Case 1
Given,
d1=10mm=0.01m (Diameter of inner pipe)
t1=80K=-193℃ (Temperature of inner pipe)
d2=15mm=0.015m (Diameter of outer pipe)
t2=280K=7℃ (Temperature of outer pipe)
ε1=0.2 (Emissivity of inner pipe surface)
ε2=0.3 (Emissivity of outer pipe surface)
l=5m (Length of both pipes)
Find: Q1-2 (Heat flow rate)
Solution:
Heat Transfer from pipe 1 to pipe 2
Q1-2=Eb1-Eb2Rt
=σ(t14-t24)1-ε1A1ε1+1A1F1-2+1-ε2A2ε2
=A1σ(t14-t24)1-ε1ε1+1F1-2+A1A2(1-ε2ε2) …(1)
As space between 2 pipes is evacuated, so resistance due to space is zero.
∴From (1)
Q1-2=π×0.01×5×5.67×10-8(804-2804)1-0.20.2+0+π×0.01×5π×0.015×5(1-0.30.3)
Q1-2=-9.7882W
Case 2
Given,
d3=12mm=0.012m (Diameter of shield pipe)
ε3=0.2 (Emissivity of shield pipe)
Find: (1) % Reduction in Q
(2) t3 (Temperature of shield pipe)
Solution:
Heat transfer from pipe 1 to pipe 3
Q1-3=σ(t14-t34)(1-ε1A1ε1+1A1F1-3+1-ε3A3ε3)
=A1σ(t14-t34)1-ε1ε1+1F1-3+A1A3(1-ε3ε3) …(2)
As space between the pipes is evacuated, so resistance due to space is zero
∴From (2)
Q1-3=π×0.01×5×5.67×10-8(804-t34)1-0.20.2+0+π×0.01×5π×0.012×5(1-0.050.05)
Q1-3=4.4906×10-10(804-t34) …(3)
Heat transfer from pipe 3 to pipe 2
Q3-2=σ(t34-t24)(1-ε3A3ε3+1A3F3-2+1-ε2A2ε2)
=A3σ(t34-t24)1-ε3ε3+1F3-2+A3A2(1-ε2ε2) …(4)
As space between the pipes is evacuated, so resistance due to space is zero
∴From (4)
Q3-2=π×0.012×5×5.67×10-8(t34-2804)1-0.050.05+0+π×0.012×5π×0.015×5(1-0.20.2)
Q3-2=4.8142×10-10(t34-2804) …(5)
As rate of heat transfer remains same, Equating (3) and (5)
4.4906×10-10(804-t34)=4.8142×10-10(t34-2804)
t3=237.8685K=-35.1614℃
Heat transfer when shield is placed between the two pipes
Q1-2=Q1-3=4.4906×10-10(804-237.86854)
Q1-2=-1.4192W
% Reduction in heat transfer
%↓Q=-9.7882-(-1.4192)-9.7882 ×100
%↓Q=85.5 %