Аuthors
Volkov A. A.*,
Sokolova A. S.**,
Druzhkova Y. A.***
,
*e-mail: aa.volkov@uec-kuznetsov.ru
**e-mail: aleksandrasokolova2@gmail.com
***e-mail: yuliadruzhkova00@gmail.com
Abstract
An overview of existing methods for constructing the profile of an axial turbine blade is presented, their advantages and disadvantages are noted. An algorithm for building a profile is given for some of the methods. The existing methods of profile construction are based on 5 control points and tangents in them. The method of forming the profile of an axial turbine blade is considered. The proposed method is based on the introduction of a new geometric parameter – the angle of bending of the leading edge. The use of this parameter in conjunction with generally recognized profile parameters allows you to uniquely determine the profile geometry. It’s shown that the developed method allows flexibly controlling the distribution of curvature of the backrest and trough of the profile for the specified geometric parameters of the profile.
Keywords:
blade profile, turbine, turbine grid, profile construction method, profile parameters, rational Bezier curve, profile curvature
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