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Cable Sizing for Fast Transient
Loads
Robert
E.
Henry,
P.
E.
Life Member
Bechtel National Inc.
P.O. ox
21 19 Richland WA 99352 USA 509-371-2775 (W) 371-2762 (F)
Abst rac t
-
The most recognized standards for
sizing
US
manufactured cables a r e ampacity
tables published in the National Electrical Code.
These tables ar e only for steady-state loads. This
paper addresses the t ransient tempera ture
response of cables undergoing fast heavy loading.
Exponential functions are analytically derived
that express responses to step changes
io
cable
currents . Formulas for coeffrcients and t ime
coostants a re derived. Cable manufac turers‘ da ta
an d othe r sources for physical proper ties ar e used
to calculate the coefficients and time constants for
thre e coppe r condu ctor sizes. Steady-state end
tempe ratures ar e based on National Electrical
Code ampacity tables. The der ived formulas are
limited to cables in open tray or free air, and in
condu it in air. The methods to develop da ta are
detailed for other conductor sizes and aluminum
conductors. Also presented a re the means to size
power cables based on calculated transient
tempe ratures. These calculated tempe ratures are
comp ared with cable temp eratu re ratings to select
a cable size. An examp le is included that
illustrates sizing feeders
for
five 2000 hp c rnsber -
conveyors.
Index Terms - Power cables, transient heating,
transient tem pera ture functions, cable sMng.
I. INTRODUCTION
The m ost widely accepted standard for cable sizing is
based on “The Calculation of the Temperature Rise
and Load Capability of Cable Systems,” by Neber
and McGrath, AIEE Paper 57-660. It is the basis for
the ampacity tables of the National Electric Code [l ]
Article 310, and IEEE 835-1994 (IPCEA Pub. P-46-
426) Standard Power Cable Ampacity Tables. For
applications where transient loads are encountered,
recommended practice, embodied in IEEE guides,
generally addresses cyclic loads varying on a daily
basis. Amp acity recommen dations do not exist for
fast, heavy loading of cables.
One load of this type is a combustion-turbine starting
system in a combined cycle power plant, wherein the
generator is
used
as a starting motor for the
0-7803-777 1-0/03/$17.00 2003
IEEE.
combustion turbine. The combustion turbine’s
exhaust is ducted to a heat-recovery boiler. A
variable-frequency drive is employed that ramps up
the shaft to a low speed,
an&
holds at this load,
consisting of the engine’s air compressor, for a
purging cycle. Then the variable-frequency drive
further ramps up the
shaft
speed to about seventy
percent, when fuel is introduced and ignited. At this
point the turbine assumes the load and the electric
motor current falls to zero. The duration
of
this
starting cycle can be about half
an
hour for a large
machine, and the motor current may reach 1600
amperes during the short period when fuel is
introduced and ignited.
This half-hour cycle is too short a period for
conductors to reach their steady-state ratings. Even
with consecutive start attempts, cables might not
reach their steady-state ratings. Also considering
that a turbine in power plant service is started rarely,
a machine’s starting circuit conductors may employ
their higher emergency temperature ratings for this
service, and more prolonged cable heating would be
necessary to reach this higher te m p er a m rating.
Other examples
of
fast heating might be found io
large crushers and conveyors. These can require
short bursts of large currents on starting and during
periodic loading, when coarse aggregate is initially
crushed. Also, electric furnaces in steel mills have
short bursts of large currents when scrap steel is first
melted. Usually, fast heating is found with variable
frequency drives that are em ployed to deliver varying
amounts of non-periodic high torque to rotating
machinely, or with rectifiers to deliver occasional
heavy currents to equipment.
This paper addresses the transient temperature
response of cables undergoing fast transient heating.
Because there are too many possible criteria, a
general method and tables for rating cables are not
developed, but a calculation guide is outlined that can
be used to size cables for fast transient loads in some
installations.
Sponsor
of
author’s p resentation is Bechtel National Inc.
of
Richland WA.
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11. TRANSIENT
EATINGF
POWER CABLES
If after a long time, a three-core power cable is
energized, its temperature will climb to a steady state
value. Depending on how it is installed and in what
it is installed, it will take a few or many hours to
reach a steady temperature. Considering a
small
cable in free air without wind, this cable will heat up
in 1 1/3 hours. A large cable will take 6 hours. If in
conduit buried in the earth, a large cable will take 16
hours.
Cables
in
Air
A single small bare cable in free air carrying a
current will heat up exponentially with time:
where
AT
‘D
t
K
R
C
Steady state temperature rise on
Kelvin or Celsius scales (“C).
Time varying rise
“ 2).
Time brs).
Time constant equal to R times
C
(hrs).
Thermal resistance between wire and
free
air (“C I
W).
Thermal capacitance ofw ire (Whr/”C).
This neglects any temperature difference within the
cable’s cross section, and assumes that the cable is
long enough that the temperature is uniform along the
cable’s length.
Here AT = Q R
(2)
where Q constant heat
loss
in the cable
(W)
.
If the current is constant, in (2), constant Q would be
assumed constant by neglecting the rise in cable
electrical resistance with temperature increase. But
over a moderate value
of
temperature rise, this is a
small change, and the average value of resistance
over the value of AT may usually be employed, or
altematively, the resistance at an average
temperature.
If the cable is insulated, and if the small radial
temperature difference through the insulation is
neglected or taken as averaged, equation
I )
is true,
but
C
must also include the insulation’s thermal
capacitance. Also, if the amount of cable is a unit
length, then the values of R, C and Q are per unit
length. The effective value of
Q
is said to be equal
to AT when time, t, reaches a value of 4K, or four
time constants. That is, when the value of the
exponential is 0.982. This is less than
2%
difference
from the valu e of the exp onentia l at infinite time.
