Computer-aided system of virtual gas turbine engine testing
- Authors: Tkachenko A.Y.1, Rybakov V.N.1, Krupenich I.N.1, Ostapuk Y.A.1, Filinov E.P.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 13, No 5-3 (2014): Special Issue
- Pages: 113-119
- Section: ISSUE WITHOUT SECTION
- URL: https://journals.ssau.ru/vestnik/article/view/2549
- DOI: https://doi.org/10.18287/1998-6629-2014-0-5-3(47)-113-119
- ID: 2549
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Full Text
Abstract
The article describes the concept of a virtual lab that includes subsystem of gas turbine engine simulation, subsystem of experiment planning, subsystem of measurement errors simulation, subsystem of simulator identification and others. The basis for virtual lab development is the computer-aided system of thermogasdynamic research and analysis “ASTRA”. The features of gas turbine engine transient modes simulator are described. The principal difference between the simulators of transient and stationary modes of gas turbine engines is that the energy balance of the compressor and turbine becomes not applicable. The computer-aided system of virtual gas turbine engine testing was created using the developed transient modes simulator. This system solves the tasks of operational (throttling, speed, climatic, altitude) characteristics calculation, analysis of transient dynamics and selection of optimal control laws. Besides, the system of virtual gas turbine engine testing is a clear demonstration of gas turbine engine working process and the regularities of engine elements collaboration. The interface of the system of virtual gas turbine engine testing is described in the article and some screenshots of the interface elements are provided. The developed system of virtual gas turbine engine testing provides means for reducing the laboriousness of gas turbine engines testing. Besides, the implementation of this system in the learning process allows the diversification of lab works and therefore improve the quality of training.
About the authors
A. Yu. Tkachenko
Samara State Aerospace University
Author for correspondence.
Email: tau@ssau.ru
Candidate of Science (Engineering)
Associate professor at Department of Theory of Aircraft Engine
Russian FederationV. N. Rybakov
Samara State Aerospace University
Email: viktor.rybakov@gmail.com
Candidate of Science (Engineering)
Lecturer at Department of Theory of Aircraft Engine
Russian FederationI. N. Krupenich
Samara State Aerospace University
Email: kru@ssau.ru
Candidate of Science (Engineering)
Associate professor at Department of Theory of Aircraft Engine
Russian FederationYa. A. Ostapuk
Samara State Aerospace University
Email: oya92@mail.ru
Student
Russian FederationE. P. Filinov
Samara State Aerospace University
Email: filinov.evg@gmail.com
Student
Russian FederationReferences
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