Evaporation of Jet Fuels


Book Description

Determining the fate and transport of JP-8 jet fuel is a complex and important problem. As part of the startup procedures for jet engines, fuel is passed through aircraft engines before combustion is initiated. Because of the extremely low temperatures at northern tier Air Force bases, the unburned fuel does not evaporate readily and may come into contact with ground crew. To determine the amount and duration of contaminant contact, the evaporation of the emitted fuel must be modeled. The amount and composition of the fuel upon reaching the ground crew may be determined by droplet evaporation models that have already been developed. The evaporation of the fuel after adhering to the skin needs to be modeled. This knowledge of the fuel's fate may then be used to determine source terms for use in toxicological studies. This research involves the comparison of two existing droplet evaporation models and the calculation of the evaporation of a film of jet fuel from a surface. The existing models are compared in order to make recommendations on which model to use to predict the amount and composition of fuel reaching the ground crew. To make the surface evaporation problem amenable to modeling, simplifying assumptions are made. The fuel is assumed to be a uniformly distributed mixture of representative hydrocarbon groups. Due to the complexity of the mixture of aviation fuels, a mixture of the predominant species were chosen as representatives to approximate the physical behavior of the entire fuel mixture. The goal of this research is to determine the most appropriate model for predicting the amount and composition of jet fuel reaching the ground crew and to extend the more appropriate fuel droplet evaporation model to describe the evaporation of a film of fuel from a surface. A validation of the resultant model is then performed by comparing the calculations to experimental data.










Toxicologic Assessment of Jet-Propulsion Fuel 8


Book Description

This report provides a critical review of toxicologic, epidemiologic, and other relevant data on jet-propulsion fuel 8, a type of fuel in wide use by the U.S. Department of Defense (DOD), and an evaluation of the scientific basis of DOD's interim permissible exposure level of 350 mg/m3







Inert Gas Scattering and Evaporation from Jet Fuel Surrogates Using Liquid Microjets


Book Description

Vacuum-based investigations into the dynamics of gas-surface collisions for high vapor pressure liquids, including water and hydrocarbon fuels, are complicated by the dense vapor cloud that forms above the surface of the liquid. Earlier surface forming techniques, relying on a liquid-coated wheel, were limited to vapor pressures of 0.005 Torr. Narrow diameter liquid jets circumvent this limitation because their small surface area minimizes evaporation; the sparse vapor cloud surrounding the thin liquid jet, suppresses collisions between solvent vapor molecules and impinging or evaporating probe gas molecules. We use liquid microjets to investigate the interfacial behavior of surrogates of JP-8, a military grade jet fuel, under conditions that mimic the temperature of a gas turbine combustion chamber. Collisions between gases and liquids control the heating and vaporization of fuel droplets in jet engines. These dynamics can be investigated by gas-liquid scattering experiments. We explored collisions of oxygen and neon with dodecane (0.1 Torr vapor pressure) and compared them to collisions with a low vapor pressure liquid, squalane (10-8 Torr). The extent of energy transfer and thermalization are remarkably high and similar for the two hydrocarbon liquids. These studies suggest that hot gas molecules readily transfer their energy and heat and vaporize fuel droplets during the combustion process. We also used liquid microjets to explore the evaporation of inert gases from fuel and fuel surrogates. We find that most gas species evaporate with a Maxwell-Boltzmann distribution of kinetic energies (2RTliq) under collision-free conditions; they follow an evaporation pathway that involves momentary binding (trapping) at the surface before they desorb. However, two weakly binding atoms, helium and neon, evaporate with super-Maxwellian distributions. The measured average energies of evaporating helium atoms range from 14% more than 2RTliq for dodecane (a pure hydrocarbon liquid) to 70% more than 2RTliq for a 7.5 M LiBr/water solution. These experiments imply that He atoms evaporate ballistically, rapidly traversing the interfacial region at high energies whose magnitude are determined by the packing, bonding, and masses of interfacial solvent molecules. The evaporation of H2 was found to be sub-Maxwellian, as predicted from its light mass and moderate polarizability.




Aviation Fuels with Improved Fire Safety


Book Description

The reduction of the fire hazard of fuel is critical to improving survivability in impact-survivable aircraft accidents. Despite current fire prevention and mitigation approaches, fuel flammability can overwhelm post-crash fire scenarios. The Workshop on Aviation Fuels with Improved Fire Safety was held November 19-20, 1996 to review the current state of development, technological needs, and promising technology for the future development of aviation fuels that are most resistant to ignition during a crash. This book contains a summary of workshop discussions and 11 presented papers in the areas of fuel and additive technologies, aircraft fuel system requirements, and the characterization of fuel fires.




Research Test Facility for Evaporation and Combustion of Alternative Jet Fuels at High Air Temperatures


Book Description

Improved gas turbine combustion performance will require the effective utilization of alternative fuels and advanced combustor concepts. Further understanding of spray combustion processes including fuel evaporation and flame propagation is required. Research is underway which features a high pressure and temperature non-vititated air system to provide air at simulated gas turbine inlet conditions. A special fuel injection system was designed to produce monodisperse sprays for the purpose of evaporation and eventual combustion experiments in our newly developed test facility. This report represents a summary of the engineering activities during the first year (of a two year contract) which was focused on the construction of a combustion test facility in which the evaporation and burning rates of jet fuels can be measured as a function of inlet conditions and fuel properties. A large heat exchanger facility which supports this research can deliver continuously non-vitiated air at flowrates up to 1 kg/sec and 600 kPa at temperatures from 300 to 900K. Details of the evaporation/combustion test section are described. Also included are the design of the fuel injection system and test results of the injector showing monodisperse sprays with drop diameters of approx. 70 micrometers.