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Wire-Gauge Ampacity

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Contents

[edit] Wire Gauge - Ampacities

[edit] AWG

American Wire Gauge (AWG) Diameter where:

d = diameter in Inches
n = AWG gauge number
A = cross-sectional area in sq inches

d = \left( \frac{460}{100} \right)^{ \frac{  36 - n  }{39  } }
n = -10.7 + 10\log_{10}{\frac{1}{A}}
A = 10^{-\frac{n+10.7}{10} }

[edit] Load Carrying Capacities or Ampacities

In part from Reference Data for Engineers: Radio, Electronics, Computer and Communications 7th Ed At 20 C

  • De-rate with +0.00393 per °C - wire carrying current capacity sitting in the insulation and conduit will not be at 20 °C You will want to derate to at least the temperature rating of your insulation. Resistance listed here are not trade maxima - most wire that is soft or annealed will be slightly higher. Resistance of hard-drawn copper is slightly greater - 2 - 3%. Stranded wire may also be higher.


AWG Dia Inch Cir Mil Dia cm Area Inch2 lb/kft ohms
/kft
Ohms
/km
CU Max
free-air
Amps
CU Max
enclosed
Amps
32 0.008 63.2 0.020 4.964E-05 0.19 164.1 538.4 .53 0.32
30 0.010 100.5 0.025 7.894E-05 0.30 103.2 338.6 .86 0.52
28 0.013 159.8 0.032 1.255E-04 0.48 64.9 212.9 1.4 0.83
26 0.016 254.1 0.040 1.996E-04 0.77 40.81 133.9 2.2 1.3
24 0.020 404.0 0.051 3.173E-04 1.22 25.67 84.22 3.5 2.1
22 0.025 642.4 0.064 5.046E-04 1.94 16.14 52.95 7.0 5.0
20 0.032 1,021.5 0.081 8.023E-04 3.09 10.15 33.30 11.0 7.5
18 0.040 1,624.3 0.102 1.276E-03 4.92 6.385 20.95 16 10
16 0.051 2,582.7 0.129 2.028E-03 7.82 4.016 13.18 22 13
14 0.064 4,106.7 0.163 3.225E-03 12.43 2.525 8.284 32 17
12 0.081 6,529.9 0.205 5.129E-03 19.77 1.588 5.210 41 23
10 0.102 10,383.0 0.259 8.155E-03 31.43 1.215 3.985 55 33
8 0.128 16,509.7 0.326 1.297E-02 49.98 0.998 3.274 73 46
6 0.162 26,251.4 0.412 2.062E-02 79.46 0.395 1.296 101 60
4 0.204 41,741.3 0.519 3.278E-02 126.35 0.248 0.8136 135 80
2 0.258 66,371.3 0.654 5.213E-02 200.91 0.156 0.5118 181 100
1 0.289 83,692.7 0.735 6.573E-02 253.34 0.123 0.4035 211 125
0 0.325 105,534.5 0.825 8.289E-02 319.46 0.0983 0.3225 245 150
00 0.365 133,076.5 0.927 1.045E-01 402.83 0.0779 0.2556 283 175
000 0.410 167,806.4 1.040 1.318E-01 507.96 0.0618 0.2028 328 200
0000 0.460 211,600.0 1.168 1.662E-01 640.53 0.04901 0.1608 380 225


  • A second version of the above table with 60°C trade derating - (effects ohms/kft and ohms/km.)

