Hostname: page-component-cd9895bd7-q99xh Total loading time: 0 Render date: 2024-12-26T06:03:55.490Z Has data issue: false hasContentIssue false
  • English
  • Français

A family of small low cost gas turbines for unmanned vehicle systems

Published online by Cambridge University Press:  04 July 2016

R. W. Chevis  and
I. J. Grant
R. W. Chevis
Affiliation:
Noel Penny Turbines Ltd, Coventry
I. J. Grant
Affiliation:
Noel Penny Turbines Ltd, Coventry
Get access Rights & Permissions [Opens in a new window]

Extract

Noel Penny Turbines Ltd (NPT) is progressively extending its family of low cost turbojet and turboshaft engines for application to unmanned vehicle systems (UVS). The family now incorporates eight distinct engine types, spanning a jet range of 50 to 1200 Ibf sea level static thrust and a turboprop/ turboshaft range of 15 to 450 SHP. The scope of these basic engines enables a wide variety of application and installational requirements to be covered. The crucial first target is low manufacturing cost.

The object of this paper is to introduce this UVS engine family and highlight highly significant design and development features necessary to meet both operational requirements and low cost.

Type
Research Article
Information
The Aeronautical Journal , Volume 87 , Issue 866 , July 1983 , pp. 199 - 209
Copyright
Copyright © Royal Aeronautical Society 1983 

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. Taylor, J. W. R. and Munson, K. Jane's Pocket Book of Remotely Piloted Vehicles. Collier Books, 1977.Google Scholar
2. Technical Committee of Association for Unmanned Vehicle Systems, AUVS. Progress in Unmanned Vehicle Systems. 1982.Google Scholar
3. Chevis, R. W. Advanced Developments in Turbomachinery for use in Small RPV Engines. First Bristol International Conference on Remotely Piloted Vehicles, 1979.Google Scholar
4. Chevis, R. W. and Varley, R. J. Centrifugal Compressors for Small Aero and Automotive Gas Turbine Engines. AGARD Conference Proceedings No. 282, Centrifugal Compressors, Flow Phenomena and Performance. 1980.Google Scholar
5. Chevis, R. W. Design and Test of two 8:1 Pressure Ratio Single Stage Centrifugal Compressors of Different Flow Size. International Symposium on Centrifugal Compressors. Canadian Aeronautics and Space Institute. Toronto, May 1982.Google Scholar