
reading / British practice / Vol D - 1990 (ocr) ELECTRICAL SYSTEM & EQUIPMENT
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Power cable system design |
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Values for RL and XL are taken from Appendix B. |
The conductor temperature after two hot starts is |
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Correcting resistance for temperature at 0.8 I n |
given by: |
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K2s2 |
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gives: |
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1 1T - |
- loge [(0 2S1 + 0)/(OFL + (3)1 |
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RL = |
959 tz12/rn at 46 ° C and XL = 82 )4C2/m |
substituting |
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2t 51 |
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Substituting in the equation gives: |
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(148) |
2 x |
(300) 2 |
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415 |
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(1021) 2 |
- |
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lo g o RO2ST + 228)/ |
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L max ------ |
-7- x |
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2 x 40 |
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Ni 3 |
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(40 + 228)] |
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2 x 10 6 |
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0.042 |
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log, [(0251 + 228)/268] |
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(100 x 0.8 x 63(959 x 0.85 + 82 x 0.53) ) |
280 |
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02sT + 228 |
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= |
111 m |
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02sT |
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52 ° C |
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Again, this value is greater than the actual route length |
Finally, to calculate the conductor temperature |
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of 85 m. In summary, a 4-core 35 mm |
2 |
cable is |
after a short-circuit fault: |
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K 2 S 2 |
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required. |
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Iic |
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4.7.2 Motor circuits |
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tsc |
log o KOSC + (3)/(0 2ST |
+ 0)] |
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substituting |
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11 kV motor |
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(148) 2 x (300) 2 |
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-s, n 11 kV ID fan motor has a rating of 3 MW. The |
(39.4 X |
103 ) 2 |
— |
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log, [(Osc |
+ 228)/ |
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0.7 |
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motor manufacturer has given a ratio of locked rotor |
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kVA to rated output of 5.4 and a starting time of 40 |
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(52 + 228)] |
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seconds. The cable route length is 100 m and is in |
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0.551 |
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log, [(t3sc + 228)/280] |
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air at an ambient temperature of 35 |
° |
C. Determine the |
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,: able size required. The back-up protection operating |
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486 |
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esc |
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228 |
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ti me is 0.7 S. |
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es c |
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258 |
° |
C |
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From Table 6.18 77 = 0.962 and cos ci) = 0.91 for |
Although the conductor temperature is 8 ° C too |
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a 3 MW motor. The full-load current is given by |
high, in reality there would be some conductor |
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kW output x 1000 |
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cooling during the sequence of events described and |
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'FL — |
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therefore a judgement is taken that the 300 mm 2 |
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x VL x i, x cosit, |
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size cable is satisfactory. |
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substituting - |
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3000 x 1000 |
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- 180 A |
(c) Sheath voltage |
There is no transposition and |
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therefore the standing voltage on the middle cable |
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N/3 x 11 000 x 0.962 x 0.91 |
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is given by:
The maximum starting current
1ST = 1.2 x 'FL X ratio x x cos0
=1.2 x 180 x 5.4 x 0.962 x 0.91
=1021 A
(a)Continuous operation The current rating of a single-core 300 mm 2 cable laid in air is given in Appendix C as 675 A at 25 ° C.
At 35 ° C the current rating
=675 x 0.91 (from Appendix E)
=614A
(b) Fault conditions The conductor temperature during normal full-load operation is given by:
°FL = 0A + (0),4 - OA) x (IFL/Ic)2
substituting = 35 -4-(90 - 35) x (180/614)2
Vs = 47rft 10 -7 1og (s/r) V/m
Taking the armour radius for a 300 mm 2 cable as 18 mm and
substituting V s = 4 X 7r. x 50 x 180 x 10 -7 x log r, (80/18)
= 0.017 V/m
The magnitude of sheath voltage on the outer cables is given by:
1 Vs = 2r fl 10 -7 [(2 log, (V2 x s/r) 2 +
1.44] 2
= 2 x r x 50 x 180 x 10 -7 x
[ (2 log, Oh x 80/18)) 2 + l.44]2
= 40° C |
I V s = 0.022 V/m |
473

1P01"
Cabling |
Chapter 6 |
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As the cable length is 100 m, the standing voltage on the centre cable is 1.7 V and on the two outer cables 2.2 V, and is therefore satisfactory.