If there are three conductors spaced together, with
each carrying the same current as the conductor
above, there is less than three times the exposed cable
surface area in the bundle. Then the value of R for
the bundle is greater than 4 the thermal resistance of
one wire, so the bundle heats up to a slightly higher
tempe rature rise than for the single wire. But the
capacitance for the bundle is three times the thermal
capacitance of one wire,
so
the value of K is slightly
greater than for the single wire. Thus, the bundle
heats up with a slightly longer heating time to the
higher temperature rise. Also, this assumes that the
small
temperature differences through the cross
section of the bundle are averaged.
Given the rated temperature rise found in ampacity
tables (see [ I ] , Table 310-67) the conductor current
rating is found in these tables. The temperature rise
with a lesser constant current value is proportional to
the square of the current ratio, if cable dielectric loss
and shield
loss
are negligible. The applicable values
for C can
be
found from manufacturers’
data and the
properties of the materials making up the cable.
Installing in Conduit
If the bundle is installed in a conduit in free air, (1)
becomes more complicated. Now there is a
resistance between the bundle and the conduit, and a
second resistance between fhe conduit and free air.
Also, the conduit’s thermal capacitance affects the
heating time. First, the resistance has increased,
increasing the heating time. Second, the conduit
doesn’t begin to heat up in the beginn ing. It doesn’t
have heat generated in it like the bundle,
so it
begins
to heat up after the bund le starts to transfer heat to
it,
which happens only as the bundle heats up. And the
conduit’s thermal capacitance adds
to
that of the
system. With both resistance and system capacitance
increased, the time constant is increased. (Here
again, the small radial temperature difference through
the conduit wall is neglected.) The exponential
function for the temperature rise (18b) is derived in
Appendix A. There are now two time constants, K’
and K”, with
K
greater than K”. The formulas for
the time constants
are
(13), (14) and (15) in
Appe ndix A. In Appe ndix B, a simplification is
developed based on the criterion, c h , which states
that, if
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.
. .
the exponential function converges to
Q
=
A T ( 1 -
e K')
and the effect of K ecomes insignificant.
o(
s the
system time constant and CI, I and R2 are defined
in Appendix A.)
Installing in Underground Ducts
Burying the conduit containing the bundle of three
wires increases the system thermal resistance, adding
now, instead of the resistance between the conduit
and free air, the increased resistance between the
conduit and through the path of heat flow to the
earth's surface. Also, the thermal capacitance of the
earth in this path increases the overall amount of
capacitance. These additions of thermal resistance
and capacitance increase yet again the system time
constant and further complicate the system
exponential response. If the added complication
from installing the cables in a conduit in free air is
projected to buying the conduit, then more
coefficients and more time constants in the
expression of the time-varying temperature rise can
be expected. The treatment
of
this response is not
addressed in this paper. Howev er, if another
simplifying criterion is postulated that is similar to
Ch, and if this criterion has the same simplifying
property, then the approximate simple exponential
response
for
the temperature rise would again result.
Such a derivation
of
this response would yield
formulas for the time constants. One o f these would
be the longest and be embodied in the simple
exponential response.
Wiseman, in his paper, An empirical method for
determining transient temperatures of buried cable
systems
[Z],
addressed this formula. His paper
reviews a large body of work by many engineers on
the subject of buried cables that was done in the
decades during and following
WW
U. Their major
concem
was
with large high voltage cables. Another
technique that may be employed to calculate transient
temperature response for buried cables is to use
digital computation.
Temperaiure Rise Values and Heat Losses
The NEC ampacity tables with their listed values of
temperature rise define values of conductor current.
Also
in the
NEC,
Table
9
lists electrical resistance
for
the standard su es of cables. Using values from this
table, generated heat can be calculated
as
the
ampacity current squared times the listed electrical
resistance for each conductor in the bundle.
(Dielectric and shield losses must be negligible).
Using this temperature rise and generated heat, the
value for thermal resistance can be obtained from
(2).
Another source for conductor electrical resistance
data is the cable manufachuer's published cable
characteristics.
The NEC table ampacities are based on published
electrical resistance values. The code states that
adjustments must be made for shield and dielectric
losses. Also, adjustments must be made for heating
from harmonic currents.
nI.
APPLICATION
F CABLE DATA
Example
of
Table Values
A
500
kcmil
5
kV single unshielded copper
conductor is used. A one-foot length is considered.
The ampacity for this cond uctor in air is 685 amperes
(Table 310-69). The resistance is 0.027 ohms per
thousand feet. Based on these values Q is 12.65
watts (per foot) and R is 3 69OCI W (per foot).
Based
on
manufacturer's data sheets, the weight of
copper is 1.54 Ibs and the weight of the insulation
and jacket is
0.511
Ibs (both per foot). The specific
heat of copper is 0.092 and the specific heat of
polyethylene is
0.50.
Converting units, the value of
C fo r the copper is 0.0749 w-h/ C and the value of C
for the insulation is 0.1347 w-h/ C. Their sum ,
0.2097 Whr/OC.
Multiplying these values for
R
and C for this large
single conductor in free air, the value for K is 0.77
hours. It would take a period of about four time
constants, or
3.1
hours, for this conductor to heat up.
Considering a one-foot length of three bund led
conductors of this sam e cable in free air, the
ampacity listed in Tab le 310-67 is
645
amperes. Q is
27.3 Watts, and R is 1 8O0C/ W. The value of C is
three times the value of one conductor: C is 0.629
whr/oc. With these values for R and C for these
three large single bundled conductors in free air, the
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value for K is 1.13 hours. It would take a period of
about four time constants,
or
about four and a half
hours, fo r this three-conductor bund le to heat up.
