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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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.
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Original Russian Text © S.A. Samipour, V.I. Khaliulin, V.V. Batrakov, 2018, published in Problemy Mashinostroeniya i Nadezhnosti Mashin, 2018, No. 3, pp. 90–95.
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Samipour, S.A., Khaliulin, V.I. & Batrakov, V.V. Development of the Technology of Manufacturing Aerospace Composite Tubular Elements by Radial Braiding. J. Mach. Manuf. Reliab. 47, 284–289 (2018). https://doi.org/10.3103/S1052618818030135
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DOI: https://doi.org/10.3103/S1052618818030135