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F-14 Re-Engining With the F110 Engine PUBLIC ACCESS

[+] Author Affiliations
O. T. Castells

General Electric Company, Evendale, OH

J. T. Strong, Jr.

Grumman Aerospace Corporation, Bethpage, NY

Paper No. 85-GT-184, pp. V001T01A004; 8 pages
doi:10.1115/85-GT-184
From:
  • ASME 1985 International Gas Turbine Conference and Exhibit
  • Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery
  • Houston, Texas, USA, March 18–21, 1985
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7938-2
  • Copyright © 1985 by ASME

abstract

The advantages of re-engining the F-14 aircraft with the F110 engine is presented. The areas of improvement and the engine development philosophy are explained. A summary description of the pertinent engine design features of the F110 are presented. The flight test results on inlet/engine compatability, afterburner operation, airplane performance, and maintainability/reliability/durability are interpreted. Finally, a description of the proposed version of the F110 engine for the F-14 is presented.

Copyright © 1985 by ASME
Topics: Engines
This article is only available in the PDF format.

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