DEVELOPMENT OF A COMPLEX OF FUNCTIONAL MODELS FOR THE PROCESS OF CONTROL AND DIAGNOSTICS OF THE TV3-117 AIRCRAFT ENGINE TECHNICAL STATE AT FLIGHT MODES
DOI:
https://doi.org/10.18372/2306-1472.81.14597Keywords:
aircraft engine, IDEF technologies, functional models, system analysisAbstract
Purpose: The purpose of this article is to develop a set of functional models for control and diagnostics of TV3-117 aircraft engine technical state in flight modes based on IDEF0 notation. Methods: The article applies the system modeling method at the stage of designing an information system for control and diagnostics of the TV3-117 aircraft engine technical state in flight modes. Results: An approach is proposed to formalize the processes of information control and diagnostics of the TV3-117 aircraft engine technical state in flight modes based on the methodology of system analysis and IDEF-technologies. A set of functional models for the control and diagnostics of the TV3-117 aircraft engine technical state in flight modes based on IDEF0 technology has been developed, which made it possible to single out the optimization problem and formulate the requirements for its implementation as part of the expert system. Discussion: The results obtained are applied within the framework of the concept of intellectualizing the process of control and diagnostics of the TV3-117 aircraft engine technical state in flight modes, one of the points of which is the intellectual processing and storage of information about the results of flight tests and operation of the TV3-117 aircraft engine based on the requirements of modern databases and knowledge bases, with the possibility of their integration into modern CASE-technologies.
References
Pashayev A.M., Askerov D.D., Ardil C., Sadiqov R.A. and Abdullayev P.S. (2007). Complex Condition Monitoring System of Aircraft Gas Turbine Engine, International Journal of Aerospace and Mechanical Engineering, vol. 1, no. 11, pp. 689-695.
Ntantis E.L. and Botsaris P.N. (2015). Diagnostic Methods for an Aircraft Engine Performance, Journal of Engineering Science and Technology, vol. 8(4), pp. 64-72. https://doi.org/10.25103/jestr.084.10
Vasiliev V.I. and Gernakov S.V. (2003). Ekspertnye systemi: Upravlenie ekspuatatsiey slozhnih tehnicheskih obektov [Expert systems: Management of operation of complex technical objects]. Ufa, Ufa State Aviation Technical University, 106 p. (in Russian)
Kalyanov G.P. (2013). Metodika obosnovaniya vibora CASE-sredstv dlya analiza s proektirovaniya system upravleniya predpriyatiem [The method of substantiating the choice of CASE-tools for the analysis and design of enterprise management systems], Innovations, no. 10 (180), pp. 112-122. (in Russian)
Gernakov S.V. (2001). Intellektualnyiy monitoring parametrov gazoturbinnyih dvigateley aktivnyimi ekspertnyimi sistemami [Intelligent monitoring of parameters of gas turbine engines by active expert systems], Automation and modern technologies, no. 11, pp. 10-15. (in Russian)
Vasiliev V.I. and Gernakov S.V. (2006). Kontrol i diagnostika tehnicheskogo sostoyaniya aviatsionnyih dvigateley na osnove intellektualnogo analiza dannyih [Control and diagnostics of aircraft engines technical condition on the basis of data mining], Bulletin of the Ufa State Aviation Technical University, vol. 7, no.2 (15), pp. 71-81. (in Russian)
Ntantis E.L. and Li Y.G. (2013). The impact of measurement noise in GPA diagnostics analysis of a gas turbine engine, International Journal of Turbo & Jet Engine, vol. 30 (4), pp. 401-408. https://doi.org/10.1515/tjj-2013-0024
Sarkar S., Mukherjee K., Ray A., Yasar M. (2008). Fault diagnosis and isolation in aircraft gas turbine engines, 2008 American Control Conference, Westin Seattle Hotel, Seattle, Washington, USA June 11-13, 2008, pp. 2166-2171. https://doi.org/10.1109/ACC.2008.4586813
Song J., Liu Y. and Yu Y. (2012). Numerical Analysis of Transmission Line Telegraph Equation Based on FDTD Method, Journal of Convergence Information Technology (JCIT), vol. 7, no. 20, pp. 258-265.
https://doi.org/10.4156/jcit.vol7.issue20.31
Vladov, S., Shmelov, Y., Pylypenko, L., Kotliarov, K., Hrybanova, S. and Husarova, O. (2019). Rozrobka informatsiinoi ta dynamichnoi modelei kontroliu i diahnostyky tekhnichnoho stanu aviatsiinoho dvyhuna TV3-117 [Research of information and dynamic models of control and diagnostics of TV3-117 aircraft engine technical state], Innovative Technologies and Scientific Solutions for Industries, no. 4 (10), pp. 44-54.