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Development of the Technology of Manufacturing Aerospace Composite Tubular Elements by Radial Braiding

  • S. A. Samipour
  • V. I. Khaliulin
  • V. V. Batrakov
New Technologies in Mechanical Engineering

Abstract

A technology for manufacturing a preform for aerospace composite tubular elements by radial weaving is considered. The procedure for selecting the material, the algorithm for determining the preform parameters, and the process of manufacturing and maintaining the accuracy of the reinforcing angle, which are proposed in this study, allow the required thermomechanical characteristics of the composite structure to be achieved.

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References

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    Samipur, S.A. and Danilov, Ya.S., Development and verification of an analytic technique to determine the stiffness parameters of braided tubular parts, Russ. Aeronaut., 2016, vol. 59, no. 4, pp. 460–465.Google Scholar
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    Samipour, S.A., Khaliulin, V.I., and Batrakov, V.V., A method for calculating the parameters for manufacturing preforms via radial braiding, J. Mach. Manuf. Reliab., 2017, vol. 46, no. 3, pp. 302–308.CrossRefGoogle Scholar

Copyright information

© Allerton Press, Inc. 2018

Authors and Affiliations

  • S. A. Samipour
    • 1
  • V. I. Khaliulin
    • 1
  • V. V. Batrakov
    • 1
  1. 1.Tupolev Kazan National Research Technical UniversityKazanRussia

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