The multi-degree-of-freedom ornithopter comprises a nose, a fuselage, a left wing, a right wing and an empennage, the machine head is located at the front end of the machine body and is of a box type structure, the interior of the machine head is divided into a speed reduction chamber and a transmission chamber from front to back, the speed reduction chamber and the transmission chamber are separated through a partition plate, a speed reduction mechanism is arranged in the speed reduction chamber, and a transmission mechanism is arranged in the transmission chamber. A flapping wing driving motor is fixedly mounted at the front end of the nose and is connected with the transmission mechanism through a speed reducing mechanism; the left wing and the right wing are distributed on the two sides of the nose in a mirror symmetry mode and connected with the transmission mechanism, and a first electromagnetic type torsion driving joint is arranged between the left wing and the transmission mechanism. A second electromagnetic torsion driving joint is arranged between the right wing and the transmission mechanism; a wing flapping amplitude adjusting mechanism is arranged between the transmission mechanism and the nose box body; the empennage is located at the rear end of the fuselage, and an empennage attitude adjusting executing mechanism is arranged between the empennage and the fuselage.
一种扑动幅度可调式多自由度扑翼飞行器,包括机头、机身、左机翼、右机翼及尾翼;机头位于机身前端,机头采用箱式结构,在机头内部由前至后分为减速室和传动室,减速室和传动室之间由隔板隔开,在减速室内设置有减速机构,在传动室内设有传动机构;在机头前端固定安装有扑翼驱动电机,扑翼驱动电机通过减速机构与传动机构相连;左机翼和右机翼镜像对称分布在机头两侧,左机翼和右机翼均与传动机构相连,在左机翼与传动机构之间设置有第一电磁式扭转驱动关节;在右机翼与传动机构之间设置有第二电磁式扭转驱动关节;在传动机构与机头箱体之间设置有机翼扑动幅度调节机构;尾翼位于机身后端,在尾翼与机身之间设置有尾翼调姿执行机构。
Multi-degree-of-freedom ornithopter with adjustable flapping amplitude
一种扑动幅度可调式多自由度扑翼飞行器
2024-12-27
Patent
Electronic Resource
Chinese
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