Samara University Repository
Welcome to the Samara University repository!
This is an open electronic archive created to preserve and disseminate the scientific results of our university. The works of researchers, faculty members, and students are available to everyone for academic and research purposes.
The repository contains dissertations, research articles, educational and methodological materials, monographs, and regulatory documents. The collections cover a wide range of fields: from aerospace technologies, engine engineering, and computer science to history, linguistics, mathematics, and ecology. The archive brings together the scientific heritage of the university, including materials prepared during the period of Samara State Aerospace University and Samara State University.
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Descriptions of all publications and articles available in the repository can be found in the libraryâs electronic catalog. Staff and students can log in via the menu "Login -> My Resource Archive" using their personal account credentials (SSAU_id).
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| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Черняев, А.И. | |
| dc.contributor.author | Трефилов, В.А. | |
| dc.date | 2016 | |
| dc.date.accessioned | 2025-08-22T12:22:00Z | - |
| dc.date.available | 2025-08-22T12:22:00Z | - |
| dc.date.issued | 2016 | |
| dc.identifier.identifier | Dspace\SGAU\20161108\59635 | |
| dc.identifier.citation | Материалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 2, с. 74-75 | |
| dc.identifier.isbn | 978-5-7883-1084-8 | |
| dc.identifier.uri | http://repo.ssau.ru/jspui/handle/123456789/14352 | - |
| dc.description | УДК 621.45.017 | |
| dc.description.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. | |
| dc.language | rus | |
| dc.publisher | Самарский университет | |
| dc.title | Определение показателей надёжности рабочих лопаток авиационного двигателя с помощью структурно-энергетической теории отказов | |
| dc.title.alternative | Application of structural power failure theory for determining the probability of failure and durability of turbine and compressor blades of aircraft engines | |
| dc.type | Article | |
| local.identifier.olduri | http://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Opredelenie-pokazatelei-nadezhnosti-rabochih-lopatok-aviacionnogo-dvigatelya-s-pomoshu-strukturnoenergeticheskoi-teorii-otkazov-59635 | |
| local.identifier.olduri | http://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Opredelenie-pokazatelei-nadezhnosti-rabochih-lopatok-aviacionnogo-dvigatelya-s-pomoshu-strukturnoenergeticheskoi-teorii-otkazov-59635 | |
| Appears in Collections: | Проблемы и перспективы развития двигателестроения | |
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