Concept of monitoring for thermostressed state and service life of aircraft gas turbine engine blades
- Авторлар: Kulikov G.1, Trushin V.1, Abdulnagimov A.1, Ganeev A.1
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Мекемелер:
- Ufa State Aviation Technical University
- Шығарылым: Том 59, № 1 (2016)
- Беттер: 77-83
- Бөлім: 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
Дәйексөз келтіру
Аннотация
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.
Авторлар туралы
G. Kulikov
Ufa State Aviation Technical University
Хат алмасуға жауапты Автор.
Email: gennadyg_98@yahoo.com
Ресей, ul. Karla Marksa 12, Ufa, 450000
V. Trushin
Ufa State Aviation Technical University
Email: gennadyg_98@yahoo.com
Ресей, ul. Karla Marksa 12, Ufa, 450000
A. Abdulnagimov
Ufa State Aviation Technical University
Email: gennadyg_98@yahoo.com
Ресей, ul. Karla Marksa 12, Ufa, 450000
A. Ganeev
Ufa State Aviation Technical University
Email: gennadyg_98@yahoo.com
Ресей, ul. Karla Marksa 12, Ufa, 450000