Automated Manufacture of Blades for Gas-Turbine Engines
- Authors: Poletaev V.A.1, Tsvetkov E.V.2, Uryadysheva A.M.1
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Affiliations:
- Solov’ev Rybinsk State Aviation-Engineering University
- PAO UDK-Saturn
- Issue: Vol 39, No 7 (2019)
- Pages: 598-601
- Section: Article
- URL: https://journal-vniispk.ru/1068-798X/article/view/227754
- DOI: https://doi.org/10.3103/S1068798X19070189
- ID: 227754
Cite item
Abstract
A new method is proposed for manufacturing the external contour of turbine blades, by means of a single coordinate system, without changing the technological bases or repositioning the workpiece. A specially designed multifunctional machine permits machining of the turbine blades and their preliminary orientation in the coordinate system.
About the authors
V. A. Poletaev
Solov’ev Rybinsk State Aviation-Engineering University
Author for correspondence.
Email: poletaev@rsatu.ru
Russian Federation, Rybinsk
E. V. Tsvetkov
PAO UDK-Saturn
Author for correspondence.
Email: egor.tsvetkov@uec-saturn.ru
Russian Federation, Rybinsk
A. M. Uryadysheva
Solov’ev Rybinsk State Aviation-Engineering University
Email: egor.tsvetkov@uec-saturn.ru
Russian Federation, Rybinsk
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