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An Adaptive Fuzzy Logic Algorithm for the Thrust Control of a Small Turbojet Engine

[+] Author Affiliations
Riccardo Amirante, Luciano Andrea Catalano, Paolo Tamburrano

Polytechnic of Bari, Bari, Italy

Paper No. GT2010-22510, pp. 369-377; 9 pages
doi:10.1115/GT2010-22510
From:
  • ASME Turbo Expo 2010: Power for Land, Sea, and Air
  • Volume 5: Industrial and Cogeneration; Microturbines and Small Turbomachinery; Oil and Gas Applications; Wind Turbine Technology
  • Glasgow, UK, June 14–18, 2010
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-4400-7 | eISBN: 978-0-7918-3872-3
  • Copyright © 2010 by ASME

abstract

This paper proposes a Fuzzy technique for the thrust control of small-scale turbo-jet engines, as an effective alternative to conventional PID techniques. Fuzzy rules have been preliminarly chosen and tuned so as to achieve rapidity and stability of response, as well as absence of overshoots, by simulating the transient operation of the Pegasus MK3 small-scale turbo-jet. Three experimental tests with large increases or decreases of set thrust have been carried out on the same engine: excellent results in terms of response speed, stability and absence of overshoots have been achieved. The proposed thrust control technique has general validity and can be applied to any small-scale turbojet engine, as well as to microturbines for electricity production, provided that thrust being substituted with the net mechanical power.

Copyright © 2010 by ASME

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