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An Approach to Selecting Gas Turbine Engine Ratings for Fixed Wing Airplanes PUBLIC ACCESS

[+] Author Affiliations
R. K. Agrawal

P&WC

Paper No. 84-GT-163, pp. V002T02A003; 5 pages
doi:10.1115/84-GT-163
From:
  • ASME 1984 International Gas Turbine Conference and Exhibit
  • Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery
  • Amsterdam, The Netherlands, June 4–7, 1984
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7947-4
  • Copyright © 1984 by ASME

abstract

This paper presents an approach to selecting the various ratings for Gas Turbine engines in the fixed wing airplane application. The approach followed is first to estimate the minimum airplane power demands to pass its certification requirements under worst operating conditions. These power demands are then checked against those available from the engine within its certification requirements. Meaningful trade off studies, involving both the airplane and engine designers, can thus be conducted fairly early on in the airplane/engine design cycle to arrive at engine rating’s which will best suit both the vehicle and its power plant within their respective certification constraints.

Copyright © 1984 by ASME
This article is only available in the PDF format.

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