Study of mechanisms of low cycle fatigue crack propagation in aero engine disks under operating conditions and disk residual life estimation
- Authors: Tumanov N.V.1, Cherkasova S.A.1, Lavrentyeva M.A.1, Vorobyeva N.A.1
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Affiliations:
- Central Institute of Aviation Motors
- Issue: Vol 10, No 3-2 (2011): Special Issue
- Pages: 175-184
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6804
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-2(27)-175-184
- ID: 6804
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Abstract
Using microfractographic observations the mechanisms of low cycle fatigue crack kinetics in aero engine disks under operating conditions have been established. On this basis the techniques for disc residual life estimation have been developed. The techniques have been verified with the data of crack growth microfractographic reconstitution and crack kinetics direct observation on a disk surface.
About the authors
N. V. Tumanov
Central Institute of Aviation Motors
Author for correspondence.
Email: tumanov@rtc.ciam.ru
Candidate of Science (Engineering)
laboratory head
S. A. Cherkasova
Central Institute of Aviation Motors
Email: info@ciam.ru
leading designer
Russian FederationM. A. Lavrentyeva
Central Institute of Aviation Motors
Email: info@ciam.ru
leading designer
Russian FederationN. A. Vorobyeva
Central Institute of Aviation Motors
Email: info@ciam.ru
leading engineer
Russian Federation