the middle of the protector without suspension clamp; f (å) for the cable outside the protector according to Eq. (1).
  • 3. Figure 2 presents the dependences T2 = f (l ) at T = 10, 15, and 19 kN. The coefficient a4 in Eq. (4) is equal to T1 at l = 0, i.e., a4 gives the value of the tensile force in the cable in the middle of the suspension clamp. Accordingly, in Eq. (5) the coeffi- cient C5 = T2 at l = 0, i.e., gives the value of the tensile force T2 in the spiral protector in the middle of the suspension clamp. We can infer from the data of Table 2 at l = 0 that a4 = T1 = f (T ) for the middle of the suspension clamp and from the data of Table 3 that C5 = T2 = f (T ). The dependences T1 = f (T ) and T2 = f (T ) can be approximated by a linear equation T1,2 = a6T + b6. (6) Table 4 presents the values of the parameters a6 and b6 in Eq. (6) used for calculating T1 and T2 (in kN) at l = 0 in the middle of the suspension clamp. Analyzing Eq. (6) and the data of Table 4 we will see that the tensile force T1 in the middle of the suspension clamp for the tested specimen of cable AS 120/19 is equal to 0.17T; in the wires of the spiral protector in the middle of the suspension clamp T2 » 0.73T. At T = 0.45TR (TR is the standard strength of the cable) permitted by the operating rules at the minimum tempera- ture, the tensile force T1 in the cable in the middle of the sus- pension clamp in relative units will be T1/TR » (0.27 ´ ´ 0.45TR)/TR » 0.127 of the standard strength of the cable. For the mean annual temperature used in the operating rules the tensile force T in the cable should not exceed 0.3TR. Un- der these conditions in the middle of the suspension clamp under the spiral protector T1/TR = (0.27 ´ 0.3TR)/TR = 0.081 of the standard strength of the cable. It should be noted that at the mean annual temperature and T < 0.133TR (according to the operating rules) cables of grades AS and AZh do not require protection from vibration. The presented results of an analysis of the distribution of forces in the protector-cable combination in the “cable AS 120/19 – spiral protector – suspension clamp PGN-5-3” system show that the use of a spiral protector mounted on the cable at T » 2 kN creates conditions under which the wires of the protector receive a part of the force T upon the growth of the latter so that the tensile force T1 in the cable under the protector in the middle of the suspension clamp amounts to 0.27T. Due to the decrease in the tensile force T1 in the cable, its part under the suspension clamp is fully protected from fatigue damage. The component of the tensile force acting over the axis of the cable in the spiral protector in the middle of the sus- Use of Spiral Protectors for Preventing Fatigue Damage of Transmission Line Cables 159 TABLE 1. Components of Forces Acting in the Cable and the Protector Parameter Tensile force T, kN Distance l of the section from the middle of the suspension clamp, mm10 15 19 ¢T1 — in the cable under the protector, kN 4.17 6.16 8.41 400 ¢T2 — longitudinal component over the axis of the cable in the wires of the protector, kN 5.83 8.84 10.59 400 ¢T2 — in the cable under the protector on the side of the protector edge, kN 6.6 11.08 16.77 900 ¢¢T2 — longitudinal component over the axis of the cable in the wires of the protector, kN 3.4 3.92 2.23 900 T2 — at the end of the protector, kN 0 0 0 1100 TABLE 2. Parameters of Eq. (4) Parameter Tensile force T, kN 10 15 19 a4 2.51899 3.69909 5.28055 b4 1.185 ´ 10–3 1.249 ´ 10–3 1.168 ´ 10–3 r4 0.97723 0.99759 0.99985 TABLE 3. Parameters of Eq. (5) Parameter Tensile force T, kN 10 15 19 a5 –5.38 ´ 10–6 –6.805 ´ 10–6 –4.98 ´ 10–6 b5 –4.14 ´ 10–4 –2.458 ´ 10 – 3 –7.59 ´ 10 – 3 C5 7.3293 11.1986 13.9036 20 15 10 5 0 500 1000 l, mm T T1 2, , kN T1 T1 T1 T2 T2 T2 Fig. 2. Variation of the components T1 [Eq. (4)] and T2 [Eq. (5)] with distance from the middle of the PGN-5-3 suspension clamp: ™, at T = 19 kN; Ï, at T = 15 kN; ˜, at T = 10 kN.
