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针对目前市场对飞行器在垂直起降、悬浮工作和稳定飞行等方面的需求,提出并设计了一种新型飞翼飞行器。使其既具有飞翼飞行器翼身融合所带来的各种优点,同时又可以像旋翼机一样实现悬浮起降。利用CATIA对飞行器翼型、旋翼机构、螺旋桨等具体结构进行详细设计。并利用Fluent对飞行器在飞行状态下的机身流场进行分析和优化。同时根据新型飞翼飞行器的结构特点为飞行器设计飞行控制原理。为新型飞翼飞行器的制造提供完整的可行性方案。
In view of the current market demand for aircraft in vertical takeoff and landing, suspension work and steady flight, a new type of flying wing aircraft is proposed and designed. So that it not only has the advantages of wing-wing aircraft fuselage fusion, but also can be the same as the rotorcraft to achieve suspension. The CATIA is used to design the detailed structure of aircraft airfoil, rotorcraft and propeller. And use Fluent to analyze and optimize the fuselage flow field in the flight state of the aircraft. At the same time, the flight control principle is designed for the aircraft according to the structural characteristics of the new flying wing aircraft. For the new wing aircraft manufacturing to provide a complete feasibility program.