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Gas Turbines For Helicopters

Published online by Cambridge University Press:  04 July 2016

A. W. Morley*
Affiliation:
D. Napier and Son Limited

Extract

Rapid developments in the use of the helicopter were made in the Korean War. These were taking place at the time when there was considerable urge to introduce the gas turbine engine into the civil aircraft market. It was also a time when much effort was being expended on various forms of reaction propulsion, mostly for missiles. A number of new helicopter projects were started, taking advantage of the new knowledge in propulsion engineering; some utilised new gas turbine designs and others various forms of tip jet reaction. Liquid fuel rockets, ram-jets, pulse-jets and air pressure jets were tried. However, the main line of development continued to be the gradual improvement of direct mechanical drive.

Since Korea the natural trend has been first to convert existing helicopters to turbine engines. When new helicopters were designed wisdom dictated mechanical drive pending the gathering of sufficient experience with other forms of rotor power, and so far the accumulated knowledge of the mechanical drive has proved of greater value to helicopter progress than the potential advantages offered by the alternative engine forms.

Type
Aircraft Propulsion
Copyright
Copyright © Royal Aeronautical Society 1958

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References

1. Miller, R. H. (1953). Some Factors Affecting Helicopter Design and Future Operations. Fourth Anglo-American Aeronautical Conference, Royal Aeronautical Society, London, 1954.Google Scholar
2. Forsyth, A. Graham (1953). Power Plants for Rotary Wing Aircraft. Fourth Anglo-American Aeronautical Conference, Royal Aeronautical Society, London, 1954.Google Scholar
3. Morley, A. W. (1956). Some Helicopter Turbine Installations. Journal of the Helicopter Association of Great Britain, Vol. 9, No. 4, p. 429, May 1956.CrossRefGoogle Scholar
4. Fitzwilliams, O. L. L. (1952). The Giant Helicopter. Journal of the. Helicopter Association of Great Britain, Vol. 5, No. 4, p. 391, April 1952.CrossRefGoogle Scholar
5. Control System of the Lycoming T-53 Engine. Aviation Age, p. 27, October 1956.Google Scholar
6. Hafner, R. (1954). The Domain of the Helicopter. Journal of the Royal Aeronautical Society, March 1954.CrossRefGoogle Scholar
7. Rotary Wing Power. Flight, 12th March 1954.Google Scholar
8. Napier Gazelle Helicopter Turbine. The Aeroplane, 19th April 1957.Google Scholar
9. Brown, J. (1955). Some Applications of Gas Turbine to Helicopter Propulsion. Journal of the Helicopter Association of Great Britain, Vol. 8, No. 3, p. 87, January 1955.CrossRefGoogle Scholar
10. The Hunting Percival P.74. Flight, p. 938, 23rd December 1955.Google Scholar
11. The Napier Oryx. Flight, p. 189, 5th August 1955.Google Scholar
12. Rotodyne Report. Flight, p. 953, 20th December 1957.Google Scholar
13. New in the Westland Range (The Wessex). The Aeroplane, p. 807, 29th November 1957.Google Scholar
14. Morley, A. W. (1958). Boost Systems for Helicopter Gas Turbines. Journal of the Helicopter Association of Great Britain, Vol. 12, No. 2, p. 66, April 1958.CrossRefGoogle Scholar
15. Stepan, A. (1958). The Pressure Jet Helicopter. Journal of the Royal Aeronautical Society, February 1958.CrossRefGoogle Scholar