  • 4. pension clamp changes from zero to 13.9 kN when the ten- sile force in the cable of the OL span changes from 2 to 19 kN. The maximum force in one wire can attain 13.9/18 = 0.772 kN and the voltage can attain 0.772/6.057 = 0.125 kN/mm2. Consequently, the protector is a reliable element of the “protector – cable – suspension clamp” system under the action of standing vibration waves on the OL. We tested the strength of the “protector – cable – suspen- sion clamp” system under the action of standing vibration waves. The tests were performed for AS 120/19, OKGT-01- 6-30, and OKGT-MT-12 (OPGW) cables. Table 5 presents the conditions of the tests. After the tests, the wires of the cable and the OPGW ex- hibited no obvious damage. The AS 120/19 cable was later tested for tensile strength at 0.45TR = 18.6 kN. The wires were not damaged. Segments of the OKGT-01-6-30 and OKGT-MT-12 cables were tested for breakage of the wires at a distance ±20 cm from the mid- dle of the PGN-2 suspension clamp. The results of the tests of OKGT-01-6-30 were as fol- lows: — the steel wires had óm = 169.8 kgf/mm2 with coeffi- cient of variation of 1.08%; — the four aluminum alloy wires had óm = 37.5 kgf/mm2; The tests of OKGT-MT-12 showed the following: — the steel wires had óm = 167.3 kgf/mm2 with coeffi- cient of variation of 0.06%; — the four aluminum alloy wires had óm = 37.23 kgf/mm2. The results of our study performed under the condition that the protector was mounted at a tensile force of 2 – 3 kN allow us to recommend that the use of vibration dampers on OL should be stopped. This will raise the reliability of over- head transmission cables due to the reduction of the number of not always reliable units. Intense vibration of a cable for over 108 vibration cycles had never led to damage of OL cables outside clamps. There- fore, the cable itself outside suspension clamps is absolutely reliable under the action of standing vibration waves. Problems arise in spans bearing cable connectors. Experience shows that OL may fail due to fatigue dam- age of cables and suspension strands caused by vibration at the sites of cable inlets to the connectors (both oval and pressed). Such damage of OL cables occurs in the presence of Stockbridge-type vibration dampers. According to the data of the Northern Electric Network of the Tyumen’énergo Company, 63 cases of cable breakage and 18 breakages of suspension strands at the inlet to connectors occurred in 1986 – 2000. Fatigue damage of OL cables at connector in- lets can be caused either by insufficiently effective absorp- tion of energy by the Stockbridge dampers or by the fact that the mass of the connector frequently plays the role of a re- flector of energy pulses. With time, standing vibration waves arise in the cable segment between the suspension clamp and the connector. Tests of OL have shown that the installation of two Stockbridge dampers at the suspension clamp does not provide effective protection of the cable at the inlet to the connector from fatigue damage. There are three ways for preventing fatigue damage of OL cables and strands. The first one is used very widely and consists in mounting special devices (vibration dampers) near the connector for absorbing the energy pulses carried by the wind. The second way consists in the use of devices that decrease the bending strains of the cable to a safe level. The third method involves a decrease in the tensile force at the mean annual temperature to T < 0.133TR. The method of reduction of bending strains of the cable at connector inlets by raising the rigidity of the cable-con- nector system is the most efficient. The simplest method for increasing the rigidity of the ca- ble-connector system for an oval connection consists in dense winding of two steel cores 3 – 4 m long, which are made from the AS cable suspended in the given OL, onto the cable and the connector. This variant was realized and tested by the VTI under the action of standing vibration waves on a “cable AS 120/19 – connector SOAS 120-3” system. The test was performed under the following conditions: tensile force of 10 kN (0.24 of the standard strength of the cable), vibration amplitude of 5 mm in the half-wave anti- node, 2.2- and 2.96-cm-long connectors in the node of adja- cent half-waves, vibration frequency of 19.68 sec–1. After the action of over 108 vibration cycles on the cable we did not detect obvious fatigue damage in the wires. In the subsequent static mode the tensile force was increased to 18.6 kN (0.45 of the standard strength of the AS 120/19 cable) and maintained for seven days. No hidden defects in the wires were detected. From the standpoint of mechanics, the distribution of forces in the protector-cable combination is determined by 160 E. L. Nikiforov TABLE 4. Parameters of Eq. (6) for Calculating T1 and T2 Parameter Calculated force T1 T2 a6 0.26989 0.73599 b6 –9,455 ´ 10–2 1.16 ´ 10–2 r 0.9952 0.99984 Note. r, Correlation coefficient. TABLE 5. Conditions of the Test Parameter AS 120/19 OKGT-01-6-30 OKGT-MT-12 Tensile force in fractions of TR 0.24 0.25 0.25 Vibration amplitude in half-wave antinode, mm 5 6.2 7.3 Half-wave length, m 2.67 5.4 3.96 Vibration frequency, sec–1 19.68 16.45 23.0 Vibration cycles 108 108 108
