by Maryam Hussain
A chemical reaction, named
“Combustion” has played major roles in human civilization. Since man
discovered how to create fire, we have relied on combustion to perform a
variety of tasks. The fire was used for heating and cooking, and later to
manufacture tools and weapons. It was not until the onset of the Industrial
Revolution in the nineteenth century that man started to obtain power from
combustion. Rapid progress in the application of combustion systems since then,
and many industries have come into existence as a direct result of this
achievement.
Combustion is one of the most
complex subjects that involve primarily such disciplines as physics, chemistry,
thermodynamics, and fluid mechanics. Thanks to the branch of engineering &
science, the thermodynamics, which enables us to calculate the energies of system
changes in composition. Combustion has a wide variety of uses. Combustion is
used for energy production in power plants, gas turbines, and engines.
Combustion is a process of
heat release in exothermic reactions, which is accompanied by mass and heat
transfer. Combustion involves a chemical transformation between a substance or
substances called fuels and other chemicals called oxidizers, both of these
being reactants.
In the process of combustion,
that is a type of chemical reactions, the nuclei of the reactants are not
altered but the bonds of the compounds are altered which involved the electrons
of the molecules and atoms. In the case of combustion, it leads to the
release of heat, while there are chemical reactions where heat is required to
form the bonds. The amount of heat, that releases in the process of chemical
bonding change, is the most interesting since this energy can be harvested and
usefully exploited. Combustion may involve all phases of matter; the phases
being solid, liquid, and gas; for example, liquid and gaseous combustion in SI
engines.
Most internal combustion engines,
spark ignition, and compression ignition obtain their energy from the combustion
of a hydrocarbon fuel with oxygen, that converts the chemical energy of the
fuel to internal energy in the gases within the engine.
The oxygen required for a
given combustion reaction comes from the air; on a volume basis, air
contains about 78% Nitrogen gas in the form of diatomic N2 molecule,
about 1 % of rare & noble gases such as helium, argon, 21 % Oxygen gas in
the form of a diatomic O2 molecule.
Combustion is the rapid reaction
of a burnable substance with oxygen. It is worth mentioning that oxidation
reactions of elements release significant quantities of energy as heat;
CARBON to carbon monoxide, carbon dioxide, CO and CO2
respectively,
HYDROGEN to water, H2O, and
NITROGEN to nitric oxide and nitrogen dioxide, NO and
NO2 respectively,
The most important of the
combustion reactions are those in which hydrocarbon fossil fuels, such as
coal, natural gas, etc. are burned to release energy that ultimately shows up
as electricity, commercial and domestic heating, and automobile motion. There
are thousands of different hydrocarbon fuel components, which consist of
hydrogen and carbon. Still there are few hydrocarbon fuels that also contain
oxygen, e.g. alcohols.
The major products of complete
combustion from practically all fuels are CO2 and water. A
combustion reaction in which CO is formed is referred to as partial combustion
or incomplete combustion, even though CO2 may also be produced.
Examples:
C3H8 + 3.5O2
⇀ 3CO
+ 4H2O Partial combustion of propane
C + O2
⇀ CO2 Complete combustion of carbon
C3H8 + 5O2
⇀ 3CO2
+ 4H2O Complete combustion of propane
The most important property of a
fuel is its heating value, which is numerically equal to its standard heat of
combustion. The heating value of a fuel is usually determined directly by
experimental measurements. The maximum amount of chemical energy that can be
released, in the form of heat energy from the fuel, is when fuel reacts
(combusts) with a stoichiometric amount of oxygen. The stoichiometric
amount of oxygen (also called theoretical oxygen) is just enough to convert all
carbon in the fuel to CO2 and all hydrogen of the fuel to H2O,
with no oxygen left over in the exhaust.
To simplify calculations without
causing any large error, the amounts of argon and other trace gases in the air
can be assumed to be a part of nitrogen gas, as all of these gases remain
neutral during the combustion reactions, and atmospheric air can be modeled as
being made up of 21% oxygen and 79% nitrogen (volume or molal basis).
Therefore, for every mole of air injected into the combustion reaction,
there are 0.21 moles of oxygen and 0.79 moles of nitrogen. For every one
mole of oxygen, there are 0.79/0.21 = 3.76 moles of nitrogen in the air intake
of the combustion chamber. So, for every mole of oxygen needed for combustion,
4.76 moles of air must be supplied: one mole of oxygen plus 3.76 moles of
nitrogen.
The stoichiometric combustion of methane with air is
given by the following equation:
CH4 + 2O2
+ 2(3.76)N2 ⇀
CO2 + 2H2O
+ 2(3.76)N2
The stoichiometric combustion of isooctane with air
is given as:
C8H18 + 12.5O2
+ 12.5(3.76)N2 ⇀
8CO2 +
9H2O + 12.5(3.76)N2
The terminologies used for the amount of air or oxygen used in
combustion are:
1). 85% stoichiometric air = 85% theoretical air = 85% air =
15% deficiency of air
2). 120 % stoichiometric oxygen = 120 % theoretical oxygen=
120 % oxygen = 20 % excess oxygen
The concept of excess air
means the introduction of air in addition to that required for combustion.
However, if one does not provide enough air, combustion may still continue but
it will generate large quantities of CO and combustibles. This is referred to
as sub-stoichiometric combustion. Process heaters, furnaces, and boilers should
NEVER be operated in this mode.
For actual combustion in an
engine, we introduce a useful term “equivalence ratio”. The equivalence
ratio is a measure of the actual fuel-air mixture relative to the
stoichiometric conditions of the fuel-air mixture. It is defined as:
ɸ = (FA)act /
(FA) stoich = (AF)stoich
/ (AF)act
where:
FA = mf
/ ma = fuel-air ratio
AF = ma
/mf = air-fuel ratio
ma = mass of air or mass flowrate of air
mf = mass of fuel or mass flowrate of fuel
Precautions for units of quantities:
During calculations, when using the mass flow rate of air,
essentially use the mass flow rate of fuel.
During calculations, when using the mass of air, essentially
use the mass of fuel.
when:
ɸ < 1 then the mass of air is more than that in
stoichiometric amounts is needed, the FAmix will be lean in fuel & oxygen
will be in exhaust gases.
ɸ > 1 then the mass of air is less than that in
stoichiometric amounts is needed, the FAmix will be rich in fuel, there will be
no oxygen in exhaust gases, but there will be CO and fuel in exhaust gases.
ɸ = 1 then FAmix will be in stoichiometric amounts,
maximum energy will be released from fuel, and there will be neither oxygen nor
CO in exhaust gases.
Spark ignition engines usually operate with an equivalence ratio in the range of 0.9 to 1.2, depending on the type of operation.
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