During a short-circuit fault the sheath voltage is given by:
Vsc = V s x
substituting for outer cable Vsc
= 2.2 x 39400/180
— 482 V
The conductor temperature after two hot starts is given by:
(IST) 2 |
K 2 S 2 |
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— logo Re2ST + i3)/(.0Ft + 3)] |
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2tst |
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substituting |
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(148) 2 x (150) 2 |
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(365)2 — |
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log, [(02sT + 2281/ |
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2 x 15 |
(27 + 228)] e 2ST = 29 ° C
The short-circuit sheath voltage is less than 2 kV and is therefore satisfactory.
In summary, one 300 mm 2 single-core cable per phase is required.
3.3 kV motor
A 3.3 kV pump motor has a rating of 300 kW. The supply is taken from a 3.3 kV FSD with a 400 A fuse. The motor manufacturer has quoted a starting time of 15 seconds. The cable is to be laid in air at an ambient temperature of 25 ° C and a route length of 110 m. Backup protection is provided by the fuse in the zone protected by the high set instantaneous overcurrent relay. Determine the size of cable required.
From Table 6.18, t = 0.945 and cos (/) = 0.91 and from Table 6.17 the motor starting ratio = 5.8. The full load current is given by:
kW output x 1000
'FL — ▪ x VL x x cost)
300 x 1000
▪x 3300 x 0.945 x 0.91
'FL = 61 A
The maximum starting current
= 1.2 x FL x ratio x x cos 43
1.2x 61 x 5.8 x 0.945 x 0.91
=365 A
(a) Continuous operation The smallest three-core 3.3 kV cable in the standard range is 150 mm 2 (because of short-circuit requirements) and it can be seen from Appendix C that this has a rating of 265 A in air at 25 ° C.
(b)Fault condition The conductor temperature during full-load operation is obtained from:
0 FL = OA + (OM — OA) (I FL /iC) 2
25 + (70 — 25) (61/265) 2 =27 ° C
The 1 2 t adiabatic line for a short-circuit temperature rise from 29 ° C to 160 ° C is now determined from:
I 2 t = K 2 S 2 log, [(Or + 3)/(Ot + 3)1
---(148) 2 x (150) 2 log, [(160 + 228)/
(29 + 228)]
= 203 x 106
The short-circuit I 2 t adiabatic line is superimposed on the fuse time versus current characteristic as shown in Fig 6.36. For the purposes of this example it is assumed that the cable is protected.
(c) Voltage regulation The motor starting voltage regulation is obtained first. The conductor resistance at the end of two hot starts temperature from
(b) is 29 ° C. From Appendix B, for a 150 mm 2 cable at 20 ° C the conductor resistance is 206 /.4.11/m and the equivalent star reactance is 80 giI/m. From the manufacturer, power factor cogb on starting is 0.5.
Conductor resistance RL
= Rc20 [1 + a20(02ST — 20)]
= 206 [1 + 0.00403(29 — 20)]
= 213 itf2/m
G/o R = 100 IL (RL cosy& + XL sin) .s./3/ 14.
=100 x 365 x 110 (213 x 0.5 + 80 x 0.87) 10_6 x V3/3300
=0.37%
This regulation is small compared with the 20% allowed at motor terminals during starting and therefore is acceptable. Because of the small value of regulation during starting, in this case there is no need to check the regulation under full load conditions.
In summary a three-core 150 mm 2 cable is required.
