Оptimization of gas turbine aircraft engine control throughout the engine service life

Оptimization of gas turbine aircraft engine control throughout the engine service life

The task of optimizing control methods in order to maintain key performance parameters of a gas turbine engine throughout the engine service life is considered. Variations in the performance characteristics of engine components in the process of operation are analyzed. To study the effect of deterio...

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Bibliographic Details
Main Authors: O. S. Gurevich, F. D. Golberg, S. A. Smetanin, M. E. Trifonov
Format: Article
Language:English
Published: Samara National Research University 2018-12-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
gas turbine engine
engine control system
compressor
deterioration
performance
on-board engine mathematical model
thrust
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/6379/6260

Internet

https://journals.ssau.ru/vestnik/article/viewFile/6379/6260

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