Abstract
In recent years, the development of UAV (Unmanned Aerial Vehicle) is rapid, but the development of structural design is slow, and the rack designed according to the experience of engineers still has great redundancy. With the rapid development of topology optimization and additive manufacturing, topology optimization design of integrated rack based on additive manufacturing is carried out. In the design process, manufacturing constraints are added and a variety of typical conditions to obtain the final optimization structure are considered. The influence of human empirical factors on the fuselage structure design is reduced scientifically and effectively by using this method. And the lightweight, topological and integrated design of the quadrotor frame is realized.
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