Carbon
dioxide (CO2) emission forms the biggest portion
of greenhouse gas emissions known to cause global warming, which can
lead to climate change. One of the most widely recommended means of
tackling CO2 emission is the carbon capture technique,
which includes oxyfuel combustion. In oxyfuel combustion, O2/CO2 oxidizer mixtures are used to lower the oxy-combustion
temperatures to make it suitable for the components of the combustion
systems. These oxidizer mixtures, depending upon the relative concentrations
of the species, exhibit distinct combustion characteristics. In this
study, flame stability of propane–air and propane–oxyfuel
combustion is studied in a non-premixed, swirl-stabilized combustor.
The combustion of air was compared to two oxyfuel mixtures, namely,
oxyfuel I and II, in terms of lean blowout limits. Oxyfuel II and
air combustion were also compared in terms of the temperature. Furthermore,
the effects of the CO2 dilution level, equivalence ratio,
swirl number, and combustor firing rate on oxyfuel flame stability
were studied. Results show that, for lean mixtures, the propane–air
flame transits from the attached flame to lifted flame before subsequent
flame extinction. This is contrary to oxyfuel I and II flames that
transit directly from the attached flame to no flame regime at all
firing rates studied. Near stoichiometry, however, the oxyfuel flames
display distinct flame transitions, including liftup before extinction
as a consequence of CO2 dilution at high firing rates.
These flame transitions before blowout were observed to be flow-induced.
NO
x
and CO emissions were seen to depend
strongly upon air and oxyfuel combustion temperatures. The amount
of CO2 required in the oxidizer at blowout was observed
to decrease significantly as the equivalence ratio decreases from
1 to 0.9, signifying an enhanced stability at stoichiometric conditions.
Further studies revealed that the oxyfuel flames are more stable at
the swirl number of 1.0 when compared to 0.6 and 1.5.