Jet Fuel Thermal Stability


Book Description

Various aspects of the thermal stability problem associated with the use of broadened-specification and nonpetroleum-derived turbine fuels are addressed. The state of the art is reviewed and the status of the research being conducted at various laboratories is presented. Discussions among representatives from universities, refineries, engine and airframe manufacturers, airlines, the Government, and others are presented along with conclusions and both broad and specific recommendations for future stability research and development. It is concluded that significant additional effort is required to cope with the fuel stability problems which will be associated with the potentially poorer quality fuels of the future such as broadened specification petroleum fuels or fuels produced from synthetic sources.




Aviation Fuel


Book Description

For technical readers in the aviation and fuel industries, and in testing laboratories, explores the history and philosophy of the thermal stability of aviation fuel, and considerations during the fuel's manufacture, storage and transport, use, and assessment. The 13 papers, representing a number of




Applications of High Pressure Differential Scanning Calorimetry to Aviation Fuel Thermal Stability Research


Book Description

High pressure differential scanning calorimetry (DSC) was studied as an alternate method for performing high temperature fuel thermal stability research. The DSC was used to measure the heat of reaction versus temperature of a fuel sample heated at a programmed rate in an oxygen pressurized cell. Pure hydrocarbons and model fuels were studied using typical DSC operating conditions of 600 psig of oxygen and a temperature range from ambient to 500 C. The DSC oxidation onset temperature was determined and was used to rate the fuels on thermal stability. Kinetic rate constants were determined for the global initial oxidation reaction. Fuel deposit formation is measured, and the high temperature volatility of some tetralin deposits is studied by thermogravimetric analysis. Gas chromatography and mass spectrometry are used to study the chemical composition of some DSC stressed fuels. Neveu, M. C. and Stocker, D. P. Glenn Research Center NASA-TM-87002, E-2547, NAS 1.15:87002 RTOP 505-40-90










Thermal Stability Enhancement of JP-5


Book Description

The objective of this work was to determine if C60 or its derivatives could enhance the oxidative thermal stability of JP-5 and similar aviation fuels. Two derivatives of C60 were prepared, n-hexyl amine and di-isopropylamine. Several conventional thermal stressing experiments were also performed: oxygen overpressure (OOP), isothermal corrosion oxidation test (ICOT), quartz crystal microbalance (QCM), and hot liquid process simulator (HLPS). In addition, a fuel stability test system (FSTS) developed at Advanced Fuel Research, Inc. (AFR) was also used. The FSTS includes fiber optic infrared transmission cells to assess fuel thermal stability during thermal stressing up to 500 deg C. The low temperature data from OOP, ICOT, QCM and HPLS show that pure C60 generally reduces the deposit formation, although the amount of this reduction is only modest (between 5 and 30%). The beneficial effects are larger under more severe conditions (higher temperatures, longer oxidation times, higher oxygen concentrations). The FSTS results were consistent with this trend, although at the highest temperatures (425-500 deg C), some potentially deleterious effects of C60 also appear to be enhanced. The effects of reactor tube activation were important for the FSTS. Additional work is warranted on exploring the beneficial effects of C60 addition which could serve to extent the operating range of common jet fuels.




An Analysis of the Thermal Stability of Conventional and Alternative Aviation Fuels


Book Description

An experimental apparatus was used to examine the thermal stability of conventional and alternative aviation fuels. The apparatus is a simplified but controllable representation of an aircraft fuel system consisting of a preheating section and a test section. The preheating section simulates the fuel conditions as it acts as a coolant on board of the aircraft while the test section simulates the conditions of the fuel injection nozzles. The apparatus measures the accumulated deposit by taking the pressure drop data across the heated test section. After thermal stressing, the pressure drop data is verified by a carbon burnoff apparatus. The fuel chemical composition is evaluated by nuclear magnetic resonance spectroscopy. Experimental results are presented and discussed in this thesis for four different types of aviation fuels to show the relationship between fuel chemical composition and coking propensity. The experiments show that fuels with aromatic content tend to produce more deposits and the alternative fuels are potentially more thermally stable than their conventional counterparts.







In-Situ Methods for Study of Fuel Thermal Stability


Book Description

The objective of this work was to develop a methodology for in-situ optical measurements of peroxide decomposition products from aviation fuels and demonstrate how this information could be related to fuel stability. Three fiber optic probes (2 Mid-IR, 1 Near-IR) were designed and constructed, and used to monitor the changes in composition of two fuels (Shell Jet A #2827 and Sun Jet A-1 #2747) after thermal stressing. Both mid-IR probes were found to be very sensitive to changes in fuel composition. The large gap (1 mm) IR cell was used to make in-situ IR transmission measurements for peroxide decomposition products, including carbonyls (free and acid form), alcohols, and CO2 (two forms). These measurements were consistent with the generally accepted free radical mechanism of fuel degradation, including the inverse relationship between oxidative and thermal stability. The data from the small gap (0.1 mm) IR cell were found to be consistent with changes in deposit formation tendencies with temperature for similar fuels reported in the literature. In an option task, an FT-Raman probe was evaluated and found to be much less sensitive than the Mid-IR probes. This disadvantage may be remedied by the use of a surface enhanced probe. The potential applications include an instrument for development and evaluation of thermally stable fuels or supercritical fuels, improved global models of fuel degradation mechanisms, and on-board monitors of fuel thermal stability.