A wing rotation structure of a flapping wing micro air vehicle, for which, wing rotations are related to and caused by wing flappings, the wing rotation structure includes: an actuator mount, a left actuator, a right actuator, a left connector, a right connector, a left flapping wing arm, a right flapping wing arm, a central base, a left rotation bevel gear, a right rotation bevel gear, a left fixed auxiliary bevel gear, a right fixed auxiliary bevel gear. Wherein, the left actuator and the right actuator are located respectively on a left side and a right side of the actuator mount. the left connector connects the left actuator to the left flapping wing arm, and the right connector connects the right actuator to the right flapping wing arm. The central base is fixed securely on the actuator mount.
WING ROTATION STRUCTURE OF FLAPPING WING MICRO AIR VEHICLE
23.09.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2024
|Passitve Wing Rotation in Flexible Flapping Wing Aerodynamics
British Library Conference Proceedings | 2012
|Flapping-wing air vehicle driving device and flapping-wing air vehicle
Europäisches Patentamt | 2022
|Adjusting structure device for flapping wing form of flapping wing air vehicle
Europäisches Patentamt | 2024
|