Empirical values for K are listed in Table 43 of
ANSUTEEE Std. 242-86 [3]. Table 43 applies to
three-conductor cab les and is repeated here:
Table 43
K Factors for Equations in
8.5.2.4
Cable Air UG Direct
No In Duct Buried
Cond Cond
<
#2 0.33
0.67
1.00 1.25
#2-4/0
1.00
1.50 2.50 3.0
2 2 5 0 MCM 1.50 2.50 4.00 6.00
The application for these table values in this standard
is similar to transient temperature calculations. The
table values are suitable for the application in the
standard, in section 8.5.2.4, which makes use of the
values for K.
The value of 1.13 hours above compares with the
table value of
1.5
hours for
500
kcmil cables.
Cables in Conduit
In Appendix
A,
formulas for the transient
temperature rise of cables within a conduit mounted
in free air are derived. The properties of these
equations are discussed in Appendix B. Values for
coefficients and time constants have been calculated
for
250
kcmil,
500
kcmil and
750
kcmil, with
5
kV
unshielded and 8 kV shielded insulation. The results
are listed in the calculation sheet included as Table
BI, and discussed in Appendix B. Referring to Table
BI, the results show that the larger the cable size, the
longer are the time constants, and time constants with
the cables in conduit are longer than the time
constants in free
air
or spaced in tray. In Table BI,
values for R and C discussed above are listed under
Rt for R, and C l for C. For
500
kcmil and
750
kcmil cable sizes, not much difference is seen
between the two similar cable insulations listed in the
table. Comparing the table time constant values with
the values in Table
43,
the values in the first two
columns in Table 43 are a fair summary for the
calculated constants in Table BI.
A criterion, introduced above, is developed in
Appendix B that converts the cable temperature rise
equation to the simple exponential form (see
Appendix B equation
20).
Values for this
Ch
criterion are listed in T able BI, and show that as cable
size increases, the simple exponential form becomes
more accurate. With the largest value of ch, 1.276
for the
250
kcmil conductor size, the simple
exponential does represent a Fdirly accurate m eans to
calculate the conductor temper ame. (For a
discussion of the error see Appendix B). The values
suggest that for smaller cables the simple exponential
form would be less accurate. A short form of the
equation, (18d) based on Fh, the fractional part of
Ch, is exact.
Applications to Fast
Transient
Loads
The best way to apply the data in Table BI is to
illustrate through an example:
Examole: Five crusher-conveyors are located two
miles from the processor plant. Each i s driven by a
2000
Hp motor fed fiom a variable frequency drive,
having rated output of
2000
hp at
4160 V
at
60
Hz.
The drive equipment is located in the processor plant.
Rated motor voltage is
4000V;
ameplate current is
250
amperes. The motor current profile for this
crusher application is shown in Table I below.
To overcome the conveyor’s inertia and stiction
during starting, an initial current of 2000 amperes at
15 Hz
s required. Th e current ramps up to this value
in
2
seconds and holds until conveyor movement
results. This takes a maximum of 30 seconds.
Conveyor loading then commences, feeding the
crusher almost immediately. The motor frequency
ramps to 60 Hz during initial loading. Biting into the
first few loadings requires a series of transient motor
current surges that average 1500 amperes, or less,
and last no more than 20 seconds each. Typically, a
couple of surges are usually required, but no more
than four are ever necessary. Each time a transient
occurs, the drive automatically lowers the frequency
to
30Hz
until the crushing is completed, thereby
providing the large torque required for the transient
crushing loads.
These transient motor currents occur with a minimum
of
2
minutes betw een each transient. The motor
current between these transients is at
230
amperes.
Afler the last transient, motor current decreases to a
nominal
80
percent, or
200
amperes at
60 Hz.
This
lasts until the next loading. The next loading requires
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the same series of
1500
ampere transients, repeating
the first cycle, except for the starting 2000 ampere
surge. These loading cycles continue
through
two
shifts. Each loading cycle takes a minimum of two
hours.
For voltage regulation considerations, a 250 kcmil
conductor is, first selected. Its impedance
characteristics.are adequate for the 10,000 foot feeder
length from the processing plant out to the motors. It
is believed that, because of the cable heating from
these large current surges, two 500 kcmil feeders in
parallel will he required.
The drive manufacturer recommends that the feeders
be installed in conduit, to provide shielding for the
high-frequency current elements, composing the
square current profiles that the drive generates for the
motor.
The square current profiles contain harmonics,
having the six-pulse characteristic profile. The six-
pulse profile is the fundamental, of unit amplitude,
and the odd harmonics except the triplens. These are
the harmonics that are divisible by three. The
amplitude of each harmonic is the reciprocal of the
harmonic number. Thus, the seventh harmonic's
amplitude is 1/7th. By taking the square of each
harmonic current, multiplying
it
by the 'increased
resistance from skin effect at the harmonic frequency,
and adding these products, the total heating effect of
the six-pulse
current
camed by the
conductor
is
calculated. This assumes that the resistance to each
harmonic current changes only
from
skin effect; that
is, there are no significant changes due to frequency
from stray induced couplings that result in increased
resistance. This is usually the case. (This is not true
in transformers where losses are frequency dependent
and harmonic losses are greater.) And here, where
the heavy loading is at 30 Hz, it is the case. The six-
pulse harmonic heating effect amounts
to
15 percent
of the heating from the fundamental current. Thus,
the equivalent current would be the square root of
1.15, or 1.073, times the fundam entalvalue.
