A method for calculating the parameters for manufacturing preforms via radial braiding


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Abstract

Technology for manufacturing preforms for tubular components from composite materials for aerospace engineering by radial braiding has been considered. A method has been proposed for determining the parameters of the preforms and the process variables to manufacture them. The method insures the specified thermomechanical characteristics of the composite structure.

About the authors

S. A. Samipour

Tupolev National Research Technical University

Author for correspondence.
Email: samipour@mail.ru
Russian Federation, Kazan, Republic of Tatarstan, 420011

V. I. Khaliulin

Tupolev National Research Technical University

Email: samipour@mail.ru
Russian Federation, Kazan, Republic of Tatarstan, 420011

V. V. Batrakov

Tupolev National Research Technical University

Email: samipour@mail.ru
Russian Federation, Kazan, Republic of Tatarstan, 420011


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