https://doi.org/10.1051/epjconf/201611402039
Diagnostics of gas turbines based on changes in thermodynamics parameters
1 Technical University in Košice, Department of Aviation Engineering, Rampová 7, 041 21 Košice, Slovak Republic
2 University of West Bohemia, Department of Power System Engineering, Univerzitní 8, 306 14 Pilsen, Czech Republic
a Corresponding author: marian.hocko@tuke.sk
Published online: 23 March 2016
This article is focused on solving the problems of determining the true state of gas turbine based on measured changes in thermodynamic parameters. Dependence between the real individual parts for gas turbines and changing the thermodynamic parameters were experimentally verified and confirmed on a small jet engine MPM-20 in the laboratory of the Department of Aviation Engineering at Technical University in Košice. The results of experiments confirm that the wear and tear of basic parts for gas turbines (turbo-compressor engines) to effect the change of thermodynamic parameters of the engine.
© Owned by the authors, published by EDP Sciences, 2016
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
