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High freezing point fuels used for aviation turbine enginesBroadened-specification aviation fuels could be produced from a greater fraction of crude source material with improvements in fuel supply and price. These fuels, particularly those with increased final boiling temperatures, would have higher freezing temperatures than current aviation turbine fuels. For the small but significant fraction of commercial flights where low fuel temperatures make higher freezing-point fuel use unacceptable, adaptations to the fuel or fuel system may be made to accommodate this fuel. Several techniques are discussed. Fuel heating is the most promising concept. One simple design uses existing heat rejection from the fuel-lubricating oil cooler, another uses an engine-driven generator for electrical heating.
Document ID
19790007028
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Friedman, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1979
Subject Category
Propellants And Fuels
Report/Patent Number
E-9804
NASA-TM-79015
Meeting Information
Meeting: Ann. Intern. Gas Turbine Conf.
Location: San Diego, CA
Country: United States
Start Date: March 11, 1979
End Date: March 15, 1979
Sponsors: ASME
Accession Number
79N15199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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