Since dissolved oxygen participates in fuel deposit formation, knowledge of the effects of dissolved oxygen concentration on fuel thermal stability is critical for fuel system design. In this work, the combined effects of dissolved oxygen availability and additives on jet fuel thermal stability are studied. Experiments with JP-8 jet fuel were conducted in a three-part heat exchanger which simulated a complex thermal and flow environment. The dissolved oxygen content at the flow inlet was varied, and deposition was studied under conditions of either fractional or complete oxygen consumption. The effects of a thermal stability additive package were also studied. An intriguing result found with JP-8 fuels is an increase in deposits formed in heated regions for decreased oxygen consumption, but inverse behavior with the additive package.
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ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition
June 10–13, 1996
Birmingham, UK
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7874-3
PROCEEDINGS PAPER
The Effects of Dissolved Oxygen Concentration, Fractional Oxygen Consumption, and Additives on JP-8 Thermal Stability
T. F. Williams,
T. F. Williams
University of Dayton, Dayton, OH
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S. P. Heneghan,
S. P. Heneghan
University of Dayton, Dayton, OH
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S. Zabarnick
S. Zabarnick
University of Dayton, Dayton, OH
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J. S. Ervin
University of Dayton, Dayton, OH
T. F. Williams
University of Dayton, Dayton, OH
S. P. Heneghan
University of Dayton, Dayton, OH
S. Zabarnick
University of Dayton, Dayton, OH
Paper No:
96-GT-132, V003T06A023; 9 pages
Published Online:
February 6, 2015
Citation
Ervin, JS, Williams, TF, Heneghan, SP, & Zabarnick, S. "The Effects of Dissolved Oxygen Concentration, Fractional Oxygen Consumption, and Additives on JP-8 Thermal Stability." Proceedings of the ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations. Birmingham, UK. June 10–13, 1996. V003T06A023. ASME. https://doi.org/10.1115/96-GT-132
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