اولين سايت تخصصي آموزش و نگهداري و تعميرات ديگ بخار، ديگ آبگرم، ديگ روغن داغ و آموزش نگهداري و طراحي تاسيسات در ايران به صورت کاملا فارسي، و با استناد به آخرين دستاوردهي تکنولوژي ديگ هاي بخار و تاسيسات مربوطه، در جهان.

 

 

 


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HEAT TRANSFER IN THE RADIANT SECTION OF PETROLEUM HEATERS (part1): 1 - 2 - 3 - 4

 
 

EMPIRICAL FURNACE EQUATIONS

The following empirical equations have been classified into two major groups according to whether they are similar to the Hudson or the DeBaufre type equation. Hudson3 correlated the data on several types of steam-boiler furnaces by the simple equation:
(1)

m = fraction of total heat input to the furnace (above the steam temperature) which is absorbed by the ultimate heat receiver.
G = air-fuel ratio, lbs. air / lb. fuel fired
C = pounds of fuel per hour per sq. ft. of water-cooled surface.

(2)

m = fraction of heat transferred above atmospheric temperature
G = air-fuel ratio, lbs. air / lb. fuel fired
Co = pounds of equivalent good bituminous coal per hour per sq. ft. of water-cooled surface.

Wilson, Lobo and Hottel 2 modified the Orrok equation and correlated the performance on ten of twelve furnaces. Their recommended equation is:

(3)

m = fraction of total heat input above 60°F. absorbed by the cold surface
a Acp = effectiveness of tube surface as compared to a continuous cold plane, sq. ft.
Q = net heat liberated from combustion of the fuel, B.t.u. per hour
G = air-fuel ratio, lbs. air per lb. fuel fired.

Hottel 5 has proposed the following type of equation:

(4)

H = total net heat input from all sources, B.t.u. per hour
N = the hourly mean heat capacity of the flue gas between the temperature of the gas leaving the chamber and a base temperature of 60° F. B.t.u./hour/°F.
f = an overall exchange factor defined by the equation:

(5)

where
q = heat transferred by radiation, B.t.u./hour
Tg = temperature of the gas or hot surface, °F. + 460
Ts = temperature of cold surface, °F. + 460.

The overall exchange factor makes allowance for variation in effective flame emissivity, arrangement of refractory and non-black conditions in the furnace chamber. The constants in the above equation are very tentative so that it is only to be considered as illustrating a method. The f concept has been satisfactorily used in the equation presented in this paper and has been defined and discussed under the derivation of the theoretical equation.

DeBaufre 6 proposed an empirical equation which is similar to the basic Stefan-Boltzmann equation:

(6)

q = heat transferred, B.t.u./hour
Ao = total tube surface exposed to radiation, sq. ft.
Tg = temperature of the products of combustion leaving the furnace chamber, °F. + 460
Ts = temperature of cold surface, °F. + 460
E = effectiveness factor of the cold surface.

DeBaufre attempted to correlate E as a function of the rate of heat liberation per unit of furnace volume but the correlation was poor. For black body conditions E would have a maximum value of 0.173, the Stefan-Boltzmann constant.

Mekler7 proposes the equation:

(7)

q = heat transferred by radiation, B.t.u./hour
Se = equivalent "effective" heating surface, sq. ft.
C = an empirical coefficient depending on the temperature used for Tg
Tg = exit gas or theoretical flame temperature, °F. + 460
Ts = temperature of cold surface, °F. + 460.

In contrast to DeBaufre, however, he evaluates Se as a function of the "fraction cold" of the furnace. An approximate graphical method is used for solving the DeBaufre type of equation. No cognizance is taken of the effect of PL on the heat transferred, and furnaces having the same geometric shape but widely different volumes are presumed to have the same fractional heat absorbtion. The effect of excess air on flame emissivity is likewise neglected. <-- page 1 -- page 3-->

 


 

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