Email this article Automated Belt Grinding of Axial-Compressor Blades in Gas-Turbine Engines
- Authors: Poletaev V.A.1, Volkov D.I.1
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Affiliations:
- Solov’ev Rybinsk State Aviation-Engineering University
- Issue: Vol 39, No 7 (2019)
- Pages: 594-597
- Section: Article
- URL: https://journal-vniispk.ru/1068-798X/article/view/227753
- DOI: https://doi.org/10.3103/S1068798X19070177
- ID: 227753
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Abstract
The finishing of the flow sections of compressor blades is considered. A sequence of operations for this purpose in an automated cycle is proposed. The development of control programs for the grinding of flow sections of the blades is discussed, with allowance for the nonuniform distribution of the margin over the blade surface.
About the authors
V. A. Poletaev
Solov’ev Rybinsk State Aviation-Engineering University
Author for correspondence.
Email: poletaev@rsatu.ru
Russian Federation, Rybinsk
D. I. Volkov
Solov’ev Rybinsk State Aviation-Engineering University
Author for correspondence.
Email: prorectnir@rsatu.ru
Russian Federation, Rybinsk
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