Affiliation:
1. University of Washington, Dept. of Mechanical Engineering, Seattle, WA 98195
Abstract
The formation of NOx in lean-premixed, high-intensity combustion is examined as a function of several of the relevant variables. The variables are the combustion temperature and pressure, fuel type, combustion zone residence time, mixture inlet temperature, reactor surface-to-volume ratio, and inlet jet size. The effects of these variables are examined by using jet-stirred reactors and chemical reactor modeling. The atmospheric pressure experiments have been completed and are fully reported. The results cover the combustion temperature range (measured) of 1500 to 1850 K, and include the following four fuels: methane, ethylene, propane, and carbon monoxide/hydrogen mixtures. The reactor residence time is varied from 1.7 to 7.4 ms, with most of the work done at 3.5 ms. The mixture inlet temperature is taken as 300 and 600 K, and two inlet jet sizes are used. Elevated pressure experiments are reported for pressures up to 7.1 atm for methane combustion at 4.0 ms with a mixture inlet temperature of 300 K. Experimental results are compared to chemical reactor modeling. This is accomplished by using a detailed chemical kinetic mechanism in a chemical reactor model, consisting of a perfectly stirred reactor (PSR) followed by a plug flow reactor (PFR). The methane results are also compared to several laboratory-scale and industrial-scale burners operated at simulated gas turbine engine conditions.
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Reference15 articles.
1. Aigner, M., Mayer, A., Schiessel, P., and Strittmatter, W., 1990, “Second-Generation Low-Emission Combustors for ABB Gas Turbines: Test Under Full-Engine Conditions,” ASME Paper No. 90-GT-308.
2. Altemark, D., and Knauber, R., 1987, “Ergebnisse von Untersuchungen an einem Vormischbrenner unter Druck mit extrem neidriger NOx-Emission,” VDI Berichte No. 645, pp. 299–311.
3. Do¨bbeling
K.
, Kno¨pfelH. P., PolifkeW., WinklerD., SteinbachC., and SattelmayerT., 1996, “Low-NOx Premixed Combustion of MBtu Fuels Using the ABB Double Cone Burner (EV Burner),” ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER, Vol. 118, pp. 46–53.
4. Joshi, N. D., Epstein, M. J., Durlak, S., Marakovits, S., and Sabla, P. E., 1994, “Development of a Fuel Air Premixer for Aero-Derivative Dry Low Emissions Combustors,” ASME Paper No. 94-GT-253.
5. Leonard
G.
, and StegmaierJ., 1994, “Development of an Aeroderivative Gas Turbine Dry Low Emissions Combustion System,” ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER, Vol. 116, pp. 542–546.
Cited by
24 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献