Combustion and Emission Characteristics in a Can-type Combustion Chamber

Combustion phenomenon will be accomplished
effectively by the development of low emission combustor. One of the
significant factors influencing the entire Combustion process is the
mixing between a swirling angular jet (Primary Air) and the
non-swirling inner jet (fuel). To study this fundamental flow, the
chamber had to be designed in such a manner that the combustion
process to sustain itself in a continuous manner and the temperature of
the products is sufficiently below the maximum working temperature
in the turbine. This study is used to develop the effective combustion
with low unburned combustion products by adopting the concept of
high swirl flow and motility of holes in the secondary chamber. The
proper selection of a swirler is needed to reduce emission which can be
concluded from the emission of Nox and CO2. The capture of CO2 is
necessary to mitigate CO2 emissions from natural gas. Thus the
suppression of unburned gases is a meaningful objective for the
development of high performance combustor without affecting turbine
blade temperature.





References:
[1] V. M. Reddy and S. Kumar, "Development of high intensity low emission
combustor for achieving flameless combustion,” Propulsion and Power
Research, Vol. 2, 2013, pp. 139–147.
[2] C. Ghenai, "Combustion of syngas fuel in gas turbine can combustor,”
Advances in Mechanical Engineering, Vol. 1, 2010, pp. 1-13.
[3] P. S. Kumar and P. P. Rao, "Design and analysis of gas turbine
combustion chamber," International Journal of Computational
Engineering Research, Vol. 3, 2012, pp. 1-6.
[4] H. Pathan, K. Partel, and V. Tadvi, "Numerical investigation of the
combustion of methane air mixture in gas turbine can-type combustion
chamber,” International Journal of Scientific & Engineering Research,
Vol. 3, No. 10, 2012, pp. 1-7.
[5] P. Koutmos and J. J. McGuirk, "Isothermal flow in a gas turbine
combustor–a benchmark experimental study,” Experiments in Fluids, Vol.
7, 1989, pp. 344-354.
[6] Y. A. Eldrainy, J. Jeffrie, and M. Jaafar, "Prediction of the flow inside a
Micro Gas Turbine Combustor,” Journal of Mechanical, vol. 25, 2008, pp.
50-63.
[7] J. A. Wunning, and J. G. Wunning, "Flameless oxidation to reduce
thermal NO-formation,” Progress in Energy and Combustion Science,
Vol. 23, No. 1, 1997, pp. 81–94.
[8] B. E. Launder and D. B. Spalding, "The numerical computation of
turbulent flows,” Computer Methods in Applied Mechanics and
Engineering, Vol. 3, 1974, pp. 269-289.
[9] M. Y. Kim, "Effect of swirl on gas-fired combustion behavior in a 3-D
rectangular combustion chamber,” World Academy of Science,
Engineering and Technology, Vol. 64, 2012, pp. 939-944.