Комплексная фрактодиагностика флаттера рабочего колеса вентилятора

Сачин В. М.; V. M. Sachin; Туманов Н. В.; N. V. Tumanov; Лаврентьева М. А.; M. A. Lavrentyeva; Черкасова С. А.; S. A. Cherkasova

doi:10.18287/2541-7533-2011-0-3-2(27)-185-194

Complex failure analysis of aero engine compressor blades

Authors: Sachin V.M.¹, Tumanov N.V.¹, Lavrentyeva M.A.¹, Cherkasova S.A.¹
Affiliations:
1. Central Institute of Aviation Motors
Issue: Vol 10, No 3-2 (2011): Special Issue
Pages: 185-194
Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
URL: https://journals.ssau.ru/vestnik/article/view/6805
DOI: https://doi.org/10.18287/2541-7533-2011-0-3-2(27)-185-194
ID: 6805

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Abstract

Techniques for blade flutter diagnostics using stationary transducers and microfractographic observations are presented. Both these methods have been applied for compressor blade failure analysis of preproduction aero engines. As a result the cause and kinetics of the failures have been established.