415 V motor
A 3 kW 415 V pump motor fed from a 415 V contactor starter has a cable route length of 80 m. The cable is
474

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Power cable system design |
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to be laid in air at an ambient temperature of 35 ° C. |
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K 2 S 2 |
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The maximum allowable voltage regulation on starting |
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— loge ROscc + t3)/(0A + .3)1 |
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Ira and on full-load 3.5%. Determine the cable |
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i, |
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(226) 2 x (2.52) 2 |
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.1ze. |
‘ppendix (.1, the maximum starting current |
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log ROscc + 234.5)/ |
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rriilmotor is 49.1 A with a full-load current |
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6 |
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a |
1 A, |
The starting time is 3.4 s and the selected |
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(35 + 234.5)1 |
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6 . |
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,ize is 32 A. |
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Oscc = 136 |
° |
C |
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COnfiIIIIOUS operation The current rating for a |
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cable in air at 25 ° C is given in |
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escH |
and Oscc are lower than the ca- |
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1-core 2.5 mm |
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Since both |
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Appendix C as 28 A. In an ambient temperature |
ble short-circuit temperature of 160 ° C the size is |
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of 35 ° C a rating factor of 0.88 is applied as given |
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satisfactory from this aspect. Finally it is necessary |
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in Appendix E. Therefore the cable current rating |
to check the maximum route length that will allow |
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i s |
24.6 A which is in excess of the motor full- |
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sufficient earth fault current to flow to clear the |
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load current of 6.1 A. |
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fuse using the method given in Section 4.6.2 of |
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(b) Fault conditions |
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The conductor temperature dur- |
this chapter. |
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ing normal full-load operation is given by: |
From Appendix B, the conductor and armour re- |
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OFt = OA |
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+ Rom — 0A)(iFt/ic) 2 ] |
sistance at 20 ° C are 7410 Aft/m and 8800 |
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= 35 + 1(70 — 35)(6.1/24.6) |
2 |
1 |
respectively. From (b), the full-load conductor |
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temperature is 37 ° C and, taking the armour tem- |
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= 37 ° C |
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perature rise to be half that of the conductor, gives |
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The conductor temperature after two hot starts |
an armour temperature of 36 ° C. Correcting the |
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resistances to these temperatures gives R, = 7905 |
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is |
obtained next: |
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Aim and R a = 9434 A-2/m. Also from (b) the |
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K 2 S 2 |
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intersection of the fuse and thermal relay (hot) |
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loge RezsT + 0)/(OFL |
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+ 13)1 |
characteristics give IF = 160 A. Therefore: |
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ST |
— |
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2t s1 |
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240 |
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(226) 2 x (2.5) 2 |
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(49.1) 2 |
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log o RO 2ST + |
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234.5)/ |
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1F (Rc + Ra) |
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2 x 3.4 |
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240 x 10 6 |
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(37 + 234.5)1 . |
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160 (7905 + 9434) |
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02yr |
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51 ° C |
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= 87 m |
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The next step is to check the conductor tempera- |
Since this maximum route length exceeds the act- |
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ture OscH for a fault immediately after two hot |
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ual route length, the cable is adequately protected |
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starts. The maximum fault let through is taken |
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against earth faults. |
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from the intersection of the fuse and thermal relay |
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(c) Voltage regulation |
The voltage regulation during |
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(hot) characteristics. For a 3 kW motor with a |
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32 A fuse this gives Isc H -= 160 A and t = 2.3 s. |
normal full-load operation is generally a more oner- |
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K 2 S 2 |
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ous condition than during starting and therefore |
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logo RescH + 3)/(02sT + |
the former is calculated first. From (b), the con- |
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ductor resistance at full-load conductor temperature |
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R1 = 7905 it.O/In and from Appendix B, XL = |
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(226) 2 x (2.5) 2 |
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100 ASZ/m. From Table 6.18 for a 3 kW motor, |
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log e [(Elsa/ + 234.5)/ |
coscb = 0.83. |
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2.3 |
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(51 + 234.5)1 |
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From Section 4.5 the maximum route length: |
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OSCH |
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109° C |
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Lmax |
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VL |
x |
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070R |
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Then the conductor temperature for a fault with |
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100 x I (RL coscb + XL sings) |
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the cable at ambient must be checked. The maxi- |
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mum fault let-through is taken from the inter- |
415 |
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3.5 x 10 6 |
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sections of the fuse and the thermal relay (cold) |
= |
x |
( 100 x 6.1(7905 x 0.83 + 100 x 0.56) |
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13 |
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characteristics. For a 3 kW motor with a 32 A fuse |
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this gives 1 = 130 A and t = 6 S. |
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= 208 m |
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475
WP"
Cabling |
Chapt er 6 |
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The motor starting voltage regulation is calculated using the conductor temperature after two hot starts which from (b) is 51 ° C. Correcting the conductor resistance for this temperature gives RL = 8313 A/m. From Table 6.20 the motor power factor during starting, cos 0= 0.28. Now:
(b)Digital signals defined as voltages or current whi ch are normally at one voltage or another with a relatively rapid change between states. Examples are plant orientated alarm signals, sequence control input and output signals (e.g., 0-48 V). They also include switched 110 V DC and 110 V AC circuits.
