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Fuel Systems for Gas Turbine Engines

Published online by Cambridge University Press:  28 July 2016

O. N. Lawrence
O. N. Lawrence*
Affiliation:
Joseph Lucas (Gas Turbine Equipment) Ltd.
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Extract

Seven years ago a paper on this same subject was read before the Main Society. This has been used as a basis from which to start.

It will be seen that great strides have been made in performance, and the projects in the Design Office and on the drawing boards particularly, would even satisfy parliamentary critics. In Derby, however, where jet lift was conceived, such things are well known. From the fuel system standpoint in general the changes in requirements have been routine, merely much greater fuel demands, greater altitudes and air speeds and hence, a greater range of fuel flow, and it is this which gives the fuel system engineer his greatest worries. Beyond this there is always the need for smaller and lighter units in fancy shapes.

Type
Research Article
Information
The Aeronautical Journal , Volume 59 , Issue 539 , November 1955 , pp. 727 - 737
Copyright
Copyright © Royal Aeronautical Society 1955

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References

1. Lawrence, O. N. (1948). Gas Turbine Accessory Systems. Journal of the Royal Aeronautical Society, Vol. 52, No. 447, pp. 151–185, March 1948.Google Scholar
2. Greatrex, F. B. ((1954). Air Intake Efficiency. Journal of the Royal Aeronautical Society, Vol. 58, No. 525, pp. 639–648, September 1954.Google Scholar
3. Smelt, R. (1946). A Critical Review of German Research on High-Speed Airflow. Journal of the Royal Aeronautical Society, Vol. 50, No. 432, pp. 899–934, December 1946.CrossRefGoogle Scholar
4. Lawrence, O. N. British Patent 709,300.Google Scholar
5. Ifield, R. J. Unpublished work.Google Scholar
6. Milliken, W. Dynamic Stability and Control Research. Third Anglo-American Aeronautical Conference, Brighton, 1951. The Royal Aeronautical Society.Google Scholar