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About relaxational resistance of the compressor’s blades from titanium alloys
- Authors: Smyslov A.M.1, Smyslova M.K.1, Dubin A.I.2
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Affiliations:
- Ufa’s state aircraft technical univercity
- Ufa’s engine-building company
- Issue: Vol 10, No 3-2 (2011): Special Issue
- Pages: 227-232
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6814
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-2(27)-227-232
- ID: 6814
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Abstract
The questions of fatigue strength and surface parameters of the compressor’s blades gas-turbine’s engine (GTE) from titanium alloy VT6 investigation are considered. The complex vacuum-plasma treatment of the surface (CVPT) comparing with serial (base) technology is described. Recommendations for practice use of CVPT technology are given.
About the authors
A. M. Smyslov
Ufa’s state aircraft technical univercity
Author for correspondence.
Email: alexey.dubin@rambler.ru
Doctor of Engineering Science, professor
Russian FederationM. K. Smyslova
Ufa’s state aircraft technical univercity
Email: alexey.dubin@rambler.ru
Candidate of Engineering Science
Russian FederationA. I. Dubin
Ufa’s engine-building company
Email: alexey.dubin@rambler.ru
the manager of the laboratory
Russian FederationReferences
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