415 |
11 x 10 6 |
5.2 Cable types |
.13 |
( 100 x 49.1 (8313 x 0.28 + 100 x 0.96) ) |
For convenience the cable types used for these classes |
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of signals can be split into three categories: |
= 222 m
These maximum lengths for voltage regulation are both considerably in excess of the actual route length of 80 m.
In conclusion, a 3-core, 2.5 mm 2 cable is required to supply this 3 kW motor.
In this example, the limiting factor for route length is the requirement to ensure sufficient current flows
during an earth fault to operate the fuse. As discussed under 415 V fuse/contactor in Section 4.6.2 of this
chapter, the accurate but more time-consuming method for obtaining the minimum earth fault current is to construct the cable I 2 t adiabatic line (hot) on the relevant fuse characteristic. This will invariably give a longer route length and may be worthwhile determining in instances where this requirement dictates the conductor size.
5 Control and instrumentation cable systems
This section deals with the cabling systems that are necessary for the following functions:
•Control and instrumentation.
•Protection, intertrips and interlocks.
•Metering.
•Telecommunications.
•Alarms.
•Computers and data logging equipment.
5.1Signal levels
The types of signal being considered can be broadly split into two classes:
(a)Analogue signals consisting of voltages that vary relatively slowly and currents such as those present in transmitter outputs (e.g., 4-20 mA), ther-
mocouple outputs (e.g., 0-40 mV) and position indicating potentiometers (e.g., 0-10 V). They also include current transformer (CT) and voltage transformer (VT) circuits for instrumentation.
(a)Multipair control cables (as described in Section 3.6 of this chapter) which are suitable for use at voltages up to 110 V AC or 150 V DC. How-
ever, these cables should not be used for circuits which contain unsuppressed 110 V AC contactor or relay coils of such a rating that they are likely to give rise to switching transients that are in excess of the 2 kV test voltage. These cables have a cross-sectional area of 0.5 mm 2 and it is recommended that the maximum current in any conductor be limited to I A, and that no more than 40% of the pairs be loaded with this current at one time.
(b)Multicore control cables (as described in Section 3.5 of this chapter) which are rated at 600/1000 V and have a conductor cross-sectional area of 2.5
mm 2 . These cables are used where the circuit voltage (continuous or transient) or circuit current is in excess of the capabilities of multipair cables. However, these cables are more expensive and also more prone to interference (see Section 5.3 of this chapter) and should not be used unless essential.
(c)Special cables such as coaxial, triaxial and low loss individually screened pair cables are necessary for particular applications. The performance of such special cables is normally prescribed by the plant contractor involved and they are frequently provided by him as free issue for the cable contractor to install. One problem with many of these special cables is that they are normally not armoured and are therefore unable to withstand the rigours of installation and service in a power station environment; so, in many cases, it is necessary to provide mechanical protection by conduit or trunking.
5.3 Cable interference
This section is intended to give an insight into basic interference theory which will be found useful in understanding why it is important to give careful consideration to signal types and the type of cable to which they are allocated. Table 6.21 contains the abbreviations, descriptions and units that will be used throughout the following interference theory.
476

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TABLE 6.21
Descriptions and abbreviations used in interference theory
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Description |
Unit |
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Nlagnetic flux density |
Webers per square (Wb/m 2 ) |
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metre |
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Permeability of free |
Henries per metre (H/m) |
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space 4T |
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Cur , ent through |
Amperes |
(A) |
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conductor |
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Electric field strength |
Voits per metre |
(V/m) |
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Charge per unit length |
Coulombs per |
(C/m) |
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metre |
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Permittivity of free |
Farads per metre (F/m) |
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space |
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Frequency |
Hertz |
( Hz) |
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V |
Voltage |
Volts |
(V) |
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CfpNOLIC TOR 15
CARRYING AMP
ATO PLANE OF PAGE;
FiG. 6.39 Magnetic field around an isolated single conductor
5.3.1 Interference in multipair cables
Bay current carrying conductor produces a magnetic field and an electric field. If we consider the hypo- thetical case of an isolated single conductor, see Fig 6.39, it will be surrounded by a magnetic field inch- ated by the dotted lines and an electric field indicated by the solid lines. The spacing of the lines gives an indication of the relative strength of the field, where
they are close it is high |
and where they are far |
apart |
it is low. |
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and |
It can be shown that the magnetic flux density |
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electric field intensity at |
any point are inversely propor- |
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tional to the distance away from the conductor: |
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(a)Magnetic flux density at a point P, r metres from the centre of the conductor is
B = |
Webers/m 2 |
2-rr
(b) Electric field intensity
E — |
V/m |
e2rr
These two expressions show how B and E decrease as r increases.
