Gas Turbines For Helicopters

Author:

Morley A. W.

Abstract

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.

Publisher

Cambridge University Press (CUP)

Reference15 articles.

1. The Pressure Jet Helicopter

2. Boost Systems for Helicopter Gas Turbines;Morley;Journal of the Helicopter Association of Great Britain,1958

3. The Napier Oryx;Flight,1955

4. The Hunting Percival;Flight,1955

5. The Giant Helicopter;Fitzwilliams;Journal of the. Helicopter Association of Great Britain,1952

Cited by 2 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. High Performance Turbine Engines;The Journal of the Royal Aeronautical Society;1962-09

2. Some Design Aspects of Tandem Rotor Helicopters;The Journal of the Helicopter Association of Great Britain;1959-10

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