Hostname: page-component-84b7d79bbc-g7rbq Total loading time: 0 Render date: 2024-07-27T22:50:22.697Z Has data issue: false hasContentIssue false
  • English
  • Français

Fuel Systems for Turbine-Engined Aircraft

Part of: Sustainable Aerospace

Published online by Cambridge University Press:  28 July 2016

J. E. Walker
Get access Rights & Permissions [Opens in a new window]

Extract

The 855th Lecture to be given before the Royal Aeronautical Society, “ Fuel Systems for Turbine-Engined Aircraft ” by Mr. J. E. Walker, A.F.R.Ae.S., was read under the auspices of the Luton Branch of the Society on the 24th April 1952 at Luton.

Type
Research Article
Information
The Aeronautical Journal , Volume 56 , Issue 501 , September 1952 , pp. 657 - 690
Copyright
Copyright © Royal Aeronautical Society 1952

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Aviation Fuels, R.Ae.S. Data Sheets, 1950.Google Scholar
2. Shellard, A. D. The Vapour Evolution Characteristics of Aviation Turbine Fuels. Thornton Research Centre, 1952.Google Scholar
3. Vapour and Air Release from Aviation Fuels. Esso Development Co. Ltd., 1952.Google Scholar
4. Aviation Fuel Volatility. Texaco “Lubricacation,” Vol. 32, No. 7, 1946.Google Scholar
5. Hunt, K. C. The Development of the Aircraft Gas Turbine in G.B. and its Influence on Petroleum Requirements. Esso Air World, Vol. 3, Nos. 5 and 6, 1951.Google Scholar
6. O'Farrell, M. Effect of Altitude Conditions on Fuels for Aero Gas Turbines. Shell A viation News, No. 135, 1949.Google Scholar
7. The Solubility of Gases in Lubricating Oils and Fuels. Thornton Aero Engine Research Laboratory Report No. 117, 1944.Google Scholar
8. Hardy, and Bigg, . Cooling of Fuel in Integral Tanks. R.A.E. Tech. Note No. Mech. Eng. 43, 1949.Google Scholar
9. Effect of Low Temperature on the Performance of the Fuel System of Turbine Engined Aircraft. Rolls-Royce Ltd., 1950.Google Scholar
10. Aviation Turbine Fuels—Filter Clogging Tendencies at Low Temperature. Thornton Research Centre Report No. R.180/470, 1947.Google Scholar
11. Design and Performance of Fuel Booster Pumps. Thornton Laboratory Report No. 123, 1945.Google Scholar
12. The Spontaneous Ignition Characteristics of Kerosene. Anglo Iranian Oil Co., Memo No. 1536/52, 1952.Google Scholar
13. Glendinning, and Parker, . Explosion Risks in Fuel Tanks. R.A.E. Report No. Ch. 325, 1941.Google Scholar
14. Summary of Data—Limits of Inflammability, Flame Speeds, Flame Temperatures and Ignition Temperatures. Thornton Research Centre, 1947.Google Scholar
15. An Investigation of the Fire Hazards associated with the use of various Petroleum Fractions. Thornton Research Centre, Report No. R.181/470, 1947.Google Scholar