The first consideration is the temperature rise
resulting from the initial 2000 ampere starting current
that lasts 30 seconds. The 250 kcmil size will be
considered first. The temperature rise can be
calculated from equation 18d in Appendix B. Listed
in Table B I are the values for the constants and time
constants for one three-conductor bundle
of 250
kcmil conduc tors. The value for AT is 2372OC,
calculated from (2) above. The heat dissipated in the
conductors is 746 watts, with a corrected current of
2146 amperes. The values
for
the exponentials after
30 seconds are 0.972 for the sub-transient, and
0.9953
for
the transient. This calculatio n shows that
the temperature rise from the initial 2000 amperes for
30 se con ds is 14.1'C.
The temperature rise from one 1500 ampere surge
can similarly be calculated. This calculation shows
that the temperature rise from an initial 1500 amperes
for 20 seconds would be 54°C .
The two-hour current profiles ar e listed in Table I. If
the rms equivalent current of these profiles
is
calculated, the temperature rise kom these profiles
can he found. The rms equivalent currents would
result in the same heating
as
with these profiles.
Each transient heating profile would plot as a
temperature rise varying about the same exponential
curve
as
that generated by its
rms
equivalent current.
The rms values in Table I were calculated by
summing the squares of the corrected currents
multiplied by their intervals. Then, dividing this sum
by the two-hour period determined the mean squared
current. Taking the square root of this mean squared
current yielded the rms value.
TABLE
I
MOTOR
LOADING
PROFILES FOR CRUSHER-
CONVEYOR
First Cycle
T i m e p
urrent
0 .5min 2000A
0.5 min 230A
0.33 miu 1500 A
2
min 230
A
0.33 min 1500
A
2 min 230 A
0.33 min 1500 A
2 min 230 A
0.33 min 1500 A
111.67min 200A
Recurring Cycles
0 .33min 1500A
2 m i n 2 3 0 A
0.33min 1500A
2 m i n 2 3 0 A
0.33min 1500A
Z m i n 2 3 0 A
0.33 min
1500
A
112.67 min 200 A
i me
Current
rms value is 286 A
Using this same m ethod, the rise from the four 1500
ampere surges in the second column, based on their
r equivalent surge current of 672.5 amperes, is
2 I . P C .
At the end of the first cycle, the. cables reach a
-temperature rise of 31.6 C. After the second cycle,
rms
value is 255 A
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the temperature rise is 35.8 C. This is from using the
combined
rms
value of both cycles, of 271 amperes.
The
full
response to steady state takes 7.
I
hours. By
this time a temperature rise of 38.0 C is reached.
Then, additional rises from each set of four 1500
ampere surges adds spikes of 21.8 C.
This makes a
peak rise of
59.8
'C for the se spikes.
With these moderate values of temperature rise with
one 250 kcmil feeder for each motor, it is clear that
only one three-conductor cable, instead of two
500
kcmil cables, is required.
The savings in installing
only five of these feeders, instead o f the assumed ten,
is estimated at 1.1 million dollars
(US).
IV. ROCEDURE
FOR
SIZING
CABLES
The steps given in the examp le above
are
as follows:
Determine the worst-case current profile.
This includes the number of repetitive
cycles.
Adjust the currents for harmonics, shield
losses and dielectric
losses.
Calculate the rms value for the profile.
Determine the maximum twenty-four hour
and seven-day-average design ambient
temperatures. Max imum peak temperature
ever recorded has little meaning for the
cable time constants.
From voltage regulation requirements, select
a trial cable size. Calculate the peak rise for
high-current surges as if they occur at the
start of th e response.
Calculate the steady-state temperature rise
fiom the
rms
current, using repeated profiles
if required.
Add the steady state and peak rises
to
the
design ambient temperature and compare
with the temperature rating o f the trial cable
size. For seldom repeated current profiles,
having some days between energizations,
compare with the cable's emergency
temperature rating.
Select a larger (or smaller) conductor size
and calculate steady-state and peak
temperatures if the first selection is
unsatisfactory.
Determine the fast heating capability of the
drive or power source. The cables' fast
heating capability should no t greatly exceed
the capability of the source to provide the
currents.
Cables that are rated for 105OC continuous operating
temperature have an emergency and an instantaneous
temperature rating of 1 3 0 T and 25OOC. This is
listed in manufacturers' data.
Limitations of the Methods
The equations and
data
do not apply to three-
conductor cable assemblies. No r do they apply to
more than three conductors in a conduit. Their
limitations with underground installations are
discussed above. If groups of three condu ctors
installed in a cable tray are not space d apart, the data
do not apply. The equations do apply to PVC and
aluminum conduit, as well
as to
other sizes of
conductors, and to aluminum conductors. Data for
these materials can be developed as was done for the
data in Table BI.
IEC
sizes can be calculated in the same way as
discussed above. Ampacity values for
IEC
sizes,
once established for local conditions, can be used in
the same way
as
hose in the NEC.
The problem with three conductors in a cable
assembly (see NEC Tables 310.71, .72, .75 and .76)
is the error in attempting to represent the cables with
one schematic node. An additional node in the
schematic, Fig.Al in Appendix A, would be required
to represent the outer covering layers and the fillers
within. With three nodes, solvin g a third-order
polynomial would be required, instead of the
quadratic,
(IO)
in Appendix A. This would yield
three time constants, with one longer than the other
two, and equations for their values similar to (12),
(13) and
(14).
Just as with a three-node
representation of an underground installation
discussed above, a criterion similar to
ch
could be
postulated, and a simplified form, like I ) above,
would be exp ected.
With some error, the solutions of Appendix A might
be extended
to
represent the three-conductor cable
assembly by adjustments in
C I
and
RI.
