Automated Manufacture of Blades for Gas-Turbine Engines


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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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