Enviar artigo por via de e-mail Automated Belt Grinding of Axial-Compressor Blades in Gas-Turbine Engines
- Autores: Poletaev V.A.1, Volkov D.I.1
-
Afiliações:
- Solov’ev Rybinsk State Aviation-Engineering University
- Edição: Volume 39, Nº 7 (2019)
- Páginas: 594-597
- Seção: Article
- URL: https://journals.rcsi.science/1068-798X/article/view/227753
- DOI: https://doi.org/10.3103/S1068798X19070177
- ID: 227753
Citar
Acesso aberto
Acesso está concedido
Somente assinantes
Resumo
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.
Sobre autores
V. Poletaev
Solov’ev Rybinsk State Aviation-Engineering University
Autor responsável pela correspondência
Email: poletaev@rsatu.ru
Rússia, Rybinsk
D. Volkov
Solov’ev Rybinsk State Aviation-Engineering University
Autor responsável pela correspondência
Email: prorectnir@rsatu.ru
Rússia, Rybinsk
Arquivos suplementares
