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The low temperature properties of aviation fuels

Published online by Cambridge University Press:  04 July 2016

G. Brunton
Affiliation:
Shell Research Ltd, Thornton Research Centre, Chester
R. R. Willock
Affiliation:
Shell Research Ltd, Thornton Research Centre, Chester
M. A. Voisey
Affiliation:
Shell Research Ltd, Thornton Research Centre, Chester

Extract

The aviation fuel market is one of the few areas in the petroleum industry where an increase in future demand can be predicted with a reasonable degree of certainty. However, this growth in demand is likely to be influenced by two major constraints, price and availability. At present aviation fuel represents only a relatively small portion of the barrel, but any increase in this fraction is limited by the need to meet specification requirements and competition from other products. The changing pattern in product demand is focusing attention on secondary refinery processes to maximise output of distillate fractions and on the use of alternative non-petroleum sources of fuel. In both of these approaches, significant upgrading of the initial product, involving both large capital outlay and high operating costs, may be necessary to produce final products within current specification limits. Under these conditions it is desirable to identify ways of easing specification requirements that will increase flexibility, but at the same time maintain product quality.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1982 

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References

1. Lewis, A. Future Aviation Fuels. The Petroleum Industry Responds to the Challenge, SAE paper 880769, 1980.Google Scholar
2. Robertson, A. and Williams, R. E. Jet Fuel Specifications: the Need for a Change. Shell Aviation News, 435, 1976, 1013.Google Scholar
3. Pasion, A. J. In-Flight Fuel Tank Temperature Survey Data. D6-48611, Boeing Commercial Airplane Co, Seattle, Wash, May 1979 (NASA CR-159569).Google Scholar
4. Barr, N. M. et al. Boeing Airplane Fuel Systems at Low Temperatures, Document D6-42386, 1975, Boeing Commercial Airplane Co, Seattle, Wash.Google Scholar
5. Pasion, A. J. and Thomas, I. Preliminary Analysis of Aircraft Fuel Systems for Use with Broadened Specification Jet Fuels, D6-44538, Boeing Commercial Airplane Co, Seattle, Wash. (NASA CR-135198).Google Scholar
6. Longwell, J. P. and Grobman, J. Alternative Aircraft Fuels, Engineering for Power, 101, 1979, 155161.Google Scholar
7. Friedman, R. High-Freezing Point Fuels Used for Aviation Turbine Engines, ASME, Paper No 79-6-7-141, March 1979.Google Scholar
8. Strawson, H. Using Turbine Fuels at Low Temperatures, Shell Aviation News, 210, December 1955. 812.Google Scholar
9. Strawson, H. The Pumpability of Aviation Turbine Fuels at Low Temperature, J. Inst Petrol, 45, 425, 129146, 1959.Google Scholar
10. Hutton, J. F. Flow Properties of Distillates at Low Temperatures. A Review, J. Inst Petrol, 45, 425, 123129, 1959.Google Scholar
11. Proposed IP Standard Method for Cold Flow Test of Aviation Turbine Fuels, J. Inst Petrol, 48, 467, 388390. 1962.Google Scholar
12. Low Temperature flow characteristics of Aviation Turbine Fuel, Report of Panel ST-B-6 of the Institute of Petroleum, Sept, 1960.Google Scholar
13. Solash, J. et al. Relation between Fuel Properties and Chemical Composition 1. Jet Fuels from Coal, Oil Shale and Tar Sands, Fuel, 57, 521528, 1978.Google Scholar
14. UK Patent Application 2 043 246 A, October 1980.Google Scholar
15. Friedman, R. and Stockemer, F. J. Temperature and Flow Measurement on Near-Freezing Aviation Fuels in a Wing-Tank Model, ASME Paper No 80-GT-63, March 1980.Google Scholar