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- Article name
- ON THE POSSIBILITIES OF EVALUATION OF THE STRESS-DEFORMED STATE OF ELEMENTS OF AVIATION GAS TURBINE ENGINE LASER OPTICAL-ACOUSTIC METHOD
- Authors
- Oleshko V. S., , ovs_mai@mail.ru, Moscow Aviation Institute (National Research University), Moscow, Russia
Karpenko O. N., , kaska79@yandex.ru, Military Educational-Scientific Center of Air Force "Air Force Academy named after professor N. E. Zhukovsky and Yu. A. Gagarin", Voronech, Russia
Popov A. V., , avpnil@rambler.ru, Military Educational-Scientific Center of Air Force "Air Force Academy named after professor N. E. Zhukovsky and Yu. A. Gagarin", Voronech, Russia
Lomonosov A. M., , lom@kapella.gpi.ru, Institute of General Physics named after A. M. Prokhorov, Russian Academy of Sciences, Moscow, Russia
- Keywords
- laser optical-acoustic method / surface acoustic wave / blade turbine engine / residual stresses
- Year
- 2014 Issue 3 Pages 36 - 41
- Code EDN
- Code DOI
- Abstract
- Possibility of the use of the laser generation of surface acoustic waves in the blades of aircraft gas turbine engines, registration, processing and analysis of the parameters of acoustic waves to assess the possibility of determination of residual stresses.
- Text
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