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Model operation of permanent deformation on the surface of the gas-turbine engine blades and determination of blade deformation after removal the surface with tempers
- Authors: 1 11, 1 11, 1 11, 1 11
-
Affiliations:
- Samara State Aerospace University
- Issue: Vol 5, No 2-1 (2006): Special Issue
- Pages: 94-98
- Section: TECHNICAL SCIENCES
- URL: https://journals.ssau.ru/vestnik/article/view/306
- DOI: https://doi.org/10.18287/2541-7533-2006-0-2-1(10)-94-98
- ID: 306
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Abstract
The article is devoted to the actual problem of the up-to-date aviation propulsion engineering – the problem of occurrence of permanent deformation on the surface of the blades of gas-turbine engine. In the article the results of the development work creation models, which permit to discount the permanent deformation during the operation designing electrochemical processing (ECM) and allow reducing time of the lapping operation. Areas of use this models are discussed.
About the authors
1 1
Samara State Aerospace University
Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation
1 1
Samara State Aerospace University
Email: sadohina@ssau.ru
Russian Federation
1 1
Samara State Aerospace University
Email: sadohina@ssau.ru
Russian Federation
1 1
Samara State Aerospace University
Email: sadohina@ssau.ru
Russian Federation
References
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- Басов К.А. ANSYS в примерах и задачах, Изд.: Компьютер-Пресс, 2002, 224 с.
- Каплун А.Б., Морозов Е.М., Олферьева М.А. ANSYS в руках инженера. Практическое руководство. Изд.: Едиториал УРСС, 2003, 272 с.
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