In: Other
Solution:
Basis: 100 kgmol stack gas SG.
S balance,
(0.076) * (F) * 32 = 0.004(100)
F = 168.42 kg
NF = (0.028) * (168.42) = 4.7158/14 = 0.33684 kgmol
N2 supplied= 81.7 - 0.33684 * (1/2) = 81.53 kmol
O2 supplied = 81.53 * (21/79) = 21.67 kmol
Assume excess be x
O2 x’s = O2theo - CO / 2 − H2 / 2
O2 x’s = 6.8 - 1.19 / 2 − 0.47 / 2 = 5.97 kmoles
% x’s air
% x’s air= 5.97 / (21.67−5.97) x100 = 38.03 %
C balance,
(% C) * (168.42) / 12 = 9.44
+1.19
%C = 0.7574* x *100 = 75.74%
%H + %O = 1 -
(0.7574+0.076+0.028)
%H + %O = 0.1386
Assume, x = %O
%H = 0.1386 - x
Let y= O2 in H2O
Actual combustion
C + O2 = CO2
9.44 9.44 = 9.44
C + 1/2O2 = CO
1.19 0.595 1.19
H2 + 1/2O2 = H2O
2y y 2y
H balance:
(168.42) * (0.1386 - x) = 0.47 * (2) + 4y equation 1
O balance:
((?) * (168.42) / 13) + 21.67 * (2) = 9.44 * (2) + 1.19 + 0.4 * (2) + 6.8 * (2) + 2 * y equation 2
Solving for x using equation 1 and 2 we get
X = 0.0245 * x * 100 = 2.46%
%H = 0.1386 - 0.0246 = 0.114 * x * 100 = 11.4 %H
Fuel analysis
7.6 %S
2.8 %N
75.74 %C
11.4 %H
2.46 %O
m3air/kg fuel is calculated as
Ps= ?73.649−7258.2296– 7.3037??296
+4.653?10−6(296)2 X 760101325
Ps =20.90mmHg
nH2Oair =(20.90)(0.85)(103.2) / 755−(20.90∗0.85) = 2.487 m3
nair =103.2 + 2.487 = 105.687m3
V = (105.687) * (0.08766)* (296) / (755 / 760) = 2584.11 m3
?3air / kg fuel = 2584.111 / 68.42 = 15.34 m3