If we now consider a balanced pair of conductors, i.e., carrying
Fic. 6.40 Magnetic field for a balanced pair of conductors
477

Cabling |
Chapter 6 |
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in the same way expressions can be stated which give the magnetic flux density and electric field strength.
It can be shown that the magnetic flux density and the electric field strength at any point P vary as the inverse of the square of the distance between P and the cable system centre. In fact the field strengths at P1 and Pi will not be identical when ri and r2 are equal because of the geometry of the arrangement, but providing that r is considerably larger than d (conductor diameter), then this approximation may be made. In our calculations we will be able to assume, generally, that r is greater than d and so the simplification will be invoked:
(a)Magnetic flux density at a point P, r metres from the centre of the twin system.
=Ald
71.r 2 |
(6.3) |
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(b) Electric field intensity at point P |
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qd |
(6.4) |
E |
Note the two implications of these formulae; firstly the flux density and field intensity vary inversely with the square of the distance from the system (and not directly as the inverse of the distance as in the isolated conductor case), and secondly that the smaller d is made the smaller the flux density/field intensity at a given point becomes.
Before we turn from looking at the magnetic/electric field produced by current carrying conductors to the interference induced in other conductors by those fields, there is one further point to consider.
The last example considered long, straight, parallel conductors. If we twist those conductors to form a twisted-pair then there is a cancellation of the magnetic/electric fields which is most easily explained by the diagram shown in Fig 6.41.
Field at P due to A is cancelled by that due to B C is cancelled by that due to D E is cancelled by that due to F,
etc.
Assuming the twisted cable to be made up of very short, straight lengths joined by transpositions it can be shown that (for short enough parallel lengths) the magnetic and electric fields, at a point P outside the cable will each be cancelled.
Since we are dealing with a twisted pair, there ar e many small geometrical considerations which will affect the amount of cancellation and thus there residual fields. These considerations include conductor geometry, twinning lay and spacing variation. usual to apply a reduction factor of about 10 for the case of a normal twisted-pair cable compared with a straight parallel-pair.
We shall now consider the way in which the magnetic field produced by (a) a single conductor and (b) a pair of conductors, affects another pair of conductors in their vicinity. In both cases straight parallel conductors are considered initially, the reduction factor above being applied at the end of the calculation.
In this situation we are primarily concerned with the magnetic coupling between the two circuits since we are working at normal power frequencies. Electrostatic coupling becomes more important as frequency rises (l0 4 kHz and above), but at mains frequency magnetic coupling dominates.
Referring to Fig 6.42, the induced voltage on a pair is a function of the magnetic field cutting them which in turn depends on the separation of the pair, their mutual separation from the current carrying conductor and other geometric considerations. Mathematically the amount of flux linking the cables may be found in several ways. To do this exactly is a relatively complicated procedure, but an approximation may be made by finding the average flux at the centre of the pair and assuming this to be constant over the area between them (safe assumption if d is small). To find the total flux cutting the pair per metre, we must then multiply this average by (2d x 1) square metres which is the area enclosed by a 1 metre length of the pair.
The voltage induced on the pair is then proportional to this flux and its rate of change, i.e., frequency. The induced voltage per metre is given by:
V = 27rf x |
x (2c1 x 1) |
(6.5) |
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27rR |
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rate of change |
x mean flux x area |
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which simplifies to
V— 2Adfl
(6.6)
The basic implications of this are that as we make d smaller and/or R larger the induced voltage drops.
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• P |
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/ 4 |
IN• |
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Flu. 6.41 Effect of twisted pair |
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Ftc. 6.42 Paired cable relative to single power cable |
478

Control and instrumentation cable systems
he pair cable is a twisted pair then a reduction I f t or of about 10 may be applied to this induced
fact
wItage as mentioned previously.
