| Title: | Определение показателей надёжности рабочих лопаток авиационного двигателя с помощью структурно-энергетической теории отказов |
| Other Titles: | Application of structural power failure theory for determining the probability of failure and durability of turbine and compressor blades of aircraft engines |
| Authors: | Черняев, А.И. Трефилов, В.А. |
| Issue Date: | 2016 |
| Publisher: | Самарский университет |
| Citation: | Материалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 2, с. 74-75 |
| Abstract: | The object of present work is to evaluate the probability of failure and durability of the aircraft engine compressor and turbine blades by structural power failure theory, based on the results of non-destructive testing and it comparison with the statistical information. For research has been prepared and remanufactured by laser, welding blades used in the fifth stage of high pressure compressor and turbine blades used in first, second and third stages of the aircraft engine. |
| Description: | УДК 621.45.017 |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/14352 |
| ISBN: | 978-5-7883-1084-8 |
| Appears in Collections: | Проблемы и перспективы развития двигателестроения |
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