Email this article Concept of monitoring for thermostressed state and service life of aircraft gas turbine engine blades
- Authors: Kulikov G.G.1, Trushin V.A.1, Abdulnagimov A.I.1, Ganeev A.A.1
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Affiliations:
- Ufa State Aviation Technical University
- Issue: Vol 59, No 1 (2016)
- Pages: 77-83
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/229573
- DOI: https://doi.org/10.3103/S1068799816010128
- ID: 229573
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Abstract
A concept of monitoring for material properties with residual life estimation of rotor blades for gas turbine engines is proposed. The structure of on-board control and conditionmonitoring system based on the intelligent pyrometer module with the algorithm for calculating the residual life of turbine rotor blades is described.
About the authors
G. G. Kulikov
Ufa State Aviation Technical University
Author for correspondence.
Email: gennadyg_98@yahoo.com
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
V. A. Trushin
Ufa State Aviation Technical University
Email: gennadyg_98@yahoo.com
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
A. I. Abdulnagimov
Ufa State Aviation Technical University
Email: gennadyg_98@yahoo.com
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
A. A. Ganeev
Ufa State Aviation Technical University
Email: gennadyg_98@yahoo.com
Russian Federation, ul. Karla Marksa 12, Ufa, 450000