Following through a similar logic for a pair cable
in,lucing voltage on another pair cable of the |
same |
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,..wometry |
(as in Fig 6.43), we find a result which may |
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[sc stated |
m |
athematically as: |
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4p.d 2 fI |
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(6.7) |
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V = |
2 ) |
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(R 2 - d |
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Using: |
V- |
2Adfl |
V/m |
where d = 7 x 10 m R = 6 x 10 -1 m
f = 50 Hz
I = 840 A
2 x 4r X 10 -7 X 7 x 10 -4 X 50 X 840
Thus V -
6x 10'
FIG. 6.43 One pair relative to another pair
this means is that the induced voltage now drops off much more quickly as d is reduced and also as R is increased. Note that in both Equations
(6.6) and (6.7) a frequency term appears on the top li ne indicating that induced voltage is directly propor-
tional to frequency. This is why transient phenomena (basically high frequency harmonics) may give rise to
interference.
If both the pair cables are twisted-pairs then a reduction factor of (10 x 10) may be applied.
The type of interference that we have calculated here is manifested as a potential difference between the cores, i.e., a voltage source connected in series ith the cable. Thus this type of interference is known mode voltage (or transverse mode voltage). It from the previous equations that both suffer a rise in potential above the local earth
potential, again dependent upon the strength of the interfering field in which the cores are situated and this is known as common mode voltage (or longitudinal oltage).
In general, the equipment at the end of the cable be examining the potential difference/current/ between the two cores and thus will sensitive to series mode interference. Common interference does not pose such a problem unless
of very large magnitude, when special isolation methods must be employed. In this examination we are concerned mainly with series mode voltages.
Two examples of interference calculations for paired
,
:ables will now be given:
(a)A twisted pair suffering interference from a single Power cable carrying 840 A, situated 600 mm away
(effects of armour, other cables and supporting steel work are ignored).
= 1.23 x 10 -4 V/m
Allowing a reduction factor of 10 since the pair is twisted,
Induced voltage = 12.3 AV/M
Note: d is calculated on the basis of a 1/0.8 mm diameter conductor with an insulation radial thickness of 0.3 mm
(b)A twisted pair suffering interference from (i) a single core, 25 mm away in the same cable and (ii), a twisted pair carrying balanced current also 25 mm away. In both cases the interfering conductor(s) is (are) carrying 1 A.
(i) |
Using: |
V |
2fidf1 |
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where d = 7 x 10 -4 m |
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R = 2.5 x 10 -2 m |
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f = 50 Hz |
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I = |
I A |
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Thus V - |
2 x 4ir x 10 -7 x 7 x 10 -4 x 50 x 1 |
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V = 3.5 x 10 -6 V/m |
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Allowing a reduction factor of 10 since one |
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pair is twisted |
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V = 0.35 AV/In |
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(ii) |
Using |
V - |
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R 2 - d |
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4 X 47 x 10 -7 X (7 x 10 -4 ) 2 x 50 x 1
V=
(2.5 x 10 -2 ) 2 - (7 X 10 -4 ) 2
V = 1.9 x 10 -7 V/m
Allowing a reduction factor of 100 since both pairs are twisted:
V = 0.0019 AV /m
479
41111111.1111mr..—___

Cabling |
Chapter 6 |
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(ii) represents an improvement of about 45 dB over (i), illustrating the importance of maintaining balanced pair working.
5.3.2 Interference in multicore cables
The basic theory given in the previous section for multipair cables is equally relevant to rnulticore cables with the obvious exception that no factors have to be taken into account for twisting.
Two examples of interference calculation will now be given:
(a)Two adjacent cores suffering interferences from a single power cable carrying 840 A, situated 600 mm away (effects of armour, other cables and cable supporting steelwork are ignored).
Using: V= |
20dfl |
V/m |
where d = 1.7 x 10 -3 m r = 6 x 10 -1 m
f = 50 Hz
I = 840 A
2 x 41- x 10 -7 x 1.7 x 10 -3 x 50 x 840
Thus V
6 x 10 -1
V = 2.99 X 10 -4
Induced voltage = 299 ILV/M
Note: d is calculated on the basis of 7/0.67 mm stranded conductor with an insulation radial thickness of 0.7 mm.
(b)Two widely spread cores within a 37-core cable suffering interference from a single power cable situated 600 mm away (effects of armour, other cables and cable supporting steelwork are ignored).