Similarly,
six conductors might also be represented.
The rub
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might be in adjusting RI. The NEC lists the
ampacity
of
six conductors in a conduit as 80% of
the ampacity of three conductors. Six conductors,
carrying
71%
of
the
current of three conductors,
generate the same heat as do the three conductors.
Does this mean that R I is 9% less for all conductor
and conduit sizes?
Some value may be found for other installations in
knowing the calculated peak rise for the same
conductors installed in a conduit in air. For example,
the calculated peak rise might be greater than the
peak rise with the conductors installed in an
underground duct.
The method used
to
divide the value of
RI +
RZ
in
Table BI may not be accurate. The effect on the
values of
K’
and
K”
has not been explored.
v.
CONCLUSIONS
This paper has presented the means to size power
cables based
on
calculating transient temperatures
resulting from fast transient heating. Analytical
methods are employed. Cable temperature ratings
are compared with these calculated temperatures to
make a cable size selection.
Data for three conductor sizes are developed and
presented. The methods to develop data for other
conductor sizes are developed. The formulas derived
herein are limited to cables spaced apart in open tray
or free air, and in conduit in air.
A
procedure for sizing cables is presented. An
example is included that sizes the feeders for five
2000 Hp crusher-conveyors.
Methods to extend the usefulness of the data to other
installations of cables are discussed. Further work is
recommended to develop more simplified rating
procedures.
VI. APPENDIX . DERIVATIONF
TRANSIENT HEA T
FLOW
EQUATION
The model for the derivation is shown in Fig. Al. In
this model, the three conductors are considered as
spaced togethcr and located in the axial center
of
the
conduit. The conduit is assumed to be suspended in
free air. The conduit and cables are regarded as long
enough to have no axial heat flow, and a unit length
of the conduit and cables is represented. Thereby, the
heat flow from the conductors is more
or
less only
radial to the inside conduit wall, and to the
surrounding air. This simp lifies the heat flow as one
dimensional. Also, any temperature differences
among the three conductors and their coverings are
ignored and assumed
as
negligible, and the small
radial temperature difference through the conduit
wall
is
neglected. The conductors are represented
in
Fig.
A I
as the left node.
CONDUCTORS CONDUIT
R I
“O+J =Jqc t R 2
T
1
Ambient Heat Sink and
Temperature Reference
Fig. A l . Schematic representation ofhea t transfer h m
three conductors in a conduit in air
The thermal resistances in this model are assumed
constant and do not change with temperature. This is
not strictly true, but the fourth-power radiant heat
transfer can be essentially proportional to
temperature difference over a moderate temperature
range, and conductive and convective coefficients
can be similarly treated. The thermal capacitances
also muqt not change with temperature. These
qualifications allow the differential equations that
follow to be of the linear type with constant
coefficients.
In this analysis, the three conductors generate over
time a constant heat loss, represented as Qo. Prior to
zero time, the conductors are de-energized, and the
conductors and conduit are at ambient temperature.
ARer zero time the currents
in
the
three
conductors
are equal and such that the heating generated in the
conductors, Qo, is constant. Also, the heat generated
in the conductors consists
of
Joule heating, dielectric
losses and shield losses in the cables. Any small
amount of heating in the conduit generated by
induced currents is neglected. For the duration of the
responses derived below, the ambient temperature is
constant in this model.
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The elements in Fig. 1A represent the following:
Constant heat flow generated in
unit leng th of the three cables (W).
Thermal capacitance of the three
cables,
Wh / “C).
Thermal capacitance of theconduit
(wh
/
“C).
Thermal resistance betwee n cables
and con duit (“C
/
W).
Thermal resistance between conduit
and air (“C / W).
That time-va rying portion of Qo
stored in mass of the cables (W).
That portion of the time-varying
heat flowing t?om the cables to
conduit that
is
stored in the
conduit’s mass (W).
Time-varying heat flowing
&om
he
conduit to air (W).
In the equations that follow:
AT
CD
OC
‘ d
QC
KI
K2
K3
Solutions
Steady-state co nductor temperature
rise abo ve ambient reached after
the transie nt responses (“C).
Timevarying temperature
r ise or
difference (“C).
Temperature degree difference of
the Kelvin or Celsius scales.
@c on dui t (“C).
ables (“C).
Time constant equal to
R1
C1
(hr).
Time constant equal to R2 C2
(hr).
Time constant equal to R2 CI (hr).
dt
= CP
condu i t, a t t im e t
=
T (2)
d t , a t t im e t
=
T (4)
(5)
Taking the Laplace transforms of equations
I ) through 5 ) :
1
-eo
S
The L aplace transform of Qo is denoted by
-
The Laplace transform o f
ql
s denoted by
q l
:
The Laplace transform of
7 )
1 -
= R , q ,
is:
Q d = -q2
=
R ,q ,
sc
The Laplace transform of aCs:
1 -
’
-q
I ’
e sc,
Solving for q2 using
(6 ) .
7), and
8 ) :
1 - -
I - I - R -
-q,
= - q 2
+
R , q ,
+
sc, sc, sR,C,
q2
.