Max ambient 60°C

AWG Dia Inch Cir Mil Dia cm Area Inch2 lb/kft ohms
/kft
Ohms
/km
CU Max
free-air
Amps
CU Max
enclosed
Amps
32 0.008 63.2 0.020 4.964E-05 0.19 199.587 654.613 .53 0.32
30 0.010 100.5 0.025 7.894E-05 0.30 125.521 411.690 .86 0.52
28 0.013 159.8 0.032 1.255E-04 0.48 78.941 258.915 1.4 0.83
26 0.016 254.1 0.040 1.996E-04 0.77 49.647 162.833 2.2 1.3
24 0.020 404.0 0.051 3.173E-04 1.22 31.223 102.407 3.5 2.1
22 0.025 642.4 0.064 5.046E-04 1.94 19.636 64.404 7.0 5.0
20 0.032 1,021.5 0.081 8.023E-04 3.09 12.349 40.504 11.0 7.5
18 0.040 1,624.3 0.102 1.276E-03 4.92 7.767 25.473 16 10
16 0.051 2,582.7 0.129 2.028E-03 7.82 4.884 16.020 22 13
14 0.064 4,106.7 0.163 3.225E-03 12.43 3.072 10.075 32 17
12 0.081 6,529.9 0.205 5.129E-03 19.77 1.932 6.336 41 23
10 0.102 10,383.0 0.259 8.155E-03 31.43 1.215 3.985 55 33
8 0.128 16,509.7 0.326 1.297E-02 49.98 0.764 2.506 73 46
6 0.162 26,251.4 0.412 2.062E-02 79.46 0.481 1.576 101 60
4 0.204 41,741.3 0.519 3.278E-02 126.35 0.302 0.991 135 80
2 0.258 66,371.3 0.654 5.213E-02 200.91 0.190 0.623 181 100
1 0.289 83,692.7 0.735 6.573E-02 253.34 0.151 0.494 211 125
0 0.325 105,534.5 0.825 8.289E-02 319.46 0.120 0.392 245 150
00 0.365 133,076.5 0.927 1.045E-01 402.83 0.095 0.311 283 175
000 0.410 167,806.4 1.040 1.318E-01 507.96 0.075 0.247 328 200
0000 0.460 211,600.0 1.168 1.662E-01 640.53 0.060 0.196 380 225

[edit] House Wiring

First, avoid the most common error in house wiring - hanging a 120Vac outlet off of a 3 conductor (L1,L2,N) 220Vac cable. It is dangerous! To do something like that you need a 4 conductor cable - (L1,L2,N,G) to provide a safety ground that is _NOT_ carrying any current.

The table below will not support any reduced ground cables and is for _Copper_wire_only_!. If you run aluminum wire you need to consult the manufactures data sheets and be sure to understand terminal block treatments! This table also in no way compensates for length of run! This table is not for wires packed in conduit - wires need to dissipate heat!

Normal House Wiring Gauge
Consult your building inspector
because your location
will have a specific building code!
Circuit
Maximum
Amperage
Minimum COPPER
wire gage
15A 14AWG
20A 12AWG
30A 10AWG
45A 8AWG
60A 6AWG
80A 4AWG
100A 2AWG
If you are running more than 100A
you probably will run Aluminum and
need a different table.

Do not use copper ratings
for aluminum!

[edit] PCB Trace Width vs Current

image:PCB_current.png

[edit] Fusing Point of Wire

H. W. Preece’s Investigation way back in 1884 provided a way to calculate the fusing current of a wire based on its diameter.

 I = kd^{\frac {3}{2}}

or

 d = \left ( \frac{I}{k} \right ) ^{\frac{2}{3}}

Where:

I is the current in Amps
d is the diameter in cm
k is the fusing constant
Materialk for d in cmMelting point°CResistivity (Ω-m) at 20 °CCoefficient*
Silver1900961.781.59×10-8.0038
Copper25301084.621.72×10-8.0039
Aluminum1870660.322.82×10-8.0039
Iron777.415381.0×10-7.005
Tin405.5231.931.09×10-7.0045
Platinum12771768.31.1×10-7.00392
Lead340.5327.462.2×10-7.0039
Tin/lead solder325.51831.44x10-7.0035

There should be a relationship between resistivity, melting temperature and k. Remember that the electrical resistivity ρ (Rho (letter)) of a material is given by:

{\rho={R \left. \frac{A}{\ell} \right.}}

where

ρ is the static resistivity (measured in ohm meters, Ω-m);
R is the electrical resistance of a uniform specimen of the material (measured in ohms, Ω);
\ell is the length of the piece of material (measured in meters, m);
A is the cross-sectional area of the specimen (measured in square meters, m²).


