The invention discloses a combined aircraft aerodynamic layout structure for cooperative tasks, and particularly relates to the field of overall design of aircrafts. The combined aircraft aerodynamic layout structure for the cooperative tasks comprises a main machine and two sub-machines, the main machine adopts the layout of a front rhombic wing and a rear sweep-forward wing, the two sub-machines are symmetrically distributed on the two sides of the main machine, each sub-machine is embedded between the rhombic wing and the sweep-forward wing of the main machine, and the main machine and the two sub-machines have a complete flying wing layout in a combined state. By the adoption of the technical scheme, the problem that gravity center change and pneumatic center change are caused by neutron machine separation of an existing combined aircraft is solved, and different flight task requirements can be met.
本发明专利公开了一种面向协同任务的组合飞行器气动布局结构,具体涉及航空器总体设计领域。一种面向协同任务的组合飞行器气动布局结构,包括主机和两个子机,所述主机采用前部菱形翼、后部前掠翼的布局,两个所述子机对称分布在主机的两侧,每个所述子机均嵌合在主机的菱形翼和前掠翼之间,所述主机和两个子机处于组合状态下具有完整的飞翼布局。采用本发明技术方案解决了现有的组合飞行器中子机分离会带来重心变化与气动中心变化的问题,可满足不同的飞行任务需求。
Combined aircraft aerodynamic layout structure for cooperative tasks
一种面向协同任务的组合飞行器气动布局结构
2022-01-14
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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