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Thermodynamic Multi-Criteria Optimization of the Unified Engine Core for the Line of Turbofan Engines

[+] Author Affiliations
Viktor N. Rybakov, Venedikt S. Kuz'michev, Andrey Y. Tkachenko, Ilia N. Krupenich

Samara State Aerospace University, Samara, Russia

Paper No. GT2016-57854, pp. V001T01A035; 6 pages
doi:10.1115/GT2016-57854
From:
  • ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition
  • Volume 1: Aircraft Engine; Fans and Blowers; Marine
  • Seoul, South Korea, June 13–17, 2016
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-4968-2
  • Copyright © 2016 by ASME

abstract

Although development of the line of gas turbine engines on the basis of a unified engine core is a widely used practice, the method of selection of the most efficient values of engine core parameters has virtually never been published.

The paper describes the method of optimization of values of engine core parameters jointly with optimization of values of every engine forming the line of engines developed on the basis of this core. Both stages of optimization are multi-objective and fulfilled using the results of simulation of engine as a subsystem of the airframe.

Copyright © 2016 by ASME

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