Technological design of carbon fiber parts with a complex geometric shape for unmanned aerial vehicles
https://doi.org/10.35164/0554-2901-2022-11-12-36-39
Abstract
In this paper, the process of technological design of small-sized carbon fiber parts with complex geometry used in the design of unmanned aerial vehicles is considered. Approaches to the placement of splicing points in preform layers are presented. Regularities have been established that relate the number and location of splicing points in the reinforcing layers of carbon fiber reinforced composite and its mechanical characteristics.
About the Authors
V. V. Sokolov
JSC «Kronshtadt»
Russian Federation
Russian Federation
Moscow
Z. V. Agashina
JSC «Kronshtadt»
Russian Federation
Russian Federation
Moscow
S. I. Voinov
JSC «Kronshtadt»
Russian Federation
Russian Federation
Moscow
P. Y. Antipov
JSC «Kronshtadt»
Russian Federation
Russian Federation
Moscow
O. A. Golishev
JSC «Kronshtadt»
Russian Federation
Russian Federation
Moscow
S. V. Dolinsky
JSC «Kronshtadt»
Russian Federation
Russian Federation
Moscow
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Review
For citations:
Sokolov V.V., Agashina Z.V., Voinov S.I., Antipov P.Y., Golishev O.A., Dolinsky S.V. Technological design of carbon fiber parts with a complex geometric shape for unmanned aerial vehicles. Plasticheskie massy. 2022;(11-12):36-39. (In Russ.) https://doi.org/10.35164/0554-2901-2022-11-12-36-39
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