Automated Belt Grinding of Axial-Compressor Blades in Gas-Turbine Engines
- 作者: Poletaev V.A.1, Volkov D.I.1
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隶属关系:
- Solov’ev Rybinsk State Aviation-Engineering University
- 期: 卷 39, 编号 7 (2019)
- 页面: 594-597
- 栏目: Article
- URL: https://journals.rcsi.science/1068-798X/article/view/227753
- DOI: https://doi.org/10.3103/S1068798X19070177
- ID: 227753
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详细
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.
作者简介
V. Poletaev
Solov’ev Rybinsk State Aviation-Engineering University
编辑信件的主要联系方式.
Email: poletaev@rsatu.ru
俄罗斯联邦, Rybinsk
D. Volkov
Solov’ev Rybinsk State Aviation-Engineering University
编辑信件的主要联系方式.
Email: prorectnir@rsatu.ru
俄罗斯联邦, Rybinsk
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