The invention provides a flexible takeoff and landing mechanism of an ornithopter and the ornithopter. The flexible takeoff and landing mechanism comprises an assembling component; the driving assembly comprises a rotary driver and a linkage rod group, and the linkage rod group is connected with the rotary driver; the clamping assembly comprises two flexible grippers, and the two linkage rod sets are connected to the two flexible grippers correspondingly; and the impact sensor is connected to the assembling assembly and is in signal connection with the two driving assemblies, and the impact sensor is arranged between the two flexible grippers. The purpose of being stably connected to a special-shaped structure can be achieved, the use flexibility of the robot can be better improved so that the robot can adapt to more changeable operation environments, even if the robot is impacted, the robot can grab nearby structures nearby, and falling damage is avoided. Compared with related structures of conventional aircrafts at the present stage, the aircraft has the remarkable advantages of being high in automation degree, wide in application range, high in connection stability, controllable, high in flexibility, long in service life and the like, and a new thought is provided for development of aircraft structures.
本发明提供一种扑翼飞行器柔性起落机构及飞行器,其包括:装配组件;驱动组件,其包括旋转驱动器及连动杆组,连动杆组连接旋转驱动器;夹持组件,其包括两个柔性抓手,两个连动杆组分别连接于两个柔性抓手;撞击传感器,其连接于装配组件,且与两个驱动组件信号连接,撞击传感器设置于两个柔性抓手之间。本发明能够实现稳定连接于异形结构的目的,其能够更好地提升其使用灵活程度以适应更为多变的作业环境,即使在受到撞击时,其也能够就近抓取附近结构,避免发生坠落损伤。相比于现阶段常规飞行器相关结构来说,本申请兼具自动化程度高、使用范围广泛、连接稳定性强、可控请及灵活性高以及使用寿命长等显著优势,为飞行器结构的发展提供新思路。
Flexible takeoff and landing mechanism of ornithopter and ornithopter
一种扑翼飞行器柔性起落机构及飞行器
2025-02-11
Patent
Electronic Resource
Chinese
IPC: | B64U |