The invention discloses a bionic butterfly aircraft and a design method thereof, and relates to the technical field of bionic aircrafts, the bionic butterfly aircraft comprises a driving system, wings, a control system and a power supply, the driving system is located at the head position of a bionic butterfly, the wings are arranged on the two sides of the driving system and are in transmission connection with the driving system, and the control system is electrically connected with the driving system; the control system and the driving system are both electrically connected with the power source, the wings comprise wing membranes and a plurality of wing veins, the wing veins are arranged on the wing membranes in a divergent mode, the gathering ends, close to each other, of the wing veins are arranged close to the driving system, and the gathering ends of the wing veins are in transmission connection with the driving system; the structure of the wings is simplified, the weight of the structure is reduced, the aerodynamic efficiency can be improved, the flight energy consumption is reduced, the endurance time is prolonged, and the flight flexibility is improved, so that the aircraft can be applied to the fields of military reconnaissance, environment monitoring and the like, and the application range of the bionic flapping-wing aircraft is expanded.
本发明公开一种仿生蝴蝶飞行器及其设计方法,涉及仿生飞行器技术领域,包括:驱动系统、翅膀、控制系统以及电源,驱动系统位于仿生蝴蝶头部位置,驱动系统的两侧均设置有翅膀,翅膀与驱动系统传动连接,控制系统与驱动系统电连接,控制系统与驱动系统均与电源电连接,翅膀包括翅膜以及多个翅脉,多个翅脉呈发散状设置在翅膜上,多个翅脉相互靠近的汇集端靠近驱动系统设置,多个翅脉的汇集端与驱动系统传动连接;本发明中简化了翅膀的结构,减轻结构的重量,可以提高气动效率,并减小飞行能耗,提高续航时间,同时提高飞行的灵活性,使得飞行器能够应用于军事侦察以及环境监测等领域,扩展了仿生扑翼飞行器的应用范围。
Bionic butterfly aircraft and design method thereof
一种仿生蝴蝶飞行器及其设计方法
2025-03-28
Patent
Electronic Resource
Chinese