Multiplying by
sc,
:
Substituting in
(6):
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1 -
q 2 + -
sR2C,
q2
1
Qo
=
S
1 -
) q 2
1
+-
2
sR,C,
+
c R 2 C 2 - sR2C2
C RI c,
+ S +
~ = ~ - + S ~ R , C , + S -, RIG,
c2 R2C2
1 -
- ) 4 2
=
R2C2
Within the quadratic, taking the coefficient of s
changing some terms and adding fractions:
Substituting the expressions for
Rs:
Rewriting ( IO ) :
K ,
i
,
i
,
Qo
= [
K , s 2 + K , S
KIK2
1 -
K , K , q 2
+ K,-
K 2 + K , + K , 1 -
s + -
K , K 2
q
o = K , [ s 2+
KlK2
The quadratic coefficient
I
, + K , +
K ,
1
[ S 2
+
s + -
KIK2 KIK2
1 1
K
K
has two roots expressed as (s +-) (s +
,
which are real and
one
is larger than the other. Let
1
1
e the lesser root and e the greater root.
K' K
Then R is larger than K .
(1 1)
Qo
1
472
=
K l (s++)(si+)'
The solution to (1
1)
can
now
be found as
the anti-transform of q2
:
Qo 1
K 1 1
q 2 =
K'
K
(See [41, Table
ofkplplace Transforms p189,
number
77.)
The expressions
for
the roots are found from the
classical quadratic solution. The second term in the
solution for the roots, which is under the radical, is
( K , + K 2 i K , ) 2-- 4
K , ~ K , ~ KIK2
*I12
Rewriting this term as
- , / ( K , + K 2 + K , ) 2 - 4 K , K ,
1
I
the expression for the roots becomes:
2KIK2
1 - K , i K , + K ,
--
K 2KIK2
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and
1
P
K ' K , K , '
K ' K = K , K , ; K ' -K = p .
P
1 -
q 3 =
2
sR2c
I
-
q = -q,, and
q3
=
dt
=
sK2 K2 =02
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VII. APPENDIX
B.
PROPERTIES OF THE
Time Constants
HEAT
FLOW
EQUATIONS
Initial Conditions
Both expressions for
92
and 43 above contain the
exponentials with time constants R and K , given in
Appendix A (IZ),
(13)
and (14). And as stated,
R
s
larger than
K ,
such that K'
- K = p
Equation
(12)
Appendix A:
P
~~
defines p. The expression for the cable temperature
rise,@.,, emb odies both heat flows, and can be
Considering the expressions for
q
and
4
from
divided into two periods of time, the sub-transient
and transient. Taking the value of time equal to
t = 4 K ,
16)
d
Y
At time t
= 0,
t
e
K'
and e
K
are each equal to one,
K
q 2
Qo
- 2 - ( I - I ) = O
P
P
43
=eo-
( K ' ( l ) - K ( l ) ) =
Qo---@ -O.
Thus,
with both
92 and
43 equal
to
zero,
Qo -
P
is equal
to
zero.
Final Conditions
At time t
= -
I
e K' nd e
K
are each equal to zero.
,
In
1
6), e
K
has disappeared before
-..
- e
K' =
0.982
This is less than
2
percent from a value
of
one minus
the exponential, reached a t infinite time. Afler t
=
(17)
4K , the value
of
Letting time from zero
to
about t
=
4 K be defined
as
the sub-transient period, then the period from this
time to about
t =
4
K' is
defined as he transient
region. To be consistent, the time beyond about t
=
4 R is considered steady state.
Sub-Transient Response
The expression for the cable temperature rise, given
in Appendix
A,
can be re-written as
( K ' - - K 2 R 1
e $ ; ] (18c)
A T [ I --
K'-K
RI +R2
e
K ,and
e
K
is zero, making
42
equal to zero.
In (17), e
'
as likewise disappeared before transient term, and the second is the transient term.
e K'
and
e K are zero, making the steady-state expone ntial with
two
coefficients,
K
and
Here, the first expone ntial term in AT
is
the sub-
Within the sub-transient term is a decaying
value
O f 43
equal to
Qo
.. These subtract from each other. The
difference in these terms responds in a way to
K2Rl
RI +R2
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account for the delay in the temperature rise of the
conduit. Until the cables have become warm and
have started to transfer heat to the conduit, the
conduit does not start to get warm because the
conduit, unlike the cables, doesn't have heat
generated in it. Thus, the conduit lags the
temperature rise of the cables. The difference in
these terms is added to the transient term, and
disapp ean b y the end of the sub-transient period.
Transient R esponse
Atter the initial sub-transient portion o f the response,
QC becomes
_
1
__
K , R , e
'1,
K'-K RI +R 2
with both e ''erms having evaporated
Q c = A T [ l -
RIK, -
RI +R2
It
can be shown that
Then, if K
(RI+R 2 )cl
= K ,
nd
Q c
collapses into the simple
IK2
R, +R2
expression:
Q c = A T (
1
- e T ) .
20)
This is the usual, expected and em pirical result that is
found, and it is a much simplified form of the
transient response. Also, to the extent that
K' =
(RI
+
R 2 )C,,
his transient response is useful
to calculate the cable temperature atter the short-
duration transient has evaporated.
Not only is the expression for the
transient
response
simplified, if the approximation is true, the
sub-
transient function is likew ise simplified. If the
approximation is true, the two sub-transient
coefficients disappear:
I
Qc=A T ( 1 -
e
K ' ) +
. .
With this approximation, the sub-transient response is
negligible, and 20) is the entire sub- and transient
response. Hence, the following criterion is def ined
AISO,
with
(RI
+
R2
)Cl
= K , +
K3
Returning to (lec), at zero time
Qc
is zero, as
discussed above. Therefore the transient and sub-
transient coefficients, with the exponentials equal to
1 at zero time, are equal and subtract. This can be
shown
by substituting
ch
in
(19)
and (18c) at zero
time, and reducing the two coefficients.
