Concept of monitoring for thermostressed state and service life of aircraft gas turbine engine blades
- 作者: Kulikov G.1, Trushin V.1, Abdulnagimov A.1, Ganeev A.1
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隶属关系:
- Ufa State Aviation Technical University
- 期: 卷 59, 编号 1 (2016)
- 页面: 77-83
- 栏目: 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
如何引用文章
详细
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.
作者简介
G. Kulikov
Ufa State Aviation Technical University
编辑信件的主要联系方式.
Email: gennadyg_98@yahoo.com
俄罗斯联邦, ul. Karla Marksa 12, Ufa, 450000
V. Trushin
Ufa State Aviation Technical University
Email: gennadyg_98@yahoo.com
俄罗斯联邦, ul. Karla Marksa 12, Ufa, 450000
A. Abdulnagimov
Ufa State Aviation Technical University
Email: gennadyg_98@yahoo.com
俄罗斯联邦, ul. Karla Marksa 12, Ufa, 450000
A. Ganeev
Ufa State Aviation Technical University
Email: gennadyg_98@yahoo.com
俄罗斯联邦, ul. Karla Marksa 12, Ufa, 450000