The invention discloses a carbon fiber flapping wing aircraft easy to disassemble and assemble. The carbon fiber flapping wing aircraft comprises a rack, a driving unit, a wing unit and a direction control unit; the rack comprises an upper framework and a lower framework which are arranged in parallel, the front ends of the upper framework and the lower framework are connected with the upper end and the lower end of the head support, the upper framework is longer than the lower framework, and the tail end of the upper framework is connected with a tail rod; the wing unit comprises a front flapping wing module and a rear flapping wing module, and the direction control unit comprises a front wing direction control module and a rear wing direction control module; and the front flapping wing module, the front wing direction control module, the driving unit, the rear flapping wing module and the rear wing direction control module are sequentially arranged between the upper framework and thelower framework from front to back. During assembly, the positions of all parts can be adjusted more conveniently, and the running smoothness of the whole aircraft is guaranteed; and in addition, parts can be quickly replaced under the condition of falling and breaking.
本发明公开了一种易拆装的碳纤维扑翼飞行器,包括机架、驱动单元、机翼单元及方向控制单元;所述机架包括平行设置的上、下两根骨架,上、下两根骨架的前端连接头部支架的上下两端,上骨架长于下骨架且末端连接有尾杆;所述机翼单元包括前扑翼模块与后扑翼模块,方向控制单元包括前翼方向控制模块与后翼方向控制模块;所述前扑翼模块、前翼方向控制模块、驱动单元、后扑翼模块及后翼方向控制模块从前向后依次排列设置于上骨架与下骨架之间。本发明组装时更加方便调节各零部件的位置,保证整个飞行器运行的流畅性;此外在摔坏的情况下,能够迅速的更换零件。
Carbon fiber flapping wing aircraft easy to disassemble and assemble
易拆装的碳纤维扑翼飞行器
26.06.2020
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |