The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a high-speed single aircraft and a combined unmanned aerial vehicle. The aircraft is composed of a front fuselage, supports, duct bodies, wings, ailerons, empennages, control surfaces, propellers, motors, flow deflectors and a rear fuselage. The front fuselage is connected to the duct body through the support, the wings are installed on the two sides of the duct body, ailerons are arranged on the wings, the motors are fixedly installed at the tail of the front fuselage, the propellers are installed on the motors, flow deflectors are arranged at the tail of the duct body, the rear fuselage is connected with the duct body through the flow deflectors, the tail of the rear fuselage is connected with the empennage, and four sets of control surfaces are installed on the empennage. High-speed and low-speed use requirements are considered, and multiple bodies can be combined.
本发明属于无人机技术领域,尤其涉一种高速单体飞行器及组合式无人飞行器。所述飞行器由前机身、支架、涵道体、机翼、副翼、尾翼、舵面、螺旋桨、电动机、导流片、后机身组成;前机身通过支架连接在涵道体上,机翼安装在涵道体两侧,机翼上设置有副翼,电动机固定安装在前机身尾部,螺旋桨安装在电动机上,涵道体尾部设置有导流片,后机身通过导流片与涵道体连接,后机身尾部连接尾翼,尾翼上安装四组舵面,兼顾高速、低速使用需求,且可以多体组合。
High-speed single aircraft and combined unmanned aircraft
一种高速单体飞行器及组合式无人飞行器
2025-02-28
Patent
Electronic Resource
Chinese
IPC: | B64U |
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