The disclosure relates to an ornithopter. The ornithopter comprises a crank transmission assembly (100), a bracket (500), and a reinforcing plate (600). The crank transmission assembly (100) is arranged at the body of the ornithopter and comprises a first transmission mechanism (101) and a second transmission mechanism (102) which are arranged in a bilateral symmetry mode with respect to the center line of the body of the ornithopter and make contact with each other, and a crank structure (103), and one end of the crank structure (103) is rotatably fixed. The other end of the crank structure (103) is rotatably connected to the first transmission mechanism (101) or the second transmission mechanism (102); the first transmission mechanism (101) and the second transmission mechanism (102) arefixedly mounted on the bracket (500); and a space for accommodating the first transmission mechanism (101) and the second transmission mechanism (102) is formed between the reinforcing plate (600) and the bracket (500).
本公开涉及一种扑翼飞行器。根据本公开的扑翼飞行器包括:曲柄传动组件(100),安装到所述扑翼飞行器的机身,并且包括以所述扑翼飞行器的机身的中心线左右对称布置并相互接触的第一传动机构(101)和第二传动机构(102)、以及曲柄结构(103),其中,所述曲柄结构(103)的一端可转动地固定,另一端可转动地连接到所述第一传动机构(101)或所述第二传动机构(102);支架(500),所述第一传动机构(101)和第二传动机构(102)固定安装在所述支架(500)上;以及加强板(600),所述加强板(600)与所述支架(500)之间形成有容纳所述第一传动机构(101)和第二传动机构(102)的空间。
Ornithopter
扑翼飞行器
2021-01-15
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |