Hostname: page-component-586b7cd67f-g8jcs Total loading time: 0 Render date: 2024-11-27T23:12:28.851Z Has data issue: false hasContentIssue false

The Design of Helicopter Powerplants

Published online by Cambridge University Press:  04 July 2016

H. C. Dabbadie*
Affiliation:
Turbomeca

Extract

Over the past twenty years a large part of the activity of Turbomeca has been directed first to the creation and next to the subsequent development of propulsion units for helicopters.

The use of the gas turbine brought with it a fundamental advantage—low specific weight which led to the exceptional expansion of this specialised branch of the aircraft industry, and without wishing to minimise the constant improvement of rotor systems, we believe that above all else the qualities of the engine have played a significant part in the success of this system of transport and in the more specific success of this or that particular helicopter.

Type
Rotorcraft Section
Copyright
Copyright © Royal Aeronautical Society 1971 

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

This lecture was given at a Rotorcraft Section half-day Symposium held on Thursday 15th January 1970.