Hostname: page-component-cd9895bd7-jn8rn Total loading time: 0 Render date: 2024-12-22T20:09:19.430Z Has data issue: false hasContentIssue false
  • English
  • Français

The Development of Small Gas Turbines for Aircraft Auxiliary Power

Published online by Cambridge University Press:  04 July 2016

C. H. Paul
C. H. Paul*
Affiliation:
AiResearch Manufacturing Company of Arizona, Division of the Garrett Corporation
Get access Rights & Permissions [Opens in a new window]

Extract

Your President and Mr. B. D. Blackwell of the Rolls-Royce company were brash enough to have suggested that I present the Halford Memorial Lecture. And 1 fear that I was impetuous in having accepted. I am sorry that I did not know Major Frank Halford, but from what I have read and from those with whom I have discussed his achievements, he was indeed a leader, an engineer, a designer, a man of much foresight, without whom our world of air transport would not have progressed so far. I know he would have been interested in the engine design trends which form the subject of my discussion—The Development of Small Gas Turbines for Aircraft Auxiliary Power.

Type
Tenth Halford Memorial Lecture
Information
The Aeronautical Journal , Volume 74 , Issue 718 , October 1970 , pp. 797 - 805
Copyright
Copyright © Royal Aeronautical Society 1970 

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. Arndt, W. E. Secondary Power Requirements of Large Transport Aircraft. SAE 680708. Presented at the Aeronautic and Space Engineering and Manufacturing Meeting, Los Angeles, California, 7th-11th October, 1968.Google Scholar
2. Dias, J. J. Gas Turbine Auxiliary Power Unit Noise and its Attenuation. SAE 670155. Presented at the Automotive Engineering Congress, Detroit, Michigan, 9th-13th January, 1967; Published in SAE Transactions, Vol. 76, 1968.Google Scholar
3. Keltto, H. S. Installation of the APU in the 747 Air plane. SAE 680709. Presented at the Aeronautic and Space Engineering and Manufacturing Meeting, Los Angeles, California, 7th-l 1th October, 1968.Google Scholar
4. Nicholls, B. H. and Meshew, A. D. Auxiliary Power Systems for 1975 Fighter Aircraft. SAE 680311. Presented at the Air Transport Meeting, New York, N.Y., 29th April-2nd May, 1968.Google Scholar