Fuel Systems for Gas Turbine Engines

Author:

Lawrence O. N.

Abstract

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.

Publisher

Cambridge University Press (CUP)

Reference6 articles.

1. Air Intake Efficiency

2. A Critical Review of German Research on High-Speed Airflow

3. Milliken W. Dynamic Stability and Control Research. Third Anglo-American Aeronautical Conference, Brighton, 1951. The Royal Aeronautical Society.

4. Lawrence O. N. British Patent 709,300.

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. The Application of Servo-Mechanism Analysis to Fuel Control Problems;Proceedings of the Institution of Mechanical Engineers;1958-06

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