The invention discloses a bionic flapping wing aircraft. The bionic flapping wing aircraft comprises a fuselage, wings, a flapping mechanism, a telescopic mechanism and a power source. The wings are rotatably installed on the two sides of the fuselage, the flapping mechanism is installed on the fuselage and is in transmission connection with the wings, the flapping mechanism is used for driving the wings to flap, the telescopic mechanism is installed on the fuselage and is in transmission connection with the wings, the telescopic mechanism is used for driving the wings to stretch out and draw back, and the power source is used for providing power for the flapping mechanism and the telescopic mechanism at the same time. The bionic flapping wing aircraft adopts a single power source to simultaneously drive the flapping mechanism and the telescoping mechanism, so that flapping and telescoping of the wings can be simultaneously performed, the coupling of flapping and telescoping is improved, the flapping mechanism and the telescoping mechanism are of mutually independent structures and are directly connected with the power source, and the flapping mechanism and the telescoping mechanism do not need to be assembled mutually, so that the cost is reduced. And the structural complexity of the aircraft is reduced.
本发明公开了一种仿生扑翼飞行器。该仿生扑翼飞行器包括机身、翼翅、扑动机构、伸缩机构、动力源。翼翅可转动地安装于机身的两侧,扑动机构安装于机身且与翼翅传动连接,扑动机构用于带动翼翅进行扑动,伸缩机构安装于机身且与翼翅传动连接,伸缩机构用于带动翼翅进行伸缩,动力源用于同时向扑动机构和伸缩机构提供动力。该仿生扑翼飞行器采用单一动力源同时驱动扑动机构、伸缩机构,使得翼翅的扑动和伸缩可以同时进行,提升了扑动和伸缩的耦合性,扑动机构和伸缩机构相互独立的结构且均直接连接动力源,两者不需要进行互相装配,降低了飞行器的结构复杂度。
Bionic flapping wing aircraft
仿生扑翼飞行器
2024-02-27
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Bionic flapping wing system and bionic flapping wing robot
European Patent Office | 2020
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