CoolDown
The model in Appendix A can be used to derive the
expressions for cool down. These will be of the form
of decaying exponentials with time constants K and
K' and coefficients similar (if not identical) to those
in (18c). The ch criterion will still be valid,
however. Just as Qc reduces to ZO), the cool-down
expression would also reduce to the approximation:
I
Q c =
AT e
K
T o the extent that ch is
nor
true, the decay can be
expressed as the sum of
two
exponentials, with time
constants
of
K' and K ' , and with coefficients that add
to
the initial cable temperature.
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The two exponential expressions can be illustrated by
constructing a semi-log plot of the cable cool-down
from steady state temperature. Starting from initial
time, the plot is the sum of
two
lines, each an
exponential decay, with slopes of
- K
and -K'. The
latter is similar to (22), except the s u m of the initial
temperatures o f both lines equals AT.
The derivation of Appendix A uses initial values of
zero for cable and conduit temperature rises. If the
derivation of Appendix A were redone, but with non-
zero constants for initial values for cable and conduit
temperatures, it would yield formulas for cable and
conduit temperatures during warm up from any
values of initial temperature rises. If these same
constants were included in a derivation for cool
down, then a complete set of analytical equations for
warm up and cool down would result. With this
full
heat-up and cool-down set of equations, the full
dynamic response to any fast transient electrical
current profile could then be calculated.
Calculation of Constants
The calculation table, Table BI, illustrates the
equations of Appendix A and the simplifications
above..
In
these calculations, Q, the heat flow
generated in the three conductors, is based
on
the
electrical resistance, Re in the table, which is taken
from the NEC, Chapter
9
Table 9.
For triplexed cables in tray or free air, R in the main
text is labeled Rt in the table. C in the main text is
C l in the table, because
C l
represents the thermal
capacitance of the conductors and their coverings
whether in tray or conduit. Thus, the time constant,
RC, is RtC l in the table.
For triplexed cables in conduit, the value for R I is
obtained by calculating R1 +
R2,
by using the
ampacity table cited in the calculation sheet, and
subtracting R2. The value of R2 is found by
multiplying Rt by the ratio of the triplexed
conductors' diameter divided by th e conduit diameter.
The diameter of a circle that circumscribes the three
conductors is used to represent the triplexed
conductors' diameter. Thi s circle's diameter is 2.155
times one conductor's diameter. No adjustments
were made for emissivity, or diameter in the conduit's
convective coefficient, comprising
R2,
because these
were considered as almost the same as for the
circumscribing circle. Th e value for R I determined
in this manner is almost always lesser than Rt. (See
the 750 kcmil size,
8
kV insulation, where they are
about equal.) This implies that the snug fit of the
cables in the conduit results in an air gap that is
thinner than the convective boundaty layer around
the warm cables in free air. Nevertheless, R I+ R2 s
based on the cited ampacity table.
The conduit size is determined as for 40% fill or the
next larger size. Thus, a
3
1R-size Schedule 40
conduit is used for 250 kcmil, a 4 size for
500
kcmil,
and a 5 size is used for 750 kcmil.
No
adjustment in
ampacity from using diameters larger than these sizes
is made in the ampacity tables.
However, a greater
value for C2, and therefore
K',
results with a larger
heavier conduit, or with Schedule
80
wall conduit as
well. This is a means to increase the time constant if
slower heating is desired.
The values for specific heat in the table are converted
from water, having a specific heat o f 0.52 74 Wh per
lb 'C.
The relative specific heat of polyethylene, of
0.50, was used in the tables for insulation and jacket.
This is not representative for PVC, which has a
relative specific heat of 0.25 [9]. Thus, lesser values
for
K'
can be expected with PV C cab le jackets.
Error Using Simple Exponential
Near the bottom of the Cable Heating Tabulation,
Table
BI,
are listed the values for the criterion,
Ch.
These are greater than unity, and the largest is for the
250 kcmil conductors, having
the
value of 1.276.
The error for the 250 kcmil conductors is shown in
the following Table
B
11.
As shown in this table, the error is large in the first
few minutes into the sub-transient period, and
decreases with time.
Therefore, if accurate cable
temperatures are needed for the early minutes, the
full expression for temperature rise must be used.
Otherwise a value smaller than the actual value is
calculated using the simplified expression.
TABLE B
I1
ERROROF
SIMPLE EXPONENTRL
250 kcmil conductor size in conduit
Time
t =K
t=K'/2 t=4K
t - Z R
17.51~1 53m 70m 3.5h
@ c i ~ ~ 0.177 0.4239
0.5090 0.8720
f
1
- e
K
0.151 0.3935 0.4819 0.8647
EKOI -14.7% -7.2% -5.3% -0.84%
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The values for Ch in Table BI increase with smaller
conductor size. With cable sizes smaller than 250
kcmil, the error will be greater than in the table
above.
Let: 1 < c h <2,hen c h
=
1 + a fraction, or
c h 1 + F h .
This is an expression of the simple exponential plus
an adjustment, calculated fro mF h, the fractional part
of
ch.
REFERENCES
[ I ]
[2]
N ation al Fire Pro tection A m . , W A 0
National Electrical Code, 2002 Ed. NFPA
Wiseman, R. J.
An
empirical method for
determining transient temperatures of buried
cable systems, AIEE Transactions on Power
Apparatus and Systems, pt.III, vo l72 , pp
545
-
562,
June
1953
IEEE Std. 242-86 Recommended Practice
for Protection and Coordination of Industrial
and Commercial Power Systems
-
Buff
Book, IEEE
G. E. Roberts and H. Kaufman, Table of
Laplace Transforms, W. B. Saunders Co.,
1966
Bateman Manuscript Staff,Table o f Integral
Transforms,
Vol.