Using: |
V — |
24fI |
V/m |
where d = 10.2 x 10 - 3 m R = 6 x 10 -1 m
f = 50 Hz
1 = 840A
Induced voltage = 1795 AV/M
Note: d is calculated for diametrically opposite cores in the outer layer of a 37-core cable, with conductor and insulation parameters as in the previous example.
5.3.3Circuit considerations
From the previous sections it can be seen that multi- core cables can be up to 150 times more susceptible
to interference than multipair cables under the con. ditions considered. The actual level of interference within multicore cables is dependent on the phys ical location of the cores which are used to complete the
electrical circuit. If the cores used are widely spaced within the cable, then the level of interference will be
greater than if adjacent cores were used. In general, little control is used over the selection of cores used
and, in practice, cores forming an electrical circuit may even be in different cables in which case the levels of interference can be significantly greater.
From Section 5.3.1 of this chapter, it can he seen that in order to reduce interference between circuits (cross-talk) and from external sources to a minimum, it is essential that balanced pair working is used. This means that the current in one core of a pair must be equal and opposite in direction of flow to that in the other core of the same pair. This is a mandatory re. quirement for analogue signals and should be adopted whenever possible for digital signals.
Also from Section 5.3.1 it can be seen that inter. ference within a control cable is inversely pro portional
to its distance from the source. Control cables |
are |
therefore separated from single-core power cables by |
at |
least 600 mm and from multicore power cables by at least 300 mm. Interference is directly proportional to the distance over which the control cable and power cables are parallel. It is therefore possible to waive these separation requirements over short distances and the requirement is not applied to cable ends where they are terminated into equipment. A general rule used is that power and control cables can be run at less than the foregoing stated separation distances provided that the summated total length does not exceed five metres.
Analogue and digital signals are normally segregated into separate cables, but separation is not required between such cables.
A further consideration when designing control cable systems should be the effects of cable capacitance. One particular aspect that needs attention is to ensure that the capacitance due to cable length or type is not such that the leakage current is sufficient to cause 'sealing in' of relay coils. Further information on the effects of capacitance is given in Volume F.
5.4 Control and instrumentation cable system design
This section deals with the design of cable systems to handle circuits used for control, protection, instrumentation and communications within a power station. This design work is now generally carried out by the CEGB who also issue the detailed working instructions and drawings to the cable installer.
The work involved on a major project such as Heysham 2 covers 36 000 control cables and well over 1 million wire terminations. Each 'cable' and each 'wire' has to be uniquely designed and identified to ensure
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Control and instrumentation cable systems |
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that the plant functions correctly. Because of the vast |
of sequence controllers and similar devices. The ex- |
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quantity of information involved, computer systems |
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a 50 V system of relays and switches. It was realised |
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1 system cable networks it is useful to consider first |
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and that the introduction of 'telephone type' cables |
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tunately, the importance of balanced paired working |
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In phase one, prior to about 1950, auxiliary control |
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Canctions within power stations were largely restricted |
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the remote control of switchgear using voltages in |
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the order of 110 V and currents that could be as high |
space requirements, the traditional 0 BA terminals |
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as 5 A. For these functions, multicore cables were used |
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shich had an imperial sized conductor equivalent to |
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the modern metric 2.5 mm 2 . All connections would be |
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'point to point', i.e., direct between equipment without |
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arshalling of cores. A typical arrangement is shown |
in quantity and complexity of control and instrumen- |
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tation equipment in the 1960s with the introduction |
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of 500 MW units, which put a heavy demand on cable |
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systems. To achieve economy of cable cost consistent |
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with the required reliability, operation and maintenance |
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CENTRAL CCNTROL PANEL |
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requirements a higher degree of marshalling was intro- |
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cabling, all terminal points have to be individually |
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designed and scheduled prior to site installation. Clear- |
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be completed until the necessary circuit and terminal |
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information has been received from the various plant |
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contractors. Because manufacturers programme plant |
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SWiTCHGEAR |
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contracts in relation to the equipment manufacture |
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and delivery dates, the design information tended to |
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be made available later than the cable system design |
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task required. Consequently the cable design activity |
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could not match the site cable installation demand |
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for information. The resulting concentration of cable |
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LOCAL CONTROL |
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design and installation activity towards the end of the |
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PANEL |
