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High Temperature Thermal Stability of JP-8+100 and Other Fuels FREE

[+] Author Affiliations
Kenneth E. Binns, Gordon L. Dieterle

University of Dayton, Dayton, OH

Paper No. 99-GT-107, pp. V002T02A012; 8 pages
doi:10.1115/99-GT-107
From:
  • ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition
  • Volume 2: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • Indianapolis, Indiana, USA, June 7–10, 1999
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7859-0
  • Copyright © 1999 by ASME

abstract

An engine trend toward maximum use of fuel as a heat sink has created interest in thermal stability information on aviation fuels for high temperature applications. Testing of the fuels has been conducted in the Extended Duration Thermal Stability Test System. This system was established for evaluating the thermal stability of JP-8+100 fuel. The specific fuels evaluated were JP-8, JP-8+100, JPTS and JP-7. The testing has been conducted at temperature and residence times that represent future aircraft/engine fuel systems. Special thermal stability tests with copper doped fuels and at low oxygen content have also been conducted. Carbon deposition information of these fuels that occur in bulk fuel and on hot surfaces is covered in this paper. The description of the test system and its operating characteristics and the test results are also included.

Copyright © 1999 by ASME
This article is only available in the PDF format.

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