Environmental Engineering Reference
In-Depth Information
Since the integral is undefined at
0 and 1, we take the limits as 0.01 (leading
edge) and 0.99 (trailing edge) so that [A] approaches 1% of the limiting value at both
limits. We then have the following definite integral:
η =
ln 1
.
1
1
( 0.01 ) n 1
1 ( 0.99 ) n 1
S t
=
4.505
+
(6.156)
n
If we assume that the mass in the adsorption zone is much smaller than the mass in
the saturated zone, the breakthrough time can be obtained:
H B − δ
V ads
t B =
,
where H B is the total height of the adsorbent bed.
E XAMPLE 6.18 B REAKTHROUGH T IME FOR AN A CTIVATED C ARBON A DSORBER
Obtain the breakthrough time for a pollutant in a carbon bed at an air mass velocity of
2.0 kg/s at 1.1 bar and 30 C with an influent pollutant concentration of 0.008 kg/m 3 .
The Freundlich isotherm parameters for the pollutant are K F = 500 kg/m 3 and n = 2.
The mass transfer coefficient is 50 s 1 . The bed length is 2 m with a cross-sectional
area of 6 m 2 and a bulk density of 500 kg/m 3 .
Gasdensity, ρ g = P/RT = ( 1.1 )( 29 )/( 303 )( 0.083 ) = 1.3 kg/m 3 . V ads = 2.0 ( 500 ) 0.5
(0.008) 0.5 /( 1.3 )( 500 )( 6 ) = 1.0 × 10 3 m/s. Hence
4.595 +
1.0 ln 1 ( 0.01 ) 1.0
2.0
( 50 )( 6 )( 1.3 )
1
δ =
= 0.047 m.
1 ( 0.99 ) 1.0
Breakthrough time, t B = ( 2.0 0.047 )/ 1.0 × 10 3
= 1953 s = 0.54 h.
6.3.2.2
Thermal Destruction
Organic compounds that form a large fraction of air pollutants in industrial effluents
can be oxidized in incinerators at high temperatures. These devices are also called
thermal oxidizers or afterburners . Both direct thermal oxidation and catalytic oxida-
tion are practiced in the industry.A schematic of a direct thermal oxidizer for gases is
shown in Figure 6.35. Thermal incineration is also used in destroying organic com-
pounds in a liquid stream or sludge.A rotary kiln incinerator is used for the latter and
a schematic is shown in Figure 6.36.
Cooper and Alley (1994) present the theory and design of a typical incinerator.
Combustion is the chemical process of rapid reaction of oxygen with chemical com-
pounds resulting in heat (Chapter 2). Most fuels are made of C and H, but may also
include other elements (S, P, N, and Cl).Although the exact mechanism of combustion
 
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