小型无人机复合材料机身壁板与梁整体制造工艺

通过介绍无人机复合材料机身的结构特点、传统制造工艺方法以及工艺所存在的诸多问题，介绍了一种中小型无人机机身复合材料整体压力垫的制造工艺，以及复合材料蜂窝夹芯板件与梁整体共固化的工艺过程，可以用于典型的梁框蜂窝夹芯结构的整体制造。结果表明，通过与传统工艺对比，可以降低无人机的生产成本，提高复合材料制件的表面质量，缩短零部件生产周期。

Co-curing Manufacturing Process for Composite Fuselage and Beam of Small-sized Unmanned Aerial Vehicles

This paper introduced the fuselage structure and traditional manufacturing process of unmanned aerial vehicle (UAV) as well as the problems appearing in the processing procedure. Furthermore, this paper also introduced a pressure-pad manufacturing process for the small-sized UAV and a co-curing process for the composite honeycomb sandwich plate with a load beam, which could be applied in the manufacture of the frame-beam honeycomb sandwich structure. Compared to the traditional process, this method can reduce the manufacture cost, improve the surface quality of composite parts and shorten the manufacture cycle of UAV.