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HEAT TRANSFER IN THE RADIANT SECTION
OF PETROLEUM HEATERS (part2):
1 -
2 -
3 -
4 |
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(a) |
At bridge wall. |
Average Deviation |
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6.85 % |
5.30 % |
(b) |
With high velocity thermocouples. |
Maximum Deviation |
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33 % |
16 % |
(c) |
Estimated from average oil temperature, inside
coefficient with allowance for coke deposit. |
% of Tests Between |
0 and 2 % Deviation.... |
17.7 % |
31.8 % |
(d) |
Net heat input from combustion of the fuel,
air preheat, and recirculation if any. |
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0 and 4 % Deviation.... |
36.5 % |
53.0 % |
(e) |
Based on flue gas duty, except for Furnaces
Nos. 1 and 8. |
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(f) |
Estimated from oil side. Applies only to
furnaces Nos. 1 and 8. |
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(g) |
Wilson, Lobo, and Hottel Empirical Radiant
Equation. |
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(h) |
Temperatures for Furnace No. 2 are average oil
temperatures. |
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(i) |
Based on exposed tube surface. |
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(j) |
Actual tube skin thermocouple
measurements. |
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(k) |
Fuel = Products of combustion from Furnace No.
10. |
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The actual heat to the oil is obtained by subtracting the enthalpy of the
flue gas leaving the radiant section from the enthalpy of the entering fuel and
air, and then subtracting the estimated external losses, plus the direct radiant
heat from the combustion chamber absorbed by the first rows of the convection
section. The latter item is obtained by a convection section heat balance , gas
side versus oil side, in which the heat lost by the gas is considered between
the actually measured true gas temperature of the gases entering and leaving the
section. A summary of the test data required and a short outline of the method
of calculation are included in the Appendix.
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Table III gives a summary of the test data and calculations for all
eighty-five tests which have been used as an independent check on the validity
of the derived theoretical equation. The ratio of the actual heat absorbed by
the oil in the radiant section to that predicted by both the empirical and
theoretical equations is given for each of the individual tests. The deviations
of any test from the average deviations for a given furnace can thus be readily
seen. <-- page 3 --
page 1 (part3)-->
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