Technological design of carbon fiber parts with a complex geometric shape for unmanned aerial vehicles

V. V. Sokolov, Z. V. Agashina, S. I. Voinov, P. Y. Antipov, O. A. Golishev, S. Dolinsky
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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.
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无人机用复杂几何形状碳纤维零件工艺设计
本文研究了用于无人机设计的复杂几何形状的小尺寸碳纤维零件的工艺设计过程。提出了预制层中拼接点的布置方法。建立了碳纤维增强复合材料增强层中剪接点的数量和位置与其力学性能之间的规律。
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