Automated Belt Grinding of Axial-Compressor Blades in Gas-Turbine Engines


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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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