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

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.