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- W2329387504 abstract "The thermal oxidative stability of several aircraft fuels at high temperatures has been evaluated in a flowing test device. The fuels studied include Jet A, JPTS, and JP-7. The tests evaluated solid deposition under various conditions, typically at maximum fuel temperatures of ∼480 °C (900 °F) at a pressure of 69 atm. Under these conditions, the dissolved oxygen in the fuel is completely consumed and the thermal-oxidative reactions are driven to completion. At test times up to 50 hours, both surface and bulk (filter) deposition was usually an approximately linear function of test time, after an initial induction time of low deposition which varied from 0 to ∼20 hours depending upon fuel quality. In tests with flow rates from 12 to 200 mL/min (1–21 lb/hr), the deposition rate (expressed in ppm) was fairly constant. These data give some guidance for extrapolating results from small flow-rate bench-scale tests to higher flow rates more realistic to aircraft fuel systems, for conditions where the oxygen is completely consumed. For conditions where the oxygen is not completely consumed, the relationship between surface and suspended bulk deposits can become quite complex. Two dispersant additives widely examined in the JP-8+100 program were studied, with the additive significantly decreasing the slope of the deposition-vs-time curve (the deposition rate) for Jet A fuels." @default.
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- W2329387504 date "1995-06-05" @default.
- W2329387504 modified "2023-09-26" @default.
- W2329387504 title "The Thermal Stability of Fuels at 480 °C (900 °F): Effect of Test Time, Flow Rate, and Additives" @default.
- W2329387504 doi "https://doi.org/10.1115/95-gt-068" @default.
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