Affiliation:
1. UCI Combustion Laboratory, University of California, Irvine, CA 92697-3550
Abstract
With the need to reduce carbon emissions such as CO2, hydrogen is being examined as potential “clean” fuel for the future. One potential strategy is lean premixed combustion, where the fuel and air are allowed to mix upstream before entering the combustor, which has been proven to curb NOx formation in natural gas fired engines. However, premixing hydrogen and air may increase the risk of autoignition before the combustor, resulting in serious engine damage. A flow reactor was set up to test the ignition delay time of hydrogen and air at temperatures relevant to gas turbine engine operations to determine maximum possible mixing times. The results were then compared to past experimental work and current computer simulations. The current study observed that ignition is very sensitive to the initial conditions. The ignition delay times follow the same general trend as seen in previous flow reactor studies: ignition within hundreds of milliseconds and relatively low activation energy. An experimentally derived correlation by Peschke and Spadaccini (1985, “Determination of Autoignition and Flame Speed Characteristics of Coal Gases Having Medium Heating Values,” Research Project No. 2357-1, Report No. AP-4291) appears to best predict the observed ignition delay times. Homogenous gas phase kinetics simulations do not appear to describe ignition well in these intermediate temperatures. Therefore, at the moment, only the current empirical correlations should be used in predicting ignition delay at engine conditions for use in the design of gas turbine premixers. Additionally, fairly large safety factors should still be considered for any design to reduce any chance of autoignition within the premixer.
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Reference37 articles.
1. Conrad, W. E., and Corrington, L. C., 1957, “NACA Research Memorandum: Hydrogen for Turbojet and Ramjet Powered Flight,” Report No. NACA RM E57D23.
2. Combustion Performance of Hydrogen in a Small Gas Turbine Combustor;Sampath;Int. J. Hydrogen Energy
3. Overview of the U.S. Department of Energy’s Office of Fossil Energy Advanced Turbine Program for Coal Based Power Systems With Carbon Capture;Dennis
4. Using Hydrogen as Gas Turbine Fuel;Chiesa;ASME J. Eng. Gas Turbines Power
5. Evaluation of a Low Emission Gas Turbine Operated on Hydrogen;Therkelsen
Cited by
34 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