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Power Level Influence on Architecture of Small Helicopter Turboshaft Engines FREE

[+] Author Affiliations
M. Giraud

Turboméca, Bordes, France

Paper No. 86-GT-191, pp. V002T02A013; 6 pages
doi:10.1115/86-GT-191
From:
  • ASME 1986 International Gas Turbine Conference and Exhibit
  • Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery
  • Dusseldorf, West Germany, June 8–12, 1986
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7929-0
  • Copyright © 1986 by ASME

abstract

In the field of helicopter turboshaft engines, TURBOMECA is present in the range of 400 to 1 600 kW with four new engines, all under development. Naturally all these engines, born of a same general philosophy, have a pronounced ≪family likeness≫ from the general mechanical and aerodynamic point of view.

Copyright © 1986 by ASME
Topics: Engines
This article is only available in the PDF format.

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