Automated manufacture of compressor-blade tailpieces
- Authors: Poletaev V.A.1, Tsvetkov E.V.1
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Affiliations:
- Solov’ev Rybinsk Aviation-Engineering University
- Issue: Vol 36, No 1 (2016)
- Pages: 74-76
- Section: Article
- URL: https://journal-vniispk.ru/1068-798X/article/view/225995
- DOI: https://doi.org/10.3103/S1068798X16010172
- ID: 225995
Cite item
Abstract
An effective method of machining the geometrically complex surfaces of compressor blades in gas-turbine engines is considered (creep-feed grinding). This method is widely used in the machining of hard materials such as high-temperature nickel alloys and cobalt alloys employed in the manufacture of gas-turbine components.
Keywords
About the authors
V. A. Poletaev
Solov’ev Rybinsk Aviation-Engineering University
Author for correspondence.
Email: poletaev@rgata.ru
Russian Federation, Rybinsk
E. V. Tsvetkov
Solov’ev Rybinsk Aviation-Engineering University
Email: poletaev@rgata.ru
Russian Federation, Rybinsk
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