Effects of Fuel Molecular Structure on Emissions in a Jet Flame and a Model Gas Turbine Combustor


Book Description

Stricter environmental requirements, worldwide air traffic growth, and unsteady fuel prices all has led to an increased interest in alternative jet fuels. Additionally, several nations are investing resources identifying local fuel sources to make the fuel supply more resilient against disruptions and flexible to use of multiple, reliable fuel stocks. The alternative jet fuels that are being defined have unusual molecular distributions relative to current fuels. These differences in molecular structure affect the gas-phase kinetics during combustion, and hence the use of alternative fuels can impact emissions differently than conventional fuels. The differences in the emission characteristics between a newly developed alternative fuel and conventional fuel highlight the need to focus the research efforts on understanding how the fundamental properties of the fuel can affect emissions. The current work focuses on investigating the chemical effects of fuel molecular structure on the emission behavior of the fuels. In particular, the study explores how the fuel composition and premixing affect the production of polycyclic aromatic hydrocarbons (PAH), hazardous air pollutants (HAPs), and soot in a combustion environment. The study uses two experimental configurations: a jet flame and a model gas turbine combustor. Laser induced incandescence (LII) and laser extinction (LE) are used to obtain two-dimensional soot volume fraction in the flames. Laser induced fluorescence (LIF) is used to obtain the two-dimensional aromatic species distribution in the flames. Additionally, numerical analysis is used to investigate the effects of premixing on the soot formation processes in the jet flames for a high molecular weight fuel.




Effects of Fuel Molecular Structures on Pollutants in Co-flow Laminar Flames


Book Description

This study is part of a larger effort to establish a science-based model to predict the emissions from gas turbine engine combustors using alternative fuels. In order to validate and improve the chemical mechanisms in the model, four binary fuel mixtures comprised of the hydrocarbon compounds representative of the classes compounds that are expected in alternative aviation fuels. In each fuel mixture, n-dodecane was the base component. The second component was m-xylene, methylcyclohexane, iso-octane, or n-heptane that were selected to represent the molecular structures of aromatic, cyclo-paraffin, iso-paraffin, and n-paraffin. The binary fuel mixture (25% m-xylene and 75% n-dodecane in liquid volume fraction) was also evaluated as a surrogate for JP-8. A burner system was developed and built to produce co-flow laminar jet flames with liquid fuel mixtures. The experimental conditions for flames were set at three equivalence ratios ([phi]) of the fuel jet--[phi]=[infinity symbol], [phi]=6, and [phi]=2--to simulate the soot-rich zones in gas turbine engine combustors. The combination of laser extinction and laser-induced incandescence (LII) was applied to obtain the spatial distributions of soot volume fraction quantitatively. "Small aromatics" and "large aromatics," containing 1-2 aromatic rings and 3-4 aromatic rings respectively, were detected by laser-induced fluorescence (LIF). A special configuration of thermocouple probe was developed to obtain the temperature distributions in the soot-free regions of the flames. Experimental results indicated that the PAH and soot from all paraffin fuels are similar, but PAH and soot of the aromatic fuel were much larger than for the paraffin fuels. The amount of soot was found to be higher in aromatic flames than in paraffin flames by a factor of between 2-4. The maximum LIF signals from both small and large aromatics along centerline were found to be approximately ten times higher in the aromatic fuel than in paraffin fuels. Similar results, especially soot volume fraction distributions, was found between JP-8 and the m-xylene/n-dodecane fuel. The experimental results were compared in detail to simulation results provided by Dr. Katta of Innovative Scientific Solutions, Inc. Basic consistent distribution trends for each fuel mixture were established with the simulation results. Similar qualitative distributions of soot volume fraction and semi-quantitative LIF signals from aromatic species as well as temperature were found for flames burnt with all fuel mixtures, even though the simulation always displayed large areas of soot and aromatics existing regions. The maximum soot volume fraction along centerline in flames was estimated with values similar to experimental data for paraffin fuels. Several potential explanations were produced for the significant discrepancy of soot distributions in aromatic flames between the simulation and experimental data. Other simulation results, including the distributions of OH and rates of soot nucleation, soot surface growth, and soot oxidation were presented to gain insight into the reasons for the discrepancies between the simulations and the experiment.







Fuel Effects on Operability of Aircraft Gas Turbine Combustors


Book Description

In summarizing the results obtained in the first five years of the National Jet Fuel Combustion Program (NJFCP), this book demonstrates that there is still much to be learned about the combustion of alternative jet fuels.




Uncertainty Quantification in Computational Fluid Dynamics and Aircraft Engines


Book Description

This book introduces design techniques developed to increase the safety of aircraft engines, and demonstrates how the application of stochastic methods can overcome problems in the accurate prediction of engine lift caused by manufacturing error. This in turn addresses the issue of achieving required safety margins when hampered by limits in current design and manufacturing methods. The authors show that avoiding the potential catastrophe generated by the failure of an aircraft engine relies on the prediction of the correct behaviour of microscopic imperfections. This book shows how to quantify the possibility of such failure, and that it is possible to design components that are inherently less risky and more reliable. This new, updated and significantly expanded edition gives an introduction to engine reliability and safety to contextualise this important issue, evaluates newly-proposed methods for uncertainty quantification as applied to jet engines. Uncertainty Quantification in Computational Fluid Dynamics and Aircraft Engines will be of use to gas turbine manufacturers and designers as well as CFD practitioners, specialists and researchers. Graduate and final year undergraduate students in aerospace or mathematical engineering may also find it of interest.










Gas Turbine Emissions


Book Description

The development of clean, sustainable energy systems is a preeminent issue in our time. Gas turbines will continue to be important combustion-based energy conversion devices for many decades to come, used for aircraft propulsion, ground-based power generation, and mechanical-drive applications. This book compiles the key scientific and technological knowledge associated with gas turbine emissions into a single authoritative source.







NASA SP.


Book Description