Abstract
Factors affecting the nitric oxide (NO) emission level of a regenerative turbine combustor are reviewed. Differences attributable to fuel type are discussed. Temperature and composition measurements obtained with a water-cooled choked sampling probe are presented for a turbine combustor operating on two different fuels: #2 diesel oil and methanol. Methods of averaging the discrete data are developed. Temperature is computed from measurement of the choked sample flow rate. Methanol displays lower NO emission because of decreased high temperature residence duration, lower flame temperature and diminished oxygen and nitrogen availability. It is found that the combustion and NO formation zones occupy a small portion of the regenerative combustor while the CO oxidation zone occupies roughly half of the combustor under investigation. Nitric oxide never reaches equilibrium values, whereas carbon monoxide exceeds equilibrium values throughout most of the combustor.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Ya. B. Zeldovich, P. Ya. Sadovnikov, and D.A. Frank-Kamenetskii, Oxidation of Nitrogen in Combustion, Publishing House of the Academy of Sciences, USSR, Moscow, 1947. (Translated by M. Shelef, Scientific Research Staff, Ford Motor Company. Copies are available from the translator).
P. Blumberg and J.T. Kummer, “Prediction of NO Formation in Spark-Ignited Engines — An Analysis of Method of Control,” Combustion Sciency and Technology, 4, 1971, p. 73.
W.R. Marshall, “Atomization of Spray Drying,” Chem. Eng. Prog. Series No. 2, Vol. 5, AIChE, New York, 1954.
Delavan Mfg. Co., Des Moines, Iowa, private communication with R. Slezak.
S. Way, “Combustion in the Turbojet Engine”, Selected Combustion Problems II, AGARD, Butterworths, London, 1956.
A.A. Ranger and J. A. Nicholls, “Aerodynamic Shattering of Liquid Drops,” AIAA Journal, 7, 2, Feb. 1969.
S.S. Penner, Chemistry Problems in Jet Propulsion, Pergamon Press, New York, 1957.
N.D. Ingebo, “Vaporization Rates and Heat Transfer Coefficients for Pure Liquid Drops,” NAC A TN 2368, July, 1951.
P.G. Parikh, R.F. Sawyer, and A.L. London, “Pollutants from Methane Fueled Gas Turbine Combustion,” Univ. of California, College of Engineering Report No. TS-70–15, Berkeley, January, 1971.
L. Caretto, R.F. Sawyer, and E.S. Starkman, “Formation of Nitric Oxide in Combustion Processes,” College of Engineering Report No. TS-68–1 Univ. of California, Berkeley, March, 1968.
A.M. Keuthe and J.D. Schetzer, Foundations of Aerodynamics, John Wiley & Sons, New York, 1959.
H. Niki, A. Warnick, and R.R. Lord, “An Ozone — NO Chemiluminescence Method for NO Analysis in Piston and Turbine Engines,”SAE Paper No. 710072.
A.G. Piken and C.H. Rouf, “Chemical Composition of Automobile Exhaust and A/F Ratio,” Scientific Research Staff, Ford Motor Company, June, 1968.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 1972 Springer Science+Business Media New York
About this chapter
Cite this chapter
LaPointe, C.W., Schultz, W.L. (1972). Measurement of Nitric Oxide Formation within a Multi-Fueled Turbine Combustor. In: Cornelius, W., Agnew, W.G. (eds) Emissions from Continuous Combustion Systems. Springer, Boston, MA. https://doi.org/10.1007/978-1-4684-1998-6_13
Download citation
DOI: https://doi.org/10.1007/978-1-4684-1998-6_13
Publisher Name: Springer, Boston, MA
Print ISBN: 978-1-4684-2000-5
Online ISBN: 978-1-4684-1998-6
eBook Packages: Springer Book Archive