1, McGraw Hill Book Co.,
1954
[3]
[4]
[ 5 ]
[6]
W. E. Boyce and R. C. DiPrima, Elementary
Differential Equations and Boundary Value
Problems, 2nd Ed., J. Wiley and Sons, 1969
Houston Wire and Cable Catalog,
1987,
Houston Wire and Cable Co., Houston TX.
Hubbel Anderson, Technical Data - A
Reference for the Power Industry, Hubbel
Anderson Power Systems, AEC lll
[9] Salamander Ceramic Infrared Emitters
Technical Manual, Physical Properties of
Materials, p
13,
Mor Electric Heating
Assoc. Inc.
Engineering Data for Copper and Aluminum
Conductor Electrical Cables, Bulletin EHB-
90,
The Okonite Company, Ramsey NJ
[7]
[8]
[ IO]
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Constant
Re Ohms1IOM)'
13
(105
DegC)
3 13sqrd Re = Q3
Temp 1 Q3
= RI
Wconductor
Ibs
Wcu
Ibs
CC
wcu
EC w-h/Deg
C
Wcond -Wcu
=
Wi
Ibs
ei w-hilb DegC
Wi ci w-hiDeg C
Wceu + wici = c
Rt I
4RtCI
Conductor Dia.
tX
2.155
Dc=
De
2.74 Dc
= Dd
min
Conduit Dia. ODd
DeJODd RI
=
U2
Id(lO5 DegC)
Source
TABLE
I
CABLE
HEATPIG
TABULATIONF CALCULATED CONSTANTS
Code: Ch 9 Tbl
9
Code:Tb1310-
67
Code: Tbl310-
67
Dam Sht.
Data Sht.
Data Sht.
Data Sht.
Data Sht.
Data Sht.
250 kcmil 500kr.mil 500 kcmil
5 kV 5 kV 8 kV Shlded
I n
open tray
or free air
0.05411000' 0.02911000' 0.02911ow
415 645
A
650
A
27.90 W 36.19 W 36.76 W
23 3 DDgnv ISOoegnV 1.77Deg/W
3.555
Ibs
6.165 Ibs 6.336 Ibs
2.316 Ibs 4.632 Ibs 4.632 Ibs
0.0485
0.0485 0.0485
0.1123 0.2247 0.2247
1.239 Ibs 1.533 Ibs 1.704 Ibs
0.264 0.264 0.264
0.3271 0.4047 0.4499
0.436 W-WC 0.629 w-h/C 0.675 w-WC
1.02 hrs 1.13 h n
1.19 hrs
4.1 h n 4.5
hra
4.8 hrs
In
steel conduit in free
air
1.14in. 1.40 in.
1.27
in.
2.451
in
3.017
in.
2.737
in.
3.12in 3.84 3.48 in.
4.000 in. 4.500 in.
4.500
in.
1.43 oeglw 121DDgnv 1.08Orgnv
750 kcmil
5 kV
0.02lIlOW
835
A
43.93 w
1A8
Dc w
9.060 Ibs
6.848 Ibs
0.0485
0.3321
2.212
Ibs
0.264
0.5839
0.9161 w-
WC
13 6 hrs
5.4 h n
1.U
n.
3.534
in.
4.49
in.
5.563
in.
0.940 Oegnu
750 kcmil
8 kV Shlded
0.02111000'
820
A
42.36 W
1.53 Deg/W
9.099 Ibs
6.848 Ibs
0.0485
0.3321
2.251 Ibs
0.264
0.5943
0.9263 w-WC
1.42 h n
5.7
hrs
1.47 n.
3.103 in.
4.03 in.
5.563 in.
0.853
D e e
Code: Tbl310-
355
A 530 A 535
A
665 A 655
A
77
.
3
Id
ylrd Re
=
Qo
20.416 W 24.44 W
24.90W
27.86 W 27.03 W
Temp 1Qo=
R I + R 2
Code: Tbl3lO- 3.18
De@
2.66
OegnV
2.61 D e w 2.33 D e w 2.40
Dew
77
RI
Is RI > R t ?
Conduit Wt. Wd
cd
Wd cd
=
C2
R I C I = K I
R2 C2
=
K 2
R2 CI = K 3
2KIK2
K l
+ K 2 + K 3
X I +KZ+K.z)sqrd
4KIK2
Rho
x
K
K ' / ( K I + K 3 ) = C h
4 K
4 K
._
1.75 DrgnV
no
Data Sht. 8.31 Ibs
Data Sht. 0.0567
O.47lw-WC
0.763
0.674
0.623
1.0285
2.060
4.2436
2.0570
1.4787
1.77
hrs
0.291
hrs
1.276
l l h n
7.1 hm
1.45 O W 1.53 oegn
no no
9.82 Ibs 9.82 Ibs
0.0567 0.0567
0.557~-WC
0.557w-NC
0.912 1.033
0.674 0.602
0.761 0.729
1 3 9 v 1.55DeglW
no Y
13.44Ibr
13.44Ibs
0.0567 0.0567
0.762
w-h/C
0.762 w-WC
1.273 1.436
0.716 0.650
0.861 0.732
~~ ~ ~~~ ~~
1.229
1.244
1.823 1.867
2.347 2.364 2.850 2.818
5.508 5.588 8.123 7.941
2.458 2.488 3.646 3.734
1.747 1.761 2.116 2.051
2.05
h r s
2.06 hrs
0.30
hn
0.30
hrs
1.225 1.169
1.2 hn 1.2hn
8.2
hrs
8.2
hn
2.48 hrs 2.43 hn
0.37
hrs
0.38 h n
1.162
1.121
1.5 hrs
1.5
hrs
9.9
hrs
9.7 hrs
32