Combustion Data and Basic Calculations
For more detail and expanded information on multiple fuels, see North American Combustion Handbook, Vol. 1, B&W Steam book, and Perry’s Chemical Engineers’ Handbook.

 

RULES OF THUMB FOR COMBUSTION AIR ESTIMATION

For air volume:
Btu/hr input/6,000 = combustion air flow, scfm

For air mass:
765 lb/air required to burn 1 MM Btu of fuel

Example:
A 10 MM Btu/hr burner running at 0% excess air requires:
10,000,000/6,000 = 1,670 scfm air or 10 x 765 = 7,650 lb/hr air



CALCULATE ADIABATIC FLAME TEMPERATURE (AFT)

Q = M x Cp x temperature difference

Temperature difference  = Q/(M x Cp)

Example:  1 mole CH4, 16 lb X LHV 21,500 Btu/lb = 344,000 Btu

At 100% excess air,  M = 568 lb for air plus fuel

Temp diff = 344,000/(568 lb x 0.282) = 2,150 F

With 60 F base temperature at standard conditions:

Adiabatic Flame Temp = 60 + temp diff = 2,210 F

Caution:  Cp varies with gas temp and gas; Use integrated heat capacities of gases in place of specific heat via equations or tables

 

SELECTED COMBUSTION CONSTANTS

COMPONENT
Mol
Weight
HHV Btu
per lb fuel
lb air reg'd
per lb fuel
Methane
16
23,896
17.3
Ethane
30
22,282
16.2
Propane
44
21,523
15.7
Hydrogen
2
60,991
34.3
Carbon Monoxide
28
4,323
2.42
Carbon Dioxide
44
--
--
Oxygen
32
--
--
Nitrogen
28
--
--


 

HEAT EXCHANGER EFFECTIVENESS

E = Ch * (Th in - Th out)/Cmin * (Th in - Tc in)

Where Cmin is the smaller of mhcph or mccpc, the hourly heat capacity

The rate of heat exchange is

Q = E Cmin * (Th in - Tc in)

Reference: F. Kreith, 3rd ed. Principles of Heat Transfer, Intext Education Publisher, NY, 1973

 

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