[edit] Watts generated in a Wire

First, an example using the formula in the above section to determine the wattage dissipated in a 1 meter length of 12 gage copper wire at 10A.


{\rho={R \left. \frac{A}{\ell} \right.}}

Rearrange to solve for R


R =  \frac{\rho\ell}{A}

Remembering that P = I2R

P =  \frac{I^2 \rho\ell}{A}

Substituting in where:

I = 10
ρ = 1.72x10 − 8Ω − m
 \ell = 1m
d = 0.205cm = .00205m
 r  =  .001025m \approx .001m
 A = \pi r^2 \approx  3.14 \mathrm{x} 10^{-6}m^2


P \approx  \frac{\left (10^2\right) 1.72\mathrm{x}10^{-8} \left ( 1 \right)}{3.14 \mathrm{x} 10^{-6}}  \approx 0.55W

[edit] Heat Rise in Wire in Still Air for the same wire

Now, to figure the temperature rise per watt.

 \dot{Q}_{12} = \epsilon A\left ( \sigma T_1^4 - \sigma T_2^4\right )

Where :

 \dot{Q}_{12} = Net radiant energy
ε = emissivity (sometimes called emittance) - the constance of likeness to a black body
ε = 1 a blackbody
ε = 0.35 a very shinny aluminum alloy
T = Absolute temperature in K
 \sigma = 5.67 \mathrm{x}10^{-8} \frac{W}{M^2 K^4} Stefan-Boltzmann constant

When T1 and T2 are not very different, it is convenient to linearize the equation by factoring the term \left( \sigma T_1^4 - \sigma T_2^4 \right ) to obtain:

 \dot{Q}_{12} = \epsilon A \sigma \left(  T_1^2 +  T_2^2 \right )\left(T_1 + T_2\right )\left(T_1 - T_2\right )
 \dot{Q}_{12} \approx \epsilon A \sigma \left( 4T_m^3\right)\left(  T_1 - T_2 \right )

When  T_1 \approx T_2 and Tm is the mean of T1 and T2

Written again as

 \dot{Q}_{12} \approx A h_r \left( T_1 - T_2 \right)

Where

 h_r = 4 \epsilon \sigma T^3_m or Radiation heat transfer coefficient with the units \frac{W}{m^2K}
 h_r = 4 \epsilon \left(5.67 \mathrm{x} 10^{-8}  \frac{W}{m^2K^4}\right)\left(298K\right)^3
 h_r \approx 6 \epsilon \frac{W}{m^2K}

Emissivity is always a fuzzy number that depends on details like surface finish and for copper can vary from 0.7 to .88 but for electrical work 0.4 works most of the time. Give it large error bands!

The surface area of our wire is

 A = \ell \pi d = \left(1m\right) .0205m \pi = .0644 m^2

Our power is 0.55 Watts and  \epsilon \approx 0.4

T_2 = 30^\circ C = 303K
 \dot{Q}_{12} = \epsilon A\left ( \sigma T_1^4 - \sigma T_2^4\right )


 0.55W = \left ( 0.4 \right ) \left ( 0.644m^2 \right ) \left [  \sigma T_1^4 - \left ( 5.67 \mathrm{x} 10^-8 \frac{W}{m^2 K^4} \right ) \left(303K\right)^4 \right ]
 \sigma T_1^4 = \left[ \frac {0.55}{ \left ( 0.4 \right ) \left ( 0.0644 \right )} + 478\right] \frac{W}{m^2}
 \sigma T_1^4 = \frac {0.55}{ \left ( 0.4 \right ) \left ( 0.0644 \right )} + 478  = 480.1\frac{W}{m^2}
 T_1 = \left [ \frac{480.1}{5.67 \mathrm{x}10^{-8}} \right]^{\frac{1}{4}} = 303.35K

or a rise of 0.35 C

We can solve for T1 generally:

 T_1 = \left( \frac{\frac{\dot{Q}_{12}}{\epsilon A} + \sigma T_2^4}{\sigma}\right)^{\frac{1}{4}}
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