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Boost Systems for Helicopter Gas Turbines

Published online by Cambridge University Press:  26 October 2023

A W Morley*
Affiliation:
D Napier & Son Ltd

Extract

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The CHAIRMAN, in introducing the Author, said that Dr Morley had been for 16 years on the scientific staff of the Engine Department of the Royal Aircraft Establishment and, at the end of the war, was Deputy Head of the Gas Dynamics Division which subsequently became the Supersonics Division Three years after that he was senior lecturer of aircraft propulsion at Cranfield In his present position as Forward Projects Engineer for the Napier Company he was engaged on technical investigations into developments in aeronautics

The recent years have seen a tremendous increase in the importance of the helicopter both as a defence aircraft, for anti mine, anti submarine and assault purposes and as a civil transport between busy centres, and it has been overwhelmingly successful in a multitude of special duties from rescue work to crop spraying, some impossible with fixed wing aircraft The wider application of the helicopter in these many roles has directed increased attention towards the enhanced engine performance possible with the gas turbine, and to the more difficult problems of coupling the greater potential output of this form of engine with the inherent safety features of the aircraft

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1958

References

1 Saunders Roe Skeeter The Aeroplane, 14th September, 1956 Flight, 18th January, 1957Google Scholar
2 Apparatus for Warming Hydrogen Peroxide by its own Controlled Decomposition J G Tschinkel and A E Graves Jet Propulsion, July, 1957Google Scholar
3 Rotodyne Prelude Flight, 3rd May, 1957Google Scholar