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Increasing the reliability of aircraft components by regulating technological residual stress
- Authors: Kirpitchyov V.A.1, Vakulyuk V.S.1, Tchirkov A.V.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 8, No 1 (2009)
- Pages: 127-133
- Section: MECHANICAL ENGINEERING AND POWER ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/642
- DOI: https://doi.org/10.18287/2541-7533-2009-0-1(17)-127-133
- ID: 642
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Abstract
The paper shows the possibility of forecasting residual stressed state of component surface layer after strengthening and the optimization of strengthening effect. Methods of defining residual stress are developed and a theory of its influence on fatigue strength is proposed.
About the authors
V. A. Kirpitchyov
Samara State Aerospace University
Author for correspondence.
Email: dean_fla@ssau.ru
Russian Federation
V. S. Vakulyuk
Samara State Aerospace University
Email: dean_fla@ssau.ru
Russian Federation
A. V. Tchirkov
Samara State Aerospace University
Email: dean_fla@ssau.ru
Russian Federation
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