The thermal conductivity of assembled armature laminations i
Solution
Thermal Conductivity = Q/t in joules/sec or watts = kA (T2 - T1)/d
where, k = thermal conductivity of material; A = Surface are; (T2 - T1) = Temperature Difference, d = thickness of the material.
Given that difference of 5 deg. Celcius (T2 - T1) cause 25 W (Q/t) to be conducted through a cross section of 2500 mm2 in Area (A) and 20 mm thick (d) measured along the lamination.
So, Thermal Conductivity measured along the lamination = 25 W = k (2500)*(5) / 20
Therefore, k = (25 * 20)/ (2500 * 5) = 0.04
Thermal Conductivity along the laminations for stack 40 mm thick (d) and 6000 mm2 in cross section area (A) with a difference of 20 deg. Celcius (T2 - T1)
Q/t = (0.04 * 6000 * 20)/ (40) = 120 W
Now, given that thermal conductivity along the laminations is 20 times as great than across the laminations.
So, Thermal Conductivity across the laminations = Thermal Condutivity along the laminations / 20
= 120/20 = 6 Watts.
