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TRANSCRIPT
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Lecture 1: Basics of Combustion EngineeringCombustion Stoichiometry
1.1 Introduction
1.2 Definitions
1.3 Combustion stoichiometry for gaseous fuels
1.4 Combustion stoichiometry for liquid and solid fuels
1.5 Combustibles burnout for solid fuels
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Examples of industrial combustion systems
Boiler fired with pulverised coal
Pulverised coal flame
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Examples of industrial combustion systems
Modern reheating furnace
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Examples of industrial combustion systems
Flameless oxidation
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1.2 Definitions
Chemical Reactions, Atoms and Molecules in Combustion
H
1
2 O H O2 2 2+
The atoms are conserved (neither created nor destroyed)
Molecules are not conserved
Water is the productHydrogen and oxygen are
reactants
Atoms relevant in combustion are: C,H,O,N,S,Cl
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1.1 Definitions
Compounds of carbon and hydrogen are called hydrocarbons.
HYDROCARBONS
Aliphatic
Alkanes CnH2n+2Alkenes CnH2nAlkynes C
n
H2n-2
Alicyclic
CH2
CH2 CH2
Aromatic
Benzene
Benzene derivatives
Naphtalene
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The first ten members of the unbranched-chain alkanes series are:
CH4 methane C6H14 hexane
C2H6 ethane C7H16 heptane
C3H8 propane C8H18 octaneC4H10 butane C9H20 nonane
C5H12 pentane C10H22 decane
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Table 1.1 Names of aliphatic hydrocarbons
CnH2n+1-CnH2n-2CnH2nCnH2n+2n
C5H11- PentylC5H8 PentyneC5H10 PenteneC5H12 Pentane5
C4H9-ButylC4H6 ButyneC4H8 ButeneC4H10 Butane4
C3H7-PropylC3H6 ButyneC3H10PropeneC3H8 Propane3
C2H5- EthylC2H2 EthyneC2H4 EtheneC2H6 Ethane2
CH3- MethylCH4 Methane1
Alkyl
group
AlkyneAlkeneAlkaneNo.of C
atoms
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Other molecules relevant in combustion are:
Haloalkanes R-X CH3Cl (chloromethane)
Alcohols R-OH C2H5OH (ethanol)
Amines R-NH2 CH3NH2 (methylamine)
Aldehyde R-COH CH3COH (ethanal)
Ketons R-CO-R CH3COCH3 (propanone)
Carboxylic Acid R-COOH CH3COOH (ethanoic acid)
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Amount of substances, mole and mass fractions
1 mole contains 6.023 x 1023 particles (atoms, molecules)
For a mixture of species:
n (total number of moles)=ni
xn
nii
= M x Mmean i i=
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Mole (volume) fractions and mass fractions:
w i = =num ber of kg of species " i"
total num ber of kg in the system
= =
n M
n M
x M
x M
i i
k kk
i i
k kk
xi = =number of moles of species "i" in 1kg of mixture
total number of moles in 1kg of mixture
= =
w M
M
w M
w M
i i
m e a n
i i
k kk
/
/
/
/1
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Equation of state for gases and gas mixtures
F p T c( , , ) = 0or
F p T( , , ) =
0The perfect gas equation:
p V n R T= or cp
R T=
= =
p M
R T
p
R Tw
M
m e a n
i
i
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The perfect gas law:
p V n R T=
Under constant pressure and temperature one mole (kmol)
of any ideal gas occupies the same volume.
At normal conditions:
p = 760 Tr (1 Tr=133,322 N/m2)
T = 273.15 K (0 C)
1 kmol of gas = 22.418 mn3
1 mol of gas = 22.418 dmn3
R = 8,314 J/kmol/K
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1.2 Combustion Stoichiometry for Gaseous Fuels
Stoichiometric Combustion
Combustion is said to be stoichiometric if fuel and oxidizer
consume each other completely forming only CO2
and H2O
CH 2O 2H O CO4 2 2 2
+ + stoichiometric
CH 3O 2H O CO O4 2 2 2 2+ + + lean
CH O H O 0.5CO 0.5CH4 2 2 2 4+ + + rich
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1.3 Combustion Stoichiometry for Gaseous Fuels
Mole fraction of fuel in a stoichiometric mixture
1 kmol fuel O products (CO H O)2 2+ + 2
xfuel stoich in oxygen, _ _ =+
=number of moles of fuel
total number of moles (fuel oxygen)
=+1
1
xfuel stoich in air, _ _ / . .=
+ =
+1
1 0 211
1 4 762
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For example:
CO 0.5O CO2 2+ xfuel,stoich_in_oxygen = 1/1.5=2/3
xfuel,stoich_in_air= 1/(1+0.5/0.21)=0.2958
C H 5O 3CO 4H O3 8 2 2 2+ +
Xfuel,stoich_in_oxygen = 1/(1+5)=1/6
xfuel,stoich_in_air= 1/(1+5/0.21)=0.0403
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Excess air ratio (air equivalence ratio)
= =( / )
( / )
( / )
( / )
x x
x x
w w
w w
air fuel
air fuel stoich
air fuel
air fuel stoich
Fuel equivalence ratio =1
Rich combustion > 1< 1
Stoichiometric combustion = 1
Lean combustion > 1