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project was a threat to the construction programme. |
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1 1 |
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MOTOR CIRCUITS |
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Although supporting steelwork could be erected and |
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PRESSURE |
PRESSURE TEMPERATURE |
power cables installed, control and instrumentation |
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cabling invariably was delayed due either to late in- |
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SWITCH |
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SWITCH |
SENSOR |
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;,..11•Cri |
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formation from contractors (and hence from the cable |
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designers) or due to lack of terminal release points |
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FIG. 6.44 'Point to point' control cable system |
from the equipment contractors. A further difficulty |
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with this type of marshalling system is that all wires |
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had to be identified by a unique number at their |
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During the second phase, in the 1950s, the increasing |
terminal points to allow identification and for fault |
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number of plant auxiliaries and level of instrumen- |
finding during commissioning and maintenance. This |
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!ation made it desirable to reduce the size of |
control |
identification usually consisted of a nine-digit alpha- |
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panels for switchgear. The same period also saw the |
numeric code formed using beads (ferrules) placed over |
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Introduction of mimic diagrams for control panels and |
the wire insulation. The termination was then com- |
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desks. The equipment developed by the GPO for tele- |
pleted by applying a crimped pin (see Section 9.3.1 |
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communications was an obvious choice to reduce size |
of this chapter) to the conductor which would in turn |
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and facilitate an increase in the complexity of |
power |
be fastened into a screw clamp terminal. The larger |
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station control functions. The use of 50 V DC inter- |
sizes of paired cables (50, 75 and 100 pairs) used for |
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Posing relays, and key and discrepancy switches there- |
trunk cables during this phase had a more complex |
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tore became common in power stations. The intro- |
colour coding than those currently used since all pairs |
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duction of such equipment allowed the development |
were identified without repetition. The net result of |
481

1•"'
Cabling |
Chapt er 6 |
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CONTROL BLOCK |
TRUNK CONTROL |
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PLANT |
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MAIN |
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CABLES |
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MARSHALLING |
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FIRST |
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iTEMS |
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MARSHALLING |
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BOXES |
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BOXES |
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MAY BE DISPENSED |
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WITH IF PLANT ITEM IS |
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NOT TO BE CONNECTED |
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TO MORE THAN ONE |
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TFILJNK CABLE: |
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FIG. 6.45 Typical arrangement of cable marshalling
these factors was that approximately 2 07o of wires were wrongly identified or terminated.
The fourth and final phase of the evolution of the cable network system began with the introduction of 660 MW units in the early 1970s, which had associated with them more sophisticated control and data logging systems. There was clearly a need to review and if possible simplify the design and installation of control cables and terminations. It was also considered desirable to try and spread the load factor on the design and site labour forces. Such considerations brought about the adoption of cable networks which utilised jumpering facilities to complete the circuitry. This type of network has been used at stations such as Littlebrook D, Dinorwig and Heysham 2; a description of the principles and equipment used is given in the next section.
5.5 Cable network system using jumpering
5.5.1 Basic principles of cable network
The cable network is a hierarchical system formed to route circuits from the 'field' (plant areas, switchrooms, etc.) to the control room area. A simplified arrangement to demonstrate the basic principles is shown in Fig 6.46. As can be seen, the network is built up using 20-pair modules to match the type of multipair cables used. These multipair cables, which are fully described
in Section 3.6 of this chapter, are constructed on a unit basis. This means that each cable consists of a number of 20-pair units, the pairs of each unit having the same colour code identification sequence, the units themselves being identified by numbers.
The network is built up in 20-pair modules from field marshalling boxes or local panels around the plant, via network marshalling boxes and trunk cables into a marshalling centre.
Similarly, central equipment such as control desks or alarm equipment is connected in 20-pair modules via trunk cables into the marshalling centre. Therefore each 20-pair module will start in a field marshalling box or in an item of control and instrumentation equipment. All pairs of the field end of the module will be made-off onto terminals and the whole module will be extended back to the marshalling centre.
Each 20-pair module is given a unique number that will appear above every block of 40 terminals that are used to terminate the module. Each wire in every module is terminated in the same terminal position in a block as shown in Fig 6.47. This means that a signal onto terminal 1A of, say, a field network box will end up on terminal 1A of the same module in the marshalling centre. Since each module is uniquely identified by a number and each pair within a module is uniquely identified by colour code, a system of attaching ferrule numbers to core terminations is not considered necessary. Since . the terminations within 20-pair modules should never need to be disturbed for correction or
482