  • 5. the compression and bending of the cable in the suspension clamp. Upon the appearance of a tensile force T, the wires of the cable in the protector-cable combination deform on the segment Äl near the suspension clamp, i.e., a tensile force T0 starts to act over the axis of the protector at an angle å to the axis of the cable. For the tested protector a = + = °arctan . , d d L c w 7539 where dc = 15.2 mm is the diameter of the cable, dw = 2.8 mm is the diameter of the wires in the spiral, and L is the spi- ral pitch. Along the axis of the cable the component T02 of the force T0 is determined as T02 = T0 cos á. The component ¢T02 of the force T0 is perpendicular to the axis of the cable T02 ¢ = T0 sin á. The force ¢T02 creates a torque that spins the spiral of the protector clockwise, which increases the force of compres- sion of the surfaces of the cable and the spiral wires. As a re- sult, the friction force of the wire surfaces increases. This in- creases T0 by a value ÄT0 upon further growth in the force T by ÄT. Then the spinning of the spiral wires of the protector propagates to the end of the protector. We performed tensile tests of the protector-cable system without suspension clamps in order to evaluate the effect of the compression of the cable and of bending of the cable in the clamp. After removing the clamp and straightening the cable of the segment of the protector-cable combination that had been under the clamp, we measured the tensile strains of the system at l = 400 mm. The results are presented in Fig. 1 [the curve f3(åm)]. Measurements showed that the mean value of the tensile force in the wires of the protector T2 »1 kN for T ranging within 10 – 19 kN, and the tensile force in the cable ¢¢T1 = T – 1 kN. It is more expedient to realize the “spiral protector – cable – suspension clamp” system for OL on the basis of protectors fabricated from nonmagnetic steel as required by the TU-3-1303-27–91 Specifications. In this case the energy losses to back magnetization of the steel of the protector’s wires will be absent. CONCLUSIONS 1. Tensile tests of the “spiral protector – cable AS 120/19 – suspension clamp PGN-5-3” system have shown that the installation of a spiral protector on an OL ca- ble under a tensile force of 2 – 3 kN with subsequent clamp- ing in the suspension clamp, bending in the clamp, and growth in the tensile force T in the cable suspended on the cross-arm of the OL pole creates conditions for an increase in the tensile force T2 in the wires of the spiral protector. As a result, a tensile force T1 = T – T2 arises in the cable under the protector, which is lower than the force acting the cable out- side the protector. The lowest value of the tensile force T1 oc- curs in the middle of the suspension clamp. At the mean an- nual temperature and a tensile force T equal to 0.3 of the standard strength of the cable, the tensile force T1 in the cable under the protector in the middle of the suspension clamp amounts to 0.081 of the strength of the cable; under these conditions fatigue damage does not arise in the wires of the cable in the case of vibration. 2. We tested the vibration resistance of the “spiral pro- tector – cable – suspension clamp” system. Under the condi- tions presented in Table 5 the wires had no fatigue damage after 108 vibration cycles. 3. The use of the “spiral protector – cable – suspension clamp” system in overhead transmission lines for reducing the tensile force in the cable under the suspension clamp to safe values makes it possible to eliminate vibration dampers in spans bearing no cable connectors. 4. In OL spans bearing cable connectors the bending strain in the wires of the cable at the inlet to the connector can be reduced to safe values by using a device from steel cores of AS cables wound on the cable and on the connector. 5. In order to avoid energy losses to back magnetization of the steel of the protector wires, it is recommended to pro- duce protector spirals from nonmagnetic steel wire. Use of Spiral Protectors for Preventing Fatigue Damage of Transmission Line Cables 161